Mmel G550 R10

U.S.
Department of Transportation
Federal Aviation Administration
Washington, DC
Master Minimum Equipment List (MMEL)

Revision: 10
Date: 07/05/2018
Gulfstream Aerospace
GV, GV-SP, GV-SP (G550), GV-SP (G500 5000 Series)
GIV-X, GIV-X (G450), GIV-X (G350)
*** FOR 14 CFR PARTS 91, 91K, 125, and 135 OPERATIONS ONLY **
Troy A. Zwicke, Chair

Flight Operations Evaluation Board (FOEB)
Federal Aviation Administration (FAA)

Long Beach Aircraft Evaluation Group (LGB-AEG)
3960 Paramount Blvd., Suite 100
Lakewood, CA 90712-4137
Telephone: (562) 627-5317

Fax: (562) 627-5281
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 10 PAGE NO. I
DATE: 07/05/2018
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP(G550/G500 TABLE OF CONTENTS
5000 SERIES)
SYSTEM NO. SYSTEM PAGE NO.
-- Cover Page --
-- Table of Contents I
-- Control Page II thru VII
-- Log of Revisions VIII thru X
-- Highlights of Change XIthru XV
-- Definitions XVI
-- Preamble XVII
-- Guidelines for (M) and (O) Procedures XVIII
Section One Line Replaceable Unit (LRU) Component Relief 1-1
21 Air Conditioning 21-1 thru 9
22 Autoflight 22-1 thru 2
23 Communications 23-1 thru 13
24 Electrical Power 24-1 thru 8
25 Equipment/Furnishings 25-1 thru 13
26 Fire Protection 26-1 thru 6
27 Flight Controls 27-1 thru 3
28 Fuel 28-1 thru 7
29 Hydraulic Power 29-1 thru 3
30 Ice and Rain Protection 30-1 thru 4
31 Indicating/Recording Systems 31-1 thru 4
32 Landing Gear 32-1 thru 3
33 Lights 33-1 thru 7
34 Navigation 34-1 thru 35
35 Oxygen 35-1 thru 2
36 Pneumatic 36-1 thru 4
38 Water/Waste 38-1 thru 2
45 Central Maintenance System 45-1
46 Information Systems 46-1
49 Airborne Auxiliary Power 49-1 thru 4
52 Doors 52-1 thru 2
71 Powerplant 71-1
73 Engine Fuel and Control 73-1 thru 2
74 Ignition 74-1
77 Engine Indicating 77-1
78 Engine Exhaust 78-1
79 Engine Oil 79-1 thru 2
80 Starting 80-1 thru 3
Section Two Crew Alerting System (CAS) Message Relief 2-1
-- Statement Page 2-2
-- CAS Messages 2-3 thru 85
REVISION NO. 10 PAGE NO. II
DATE: 07/05/2018
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 CONTROL PAGE
5000 SERIES)
SYSTEM NO. PAGE NO. REV. NO. DATE
Cover Page -- 10 07/05/2018
Table of Contents I 10 07/05/2018
Control Page II thru VII 10 07/05/2018
Log of Revisions VIII thru IX 9 12/18/2017
X 10 07/05/2018
Highlights of Change XI thru XV 10 07/05/2018
Definitions XVI 8 11/07/2014
Preamble XVII 8 11/07/2014
Guidelines for (M) and (O) Procedures XVIII 10 07/05/2018
Section One
Line Replaceable Unit (LRU) Component 1-1 10 07/05/2018
Relief
21Air Conditioning 21-1 6 07/24/2007
21-2 6 07/24/2007
21-3 7 02/04/2010
21-4 6 07/24/2007
21-5 7 02/04/2010
21-6 8 11/07/2014
21-7 10 07/05/2018
21-8 10 07/05/2018
21-9 6 07/24/2007
22 Autoflight 22-1 7a 11/08/2010
22-2 10 07/05/2018
23 Communications 23-1 9 12/18/2017
23-2 10 07/05/2018
23-3 10 07/05/2018
23-4 10 07/05/2018
23-5 10 07/05/2018
23-6 8 11/07/2014
23-7 8 11/07/2014
23-8 10 07/05/2018
23-9 10 07/05/2018
23-10 10 07/05/2018
23-11 9 12/18/2017
23-12 9 12/18/2017
23-13 8a 08/24/2015
24 Electrical Power 24-1 10 07/05/2018
24-2 10 07/05/2018
24-3 10 07/05/2018
24-4 8 11/07/2014
24-5 8 11/07/2014
24-6 8 11/07/2014
24-7 10 07/05/2018
24-8 9 12/18/2017
REVISION NO. 10 PAGE NO. III
DATE: 07/05/2018
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP(G550/G500 CONTROL PAGE
5000 SERIES)
25 Equipment/Furnishings 25-1 10 07/05/2018
25-2 10 07/05/2018
25-3 10 07/05/2018
25-4 10 07/05/2018
25-5 8 11/07/2014
25-6 8 11/07/2014
25-7 10 07/05/2018
25-8 9 12/18/2017
25-9 10 07/05/2018
25-10 10 07/05/2018
25-11 10 07/05/2018
25-12 10 07/05/2018
25-13 10 07/05/2018
26 Fire Protection 26-1 10 07/05/2018
26-2 7a 11/08/2010
26-3 10 07/05/2018
26-4 10 07/05/2018
26-5 7 02/04/2010
26-6 10 07/05/2018
27 Flight Controls 27-1 10 07/05/2018
27-2 10 07/05/2018
27-3 10 07/05/2018
28 Fuel 28-1 9 12/18/2017
28-2 10 07/05/2018
28-3 10 07/05/2018
28-4 9 12/18/2017
28-5 7 02/04/2010
28-6 9 12/18/2017
28-7 9 12/18/2017
29 Hydraulic Power 29-1 10 07/05/2018
29-2 8 11/07/2014
29-3 8 11/07/2014
30 Ice and Rain Protection 30-1 7 02/04/2010
30-2 7a 11/08/2010
30-3 7 02/04/2010
30-4 10 07/05/2018
31 Indicating/Recording Systems 31-1 10 07/05/2018
31-2 9 12/18/2017
31-3 8 11/07/2014
31-4 10 07/05/2018
32 Landing Gear 32-1 10 07/05/2018
32-2 10 07/05/2018
32-3 8 11/07/2014
REVISION NO. 10 PAGE NO. IV
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
33 Lights 33-1 10 07/05/2018
33-2 10 07/05/2018
33-3 7a 11/08/2010
33-4 7 02/04/2010
33-5 9 12/18/2017
33-6 10 07/05/2018
33-7 9 12/18/2017
34 Navigation 34-1 7 02/04/2010
34-2 7a 11/08/2010
34-3 7a 11/08/2010
34-4 7 02/04/2010
34-5 10 07/05/2018
34-6 8 11/07/2014
34-7 10 07/05/2018
34-8 7 02/04/2010
34-9 9 12/18/2017
34-10 7 02/04/2010
34-11 7 02/04/2010
34-12 10 07/05/2018
34-13 9 12/18/2017
34-14 9 12/18/2017
34-15 7a 11/08/2010
34-16 7a 11/08/2010
34-17 7 02/04/2010
34-18 4a 06/02/2006
34-19 8 11/07/2014
34-20 7a 11/08/2010
34-21 10 07/05/2018
34-22 9 12/18/2017
34-23 9 12/18/2017
34-24 9 12/18/2017
34-25 8 11/07/2014
34-26 7a 11/08/2010
34-27 8 11/07/2014
34-28 10 07/05/2018
34-29 10 07/05/2018
34-30 10 07/05/2018
34-31 10 07/05/2018
34-32 10 07/05/2018
34-33 10 07/05/2018
34-34 10 07/05/2018
34-35 9 12/18/2017
35 Oxygen 35-1 10 07/05/2018
35-2 10 07/05/2018
REVISION NO. 10 PAGE NO. V
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
36 Pneumatic 36-1 10 07/05/2018
36-2 10 07/05/2018
36-3 10 07/05/2018
36-4 7 02/04/2010
38 Water/Waste 38-1 10 07/05/2018
38-2 10 07/05/2018
45 Central Maintenance System 45-1 7 02/04/2010
46 Information Systems 46-1 7 02/04/2010
49 Airborne Auxiliary Power 49-1 10 07/05/2018
49-2 7 02/04/2010
49-3 9 12/18/2017
49-4 6 07/24/2007
52 Doors 52-1 10 07/05/2018
52-2 10 07/05/2018
71 Powerplant 71-1 7 02/04/2010
73 Engine Fuel and Control 73-1 7a 11/08/2010
73-2 10 07/05/2018
74 Ignition 74-1 10 07/05/2018
77 Engine Indicating 77-1 8 11/07/2014
78 Engine Exhaust 78-1 10 07/05/2018
79 Engine Oil 79-1 10 07/05/2018
79-2 10 07/05/2018
80 Starting 80-1 10 07/05/2018
80-2 10 07/05/2018
80-3 10 07/05/2018
Section Two
Crew Alerting System (CAS) Message 2-1 8 11/07/2014
Relief
Statement Page 2-2 10 07/05/2018
CAS Messages 2-3 9 12/18/2017
2-4 8 11/07/2014
2-5 8 11/07/2014
2-6 9 12/18/2017
2-7 10 07/05/2018
2-8 8 11/07/2014
2-9 8 11/07/2014
2-10 8 11/07/2014
2-11 9 12/18/2017
2-12 10 07/05/2018
2-13 8 11/07/2014
2-14 8 11/07/2014
2-15 8 11/07/2014
2-16 8 11/07/2014
2-17 10 07/05/2018
2-18 10 07/05/2018
REVISION NO. 10 PAGE NO. VI
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
2-19 8 11/07/2014
2-20 8 11/07/2014
2-21 8 11/07/2014
2-22 8 11/07/2014
2-23 8 11/07/2014
2-24 8 11/07/2014
2-25 8 11/07/2014
2-26 8a 08/24/2015
2-27 8 11/07/2014
2-28 8 11/07/2014
2-29 8 11/07/2014
2-30 8 11/07/2014
2-31 8 11/07/2014
2-32 8 11/07/2014
2-33 8 11/07/2014
2-34 8 11/07/2014
2-35 8 11/07/2014
2-36 8 11/07/2014
2-37 8 11/07/2014
2-38 8 11/07/2014
2-39 8 11/07/2014
2-40 8 11/07/2014
2-41 10 07/05/2018
2-42 9 12/18/2017
2-43 9 12/18/2017
2-44 9 12/18/2017
2-45 9 12/18/2017
2-46 9 12/18/2017
2-47 10 07/05/2018
2-48 10 07/05/2018
2-49 8 11/07/2014
2-50 9 12/18/2017
2-51 8 11/07/2014
2-52 9 12/18/2017
2-53 8 11/07/2014
2-54 8 11/07/2014
2-55 10 07/05/2018
2-56 10 07/05/2018
2-57 8 11/07/2014
2-58 8 11/07/2014
2-59 8 11/07/2014
2-60 8 11/07/2014
2-61 10 07/05/2018
2-62 8 11/07/2014
2-63 9 12/18/2017
2-64 9 12/18/2017
REVISION NO. 10 PAGE NO. VII
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
2-65 8 11/07/2014
2-66 10 07/05/2018
2-67 9 12/18/2017
2-68 8 11/07/2014
2-69 8 11/07/2014
2-70 8 11/07/2014
2-71 8 11/07/2014
2-72 8a 08/24/2015
2-73 9 12/18/2017
2-74 9 12/18/2017
2-75 9 12/18/2017
2-76 9 12/18/2017
2-77 9 12/18/2017
2-78 9 12/18/2017
2-79 8 11/07/2014
2-80 8 11/07/2014
2-81 8 11/07/2014
2-82 10 07/05/2018
2-83 8a 08/24/2015
2-84 9 12/18/2017
2-85 8 11/07/2014
REVISION NO. 9 PAGE NO. VIII
DATE: 12/18/2017
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 LOG OF REVISIONS
5000 SERIES)
REV NO. DATE PAGE NO.
1 08/19/1998 HIGHLIGHTS OF REV., DEFINITIONS, 21-1, 21-2, 21-5, 21-6, 21-9, 22 1,
22-2, 23-1, 23-2, 23-3, 23-4, 24-1, 24-2, 24-3, 24-4, 24-5, 24-6, 25 1, 25 2,
25-3, 25-4, 25-5, 25-6, 26-1, 26-2, 26-3, 26-4, 26-5, 27-1, 28 2, 28 3, 28-4,
28-5, 29-1, 29-2, 30-1, 30-2, 30-3, 30-4, 31-1, 33-1, 33 2, 33 3, 33-4, 34-1,
34-2, 34-3, 34-4, 34-5, 34-6, 34-7, 34-8, 34-9, 34 10, 34-11, 34-12, 34-13,
35-1, 38-1, 49-1, 49-2, 49-3, 49-4, 52-1, 71 1, 73-1, 73-2, 78-1, 79-1.
2 06/04/2001 21-1, 21-2, 21-3, 21-4, 21-5, 21-6, 21-7, 21-9, 22-1, 22-2, 23-1, 23-2, 23 3,
23-4, 23-5, 23-6, 23-7, 24-1, 24-2, 24-3, 24-4, 24-5, 24-6, 25-1, 25 2, 25-3,
25-4, 25-5, 25-6, 25-7, 25-8, 25-9, 25-10, 25-11, 26-1, 26-2, 26-3, 26-4,
26-5, 27-1, 28-1, 28-2, 28-3, 28-4, 28-5, 29-1, 29-2, 30-1, 30 2, 30-3, 30-4,
31-1, 31-2, 32-1, 33-1, 33-2, 33-3, 33-4, 34-2, 34-3, 34 4, 34-5, 34-6, 34-7,
34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34-14, 34 15, 34-16, 35-1, 35-2,
36-1, 36-2, 36-3, 38-1, 49-1, 49-2, 49-3, 52-1, 73-1, 73-2, 78-1, 79-1, 80-1.
2a 11/09/2001 HIGHLIGHTS OF REV., DEFINITIONS, 34-2, 34-3, 34-4, 34-5, 34-6, 34 7,

34-8, 34-9, 34-11, 34-12, 34-13, 34-14, 34-15, 34-16.

23-6, 23-7, 24-1, 24-2, 24-5, 24-6, 25-2, 25-3, 25-4, 25-5, 25-10, 25-11,
25-12, 25-13, 25-14, 26-1, 26-3, 26-4, 26-5, 26-6, 27-1, 27-2, 28 1, 28-2,
28-5, 30-1, 30-2, 31-1, 31-2, 31-3, 32-1, 33-5, 33-6, 34-2, 34 3, 34-4, 34-5,
34-6, 34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34 14, 34-15, 34-16,
34-17, 34-18, 34-19, 34-20, 34-21, 34-22, 36-3, 38 1, 38-2, 49-1, 49-2,
49-3, 52-1, 73-2, 77-1, 77-2, 80-1, 80-2.

22-2, 23-1, 23-2, 23-3, 23-4, 23-5, 23-6, 23-7, 23-8, 23-9, 24-1, 24 5, 24-6,
25-3, 25-5, 25-6, 25-10, 25-11, 25-12, 25-13, 25-14, 26-1, 26 2, 26-3,
26-4, 26-5, 26-6, 27-1, 27-2, 28-1, 28-2, 28-3, 28-4, 28-5, 29 1, 30-1, 30-2,
30-3, 30-4, 31-1, 31-2, 31-3, 31-4, 32-1, 33-2, 33-3, 33 4, 33-5, 33-6, 34-2,
34-3, 34-4, 34-5, 34-6, 34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 34-13,
34-14, 34-15, 34-16, 34-17, 34-18, 34-19, 34-20, 34 21, 34-22, 34-23,
34-24, 34-25, 36-1, 36-2, 36-3, 38-1, 38-2, 49-1, 49 2, 49-3, 49-4, 73-1,
73-2, 74-1, 77-1, 77-2, 79-1, 79-2, 80-1, 80-2, 80 3.
4a 06/02/2006 HIGHLIGHTS OF REV., DEFINITIONS, 23-2, 23-5, 23-6, 23-7, 23-8, 25 1,

25-3, 25-4, 25-5, 25-11, 25-12, 25-13, 25-14, 25-15, 25-16, 34-4, 34-5,
34-6, 34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34-14, 34-15, 34-16,
34-17, 34-18, 34-19, 34-20, 34-21, 34-22, 34-23, 34-24, 34-25, 34 26.
4b 07/05/2006 HIGHLIGHTS OF REV., DEFINITIONS, 25-15, 25-16, 25-17.
5 06/18/2007 ISSUED IN ERROR, THEN RETRACTED.

REVISION NO. 9 PAGE NO. IX
DATE: 12/18/2017
AIRCRAFT:
5000 SERIES)
21-7, 21-8, 21-9, 22-1, 22-2, 23-2, 23-3, 23-4, 23-5, 23-8, 23-9, 23 10,
23-11, 23-12, 24-1, 24-2, 24-3, 24-5, 24-6, 24-7, 25-4, 25-5, 25-6, 25-12,
25-13, 25-14, 25-15, 26-1, 26-3, 26-4, 26-5, 26-6, 27-1, 27-2, 27 3, 28-1,
28-2, 28-3, 28-4, 28-5, 28-6, 29-2, 30-1, 30-2, 30-3, 30-4, 30 5, 30-6, 31-1,
31-2, 31-3, 31-4, 33-1, 33-4, 33-6, 34-1, 34-2, 34-3, 34 4, 34-5, 34-6, 34-8,
34-10, 34-11, 34-14, 34-15, 34-20, 34-21, 34-22, 34-23, 34-25, 34-26,
34-28, 34-29, 35-1, 36-1, 36-2, 36-3, 45-1, 49-1, 49 2, 49-3, 49-4, 52-2,
71-1, 73-1, 73-2, 74-1, 77-1, 78-1, 79-1, 79-2, 80 1, 80-2.

22-2, 23-1, 23-2, 23-3, 23-4, 23-5, 23-6, 23-7, 23-8, 23-9, 23-10, 23-11,
23-12, 24-1, 24-2, 24-3, 23-4, 24-5, 24-6, 24-7, 25-1, 25-2, 25-3, 25-4,
25-5, 25-6, 25-7, 25-8, 25-9, 25-10, 25-11, 25-12, 25-13, 25-14, 25 15,
25-16, 25-17, 25-18, 26-1, 26-2, 26-5, 27-1, 27-2, 28-1, 28-2, 28 3, 28-4,
28-6, 29-2, 30-1, 30-2, 30-3, 30-4, 30-5, 31-1, 31-2, 31-3, 31 4, 32-1, 32-2,
32-3, 33-1, 33-2, 33-3, 33-4, 33-5, 33-6, 33-7, 33-8, 34 1, 34-2, 34-3, 34-4,
34-5, 34-6, 34-7, 34-8, 34-9, 34-11, 34-12, 34-13, 34-14, 34-15, 34-17,
34-18, 34-19, 34-20, 34-21, 34-22, 34-23, 34-24, 34 25, 34-26, 34-27,
34-28, 34-29, 34-30, 34-31, 35-1, 35-2, 36-1, 36-2, 36-3, 36-4, 36-5, 38-2,
45-1, 46-1, 46-2,49-1, 49-2, 49-3, 52-1, 52-2, 71 1, 73-1, 73-2, 74-1, 77-1,
78-1, 79-1, 79-2, 80-1, 80-2, 80-3.
7a 11/08/2010 HIGHLIGHTS OF REV., DEFINITIONS, 22-1, 23-8, 23-9, 23-10, 23-12,

24-1, 24-6, 25-1, 25-5, 25-6, 25-7, 25-8, 25-13, 25-15, 25-16, 26-2, 30-2,
31-1, 31-2, 32-1, 32-2, 33-1, 33-2, 33-3, 33-6, 34-3, 34-4, 34-13, 34-14,
34-15, 34-16, 34-20, 34-21, 34-22,34-26, 34-27, 34-28, 34-33, 34-34, 35 2,
36-1, 36-2, 36-4, 38-1, 73-1, 73-2, 73-3.
8 11/07/2014 21-6, 22-2, 23-1, 23-2, 23-4, 23-5, 23-6, 23-7, 23-8, 23-9, 23-10, 23-13,
23-14, 23-15, 23-16, 23-17, 24-1, 24-4, 24-5, 24-6, 25-5, 25-6, 25-7, 25
13, 25-17, 27-3, 29-1, 29-2, 29-3, 30-3, 30-5, 31-3, 32-2, 32-3, 33-1, 33-4,
33-5, 34-6, 34-7, 34-19, 34-22, 34-23, 34-25, 34-27, 34-28, 34-29, 34-31,
34-35, 35-2, 36-2, 36-3, 38-1, 38-2, 52-1, 52-2, 74-1, 77-1, 79-1,
Section Two, 2-1 thru 2-85, Section One.
8a 08/24/2015 TOC, Control Page, Highlights, 23-17, 25-18, 28-1, 28-2, 34-13, 34-14,
34-31, 52-2, 79-1, Section Two, 2-12, 2-26, 2-43, 2-64, 2-72, 2-83, 2-84.
9 12/18/2017 Section One – TOC, Control Page, Highlights, 21-7, 22-2, 23-1, 23-2, 23 4,
23-5, 23-8, 23-9, 23-11, 23-12, 24-1, 24-2, 24-3, 24-7, 24-8, 25-2, 25-4,
25-5, 25-8, 25-9, 25-12, 25-13, 25-14, 26-1, 26-4, 26-6, 27-2, 27-3, 28-1,
28-2, 28-3, 28-5,28-6, 29-1, 30-3, 30-5, 31-1, 31-2, 31-4, 33-1, 33 2, 33-5
thru 33-7, 34-5, 34-7, 34-9, 34-12 thru 34-14, 34-21 thru 34 24, 34-28 thru
34-32, 34-33 thru 34-35, 35-2, 36-1, 49-1, 49-3, 52 2, 74-1, 79-1, 79-2,
80-1, 80-2, Section Two: 2-3, 2-6, 2-11, 2-12, 2-41 thru 2-46, 2-48, 2-50,
2-52, 2-56, 2-61, 2-63, 2-64, 2-67, 2-73 thru 2-78, 2-82, 2-84.
REVISION NO. 10 PAGE NO. X
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
10 07/05/2018 Section One –
Cover Page, TOC, Control Page, Log of Revisions,Highlights of Change,

Guidelines for M & O Procedures, 1-1, 21-7, 21-8, 22-2, 23-2, 23-3, 23-4,
23-5, 23-8, 23-9, 23-10, 24-1, 24-2, 24-3, 24-7,25-1, 25-2, 25-3,25-4, 25-7,
25-9, 25-10, 25-11, 25-12, 25-13, 26-1, 26-3, 26-4,26-6, 27-1, 27-2, 27-3,
28-2, 28-3, 29-1, 30-4, 31-1, 31-4, 32-1, 32-2, 33-1, 33-2, 33-6, 34-5, 34-
7,34-12, 34-21, 34-28, 34-29, 34-30, 34-31, 34-32,34-33, 34-34, 35-1, 35-
2, 36-1, 36-2, 36-3, 38-1, 38-2, 49-1, 52-1, 52-2,73-2, 74-1, 78-1, 79-1, 79-
2, 80-1, 80-2, 80-3.
Section Two –
2-2, 2-7, 2-12, 2-17, 2-18, 2-41, 2-47, 2-48, 2-55, 2-56, 2-61, 2-66, 2-82.
REVISION NO. 10 PAGE NO. XI
DATE: 07/05/2018
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 HIGHLIGHTS OF CHANGE
5000 SERIES)
EFFECTIVE ABOVE DATE, this is a Revision to the Gulfstream Aerospace GIV-X (G450/G350), GV,
GV-SP(G550/G500, 5000 SERIES)Master Minimum Equipment List (MMEL).
PAGE NO. EXPLANATION OF CHANGE

General Minor editorial corrections and plurals were made throughout the document that do
not affect the reliefs and are not indicated with change bars. These editorial
corrections may be adopted in Minimum Equipment Lists (MEL) at the operator’s
discretion.
21-3 Item 21-4, Removed Plural
21-4 Item 21-8. Capitalization correction.
Item 21-9-11. Removed Plurals
21-7 Item 21-15. Changed A/C to AC.
21-8 Item 21-17-02, Deleted item from MMEL.
22-2 Item 22-7-10, Remove plurals
23-3 Item 23-2-2 and 3, corrected numbering
Item 23-4-02, Updated per Policy Letter 120 r2.
23-4 Items 23-4-03, -04, -05, Updated per Policy Letter 120 r2.
Item 23-5, removed heading relief requirement.
Item 23-5 (a) updated relief category.
Item 23-5.2 – Updated title.
23-5 Item 23-8-1, Updated per Policy Letter 09.
23-8 Item 23-8 14.1(b) updated relief categories.
23-9 Item 23-15(b), remove invalid “B’ relief.
23-10 Item 23-17-02, Updated per Policy Letter 106 r5.
24-1 Item 24-1, Added 2 Notes.

REVISION NO. 10 PAGE NO. XII
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
24-2 Item 24-3, Reinstated (M) per 8900.1, Vol.4, Ch.4, Sec.3, para.4-684, Sub E.
Item 24-4, Inserted ‘and’ to proviso.
24-3 Item 24-4,-5 Reinstated (M) per 8900.1, Vol.4, Ch.4, Sec.3, para.4-684, Sub E.
Item 24-5, Updated proviso.
24-7 Item 24-15, Reinstated (M) per 8900.1, Vol.4, Ch.4, Sec.3, para.4-684, Sub E.
25-1 Item 25-2-01, -2. Updated per Policy Letter 79 r9.
25-4 Item 25-3. Deleted relief for Crewmember Shoulder Harnesses.
25-5 Item 25-5, removed plural.
Item 26-6, updated note.
25-8 Item 25-10, updated proviso.
25-10 Item 25-15-1, -2, -3. Added (M) procedure.
Item 25-17. Deleted item and removed from MMEL.
25-11 Items 25-18, 25-19, 25-20, and 25-21 renumbered, plurals removed.
25-12 Item 25-22-01. Deleted item and removed from MMEL.
25-13 Item 25-26 renumbered.
25-14 Item 25-27 renumbered.
26-1 Item 26-3. Reinstated (M) per 8900.1, Vol.4, Ch.4, Sec.3, para.4-684, Sub E.
26.3 Item 26-5 Added D proviso.
26-4 Item 26-6. Added (M) procedure and D proviso.
27-1 Item 27-7. Added (O) procedure.

REVISION NO. 10 PAGE NO. XIII
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
27-2 Item 27-8, -9, -10, -11, -12, -13. Reinstated (M) per 8900.1, Vol.4, Ch.4, Sec.3,
para.4-684, Sub E.
29-1 Item 29-6, -7. Added (O) procedure.
30-5 Item 30-10. Added (M) procedures. Modified relief for clarity.
31-1 Item 31-2, Updated proviso to Policy Letter 87 r10.
31-2 Item 31-2. Removed extra wording.
32-1 Item 32-3. Deleted Landing Gear Position Indicators.
33-1 Item 33-1. Removed NVG Note.
Item 33-3. Removed note below item title.
33-2 Item 33-3. Added (O) procedure requirement.
33-5 Item 33-23. Added (GIV-X).
33-6 Item 33-27, deleted, relief already exists at ATA 25-20.
Item 33-28. Updated proviso.
Item 33-29. Change in proviso verbiage to meet 14 CFR requirements.
34-5 Item 34-8. Updated per Policy Letter 76 r7.
34-7 Item 34-12. Clarified proviso.
34-12 Item 34-13-1. Class C TAWS – ‘Note’ verbiage updated.
34-13 Item 34-13-15 and 15-1, removed plural.
34-14 Item 34-16 and 16-1, removed plural.

REVISION NO. 10 PAGE NO. XIV
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
34-21 Item 34-24-01. Added (M) procedure requirement.
Item 34-24-02. Changed proviso.
Item 34-24-03. Added (M) procedure requirement.
34-22 Item 34-26. Deleted ‘are’ from proviso.
34-28 Item 34-44-02. Added (O) procedure.
34-29 Item 34-15-1-a, Updated title.
Item 34-45-1, Updated to PL-98.
Item 34-46, Updated title.
34-30 Item 34-45. Changed Item name, Changed to Category C, Added (O) procedure,
amended proviso
34-31 Item 34-46. Changed to Category C, Added (O) procedure, amended proviso.
34-32 Item 34-47-01. Changed to Category C, Added (O) procedure, amended proviso.
34-34 Item 34-50. Reinstated (M) and (O) per 8900.1, Vol.4, Ch.4, Sec.3, para.4-684,
Sub E.
35-1 Item 35-4. Updated relief to “C”.
36-1 Item 36-1-2. Added (M) procedure.
36-2 Item 36-1-1, -2. Added (M) procedures.
36-3 Item 36-2-1, -2. Added (M) procedures.
38-1 Item 38-1. Updated proviso.
38-2 Item 38-3. Added (M) procedure.
49-1 Item 49-1-3. Added (O) procedure and proviso.
Item 49-2 and 49-3, removed plural and updated proviso.

REVISION NO. 10 PAGE NO. XV
DATE: 07/05/2018
AIRCRAFT:
5000 SERIES)
52-1 Item 52-7. Added (M) procedure.
52-2 Item 52-10, Added three asterisks and (O) procedure.
Item 52-11. Added (M) procedure.
73-2 Item 73-2. Deleted Notes.
74-1 Item 74-1. Minor verbiage change.
79-1 Item 79-3. Added (M) procedure, removed plural.
79-2 Item 79-5. Added (M) procedure, removed plural.
80-1 Item 80-1. Added (M) and (O) procedures.
80-2 Item 80-3. Added 2 (M) procedures and 1 (O) procedure.
80-3 Item 80-4. Added (M)& (O) procedures.
Section 2, 2-2 Added Policy Letter 119 reference.
Section 2, 2-7 Updated ADS-B Dispatch Consideration.
Section 2, 2-12 Updated Dispatch Considerations.
Section 2, 2-41 Updated Dispatch Consideration.

REVISION NO. 8 PAGE NO. XVI
DATE: 11/07/2014
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 DEFINITIONS
5000 SERIES)
Refer to the current FAA MMEL Policy Letter PL-25 for the most current list of definitions.
REVISION NO. 8 PAGE NO. XVII
DATE: 11/07/2014
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 PREAMBLE
5000 SERIES)
For FAA, insert Preamble from Policy Letter PL-34 for Part 125 and 135 certificate holders, or PL-36 for
Part 91 operators.
REVISION NO. 10 PAGE NO. XVIII
DATE: 07/05/2018
AIRCRAFT:
GIV-X (G450/G350), GV, GV-SP (G550/G500 GUIDELINES FOR (M) AND (O) PROCEDURES
5000 SERIES)
Guidelines for (M) and (O) Procedures should be based on the Maintenance and Operational
Procedures Manual for the Minimum Equipment List (insert aircraft manufacturer and aircraft make and
model) (M) and (O) Procedures,published by Gulfstream Aerospace.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
REVISION NO. 10 PAGE NO. 1-1
DATE: 07/05/2018
AIRCRAFT: LRU COMPONENT RELIEF
GIV-X (G450/G350), GV, GV-SP (G550/G500
5000 SERIES)
SECTION ONE
LINE REPLACEABLE
UNIT (LRU)
COMPONENT RELIEF
DATE: 07/24/2007
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
GIV-X (G450/G350), GV, GV-SP (G550/G500 2. NO. INSTALLED
5000 SERIES) 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar
1. Cabin Altitude Indicator C 1 0 May be inoperative provided cabin

(Overhead Panel) altitude is available on EICAS
Synoptic display.
C 1 0 May be inoperative provided:

a) Cabin Pressure Selector
Panel is operative, and
b) Pressurization is operated in
AUTO mode.

a) Cabin Differential Pressure
Indicator is operative, and
b) A chart is provided to crew to
convert Cabin Differential
Pressure to Cabin Altitude.
D 1 0 May be inoperative provided airplane

is equipped with additional pneumatic
three-in-one cabin pressurization
monitoring instrument, and Cabin
Altitude Indicator portion is fully
operative.
C 1 0 (O) May be inoperative provided

airplane is operated in unpressurized
configuration.
DATE: 07/24/2007
TABLE KEY
Change
2. Cabin Differential D 1 0 May be inoperative provided cabin

Pressure Indicator differential pressure is available on
EICAS Synoptic display.

a) Cabin Pressure Selection
Panel is operative, and
b) Pressurization is operated in
AUTO mode.
D 1 0 May be inoperative provided:

a) Cabin Altitude Indicator is
operative, and
b) A chart is provided to crew to
convert Cabin Altitude to
Cabin Differential Pressure.
D 1 0 May be inoperative provided airplane

is equipped with additional pneumatic
three-in-one cabin pressurization
monitoring instrument, and Cabin
Altitude Indicator portion is fully
operative.

configuration.
3. Cabin Rate of Climb D 1 0

Indicator
DATE: 02/04/2010
TABLE KEY
Change
4. Automatic Pressurization B 2 0 (O) Except for ER operations, may be

Control System inoperative provided:
a) Manual Pressurization Control
System is operative,
b) Cabin Altitude and Differential
Pressure Indicators are
operative,
c) Cabin Rate of Climb Indicator
is operative,
d) Autopilot is operative, and
e) Airplane is operated in
accordance with
AFM Limitations.
B 2 0 (O) Except for ER operations, may be

inoperative provided airplane is
operated in unpressurized
configuration.
5. Manual Pressurization C 1 0 May be inoperative provided both

Control System Automatic Pressurization Control
Systems are operative.
6. Semi-Auto C 1 0
Pressurization Control
System
DATE: 07/24/2007
TABLE KEY
Change
7. Cabin Altitude Pressure C 1 0 May be inoperative provided:

Warning System a) Cabin Altitude and Differential
operative,
b) Cabin Oxygen On Warning
System is operative, and
c) Airplane is operated in
accordance with
AFM Limitations.

configuration.
8. Pressurization Outflow C 1 0 May be inoperative provided all other

Valve Position Indicator components of the Cabin Pressure
Control Panel and Cabin Pressure
Indicator are operative.
DATE: 02/04/2010
TABLE KEY
Change
9. Cockpit Zone C 3 2
Temperature Control
System & Cabin Zone
Temperature Control
System
C 3 1 (O) May be inoperative provided:

a) Ram Air is operative, and
b) Airplane is operated in
unpressurized configuration.
1) Automatic System C 3 0 May be inoperative provided:

a) Associated manual control
system is operative, and
b) Associated temperature
indicator is operative.
2) Manual System C 3 0 May be inoperative provided:

a) Associated Automatic Control
b) Associated temperature
indicator is operative.
10. Cockpit/Cabin Zone D 3 0 May be inoperative provided

Temperature Indicator associated Automatic Temperature
(Overhead Panel) Control System is operative.
D 3 0 May be inoperative provided

associated zone temperature is
available on EICAS Synoptic display.
   D 3 0 May be inoperative provided

associated Manual
Temperature Control System
is operative.
11. Duct Temperature D 3 0

Indicator
(Overhead Panel)
DATE: 11/07/2014
TABLE KEY
Change
12. Environmental Control

System (ECS) Packs
1) Pressurized C 2 1 Except for ER operations, may be

Configuration inoperative provided:
a) Inoperative ECS Pack is
selected OFF,
b) Bleed Air Isolation Valve is
CLOSED and operative,
c) Right Main TRU is operative,
d) Airplane is operated at or
below FL 410, and
e) Autothrottle must be operative
and engaged at or above
FL 400.
2) Unpressurized C 2 0 Except for ER operations, may be

Configuration inoperative provided outflow valve is
operative.
13. Three-In-One Cabin C 1 0 May be inoperative provided primary

*** Pneumatic Cabin Altitude and primary Cabin
Pressurization Differential Pressure Indicators are
Monitoring Instrument operative either in the overhead
panel or on the Synoptic Display.
14. Air Conditioning System C 2 1 (M) Except for ER operations, may be

Pack Inlet Valve inoperative provided:
a) Affected Valve is CLOSED
and deactivated electrically,
b) Associated Air Conditioning
Pack is selected OFF, and
accordance with
AFM Limitations.
DATE: 07/05/2018
TABLE KEY
Change
15. Outflow Valve System C 1 0 (M)(O) May be inoperative provided:
a) Outflow valve is positioned to full
OPEN position and electrically
isolated,
unpressurized configuration, and
c) Extended overwater operations
are not conducted.
1) AC Motor C 2 1 May be inoperative provided: |

a) DC motor is operative, and
accordance with
AFM Limitations.
16. Pressure Relief Valve C 1 0 May be inoperative provided:

a) Cabin differential pressure
and cabin altitude displays are
operative,
b) Selected cabin altitude is
1,000 feet higher than normal
cabin altitude for the cruise
flight level, and
c) Flightcrew monitors actual
cabin differential pressure and
maintains it at or below
9.5 psi.

configuration.
DATE: 07/05/2018
TABLE KEY
Change
17. Cabin Pressure Indicator

and Control Panel
1) Manual Light C 1 0
|
2) Flight/Landing Switch C 1 0
(Light Function Only)
3) Fault/Manual Switch C 1 0
4) Auto/Semi Switch C 1 0
18. Selector Panel B 1 0 May be inoperative provided:

(Semi-Auto) a) Auto system (Cabin Pressure
Control Panel) is operative,
and
b) Semi-auto mode is
considered inoperative.
19. Remote Filter B 1 0

(Pressure Relief Valve
PRV)
20. CPAM (Cabin Pressure C 1 0 May be inoperative provided both

Acquisition Module) auto systems are operative.
DATE: 07/24/2007
TABLE KEY
Change
21. Ram Air System
1) Pressurized C 1 0 May be inoperative provided:

Configuration a) Automatic Pressurization
Control System is operative,
b) Manual Pressurization Control
c) Bleed Air Pressure Regulating
and Shut-Off Systems are
operative, and
d) Airplane is operated in
accordance with AFM
Limitations and Procedures.
2) Unpressurized C 1 0 (O) May be inoperative provided:

Configuration a) Airplane is operated in
unpressurized configuration,
and
accordance with AFM
Limitations and Procedures.
22. PSU Fan C 1 0 (O) May be inoperative provided:

a) Ambient Temperature is
95 degrees F (35 degrees C)
or cooler,
b) TRU electrical loads are
50 percent or less,
c) Right main TRU is operative,
and
d) Both Environmental Control
System (ECS) Packs are
operative.
REVISION NO. 7a PAGE NO. 22-1
DATE: 11/08/2010
TABLE KEY
22.Autoflight
Change
1. Authothrottle System C 2 0
2. Performance C 2 0 May be inoperative provided Quick

Management System Reference Handbook is immediately
(SmartPerf/TOLD)(GV) available to the flightcrew.
(GV-SP, GIV-X) C 2 0 May be inoperative provided

Performance Handbook is
immediately available to the
flightcrew.
3. Control Wheel Autopilot C 2 1 May be inoperative provided:

Disconnect Button a) Autopilot is not utilized below
1,500 feet AGL,
b) Approach minimums do not
require the use of the
autopilot, and
c) Airplane is piloted from the
side with operative button.
4. Autothrottle Disconnect C 2 1
Button (on Thrust Lever
Handles)
C 2 0 May be inoperative provided

Autothrottle is not used.
5. Autothrottle C 2 1
Engage/Disengage
Switch (on Thrust Lever
Stem)
C 2 0 May be inoperative provided

Autothrottle is not used.
6. Touch Control Steering D 2 0

Switch (TCS)
DATE: 07/05/2018
TABLE KEY
22.Autoflight
Change
7. Autopilot (Flight C 2 1 (O) Except for ER operations or

Guidance Computer where enroute operations or
(FGC)/Flight Director) approach minimums require its use,
may be inoperative provided airplane
is operated in accordance with
AFM Limitations in the event
operative FGC fails and Yaw Damper
is inoperative.
NOTE: AP/FGC is required for

MNPS, RVSM, RNP, and
PRNAV operations.
8. Yaw Damper System C 2 1 (O) Except for ER operations, may be

operated in accordance with
AFM Limitations.
9. Takeoff/Go-Around C 2 1 May be inoperative provided

(TO/GA) Button (on approach minimums do not require its
Power Lever Handle) use.

a) Both power levers are
operated manually for takeoff
and go-around, and
b) Autopilot and Flight Director
are not used below 500 feet
or MDA, whichever is higher.
NOTE: Flight Director Takeoff and

Go-Around guidance and
Autothrottle are not available
with both TO/GA switches
inoperative. Missed approach
if needed must be selected
via the MCDU.
10. Mach Trim System C 2 1 |

(GV-SP/GIV-X only)
DATE: 12/18/2017
TABLE KEY
23. Communications
Change
1. Communications System D - - Any in excess of those required by

(VHF, UHF) 14 CFR may be inoperative provided
it is not powered by the Emergency
AC Bus, Emergency DC Bus, Battery
Bus, Battery Direct Bus, or the DC
Transfer Bus and not required for
emergency procedures.
NOTE: Comm 1 is powered by the

Emergency Bus.
1) VHF Communication
Control Panel
a) Frequency Transfer Light C - 0

***
b) Frequency Transfer C - 0
*** Switch
c) Frequency Selector C - 2
*** Knob
d) Frequency Indication C - 2
***
DATE: 07/05/2018
TABLE KEY
23. Communications
Change
2. Cockpit Voice Recorder A 1 0 May be inoperative provided:

(CVR) (with Flight Data a) Flight Data Recorder (FDR) is
Recorder (FDR) operative, and
Installed) b) Repairs are made within
3 flight days.
1) Independent Power C 1 0
*** Source
Cockpit Voice Recorder A 1 0 May be inoperative provided repairs

(CVR) (Without Flight are made within three (3) flight days.
Data Recorder (FDR)
Installed)
2) Independent Power C 1 0 |
*** Source
Cockpit Voice Recorder A 1 0 May be inoperative provided repairs

(CVR) (Operator Other are made in accordance with
Than a Holder of an Air applicable 14 CFRs.
Carrier or Commercial
Operator Certificate)
3) Independent Power C 1 0 |
*** Source
3. Selective Call System C - 0 (O) May be inoperative provided

*** (SELCAL) alternate procedures are established
and used.
D - 0 May be inoperative provided

procedures do not require its use.
1) Channels C - 0 (O) May be inoperative provided

*** alternate procedures are established
and used.

DATE: 07/05/2018
TABLE KEY
23. Communications
Change
4. Emergency Locator
Transmitter (ELT)
1) Survival Type ELT D - - Any in excess of those required by

*** 14 CFR may be inoperative or
missing.
2) Fixed ELT A - 0 (M) May be inoperative provided:

*** a) System is deactivated, and
b) Repairs are made within
90 days, and |
c) Placard stating, “ELT not |
installed” is placed in view of |
the pilot. |
A - 0 May be missing provided: |

a) Repairs are made within |
90 days, and |
b) Placard stating, “ELT not |
the pilot. |
D - - (M) May be inoperative provided: |

a) Any in excess of those |
required by 14 CFR may be |
inoperative provided system is |
deactivated, and |
the pilot. |
D - - May be missing provided: |

a) Any in excess of those |
required by 14 CFR may be |
missing, and |
the pilot. |
(Continued)
DATE: 07/05/2018
TABLE KEY
23. Communications
Change
4. Emergency Locator |
Transmitter (ELT) |
(Cont’d) |
|
|
3) Remote ELT Switch D - - May be inoperative provided: |
*** a) Remote ELT Switch is |
deactivated, and |
b) ELT Switch is placed in the |
ARMED mode. |
4) ELT Indicator Light D - 0 |
*** |
|
5) ELT Aural Alarm D - 0 |
*** |
5. Crewmember Interphone |
*** System
1) Passenger Configuration
a) Flight Deck to Cabin, C - - (O) May be inoperative provided |

Cabin to Flight Deck alternate communication procedures
Function are established and used.
D - - May be inoperative provided

2) Flight Deck to Ground C - 0 (O) May be inoperative provided |

Function alternate procedures are established |
and used.

6. Interphone System D - 0
***
7. Cockpit Speaker C 2 0 May be inoperative provided:

a) Affected speaker is not
required for aural warnings,
and
b) An operative headset is
provided for each person on
cockpit duty.
DATE: 07/05/2018
TABLE KEY
23. Communications
Change
8. Passenger Address
*** Systems (PA)
1) Passenger Configuration C 1 0 (O) May be inoperative provided |

alternate, normal and emergency
procedures, and/or operating
restrictions are established and used.
a) Lavatory Speaker C - - (O) May be inoperative provided

alternate procedures are established
and used.
2) Cargo Only C 1 0 (O) May be inoperative provided

Configuration alternate, normal, and emergency
(Courier/Supernumerary procedures are established and used.
Address System)

a) Lavatory Speaker C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

9. Satellite Communication D - 0 May be inoperative provided

*** System procedures do not require their use.
10. Prerecorded Passenger C - 0 (O) May be inoperative provided

*** Announcement System alternate procedures are established
and used.

DATE: 11/07/2014
TABLE KEY
23. Communications
Change
11. Flight Deck Hand C - 0 May be inoperative provided

Microphone associated boom microphone
HOLDER OF AN AIR operates normally.
CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
D - 0 Any in excess of those required by

regulation may be inoperative.
12. Flight Deck Headset

Earphone/Headphone
and Boom Microphone
HOLDER OF AN AIR
CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
1) Headset Boom A - 0 May be inoperative provided:

Microphone a) Associated hand microphone
is installed and operates
normally, and
3 flight days.
D - - Any in excess of those required by

2) Headset C - 1 May be inoperative provided

Earphone/Headphone associated flight deck speaker
operates normally.

3) Active Noise D - 0 May be inoperative provided normal

Canceling/Reduction audio function of headset is
Function operative.
(Continued)
DATE: 11/07/2014
TABLE KEY
23. Communications
Change
12. Flight Deck Headset

Earphone/Headphone
and Boom Microphone
OPERATOR OTHER
THAN A HOLDER OF
AN AIR CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
(Cont’d)
1) Headset Boom A - 0 May be inoperative provided:

Microphone a) Associated hand microphone
is installed and operates
normally, and
b) Repairs are made in
accordance with applicable
regulations.

2) Headset C - 1 May be inoperative provided

Earphone/Headphone associated flight deck speaker
operates normally.
3) Active Noise D - 0 May be inoperative provided normal

Canceling/Reduction audio function of headset is
Function operative.
13. Right Side Radio C 1 0 May be inoperative provided:

Frequency Management a) Cross-side tuning function of
Unit (RFMU) (GV) the left RFMU is operative,
b) Radio tuning function of both
FMSs is operative, and
c) Inoperative RFMU is selected
OFF.
DATE: 07/05/2018
TABLE KEY
23. Communications
Change
14. Alerting Systems

*** (Audio/Visual)
***
a) Flight Deck Call Visual D 1 0 May be inoperative provided the flight

*** Alerting System deck audio alerting system is
operative.
|
b) Flight Attendant Visual C 1 0 (O) May be inoperative provided |
*** Alerting System alternate procedures are established
and used.
NOTE 1: Passenger to Attendant Call

System is considered a
Non-Essential Equipment
and Furnishings (NEF).
NOTE 2: Any visual alerting system

function(s) that are
operative may be used.
D - 0 May be inoperative provided |

procedures do not require its use. |
c) Flight Attendant Audio C - 0 (O) May be inoperative provided

*** Alerting System alternate procedures are established
and used.

DATE: 07/05/2018
TABLE KEY
23. Communications
Change
15. Handset Systems
a) Flight Deck C 1 0 (O) May be inoperative provided:

a) Flight Deck to cabin
communication operates
normally, and
b) Alternate procedures are
established and used.

b) Cabin D - 0 May be inoperative |

providedprocedures do not require its |
use.
16. Radio Tuning Function See item 34-45 MCDU for GV-SP,
(GV-SP, GIV-X) GIV-X Radio Tuning Function relief.
DATE: 07/05/2018
TABLE KEY
23. Communications
Change
17. High Frequency (HF) D - - Any in excess of those required by

Communication System 14 CFR may be inoperative.
|
C - 1 (O) May be inoperative while |
conducting operations that require
two LRCS provided:
a) Aircraft SATVOICE system |
operates normally,
b) SATVOICE services are
available as a LRCS over the
intended route of flight.
c) The ICAO flight plan is
updated (as required) to notify
ATC of the communication
equipment status of the
aircraft, and
d) Alternate procedures are
18. NAVCOM Radio C 1 0 May be inoperative provided

(GV-SP, GIV-X) operations do not require its use.
19. Audio Interface Unit B 2 1 May be inoperative provided flight

(AIUs) (GV only) does not require use of HF radio.
DATE: 12/18/2017
TABLE KEY
23. Communications
Change
20. Datalink System C - 0 (O) May be inoperative provided

*** (GV) alternate procedures are established
and used.
NOTE 1: Data Link system is

required for ADS-C and/or
CPDLC operations.
NOTE 2: Datalink must be operative

whenever flights in RNP 4
airspace are conducted.
D - 0 May be inoperative provided routine

NOTE 1: Data Link system is

required for ADS-C and/or
CPDLC operations.
NOTE 2: Datalink must be operative

21. Modular Radio Cabinet A 2 1 May be inoperative provided:

(MRC) Power Source a) Associated Comm and Nav
(GV-SP, GIV-X) radios and opposite ATC are
operative, and
1 flight day.
NOTE: Dispatch is acceptable with a

MRC 1 or MRC 2 failed and
EICAS blue messages
“APM FAIL” and “ASCB FAIL”
displayed.
22. Headset Combined with Item 12 in Rev. 8.

DATE: 12/18/2017
TABLE KEY
23. Communications
Change
23. Flight Deck Hand D - 0 Any in excess of those required by

Microphone regulations may be inoperative.
OPERATOR OTHER
THAN A HOLDER OF
AN AIR CARRIER OR
COMMERCIAL
OPERATOR
CERTIFICATE
C - 0 May be inoperative provided

associated boom microphone
operates normally.
24. Communications C - 0 (O) May be inoperative provided

*** Management alternate procedures are established
Function/CMF and used.
(GV-SP, GIV-X)
NOTE 1: CMF system is required for
ADS-C and/or CPDLC
operations.
NOTE 2: CMF must be operative

D - 0 May be inoperative provided routine

NOTE 1: CMF system is required for

ADS-C and/or CPDLC
operations.
NOTE 2: CMF must be operative

DATE: 08/24/2015
TABLE KEY
23. Communications
Change
25. Controller Pilot Data Link

*** Communication
(CPDLC)
1) ATN B1 D 1 0 (O) May be inoperative provided

*** (PM-CPDLC/Link 2000+) enroute operations do not require its
use.
2) FANS 1/A D 1 0 (O) May be inoperative provided

*** (ADS-C/CPDLC) enroute operations do not require its
use.
DATE: 07/05/2018
TABLE KEY
24. Electrical Power
Change
1. Engine Generator B 2 1 (O) Except for ER operations, may be |

(GV, GV-SP) inoperative provided:
a) APU Generator is used for all
phases of flight,
b) Airplane is operated at or
below FL 450, and
c) Standby Electrical System is
operative.
NOTE 1: This relief only applies to |

airplanes not affected by |
AD 2017-20-08. |
NOTE 2: Crew must verify and abide |

by AD and AFM APU |
limitations. |
(GIV-X) B 2 1 (O) Except for ER operations, may be

inoperative provided:
a) APU Generator is used for all
phases of flight,
below FL 370,
operative, and
d) FSECU SPOST is performed
manually prior to the first flight
of the day for airplanes
equipped with ASC 086 and
dispatching with the left
generator inoperative.
NOTE 1: This relief only applies to |

airplanes not affected by |
AD 2017-20-08. |
NOTE 2: Crew must verify and abide |

by AD and AFM APU |
limitations. |
DATE: 07/05/2018
TABLE KEY
Change
2. APU Generator B 1 0 (M) Except for ER operations, may be

a) Both Engine Generators are
operative, and
b) Standby Electrical System is
operative.
C 1 0 (M) Except for ER operations, may be

inoperative provided APU is not used.
3. Transformer-Rectifier B 5 4 (M) May be inoperative provided: |

Unit (TRU) a) Both Generators are
operative,
b) Both essential TRUs are
operative,
c) Auxiliary TRU is operative,
d) APU Generator is operative,
e) Both Battery chargers are
operative,
f) Both Main Airplane Batteries
are operative, and
g) Associated circuit breaker is |
pulled and collared. |
4. Battery Charger B 2 1 (M) May be inoperative provided: |

a) Both Engine Generators are
operative,
b) APU Generator is operative,
c) Associated circuit breaker(s) |
is pulled and collared, and |
d) Standby Electrical System is
operative.
DATE: 07/05/2018
TABLE KEY
Change
5. Main Airplane Battery B 2 1 (M) May be inoperative provided: |

a) There are no other electrical
power source failures,
b) Associated Battery cables are
disconnected and secured,
and |
c) Associated circuit breakers |
are pulled and collared.
B 2 1 (M) May be inoperative provided: |

a) Airplane is operated in Day |
VMC only, |
operative,
c) Associated Battery cables are
disconnected and secured,
and |
d) Associated circuit breakers |
DATE: 11/07/2014
TABLE KEY
Change
6. Battery Ammeter C 2 0 May be inoperative provided:

(Overhead Panel) a) Associated voltmeter is
operative, and
b) Both battery charger fail
messages are operative.
C 2 0 May be inoperative provided battery

ammeter indications are available in
EICAS.
(EICAS Indication) C 2 0 May be inoperative provided the

battery ammeters in overhead panel
are operative.
7. Battery Voltmeter C 2 0 May be inoperative provided

(Overhead Panel) associated ammeter is operative.
C 2 0 May be inoperative provided Battery

Voltmeter indications are available on
EICAS.
(EICAS Indication) C 2 0 May be inoperative provided Battery

Ammeters indications are available
on EICAS.
C 2 0 May be inoperative provided Battery

Voltmeters in overhead panel are
operative.
DATE: 11/07/2014
TABLE KEY
Change
8. Electrical Power System

EICAS Display
1) L Gen Voltmeter C 1 0 May be inoperative if the frequency

and loadmeter are operative.
2) L Gen Frequency Meter C 1 0 May be inoperative if the voltmeter

3) L Gen Loadmeter C 1 0 May be inoperative if the voltmeter

and frequency meter are operative.
4) R Gen Voltmeter C 1 0 May be inoperative if the frequency

5) R Gen Frequency Meter C 1 0 May be inoperative if the voltmeter

6) R Gen Loadmeter C 1 0 May be inoperative if the voltmeter

7) APU Voltmeter C 1 0 May be inoperative if the frequency

meter and loadmeter are operative.
8) APU Frequency Meter C 1 0 May be inoperative if the voltmeter

9) APU Loadmeter C 1 0 May be inoperative if the voltmeter

10) Ext AC Pwr Voltmeter D 1 0 May be inoperative provided:

a) The frequency meter and
loadmeter are operative, and
b) External AC power is not
used.
(Continued)
DATE: 11/07/2014
TABLE KEY
Change
8. Electrical Power System

EICAS Display
(Cont’d)
11) Ext AC Pwr Frequency D 1 0 May be inoperative if the voltmeter

Meter and loadmeter are operative.
D 1 0 May be inoperative if external AC

power is not used.
12) Ext AC Loadmeter D 1 0 May be inoperative if the frequency

and voltmeter are operative.
D 1 0 May be inoperative if external AC

power is not used.
13) Main, Essential, and C 5 0 May be inoperative if loadmeters are

AUX TRU Voltmeter operative.
14) Main, Essential, and C 5 0 Maybe inoperative if the voltmeters

AUX TRU Loadmeter are operative.
(GV-SP, GIV-X)
(GV) C 5 0 May be inoperative provided:

a) Voltmeters are operative, and
accordance with
AFM Limitations.
15) Ext DC Pwr Voltmeter D 1 0 May be inoperative if the loadmeter is

operative.
D 1 0 May be inoperative if external DC

power is not used.
16) Ext DC Pwr Loadmeter D 1 0 May be inoperative if the voltmeter is

operative.
D 1 0 May be inoperative if external DC

power is not used.
DATE: 07/05/2018
TABLE KEY
Change
9. Master Power Switch C 4 3 May be inoperative provided

Light associated AC loadmeter and
(Left, Right, APU, EXT) voltmeter are operative and selected
for monitoring on the AC Synoptic.
10. Battery Temperature D 1 0

*** Indicating System
11. Standby Electrical C 1 0 May be inoperative provided both

System engine driven generators and APU
generator are operative.
12. External Power System D 1 0
13. Low Battery Power D 1 0

*** Audible Warning System
(Sonalert)
14. Ground Service Bus D 1 0

System
15. 50Hz/60Hz AC Electrical D - 0 (M) May be inoperative provided |

*** Power System associated circuit breaker is pulled |
and collared. |
DATE: 12/18/2017
TABLE KEY
Change
16. IRU Back Up Battery A 2 0 May be inoperativeprovided:

(GV) a) Airplane is operated in Day
VMC conditions, and
1 flight day.
A 2 0 May be inoperative provided:

a) All other components of the
Electrical Power system are
operative, and
1 flight day.
IRU Back Up Battery B 2 1 May be inoperative provided that the

(GV-SP, GIV-X) affected battery is located in the #2
and #3 IRU back up battery position.

a) Airplane is operated in Day
VMC conditions, and
1 flight day.
NOTE: EICAS message “IRU SEC

PWR FAIL” will be displayed.

a) All other components of the
Electrical Power system are
operative, and
1 flight day.
17. Standby Inverter B 1 0 (O) May be inoperative provided:

a) APU generator is operative,
b) HMG is operative,
c) No failure exists in the CPCS
system prior to each takeoff,
and
d) Flightcrew briefs pilot
responsibilities and actions in
the event of a dual generator
failure.
DATE: 07/05/2018
TABLE KEY
25. Equipment/Furnishings
Change
1. Overwater Equipment D - - As required by 14 CFR.
2. Passenger Seat
|
|
1) Passenger Seat D - - May be inoperative provided: |
(Includes all a) Seat does not restrict access |
Configurations and to any emergency exit, egress |
Locations) route, or main aisle, and |
b) The affected seat(s) is |
blocked and placarded
“DO NOT OCCUPY”.
NOTE 1: A seat with an inoperative

seat belt or shoulder |
harness is considered |
inoperative.
|
NOTE 2: Affected seat(s) may
include the seat(s) behind
and/or adjacent outboard
seats.
2) Positioning Controls for D - - (M) May be inoperative and seat |

Taxi, Takeoff, and occupied provided seat is secured in |
Landing (TTL) the taxi, takeoff, and landing (TTL) |
(Mechanical and/or position. |
Electrical) |
D - - May be inoperative and seat

occupied provided seat back is
immovable in the taxi, takeoff, and |
landing (TTL) position. |
(Continued)
DATE: 07/05/2018
TABLE KEY
Change
2. Passenger Seat
(Cont’d) |
3) Under Seat Baggage C - - (O) May be inoperative provided: |

*** Restraining System a) Baggage is not stowed under
seat with inoperative
restraining system, |
b) Associated seat is placarded
“DO NOT STOW BAGGAGE
UNDER THIS SEAT”, and
c) Procedures are established to
alert Cabin Crew of
inoperative restraining |
system. |
4) Armrest |
a) With Seat Positioning D - - (M) May be inoperative or missing |

Controls for Taxi, and seat occupied provided: |
Takeoff, and Landing a) Armrest does not restrict |
(TTL) and/or Other access to any Emergency |
Controls Exit, egress route, or main |
aisle, and |
b) If Armrest with seat control is |
missing or removed, seat is |
secured in taxi, takeoff, and |
landing (TTL) position. |
b) Without Seat Positioning D - - May be inoperative or missing and |

Controls for Taxi, seat occupied provided it does not |
Takeoff, and Landing restrict access to any emergency exit, |
(TTL) and/or Other egress route, or main aisle. |
Controls |
5) Divan High Back C - - Relief incorporated in item 25-2-1. |

Revision 10. |
6) Electrical/Electronic C - - (M) May be inoperative and seat |

*** System/Component occupied provided associated
component(s) is deactivated.
DATE: 07/05/2018
TABLE KEY
Change
3. Crewmember Shoulder Deleted Rev. 10 |

Harness
4. Observer Seat(s)
1) Primary Observer Seat A - - May be inoperative provided:

(including associated a) A passenger seat in the
equipment) passenger cabin is made
available to an FAA inspector
for the performance of official
duties, and
2 flight days.
A - - May be inoperative provided:

a) Required minimum safety
equipment (safety belt and
oxygen) is available,
b) Seat is acceptable to the
FAA inspector for
performance of official duties,
and
c) Repairs are made within
2 flight days.
DATE: 07/05/2018
TABLE KEY
Change
4. Observer Seat(s) NOTE 1: These provisos are

(Cont’d) intended to provide for
occupancy of the above
seats by an FAA inspector
when the minimum safety
equipment (oxygen and
safety belt) is functional and
the inspector determines
the condition to be
acceptable.
NOTE 2: The pilot-in-command will

determine if the minimum
safety equipment is
functional for other persons
authorized to occupy any
observer seat(s).
2) Observer Seat Not D - 0 NOTE: The pilot-in-command will

Required by 14 CFR determine if the minimum
(including associated safety equipment is functional
equipment) for other persons authorized
to occupy any observer
seat(s).
5. Megaphone D - -
***
6. Flotation Device D - - Any in excess of those required by

14 CFR may be missing or
inoperative.
NOTE: Inoperative floatation device |

is tagged inoperative, |
removed from the installed |
location, and placed out of |
sight so it cannot be mistaken |
for a functional device. |
DATE: 11/07/2014
TABLE KEY
Change
7. “Fasten Seat Belt While C - - One or more signs or placards may

*** Seated” Sign or Placard be illegible or missing provided a
legible sign or placard is readable
from each occupied passenger seat.
8. Storage Bin/Cabin, C - - (M) May be inoperative provided:

*** Galley, and Lavatory a) Procedures are established to
Storage secure the affected bin,
Compartment/Closet compartment, or closet in the
closed position,
b) Associated bin, compartment,
or closet is prominently
placarded “DO NOT USE”,
c) Any emergency equipment
located in affected
compartment is considered
inoperative, and
d) Affected bin, compartment, or
closet is not used for storage
of any items except for those
permanently affixed.
NOTE: For overhead bins, if no

partitions are installed, the
entire overhead bin is
(Continued)
DATE: 11/07/2014
TABLE KEY
Change
8. Storage Bin/Cabin, C - - (M)(O) May be inoperative provided:

*** Galley, and Lavatory a) For non-retractable doors,
Storage affected door is removed,
Compartment/Closet b) For retractable doors, affected
(Cont’d) door is removed or secured in
the retracted (fully open)
position,
c) Affected bin, compartment or
closet is not used for storage
of any items, except those
permanently affixed,
d) Affected bin, compartment, or
closet is prominently
placarded “DO NOT USE”,
e) Procedures are established
and used to alert crew
members and passengers of
inoperative bins,
compartments or closets, and
f) Passengers are briefed that
associated bin, compartment,
or closet is not used.
NOTE 1: For overhead bins, if no

partitions are installed, the
entire overhead bin is
NOTE 2: Any emergency equipment

located in the affected bin,
compartment, or closet
(permanently affixed) is
available for use.
1) Storage Compartment D - 0 (M) May be inoperative in unlocked

*** Key Lock position provided doors can be
secured by other means.
DATE: 07/05/2018
TABLE KEY
Change
9. Cargo Restraint System A - - (M) May be inoperative, or missing |

*** provided:
a) Acceptable cargo loading
limits from an approved
source, i.e., an Approved
Cargo Loading Manual, or
Weight and Balance
Document are observed, and
b) Repairs are made prior to the
completion of the next heavy
maintenance visit.
C - - May be inoperative, or missing

provided cargo compartment remains
empty.
10. Flight Attendant Seat D 1 0 May be inoperative provided:

*** Assembly (with only a) Affected seat is not occupied, |
One (1) flight Attendant and
Seat) b) Folding type seat stows
automatically or is secured in
the retracted position.
NOTE 1: An automatic folding seat

that will not stow
automatically is considered
inoperative.
NOTE 2: A seat position with an

inoperative or missing
restraint system is
1) All Cargo Configuration D - - May be inoperative provided affected

seat or seat assembly is not
occupied.
DATE: 12/18/2017
TABLE KEY
Change
11. Galley/Cabin Waste C - - (M)(O) May be inoperative provided:

*** Receptacle Access a) The container is empty and
Door/Cover the access is secured to
prevent waste introduction
into the compartment, and
b) Procedures are established to
ensure that sufficient
galley/cabin waste
receptacles are available to
accommodate all waste that
may be generated on a flight.
12. Exterior Lavatory Door

*** Ashtray
1) Airplanes with multiple A - - Up to and including 50 percent may

exterior lavatory door be missing or inoperative for 10 days.
ashtray installed
A - - More than 50 percent may be missing

or inoperative for three days.
NOTE: Crew lavatories are included

in the total aircraft exterior
lavatory door ashtray count.
2) Airplanes with only one A 1 0 May be missing or inoperative for

exterior lavatory door 10 days.
ashtray installed
13. External Camera System D 1 0

***
14. Emergency Vision D - 0 May be inoperative or removed.

*** Assurance System
(EVAS)
STC No. SA00892LA
DATE: 07/05/2018
TABLE KEY
Change
15. Pilot Seat(s)
1) Vertical Adjustment C - - (M) May be inoperative provided: |

a) Seat is secured at the
individual crewmember’s
requirements, and
b) Fore-aft adjustment is
operative.
2) Armrest C - - (M) May be inoperative provided: |

a) Affected armrest is in the
upright position or removed,
and
b) Seat is acceptable to the
affected crewmember.
3) Recline Adjustment C - - (M) May be inoperative provided: |

a) Seat is secured at a position
acceptable to the affected
crewmember, and
b) Seat is able to move full
Fore-Aft on its track.
4) Lumbar Support C - - May be inoperative provided seat is

crewmember.
5) Thigh Support C - - May be inoperative provided seat is

crewmember.
16. Rudder Pedal C 2 0 (M) May be inoperative provided: |

Adjustment a) Adjustments can be secured
in a position that suits
individual pilot(s), and
b) Position of pedal(s) permits
normal full flight control
movement.
|
DATE: 07/05/2018
TABLE KEY
Change
17. Keyed Lock D - 0 May be inoperative provided the |

associated access panel, door,
compartment, or cap is verified
secure before each departure.
18. Airplane Ladder C - 0 (O) May be inoperative or removed. |
1) Ladder Hardware D - 0
(Pit Pins, Lanyards, etc.)
19. Baggage Compartment |

*** Shelve
1) Shelf Stowage Strap D - 0 May be inoperative or removed

*** provided the shelves remain in the
down position.
2) Shelf Support Strap D - 0 May be inoperative or removed

*** provided the shelves remain in the
stowed (up) position and are not
used.
20. Crewmember Flashlight C - 0 May be inoperative or missing |

Holder Assembly provided crewmember has a
(including Flashlight) flashlight of equivalent characteristics
readily available.
DATE: 07/05/2018
TABLE KEY
Change
21. Non-Essential |
Equipment & Furnishings
(NEF)
|
1) Non-Essential - - 0 May be inoperative, damaged or |
*** Equipment and missing provided item(s) is deferred
Furnishings (NEF) in accordance with operator’s NEF
deferral program. The NEF program,
procedures and processes are
outlined in the operator’s (insert
name) Manual. (M) and (O)
procedures, if required, must be
available to flightcrew and included in
appropriate operator’s document.
NOTE: Exterior lavatory door

ashtrays are not considered
NEF items.
22. Automatic External D - - Any in excess of those required by |

*** Defibrillator (AED) and/or 14 CFR may be incomplete, missing,
Associated Equipment or inoperative.
23. Emergency Medical Kit D - - Any in excess of those required by |

*** (EMK) and/or Associated 14 CFR may be incomplete, missing,
Equipment or inoperative.
24. First Aid Kit (FAK) and/or D - - Any in excess of those required by |
*** Associated Equipment 14 CFR may be incomplete, missing,
or inoperative.
DATE: 07/05/2018
TABLE KEY
Change
25. Flightcrew Sleeping C - 0 (M)(O) May be inoperative provided |

*** Facility – Crew Seat crew seat is secured in a position
(includes crew seat acceptable to the crewmember(s)
recline mechanism, who will occupy the crew seat.
berthing mechanism,
armrests, swivel NOTE: All other equipment in the
mechanism, and flightcrew sleeping facilities is
electrical/electronic covered by the NEF program.
systems/components)
D - 0 May be inoperative provided:

a) Crew seat is not occupied,
and
b) Crew Rest is placarded
“INOPERATIVE – DO NOT
USE.”
DATE: 07/05/2018
TABLE KEY
Change
26. Cabin Management D 1 0 |

System
1) Cabin Power Bus D 1 0

*** Controller (043A1)
2) Advanced Cabin Server D 2 0

*** (428A4, 428A5)
3) GCMS Controller D 2 0
*** (179A5, 179A6)
4) I/O Concentrator D 2 0
*** (178A1, 178A2)
5) Aft I/O Concentrator D 2 0

*** (178A3, 178A4)
6) AVDS Node D 4 0
***
7) Galley Touch Screen D 1 0

*** (502S2)
8) Vestibule Touch Screen D 1 0

*** (482S1)
9) Maintenance Server D 1 0
***
10) Switching Node D 25 0

***
DATE: 07/05/2018
TABLE KEY
26. Fire Protection
Change
1. Portable Fire D - - Any in excess of those required by

Extinguisher 14 CFR may be inoperative or
missing provided:
a) Inoperative fire extinguisher is
tagged inoperative, removed
from the installed location,
and placed out of sight so it
cannot be mistaken for a
functional unit, and
b) Required distribution is
maintained.
2. Wing Overheat Warning C 2 0 Except for ER operations, may be

System inoperative provided:
a) Wing Anti-Ice is not used, and
b) Airplane is not operated in
known or forecast icing
conditions.
3. APU Fire Detection C 1 0 (M) Except for ER operations, may be |

a) APU is considered |
inoperative, and |
b) Associated circuit breakers |
DATE: 11/08/2010
TABLE KEY
26. Fire Protection
Change
4. Rear Baggage C - 0 May be inoperative provided:

Compartment Smoke a) Internal baggage door
Detector System remains OPEN, and
below FL 400.
C - 0 May be inoperative provided:

a) Rear baggage compartment is
not used,
b) Internal baggage door
remains CLOSED,
c) Flightcrew investigates
baggage compartment for
possible fire in the event the
“BAG EER HOT” message
displays, and
accordance with
AFM Limitations.
DATE: 07/05/2018
TABLE KEY
26. Fire Protection
Change
5. Lavatory Smoke C - - (M)(O) For each lavatory, the lavatory

*** Detection System smoke detection system may be
a) Lavatory waste receptacle is
empty,
b) Associated lavatory door is
LOCKED, CLOSED, and
placarded, “INOPERATIVE–
DO NOT ENTER”, and
c) Lavatory is used only by
crewmember.
NOTE 1: These provisos are not

intended to prohibit lavatory
use or inspections by
crewmembers.
NOTE 2: Lavatory smoke detection

system is not required for
all-cargo operations.
D - 0 Any in excess of that required by |

14 CFR may be inoperative. |
DATE: 07/05/2018
TABLE KEY
26. Fire Protection
Change
6. Lavatory Fire C - - For each lavatory, the lavatory fire

*** Extinguisher System extinguisher system may be
inoperative provided Lavatory Smoke
Detection system operates normally. |
C - - (M) For each lavatory, the lavatory |

fire extinguisher system may be
a) Lavatory waste receptacle is
empty,
LOCKED, CLOSED, and
placarded, “INOPERATIVE –
DO NOT ENTER”, and
c) Lavatory is used only by
crewmembers.
NOTE 1: These provisos are not

intended to prohibit lavatory
use or inspections by
crewmembers.
NOTE 2: A lavatory fire extinguisher

system is not required for
all-cargo operations.
D - 0 Any in excess of that required by |

14 CFR may be inoperative. |
7. Galley Smoke Detection D - 0

*** System
8. Galley Fire Extinguishing D - 0

*** System
DATE: 02/04/2010
TABLE KEY
26. Fire Protection
Change
9. Engine Fire Detection C 2 1 Except for ER operations, one

System complete loop (A or B) may be
inoperative provided the Fault
Switch/Light is pressed to isolate the
faulty loop and illuminate the OFF
portion of the switch light.
10. Flame Detector D - -

***
11. Electronic Equipment C - 0

Rack Overheat Warning
System
12. Passenger Compartment D - 0 May be inoperative provided door

*** Closet Smoke Detector remains OPEN for visual check from
crew stations.
13. Entranceway Baggage D - - May be inoperative provided door

*** Compartment Smoke remains OPEN for visual check from
Detector crew stations.
14. Cargo Compartment Fire C - 0 (O) May be inoperative provided

*** Detection/Suppression procedures are established and used
System to ensure the associated cargo
compartment remains empty, or is
verified to contain only empty cargo
handling equipment, ballast
(ballast may be loaded in ULDs)
and/or fly away kits.
NOTE 1: Operators MELs should

define which items are
approved for inclusion in the
fly away kits and which
materials can be used as
ballast.
NOTE 2: Class E cargo

compartments require only
the installation of smoke or
fire detection system
(not suppression).
DATE: 07/05/2018
TABLE KEY
26. Fire Protection
Change
15. APU Fire Bottle C 1 0 (M)(O) Except for ER operations, |

*** may be inoperative provided:
a) APU is considered
inoperative,
b) Both engine driven generators
are operative,
c) Standby electrical system is
operative, and
are pulled and collared. |
DATE: 07/05/2018
TABLE KEY
27. Flight Controls
Change
1. Rudder Limit Indication C 1 0 May be inoperative provided Single

System Rudder Indication System is
operative.
2. Single Rudder Indication C 1 0 May be inoperative provided Rudder

System Limit Indication System is operative.
3. Automatic Ground C 1 0 (O) May be inoperative provided

Spoiler System airplane is operated in accordance
with AFM Limitations.
4. Electric Elevator Trim C 1 0 (O) May be inoperative provided:

System a) Electric Elevator Trim remains
OFF,
b) Both Flap/Stabilizer Control
Channels are operative, and
accordance with
AFM Limitations.
5. Control Wheel Elevator C 2 1 (O) May be inoperative provided pilot

Trim Switch flying has operative switch.
6. Flap/Stabilizer Control B 2 1 Channel may be inoperative

Channel provided:
a) Electric Pitch Trim System is
operative, and
b) Alternate control is verified to
be operative before each
departure.
7. Single Speed Brake C 1 0 (O) May be inoperative provided |

Indication System Single Rudder Indication System is
operative.
DATE: 07/05/2018
TABLE KEY
27. Flight Controls
Change
8. Elevator Trim Actuator C 2 0 (M) May be inoperative provided the

*** Heater System associated circuit breaker(s) is pulled |
and collared. |
9. Aileron Trim Actuator C 1 0 (M) May be inoperative provided the

*** Heater associated circuit breaker is pulled |
(GV-SP) and collared. |
10. Autopilot Elevator Servo C 2 1 (M) May be inoperative provided the

(GV-SP, GIV-X) associated circuit breaker is pulled |
and collared. |
11. Autopilot Pitch Trim C 2 1 (M) May be inoperative provided the

Servo (GV-SP, GIV-X) associated circuit breaker is pulled |
and collared. |
12. Autopilot Aileron Servo C 2 1 (M) May be inoperative provided the

(GV-SP, GIV-X) associated circuit breakeris pulled |
and collared. |
13. Autopilot Yaw Damper C 2 1 (M) May be inoperative provided the

Servo (GV-SP, GIV-X) associated circuit breaker is pulled |
and collared. |
DATE: 07/05/2018
TABLE KEY
27. Flight Controls
Change
14. Stall Barrier System A 2 1 (M)(O) May be inoperative provided: |

a) Angle of Attack indication is
available on both PFDs,
b) Associated circuit breakers |
are pulled and collared, |
c) Alternate procedures are
established and used, and
d) Repairs are made within
2 flight days.
15. Flight Control Synoptic C 1 0 May be inoperative provided the

Display (GV) affected control surface is visually
checked for full, free, and correct
movement prior to each flight.
(GV-SP, GIV-X) C - 0 May be inoperative provided the

affected control surface is visually
checked for full, free, and correct
movement prior to each flight.
16. Gust Lock C 1 0 (O) May be inoperative provided flight

controls are secured in an alternate
manner.

airplane is parked in sheltered area
unaffected by atmospheric
conditions.
DATE: 12/18/2017
TABLE KEY
28. Fuel
Change
1. Fuel Tank Temperature C 2 0 (O) May be inoperative provided:

System a) Total Air Temperature is used
(GV, GV-SP) as an indication of fuel
temperature, and
accordance with
AFM Limitations.
Fuel Tank Temperature C 1 0 (O) May be inoperative provided:

System a) Total Air Temperature is used
(GIV-X) as an indication of fuel
temperature, and
accordance with
AFM Limitations.
2. EICAS or Standby C 2 1 (M) May be inoperative provided:

RFMU (GV)/MCDU a) Associated Standby Fuel
(GV-SP, GIV-X) Fuel Quantity Indicating System or
Quantity Indicating EICAS Fuel Quantity
System Indicating System is
operative, and
b) Either the primary or the
standby fuel quantity
indication displays Left and
Right Fuel Quantity.
(Continued)
DATE: 07/05/2018
TABLE KEY
28. Fuel
Change
2. EICAS or Standby C 2 1 (M)(O) Except for ER operations, |

RFMU (GV)/MCDU either Left or Right Fuel Quantity
(GV-SP, GIV-X) Fuel display may be inoperative provided:
Quantity Indicating a) Both tanks are completely
System filled using over wing
(Cont’d) refueling,
b) Both fuel flow meters are
operative,
c) After takeoff, power is set by
matching fuel flow indications
on both engines, and
d) Flightcrew maintains a log of
fuel burned.
NOTE 1: Failure to display either Left

or Right Fuel Quantity
exists in both the primary
and secondary fuel quantity
indications.
NOTE 2: Total fuel indication will be

invalid with an inoperative
indicator.
(Continued)
DATE: 07/05/2018
TABLE KEY
28. Fuel
Change
2. EICAS or Standby C 2 1 (M)(O) Except for ER operations, |

RFMU (GV)/MCDU either Left or Right Fuel Quantity
(GV-SP, GIV-X) Fuel display may be inoperative provided:
Quantity Indicating a) Affected tank is defueled
System before each refueling,
(Cont’d) b) Affected tank is fueled with a
known quantity of fuel,
c) Both fuel flow meters are
operative,
d) After takeoff, power is set by
matching fuel flow indications
on both engines, and
e) Flightcrew maintains a log of
fuel burned.
NOTE 1: Failure to display either Left

or Right Fuel Quantity
exists in both the primary
and secondary fuel quantity
indications.
NOTE 2: Total fuel indication will be

invalid with an inoperative
indicator.
DATE: 12/18/2017
TABLE KEY
28. Fuel
Change
3. Fuel Low Quantity C 2 0 May be inoperative provided:

Warning System a) Both Fuel Quantity Indicating
Systems are operative,
b) All Fuel Boost Pumps are
operative, and
c) Fuel Crossflow Valve is
OPENED when either wing
tank contains 2,000 lbs. or
less fuel.
4. Fuel Boost Pump C 4 3 Except for ER operations, may be

a) Fuel Crossflow Valve is
operative,
b) Fuel Intertank Valve is
operative,
c) Both Fuel Low Quantity
Warning Systems are
operative, and
accordance with
AFM Limitations.
DATE: 02/04/2010
TABLE KEY
28. Fuel
Change
5. Fuel Intertank Valve C 1 0 (M) Except for ER operations, may be

a) All Fuel Boost Pumps are
operative,
b) Fuel Crossflow Valve is
operative,
c) Fuel Quantity Indicating
d) Intertank Valve is verified
CLOSED and electrically
deactivated.
6. Heated Fuel Return C 2 0 May be inoperative provided:

System (HFRS) a) Flightcrew monitors fuel tank
(GV, GV-SP) temperature, and
accordance with
AFM Limitations.
7. Fuel Boost Pump C 4 3 (O) Except for ER operations, may be

Warning System inoperative provided:
a) Fuel Crossflow Valve is
operative,
operative, and
accordance with
AFM Limitations.
DATE: 12/18/2017
TABLE KEY
28. Fuel
Change
8. Fuel Crossflow Valve
1) Failed CLOSED C 1 0 (O) Except for ER operations, may be

operative,
operative,
d) Fuel Intertank Valve is OPEN
when either wing tank
contains 2,000 lbs. or less
fuel, and
accordance with
AFM Limitations.
NOTE: Avoid uncoordinated

maneuvers when Fuel
Intertank Valve is OPEN.
2) Failed OPEN C 1 0 Except for ER operations, may be

operative,
operative,
accordance with
AFM Limitations, and
e) Fuel tank temperature system
must be operative.
NOTE: Avoid uncoordinated

maneuvers when Fuel
DATE: 12/18/2017
TABLE KEY
28. Fuel
Change
9. Pressure Fueling System D 1 0 (M) May be inoperative provided

(Single Point Refueling) procedures are established to
deactivate Pressure Fueling System.
10. Ground Service Control D 1 0

Panel
11. Automatic Fueling D 1 0

System
12. Fuel Cap Chain D - 0
13. Single Point Refueling C 1 0 May be inoperative or missing

Cap provided the single point refueling
receptacle is checked for leaks
before every takeoff.
14. Mid Wing Ejector (MWE) C 2 0 May be inoperative provided the

*** System maximum fuel load for dispatch is
(GV, GV-SP only) limited to 9,000 lbs. per tank for a
total fuel load of 18,000 lbs.
DATE: 07/05/2018
TABLE KEY
29. Hydraulic Power
Change
1. Brake Accumulator D 1 0
Pressure Gauge
(Nose Wheel Well)
2. Auxiliary Hydraulic Pump C 1 0 May be inoperative provided cockpit

Pressure Indication Brake Accumulator pressure gauge is
operative.
3. Power Transfer Unit C 1 0 (O) May be inoperative provided:

(PTU) Hydraulic a) Left Hydraulic Pressure
Pressure Indication Indication is operative,
b) PTU Hydraulic system is
operative, and
c) Before left engine start, HMG
operational check is
performed.
4. PTU Hydraulic Pump C 1 0 May be inoperative provided manual

(Auto Mode) mode is verified to be operative
before every flight.
5. Auxiliary Hydraulic Pump C 1 0 May be inoperative provided Auxiliary

(Auto Mode) pump is selected ON for takeoff and
landing.
6. Left Hydraulic System D 1 0 (O) May be inoperative provided |

Quantity Gauge (Ground quantity is checked by reservoir
Service Control Panel – indicator or using hydraulic quantity
Aft Equipment Area) indication on hydraulic synoptic
before each departure.
7. Right Hydraulic System D 1 0 (O) May be inoperative provided |

Quantity Gauge (Ground quantity is checked by reservoir
Service Control Panel – indicator or using hydraulic quantity
Aft Equipment Area) indication on hydraulic synoptic
before each departure.
DATE: 11/07/2014
TABLE KEY
29. Hydraulic Power
Change
8. Left Hydraulic System C 1 0 May be inoperative provided quantity

Quantity Indication is checked by reservoir indicator or
(EICAS) Ground Service Control Panel Left
Hydraulic Quantity gauges before
each departure.
9. Right Hydraulic System C 1 0 May be inoperative provided quantity

Quantity Indication is checked by reservoir indicator or
(EICAS) Ground Service Control Panel Right
Hydraulic Quantity gauges before
each departure.
10. Hydraulic Reservoir C 2 0 NOTE: Accuracy of hydraulic quantity

Temperature Sensor indication will be degraded
during long flights in cold soak
conditions. If Right Hydraulic
System (R SYS) sensor has
failed in flight, there is no
protection against overheating
R SYS pumps during Power
Transfer Unit (PTU)
operation. In flight, with either
or both sensors failed, there is
no warning of hot hydraulic
system temperatures.
11. Hydraulic Reservoir D 1 0 (M) May be inoperative provided

Replenishing System hydraulic reservoirs are replenished
as needed using approved servicing
techniques.
DATE: 11/07/2014
TABLE KEY
29. Hydraulic Power
Change
12. Brake Accumulator C 1 0 May be inoperative provided the

Pressure Gauge Brake Synoptic Page Accumulator
(cockpit dial) Pressure Indication is operative.

a) Brake accumulator gauge in
the nose wheel well is
operative and checked before
each takeoff, and
b) Auxiliary hydraulic pump is on
and running for every takeoff
and landing.
13. Brake Synoptic Page C 1 0 May be inoperative provided the

Accumulator Pressure Brake Accumulator Pressure Gauge
Indication (cockpit dial) is operative.

a) Brake accumulator gauge in
the nose wheel well is
each takeoff, and
b) Auxiliary hydraulic pump is on
and running for every takeoff
and landing.
DATE: 02/04/2010
TABLE KEY
30. Ice and Rain Protection
Change
1. Cowl Anti-Ice Pressure B 2 0 Except for ER operations, may be

Indication System inoperative provided both EICAS
Cowl Anti-Ice Indications are
operative.
B 2 0 Except for ER operations, may be

operated at greater than
+10 degrees C SAT.
B 2 0 Except for ER operations, may be

a) Airplane is operated in VMC,
and
visible moisture.
2. Wing Anti-Ice System C 2 0 Except for ER operations, may be

inoperative provided airplane is not
operated in known or forecast icing
conditions.
1) Automatic Function C 2 0 May be inoperative provided airplane

AFM Limitations.
3. Windshield Heat System C 2 1 Except for ER operations, may be

operated in known or forecast icing
conditions.
1) Windshield Heat Sensor D 4 2 One sensor may be inoperative for

each Windshield Heat System.
DATE: 11/08/2010
TABLE KEY
Change
4. Side Window Heat C 2 0

System
1) Side Window Heat D 4 2 One Side Window Heat Sensor may

Sensor be inoperative for each Side Window
Heat System.
C 4 0
5. Anti-Ice Heater Switch B 4 0 (M)(O) May be inoperative provided

Light all other elements of the anti-ice
heater indicating system are verified
to operate normally.
6. Pitot Heater B 4 3 (O) Except for ER operations, may be

(GV, GV-SP) inoperative provided airplane is not
operated in visible moisture and
known or forecast icing conditions.
(GIV-X) B 3 2 (O) Except for ER operations, may be

operated in visible moisture and
known or forecast icing conditions.
7. Ice Detection System C 2 0 (O) May be inoperative provided

airplane is operated in accordance
with alternate AFM procedures.
NOTE: With Ice Detection Systems

inoperative, automatic anti-ice
is not available.
DATE: 02/04/2010
TABLE KEY
Change
8. Cowl Anti-Ice System C 2 0 (M) Except for ER operations, may be

a) Affected Valve(s) are verified
CLOSED, and
conditions.
C 2 1 (M) May be inoperative provided:

a) Affected Valve is verified
OPEN,
b) All components of both
HP Bleed Air Systems are
operative,
c) Both Environmental Control
Systems (ECS) Packs are
operative,
d) Performance Computer is
initialized with COWL
ANTI-ICE selected ON for
either takeoff or landing when
COWL ANTI-ICE valve is
pressurized, and
accordance with
AFM Limitations and
Performance.
1) Automatic Function C 2 0 May be inoperative provided airplane

alternate AFM procedures.
9. Cowl Pressure C 1 0 May be inoperative provided Cowl

Differential Indication Anti-Ice Pressure Indications are
System operative.
DATE: 07/05/2018
TABLE KEY
Change
10. Windshield Blower D 1 0 (M) May be inoperative provided the |

*** System Surface Seal coating has been
checked to be serviceable in
accordance with the Maintenance
Manual within the last 12 months or
500 flight-hours, whichever occurs
first.
|
D 1 0 May be inoperative provided there is
no precipitation falling on the
departure and arrival airport at the
time of taxi, takeoff, and landing.
1) Windshield Surface Seal D 2 0 May be inoperative provided airplane

Protection System is not operated in precipitation within
5 NM of the airport of takeoff or
intended landing.
11. Cabin Window Heat D 1 0 (M) May be inoperative provided:

System a) Cabin Window Heat switch is
selected OFF, and
b) Cabin Window Heat System
circuit breakers are pulled and
collared.
a) Cabin Window Heating D - 0 (M) May be inoperative provided the

Element associated Window Heat circuit
breakers are pulled and collared.
DATE: 07/05/2018
TABLE KEY
31. Indicating/Recording Systems
Change
1. Clock (Cockpit) D - 1
2. Flight Data Recorder C - 1 Any in excess of those required by

(FDR) System 14 CFR may be inoperative.
(Includes FDR function A - 0 May be inoperative provided:

of Combined Voice and a) Cockpit Voice Recorder
Flight Data Recorder (CVR) operates normally, |
(CVFDR)) b) Airplane is not dispatched
from a designated airport as
listed in the operator’s MEL
unless:
1. The FDR failure occurs
after pushback but before
takeoff, or
2. The FDR repair was
attempted but was not
successful.
c) In those cases where repair is
attempted but not successful,
the airplane may be
dispatched on a flight or
series of flights until the next
designated airport where
repair must be accomplished
prior to dispatch, and
3 flight days.
(Continued)
DATE: 12/18/2017
TABLE KEY
Change
2. Flight Data Recorder

(FDR) System
(Cont’d)
FDR Recording A - - Up to 3 recording parameters may be

Parameters required by inoperative provided:
14 CFR a) Cockpit Voice Recorder
(CVR) operates normally, and
20 calendar days.
FDR Recording A - - May be inoperative provided repairs

Parameters not required are made before the completion of
by 14 CFR the next heavy maintenance visit.
Flight Data Recorder C - 1 Any in excess of those required by

(FDR) System (Operator 14 CFR may be inoperative.
Other Than a Holder of
an Air Carrier of
Commercial Operator
Certificate)
A - 0 May be inoperative provided repairs

are made in accordance with
applicable 14 CFRs.
3. Brake Temperature C 1 0 May be inoperative provided airplane

Monitoring System is operated in accordance with AFM
(BTMS) Appendix on Brake Kinetic Energy
and Carbon Brake Cooling.
NOTE: This item includes the BTMS

displayed on the brakes
synoptic page.
DATE: 11/07/2014
TABLE KEY
Change
4. G Monitor System D 1 0
5. Electronic Checklist C 2 1 May be inoperative provided the

(GV) checklist module in Fault Warning
Computer (FWC) 1 is operative.
Electronic Checklist C 1 0 May be inoperative provided the

(GV-SP, GIV-X) current AFM is carried on board the
airplane.
6. Data Acquisition Unit B 4 3

(DAU) Channel
(GV)
7. Security System D 1 0
***
8. Engine Cowl Open D 1 0 May be inoperative provided right

*** Indicating System engine cowl is visually confirmed
CLOSED before starting APU on the
ground.
9. Airplane Personality C 4 3
Module (APM)
(GV-SP, GIV-X)
10. Plastic Guard Switch D - 1 May be inoperative provided APU fire

Cover bottle switch cover is installed and
operative.
DATE: 07/05/2018
TABLE KEY
Change
11. Configuration C 2 1
Management System
(GV-SP, GIV-X)
12. InfraRed Counter D 1 0

*** Measures System
(IRCM) or Directional
InfraRed Counter
Measures System
(DIRCM)
13. Quick Access Recorder D 1 0

*** (QAR)
14. XM Weather Receiver D 1 0

***
15. Modular Avionics Unit A 6 5 (M)(O) May be inoperative provided: |

(MAU) Channel a) Failed channel is not MAU 1A
(GV-SP, GIV-X) or MAU 2B,
b) No other failures exist in the
Avionics System,
c) Associated circuit breakers |
are pulled and collared, |
e) Repairs are made within
2 flight days.
DATE: 07/05/2018
TABLE KEY
32. Landing Gear
Change
1. Anti-Skid System C 1 0 (O) May be inoperative provided

airplane is operated in accordance
2. Rudder Pedal Steering C 1 0 May be inoperative provided Nose

System Wheel Tiller Steering System is
operative.
|
3. Variable Gain Nose C 1 0 (O) May be inoperative provided the |
Wheel Steering fixed gain steering mode is operative.
4. Nose Wheel Steering D - 0 May be inoperative or missing. |

Accessory Hardware
(Torque Link Lanyard)
5. Emergency Landing B 1 0 May be inoperative provided |

Gear Extension Bottle Emergency Landing Gear Extension
Pressure Gauge Bottle Pressure Cockpit CAS
(Nose Wheel Well) Indication (Summary Page) is
operative and checked prior to each
flight.
6. Emergency Landing B 1 0 May be inoperative provided |

Gear Extension Bottle Emergency Landing Gear Extension
Pressure Cockpit CAS Bottle Pressure Gauge (Nose Wheel
Indication Well) is operative and checked prior
(Summary Page) to each flight.
DATE: 07/05/2018
TABLE KEY
32. Landing Gear
Change
7. Landing Gear A 1 0 (O) May be inoperative provided: |

Extension/Retraction a) Airplane is operated with the
System landing gear in the extended
(includes dump valve, position,
gear handle, and blow b) Landing gear handle remains
down bottle) in the down position,
(GIV-X) c) Ground lock pins are installed
to ensure that all
3 landing gears are LOCKED
down throughout flight,
d) Both pilots use cockpit
headsets,
e) Operations are not conducted
in known or forecasted icing
conditions,
f) Extended over water
operations are prohibited,
g) Flight is conducted in
accordance with
AFM Supplement
No. GIV-2009-01,
h) Category II operations are
prohibited,
i) EFVS operations below
200 feet above touchdown
zone elevation are prohibited,
and
j) Repairs are made within
1 flight day.
DATE: 11/07/2014
TABLE KEY
32. Landing Gear
Change
8. Landing Gear A 2 0 (O) May be inoperative provided:

Extension/Retraction a) Airplane is operated with the
System landing gear in the extended
(includes dump valve, position,
gear handle, and blow b) Landing gear handle remains
down bottle) in the down position,
(GV/GV-SP) c) Ground lock pins are installed
to ensure that all
3 landing gears are LOCKED
down throughout flight,
d) Both pilots use cockpit
headsets,
e) Operations are not conducted
in known or forecasted icing
conditions,
f) Extended over water
operations are prohibited,
g) Flight is conducted in
accordance with
AFM Supplement
No. GV-2009-02,
h) Category II operations are
prohibited,
i) EFVS operations below
200 feet above touchdown
zone elevation are prohibited,
and
1 flight day.
DATE: 07/05/2018
TABLE KEY
33. Lights
Change
1. Cockpit/Flight C - - Individual lights may be inoperative

Deck/Flight provided:
Compartment and a) Remaining Lighting System
Instrument Lighting lights are sufficient to clearly
System (Excluding EFIS illuminate all required
and EICAS) instruments, controls, and
other devices for which they
are provided,
b) Remaining Lighting System
lights are positioned so that
direct rays are shielded from
flightcrew members’ eyes,
c) Lighting configuration and
intensity is acceptable to the
flightcrew,
d) Emergency flight deck lighting
is operative, and
e) Cockpit flood or flashlights
can be utilized to illuminate
the panel if required.
NOTE 1: Individual button/switch

lights and/or
annunciations/indications
are excluded from this
relief.
|
1) Inter Tank Valve C 1 0 May be inoperative if switch position
Switchlight is verified by the synoptic page and
CAS.
2) Crossflow Valve C 1 0 May be inoperative if switch position

Switchlight is verified by the synoptic page and
CAS.
DATE: 07/05/2018
TABLE KEY
33. Lights
Change
2. Passenger Cabin Interior D - - May be inoperative provided:

Illumination System a) Cabin emergency lighting is
operative,
b) Sufficient lighting is operative
for crew to perform required
duties, and
c) Lighting configuration at
dispatch is acceptable to
flightcrew.
3. Passenger Lighted
Information Sign
|
1) Passenger Lighted C - - (O) May be inoperative provided |
Information Sign alternate procedures are established
and used to notify cabin occupants.
4. Position Light Bulb C 6 3 May be inoperative provided one light

bulb is operative at each position.
C 6 0 May be inoperative provided airplane

is not operated sunset to sunrise.
5. Beacon Light C 1 0 May be inoperative provided Strobes

(Anti Collision Lights) are installed
and operative.
DATE: 11/08/2010
TABLE KEY
33. Lights
Change
6. Strobe C 6 3 Bulbs may be inoperative provided

(Anti-Collision Lights) one bulb is operative at each position
(wingtip and tail).

a) At least one bulb is operative
at wingtip, and
b) Airplane is not operated at
night.
7. Wing Inspection Light C 2 0 May be inoperative provided ground

(Airplanes With Wing deicing procedures do not require
Critical Surfaces Not their use.
Visible From Flight Deck)
8. Landing Light B 2 1 May be inoperative provided all three

bulbs of the taxi light are operative.

is not operated at night.
9. Taxi Light System C 1 0
1) Individual Light Bulbs C 3 0
10. Wing Tip Taxi Light C 2 0

*** System
11. Floor Proximity C - - One lamp in each of the solid red

*** Emergency Escape Path light assembly pairs and 2 lamps of
Marking System Lights the 5 lamp floodlight and exit sign
emergency floor path lighting
assemblies may be inoperative.
DATE: 02/04/2010
TABLE KEY
33. Lights
Change
12. Pulse Light System D - 0

*** (Identification Light)
13. Recognition Light D 1 0

*** System
14. Logo Light System D 1 0

***
15. Ramp Light System D - 0

***
16. Flashlight Charging D - 0

*** System
17. Aft Compartment Light D - 0

(Boiler Room)
18. Cargo Compartment D 1 0 May be inoperative provided no

*** Light emergency equipment is carried in
Cargo Compartment.
D 1 0 May be inoperative provided an

operative flashlight is installed in
Cargo Compartment.
DATE: 12/18/2017
TABLE KEY
33. Lights
Change
19. Pylon Mounted Exterior D - 0

*** Baggage Loading Light
System
20. Wheel Well Light D 3 0
21. Exterior Emergency C 1 0 May be inoperative provided airplane

Evacuation Lighting is not operated at night.
System
1) Exterior Emergency B 12 6 One bulb may be inoperative in each

Evacuation Lighting recess.
System Bulb
22. Service Door Light D - 0
23. Dim and Test C - - May be inoperative provided the

Annunciator Channels switch capsule is not used in an
emergency procedure where the
actuation of the switch is not
displayed elsewhere in the cockpit.
NOTE: The following switches 1-4

may not be inoperative:
1. GPWS/Ground Spoiler
Override,
2. Terrain Display (GV)/,
Terrain Inhibit
(GV-SP)(GIV-X),
3. CPCS Panel
Flight/Landing (2), and
4. Door Safety.
24. Airstair Light D - 0 May be inoperative provided an

alternate means (e.g. flashlight) is
used to illuminate the airstairs.
25. Dome Light D - 0 May be inoperative provided an

alternate means (e.g. flashlight) is
used to illuminate the vestibule area.
DATE: 07/05/2018
TABLE KEY
33. Lights
Change
26. Baggage Compartment D 1 0 May be inoperative provided no

Light emergency equipment is carried in
the baggage compartment.
D 1 0 May be inoperative provided an

operative flashlight is installed in
baggage compartment.
27. Cockpit Flashlight Relief exists at ATA 25.20, |

Revision 10 |
28. Wing Tip Position Light C 4 2 One may be inoperative per wing tip. |
*** LED Element Bank

is not operated sunset to sunrise.
29. Tail Position Light LED C 2 1

*** Element Bank

is not operated sunset to sunrise. |
30. LoPresti Boom Beam C 2 0 May be inoperative provided airplane

*** HID Landing Light is not operated at night.
System
STC No. ST02893AT/
LSM-500-126
1) LoPresti Boom Beam C 6 3 May be inoperative provided all

*** HID Landing Light factory installed taxi lights are
Element operative.
2) LoPresti Boom Beam C 6 0 May be inoperative provided Boom

*** HID Landing Light Beam taxi lights are operative.
Element with LoPresti
Boom Beam Taxi Lights
Installed
DATE: 12/18/2017
TABLE KEY
33. Lights
Change
31. LoPresti Boom Beam C 1 0 May be inoperative for night

*** HID Taxi Light System operations provided landing lights are
STC No. ST02893AT/ operative.
LSM-500-125
1) LoPresti Boom Beam C 3 1 Up to 2 elements may be inoperative.

*** HID Taxi Light Element
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change
1. Directional Compass B 3 2 (O) May be inoperative provided both

Reference Sensor PFD Heading Indicating Systems
operate independently.
2. Attitude Reference B 3 2 (O) May be inoperative provided:

Sensor a) Both PFD Attitude Indicating
Systems operate
independently, and
b) Standby Attitude Indicator is
operative.
3. Standby Flight Display C - 0 Except for ER operations, may be

inoperative provided not required by
14 CFR.
1) Standby Attitude B - 0 May be inoperative provided:

*** Indicator a) Operations are conducted in
(Electro-Mechanical Day VMC only, and
Gyro Horizon) b) Operations are not conducted
into known or forecast
VFR-on-Top Conditions
a) Glideslope/Localizer C 1 0
*** Indicator
2) Standby C 1 0 May be inoperative provided airplane

*** Altimeter/Airspeed is operated in Day VMC only.
Indicator (combined unit)
(Continued)
DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
3. Standby Flight Display

(Cont’d)
3) 3-in-1 Standby Attitude, C - 0 Except for ER operations, the Attitude

*** Altitude, Airspeed position indicator may be inoperative
Indicator Heading provided not required by 14 CFR.
(Color Video Display)
(GV Only)
B - 0 Attitude position indicator may be

a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
VFR-on-Top Conditions.
a) Standby Air Data Unit C 1 0 May be inoperative provided the

*** (Altitude and Airspeed airplane is operated in Day VMC
Function) only.
b) Standby Heading C 1 0 May be inoperative provided all three

*** Display Heading Reference Systems are
operative.
c) Glideslope/Localizer C 1 0
*** Function
d) DME Display C - 0
***
e) FMS Navigation C 1 0
*** Function
(Continued)
DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
3. Standby Flight Display

(Cont’d)
4) 4-in-1 Standby Attitude, C - 0 Except for ER operations, the Attitude

*** Altitude, Airspeed position indicator may be inoperative
Indicator Heading provided not required by 14 CFR.
(Color Video Display)
(GV-SP, GIV-X)
B - 0 Attitude position indicator may be

a) Operations are conducted in
Day VMC only, and
VFR-on-Top Conditions.
a) Standby Air Data Unit C 1 0 May be inoperative provided the

*** (Altitude and Airspeed airplane is operated in Day VMC
Function) only.
b) Standby Heading C 1 0 May be inoperative provided all three

*** Display Heading Reference Systems are
operative.
c) Glideslope/Localizer C 1 0
*** Function
d) DME Display C - 0
***
e) FMS Navigation C 1 0
*** Function
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change
4. Weather Radar System C - - Except for ER operations, as required

by 14 CFR.
5. VOR/ILS Navigation C - - As required by 14 CFR and no relief

System may be provided to an inoperative
systems or component if powered by
an emergency bus.
6. Marker Beacon System C 3 0 May be inoperative provided

(GV-SP, GIV-X) approach procedures do not require
its use.
(GV only) C 2 0 May be inoperative provided

approach procedures do not require
its use.
7. Automatic Direction C 2 - As required by 14 CFR.

Finding System
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
8. ATC Transponder and B - 0 May be inoperative provided:

Automatic Altitude a) Operations do not require its
Reporting System use, and
b) Prior to flight, approval is |
obtained from ATC facilities
having jurisdiction over
planned route of flight.
D - 1 Any in excess of those required by

14 CFR may be inoperative.
|
1) Elementary and A - 0 May be inoperative provided:
*** Enhanced Downlink a) Operations do not require its
Aircraft Reportable use, and |
Parameters not Required b) Repairs are made prior to
by 14 CFR completion of the next heavy
maintenance visit.
2) ADS-B Squitter (Relief is provided in 34-49-01) |

*** Transmission
DATE: 11/07/2014
TABLE KEY
34. Navigation
Change
9. Distance Measuring D - - Except where enroute operations or

Equipment (DME) approach minimums require its use,
System any in excess of those required by
14 CFR may be inoperative.
10. Standby RMI C 1 0 May be inoperative provided all

(Electro-Mechanical) 3 IRSs are operative.
(GV)
1) Standby Navigation C 1 0 May be inoperative provided all

*** Display (Color Video) 3 IRSs are operative.
2) DME Display C 2 0
***
3) EBDI (Electronic C 1 0 May be inoperative provided all

*** Bearing/Distance 3 IRSs are operative.
Indicator)
(GV-SP, GIV-X)
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
11. Radio Altimeter System C 2 0 May be inoperative provided:

a) Landing weather minimums or
operating procedures do not
require its use, and
b) Other systems affected
(EGPWS, TCAS, Flight
Director, Autopilot,
Autothrottle, Altimeter Ground
Awareness Display, Synthetic
Vision Primary Flight Display)
are considered.
12. Long Range Navigation C - - May be inoperative except where

System operations require the use of the |
(IRS, GPS, and GNSSU) associated system. |
NOTE: IRS Navigation Function only.

See Attitude Reference
Sensors for IRS Attitude
Function.
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change
13. Terrain Awareness and

Warning System (TAWS)
Class A TAWS
Equipment Required
1) GPWS A 1 0 (O) May be inoperative provided:

a) Alternate procedures are
2 flight days.
a) Modes 1-4 A 4 0 (O) May be inoperative provided:

2 flight days.
b) Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered
inoperative, and
2 flight days.
c) Glideslope Deviation(s) C - 1
Mode 5
B - 0
(Continued)
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change

(Cont’d)
d) Advisory Callouts B - 0 (O) May be inoperative provided

and used.
C - 0 (O) May be inoperative provided:

a) Advisory callout not required
by 14 CFR, and
e) Windshear Mode B 1 0 (O) May be inoperative provided

*** (Reactive) alternate procedures are established
and used.
NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.

b) Windshear Detection and
Avoidance System
(Predictive) operates
normally.
(Continued)
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change

(Cont’d)
2) Terrain System – B 1 0 (O) May be inoperative provided

Forward Looking Terrain alternate procedures are established
Avoidance (FLTA) and and used.
Premature Descent Alert
(PDA) Functions
3) Terrain Display C - 1
***
B - 0
4) Runway Awareness & C 1 0

*** Advisory System (RAAS)
Class B
TAWSEquipment
Required
1) GPWS A 1 0 (O) May be inoperative provided:

2 flight days.
a) Modes 1 & 3 A 2 0 (O) May be inoperative provided:

2 flight days.
(Continued)
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change

(Cont’d)
b) Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered
inoperative, and
2 flight days.
c) Modes 2, 4, & 5 C 3 0
***
d) Advisory Callouts B - 0 (O) May be inoperative provided

and used.

a) Advisory callout not required
by 14 CFR, and
e) Windshear Mode C 1 0 (O) May be inoperative provided

*** (Reactive) alternate procedures are established
and used.
2) Terrain System – B 1 0
Forward Looking Terrain
Avoidance (FLTA) and
Premature Descent Alert
(PDA) Functions
(Continued)
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change

(Cont’d)
3) Terrain Display C - 0
***
4) Runway Awareness & C 1 0

*** Advisory System (RAAS)
Class C TAWS
Equipment
1) TAWS/GPWS C 1 0 (O) May be inoperative provided

and used.
NOTE: Any mode that operates |

normally may be used. |
14. Lasertrak NDU C 1 0 May be inoperative provided at least

*** (GV) 1 flight Management System is
operative.
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
15. Flight Management B - 0 Except where enroute operations or

System (CDU & Nav approach minimums require its use,
Computer Only) may be inoperative provided:
(GV Only) a) Affected system is not
required for IRS alignment,
b) Long Range Navigation is not
dependent on its use,
c) Procedures do not require its
use, and
d) Both RFMUs are operative.
NOTE: Two systems are required for

dispatch into MNPS or
RNP-10 airspace. One
system is required in PRNAV,
BRNAV, RNAV 1, and
RNAV 2 airspace.
1) Navigation Database A - 0 May be inoperative provided:

a) Operations do not require its
use,
b) It is not used in a primary
navigation system required by
14 CFR,
developed and used,
d) The ICAO Flight Plan is
ATC of the navigation
aircraft, and
e) Is repaired within
10 flight days.
NOTE: An out-of-currency or
out-of-date navigation
database is not authorized
MMEL relief per 14 CFR.
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
16. Navigation Management B - 0 Except where enroute operations or

*** System approach minimums require its use,
(GV Only) may be inoperative provided:
a) Affected system is not
dependent on its use,
use, and
d) Both RFMUs are operative.

RNP-10 airspace. One
system is required in PRNAV,
BRNAV, RNAV 1, and
RNAV 2 airspace.
1) Navigation Database A - 0 May be inoperative provided:

a) Operations do not require its
use,
b) It is not used in a primary
navigation system required by
14 CFR,
developed and used,
d) The ICAO Flight Plan is
ATC of the navigation
aircraft, and
e) Is repaired within
10 flight days.
NOTE: An out-of-currency or
out-of-date navigation
database is not authorized
MMEL relief per 14 CFR.
17. Lightning Sensor System D - 0

*** (LSS)
18. Stormscope D - 0
***
DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
19. Traffic Alert and Collision B - 0 (M) May be inoperative provided:

Avoidance System a) System is deactivated and
(TCAS I) secured, and
b) Enroute or approach
procedures do not require its
use.
C - 0 (M) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
c) Enroute or approach
use.
Traffic Alert and Collision B - 0 (M) May be inoperative provided:

Avoidance System a) System is deactivated and
(TCAS II) secured, and
use.
C - 0 (M) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
use.
(Continued)
DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
19. Traffic Alert and Collision

Avoidance System
(TCAS I)
(Cont’d)
1) Combined Traffic Alert C 2 1 May be inoperative on the non-flying

(TA) and Resolution pilot side provided:
Advisory (RA) Dual a) TA and RA visual display is
Display System(s) operative on the flying pilot
side, and
b) TA and RA audio function is
operative on the flying pilot
side.
2) Resolution Advisory (RA) C 2 1 May be inoperative on the non-flying

Display System(s) pilot side.

a) Traffic Alert (TA) visual
display and audio functions
are operative,
b) TA only mode is selected by
the crew, and
use.
3) Traffic Alert Display C - 0 (O) May be inoperative provided:

System(s) a) RA visual display and audio
functions are operative, and
use.
4) Audio Functions B 1 0 May be inoperative provided enroute

or approach procedures do not
require use of TCAS.
5) Airspace Selection C - 0
*** Function
(Above/Normal/Below)
DATE: 02/04/2010
TABLE KEY
34. Navigation
Change
20. Microwave Landing D - - As required by 14 CFR.

*** System (MLS)
21. Symbol Generator C 3 2 (M)(O) May be inoperative provided:

(GV) a) EFIS displays at pilot’s and
copilot’s stations are operative
from independent Symbol
Generators, and
b) Both EICAS displays are
operative.
DATE: 06/02/2006
TABLE KEY
34. Navigation
Change
22. Guidance Panel Digital

Indications and Mode
Select Indications
1) Speed Display C 1 0 May be inoperative provided the

associated value is available in the
Primary Flight Display.
2) Heading Display C 1 0 May be inoperative provided the

3) VS/FPA Display C 1 0 May be inoperative provided the

4) Altitude Select Display C 1 0 May be inoperative provided the

5) LNAV C 1 0 May be inoperative provided the

6) VNAV C 1 0 May be inoperative provided the

7) FLCH C 1 0 May be inoperative provided the

8) Manual Speed C 1 0 May be inoperative provided the

(Continued)
DATE: 11/07/2014
TABLE KEY
34. Navigation
Change
22. Guidance Panel Digital

Indications and Mode
Select Indications
(Cont’d)
9) Bank Select C 1 0 May be inoperative provided the

10) BC Select C 1 0 May be inoperative provided the

11) Heading Select C 1 0 May be inoperative provided the

12) VS/FPA Select C 1 0 May be inoperative provided the

13) Alt Hold Select C 1 0 May be inoperative provided the

14) Approach C 1 0 May be inoperative provided the

15) PFD Command L/R C 1 0 (O) May be inoperative provided the

16) APR Switch C 1 0 May be inoperative provided the

DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
23. Altitude Alerting System A - 0 (O) May be inoperative provided:

a) Autopilot with altitude hold,
and altitude capture operates
normally,
b) Enroute operations
(i.e., RVSM) do not require its
use,
c) Airplane does not depart from
a designated airport (as listed
in the operator’s MEL) where
repair or replacement can be
made, and
3 flight days.
1) Aural Alert C - 0 May be inoperative provided:

a) Visual alert operates normally,
and
b) Autopilot with altitude hold
normally.
2) Visual Alert C - 0 May be inoperative provided:

a) Aural alert operates normally,
and
b) Autopilot with altitude hold
normally.
24. Display Unit(GV) C 6 5 (M)(O) May be inoperative provided:

*** a) Inoperative tube is located in
the Copilot’s Navigation
Display Position (DU #5),
operative,
c) Standby RMI is operative, and
developed for operation
without the Copilot’s
Navigation displays.
(Continued)
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
24. Display Unit(GV)

*** (Cont’d)
*** Display Unit (GV) C 6 5 (M)(O) May be inoperative provided: |

For DU-885 Equipped a) Inoperative tube is located in
Airplanes the Copilot’s Navigation
Display Position (DU #5),
operative,
c) Standby RMI is operative,
Navigation displays, and
e) Terminal charts for the origin,
destination and alternate
airports are verified to be
current and onboard the
aircraft.
*** Display Unit Cooling C 6 5 (M)(O) May be inoperative provided:

Fan (GV) a) Tube with inoperative fan is
For DU-885 Equipped located in the Copilot’s
Airplanes Navigation Display Position
(DU #5),
operative,
c) Standby RMI is operative,
Navigation displays,
e) Terminal charts for the origin,
aircraft, and
f) Associated circuit breaker is |
pulled and collared. |
Display Unit C 4 3 (M)(O) May be inoperative provided: |

(GV-SP, GIV-X) a) The unit is located in the
DU #3 position, and
b) The pilot in the left seat flies
the airplane.
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
25. Standby Magnetic C 1 0 May be inoperative provided all three

Compass System Heading Reference systems are
(Flux Valve) (GV) operative.
*** Magnetometer C 1 0 May be inoperative provided all three

(GV-SP, GIV-X) IRSs are operative.
26. Non-Stabilized Magnetic B 1 0 May be inoperative provided any

*** Compass combinations of three Gyro or INS
(IRU) Stabilized Compass Systems
are operative.
B 1 0 May be inoperative provided:

a) Any combination of two Gyro
or INS (IRU) Stabilized
Compass Systems operate
normally, and
b) Airplane is operated with Dual
Independent Navigation
Capability and under Positive
Radar Control by ATC on the
enroute portion of the flight.
B 1 0 May be inoperative for flights that are

entirely within areas of magnetic
unreliability provided at least two
Stabilized Directional Gyro Systems
are installed, operate normally, and
used in conjunction with accepted
Free Gyro Navigation Techniques.
27. Head Up Display System D 1 0 May be inoperative provided landing

*** weather minimums or operating
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
28. Airborne Flight D - 0

*** Information System
(AFIS)
1) AFIS Printer D - 0
29. Slip-Skid Indicator B 2 1 May be inoperative provided:

a) Third attitude indicator is
installed and operative, and
b) An operative slip indication is
obtained by selecting another
IRS source via the Display
Controller.
(GV Only) Deleted in Revision 9.
30. Data Loader (GV) D 1 0

***
Data Management Unit D - 0

(DMU) (GV-SP, GIV-X)
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
31. Air Data

Computers/Systems
1) Micro Air Data Computer C 3 2 (M)(O) May be inoperative provided:

(GV) a) Manual Pressurization Control
operative,
is operative,
accordance with
AFM Limitations.
NOTE 1: Two systems are required

for operations in RVSM
airspace.
NOTE 2: For airplanes equipped with

ADS-B (ASC 192 or
ASC 214) if MADC 1 is the
failed MADC, select ATC 2
and if MADC 2 is the failed
MADC select ATC 1.

is operated in unpressurized
configuration.
NOTE: For airplanes equipped with

ADS-B (ASC 192 or
ASC 214) if MADC 1 is the
failed MADC, select ATC 2
and if MADC 2 is the failed
MADC select ATC 1.
(Continued)
DATE: 11/07/2014
TABLE KEY
34. Navigation
Change
31. Air Data

Computers/Systems
(Cont’d)
2) Air Data System (ADS) C 3 2 (M) May be inoperative provided:

(GV-SP, GIV-X) a) Manual Pressurization Control
operative,
is operative,
accordance with
AFM Limitations.
NOTE 1: Two systems are required

for operation in RVSM
airspace.
NOTE 2: If ADS 2 is failed, the WOW

indications on the copilot’s
flight control synoptic will be
crosshatched. Dispatch is
still allowed if the WOW
indications on the pilot’s
flight control synoptic are
shown as valid.
DATE: 11/08/2010
TABLE KEY
34. Navigation
Change
32. Integrated Avionics C - 2 May be inoperative provided two bus

*** Computer (IAC) controllers are operative for dispatch.
(GV)
NOTE: The FMS/PMS/Autothrottle
function of the operative IACs
may be inoperative as stated
elsewhere in this section. The
Autopilot is addressed in
ATA 22.
33. Bus Controller C - 2

(GV)
34. Airshow Controller D - 0

*** System
1) Cockpit Airshow Display D - 0

*** System
2) Cabin Airshow Display D - 0

*** System
35. Windshear Warning and C - 0 (O) May be inoperative provided

*** Flight Guidance System alternate procedures are established
(Reactive) and used.
DATE: 11/07/2014
TABLE KEY
34. Navigation
Change
36. Windshear Detection C - 0 (O) May be inoperative provided

*** and Avoidance System alternate procedures are established
(Predictive) and used.
37. Cockpit Video Monitor D - 0

***
38. Heads Up Checklist D - 0

***
39. Enhanced Vision System D 1 0

*** (EVS)
1) EVS Window Heat D 1 0

***
2) Secondary (non-HUD) D 1 0 May be inoperative provided

*** EVS Display Repeater procedures are not dependent on its
use.
40. Terrain Server C 2 0 NOTE: Synthetic Vision PFD

Function/EGPWM synthetic terrain will not be
Modules available with dual Terrain
(GV-SP, GIV-X) Server failures, but the full
PFD may be used without
restriction.
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
41. Electronic Flight Bag Moved to ATA 46 in Rev. 7.

***
42. Advanced Graphics C 4 3 (M)(O) May be inoperative provided:

Module (AGM) a) The inoperative AGM is
(GV-SP, GIV-X) located in the AGM 3 position,
and
b) Crew actions for subsequent
failures are established.
Advanced Graphics C 4 3 (O) May be inoperative provided:

Module (AGM) a) The inoperative AGM is
(GV-SP, GIV-X) electronically switched to the
(ASC 904 - Cert Charlie AGM 3 position resulting in
and ASC 905 - Cert DU 3 Red Xing, and
Charlie II and any later b) Crew actions for subsequent
revision to the operating failures are established.
software)
43. Cockpit Printer D 1 0
44. Cursor Control Device C 2 0 May be inoperative provided:

(GV-SP, GIV-X) a) Both Display Controllers,
Weather Radar Controllers,
and two MCDUs are
operative, and
b) Terminal charts for the origin,
aircraft.
*** Cursor Control Device C 2 0 (M)(O) May be inoperative provided: |

(GV Only) a) Both Display Controllers are
operative, and
b) Terminal charts for the origin,
aircraft.
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
45. Multifunction Control C 3 2 (M) May be inoperative provided:

Display Unit (MCDU) a) The FMS functions and Radio
(GV-SP, GIV-X) Tuning functions are operative
on the remaining MCDUs, and
b) The inoperative MCDU is
located in the No. 2 position.
NOTE: MCDU 3 has Backup Radio
Tuning functions.
1) Flight Management B 3 1 Except where enroute operations or

System (FMS) Function approach minimums require its use,
(GV-SP, GIV-X) may be inoperative provided:
a) Affected system is not
dependent on its use, and
use.
RNP-10 airspace. RNP RNAV
including PRNAV and BRNAV
only require a single FMS.
a) Navigation Database C - - May be inoperative provided: |

a) Operations do not require its |
use, |
b) It is not used in a primary |
navigation system required by |
14 CFR, |
c) Alternate procedures are |
developed and used, |
d) The ICAO Flight Plan is |
updated (as required) to notify |
ATC of the navigation |
equipment status of the |
aircraft, and |
e) Is repaired within |
10 flight days. |
NOTE: An out-of-currency or |
out-of-date navigation |
database is not authorized |
MMEL relief per 14 CFR. |
(Continued)
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
45. Multifunction Control

Display Unit (MCDU)
(GV-SP, GIV-X)
(Cont’d)
2) Radio Tuning Function B 3 2

(GV-SP, GIV-X)
46. Advanced Graphics C - 0 (O) May be inoperative provided: |

Module (AGM) Database a) Operations do not require its |
(GV-SP, GIV-X) use, and |
b) Alternate procedures are |
developed and used. |
47. Charts Function D 2 0 May be inoperative provided current

(GV-SP, GIV-X, GV for aeronautical charts are carried on
DU-885 Equipped board the airplane and available to
Airplanes) the flightcrew.
1) Charts Database C 4 0 (O) May be inoperative provided: |

a) Operations do not require its |
use, and |
b) Alternate procedures are |
developed and used. |
48. Video Function D 1 0 Any video presented on Display Units

(GV-SP, GIV-X) 1, 2, 3, and 4 may be inoperative.
NOTE: Some Enhanced Flight Vision

System (EVS) operations may
require the use of the EVS
video display.
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
49. Automatic Dependent C - 0 (O) May be inoperative provided: |

*** Surveillance-Broadcast a) Alternate procedures are |
(ADS-B) System established and used, and |
b) It is not required by 14 CFR. |
|
NOTE: Any ADS-B function that |
operates normally may be |
used. |
|
D - 0 May be inoperative provided: |
a) Enroute operations do not |
require its use, and |
|
used. |
|
C - 1 One must be operative as required by |
14 CFR. |
|
used. |
|
1) ADS-B Out Extended C - 0 (O) May be inoperative provided: |
*** Squitter Transmission a) Alternate procedures are |
established and used, |
b) Authorization is obtained from |
ATC facilities having |
jurisdiction over planned route |
of flight, and |
c) It is not required by 14 CFR. |
|
used. |
|
14 CFR. |
|
used. |
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
49. Automatic Dependent |

*** Surveillance-Broadcast |
(ADS-B) System |
(Cont’d) |
|
|
2) ADS-B Out UAT C - 0 (O) May be inoperative provided: |
*** Transmission a) Enroute operations do not |
require its use, |
b) Authorization is obtained from |
ATC facilities having |
jurisdiction over planned route |
of flight, and |
c) It is not required by 14 CFR. |
|
used. |
|
14 CFR. |
|
used. |
|
3) ADS-B In Transmission C - 0 (O) May be inoperative provided |
*** alternate procedures are established |
and used. |
|
used. |
|
D - 0 May be inoperative provided |
operations do not require its use. |
|
used. |
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
50. Right Side Display A 1 0 (M)(O) May be inoperative provided: |

Controller a) The weather at the destination
(GV Only) is forecast to be VFR
(1,000 feet ceiling and
three miles visibility),
b) An alternate airport is
specified in the flight plan
which has VFR weather
forecast (1,000 feet ceiling
and three miles visibility),
c) Both VOR and ADF
navigation receivers are
operative,
d) Flight is conducted based on
short range navigation
sources only being available,
e) Navigation suffix in the IFR
flight plan clearly indicates
that the airplane is not
capable of any RNP required
navigation capability,
f) Flight is conducted in airspace
where the availability of
navigation by short range
navigation receivers
(VOR/ADF) is assured,
g) One DBDI or Standby RMI or
Secondary Navigation Display
is operative,
h) Associated circuit breaker is |
pulled and collared, |
i) Alternate procedures are
1 flight day.
DATE: 07/05/2018
TABLE KEY
34. Navigation
Change
50. Right Side Display A 1 0 (M)(O) May be inoperative provided: |

Controller a) FMS is the navigation source
(GV-SP, GIV-X) on both PFDs,
b) Destination and alternate
airports have either LPV,
GPS, or FMS overlay
approaches available without
NOTAM restrictions for
airplanes not equipped with
Enhanced Navigation
Package,
c) Destination and alternate
airports have either LPV,
GPS, FMS overlay, or ILS
approach available without
NOTAM restrictions for
airplanes equipped with
Enhanced Navigation
Package,
d) No other display system
failures exist,
e) Associated circuit breaker is |
pulled and collared, |
f) Alternate procedures are
g) Repairs are made within
2 flight days.
DATE: 12/18/2017
TABLE KEY
34. Navigation
Change
51. Synthetic Vision Primary D 2 0

*** Flight Display (SV-PFD)
Functions
52. DDA (Digital to Discrete D 2 0 May be inoperative provided

*** Adapter) approach minimums do not require its
(GV only) use.
53. GNSSU WAAS D 2 0 WAAS function may be inoperative

*** (Wide Area provided enroute and approach
Augmentation System or procedures do not require its use.
SBAS – Space Based
Augmentation System)
Function
1) LPV Enable Switch C 2 0 May be inoperative provided

*** (GV Only) approach procedures do not require
its use.
54. CAS Scroll Switch D 2 0 May be inoperative provided both

(GV-SP, GIV-X) CCDs are operative.
DATE: 07/05/2018
TABLE KEY
35. Oxygen
Change
1. Passenger Oxygen B - - As required by 14 CFR.

System and Supply
2. Cabin Oxygen ON C 1 0 May be inoperative provided:

Warning System a) Cabin Altitude and Differential
operative, and
b) Cabin Altitude Pressure
Warning System is operative.

configuration.
3. Oxygen Service Panel D 2 0 May be inoperative provided

Pressure Gauge associated cockpit gauge is operative
and monitored.
4. Portable Oxygen C - - Any in excess of those required by |

*** Dispensing Unit 14 CFR may be inoperative or
(Bottle and Mask) missing provided required distribution
is maintained throughout airplane.
NOTE: Any bottle not properly

serviced is considered
inoperative and should be
removed.
5. Oxygen Supply Warning C 2 0 May be inoperative provided

System associated cockpit gauge is operative
and monitored.
DATE: 07/05/2018
TABLE KEY
35. Oxygen
Change
6. Portable Protective D - - Any in excess of those required by

*** Breathing Equipment 14 CFR may be inoperative or
(PBE) missing provided: |
a) Inoperative PBE remains in a |
certified location or is |
removed from the aircraft, |
b) Location placarding is |
removed or obscured, and |
c) Required distribution is |
maintained. |
|
NOTE: Inoperative PBE units |
removed from a certified |
location, orremoved from the |
aircraft, are subject to 49 CFR |
dangerous goods regulations. |
7. Electronic Equipment D - 0 May be inoperative provided cockpit

*** Rack Oxygen Pressure gauges are operative.
Gauge
8. Cockpit Oxygen C - 0 May be inoperative provided:

Pressure Indication a) Oxygen Service Panel
Pressure Gauges are
every takeoff, and
b) Crew Oxygen Off and
Passenger Oxygen Off
messages are not displayed
on the CAS prior to every
takeoff.
9. Therapeutic Oxygen D - - May be inoperative or missing.
10. High Landing Field D 1 0 May be inoperative provided the

*** Elevation Passenger maximum Landing Field Elevation
Oxygen Controller High does not exceed 14,500 feet.
Altitude Switch
(GV-SP, GIV-X)
1) High Altitude Switch D 1 0 May be inoperative provided the

*** Light switch position is verified to be
(GV-SP, GIV-X) depressed in whenever the Landing
Field Elevation exceeds 14,500 feet.
DATE: 07/05/2018
TABLE KEY
36. Pneumatic
Change
1. Bleed Air Systems

(GV, GV-SP only)
1) Pressurized C 2 1 (M) Except for ER operations, may be

a) Inoperative Bleed Control
Valve is CLOSED and
deactivated electrically when
associated Engine Bleed Air
System is selected OFF,
b) Opposite Engine Bleed Air
c) Isolation Valve is verified to
be operative and selected
OPEN, and
accordance with
AFM Limitations.
NOTE: Autothrottle will be inoperative

with Isolation Valve OPEN.
2) Unpressurized C 2 0 (M)(O) Except for ER operations, |

Configuration may be inoperative provided:
Valve is CLOSED and
forecast or known icing
conditions, and
accordance with
AFM Limitations.
DATE: 07/05/2018
TABLE KEY
36. Pneumatic
Change
1. Bleed Air System

(GIV-X only)
1) Pressurized C 2 1 (M) Except for ER operations, may be |

Valve is CLOSED and
OPEN,
d) Airplane is not operated in
conditions, and
accordance with
AFM Limitations.


a) Affected Valve(s) is verified
CLOSED,
conditions, and
accordance with
AFM Limitations.

DATE: 07/05/2018
TABLE KEY
36. Pneumatic
Change
2. Bleed Air Hot Warning

System
1) Pressurized C 2 1 (M) Except for ER operations, may be |

a) Associated Bleed Control
Valve is CLOSED and
OPEN,
d) Airplane is not operated in
conditions, and
accordance with
AFM Limitations.


a) Associated Bleed Control
Valve is CLOSED and
conditions, and
accordance with
AFM Limitations.
DATE: 02/04/2010
TABLE KEY
36. Pneumatic
Change
3. Isolation Valve C 1 0 (M) May be inoperative provided:

a) Both Bleed Air Systems are
operative,
b) Both Environmental Control
System (ECS) Packs are
operative,
c) Isolation Valve is electrically
deactivated,
d) Isolation Valve is verified
CLOSED, and
accordance with
AFM Limitations.
NOTE: Valve must be OPENED

manually during left engine
start.
4. Bleed Air System Switch C 4 0 May be inoperative provided Bleed

Capsule Light Air System indications are available
on the Synoptic display.
DATE: 07/05/2018
TABLE KEY
38. Water/Waste
Change
1. Potable Water System C - - (M) Individual components may be

a) Associated components are
deactivated or isolated,
b) Associated system
components are verified not to
have leaks.
|
NOTE: Any portion of system which
operates normally may be
used.
C - - (M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to
ensure that system is not
serviced, and
c) Passengers are advised of |
the inoperative water system. |
DATE: 07/05/2018
TABLE KEY
38. Water/Waste
Change
2. Lavatory Waste System C - - (M) Individual components may be

deactivated or isolated, and
b) Associated system
components are verified not to
have leaks.
NOTE: Any portion of system which

operates normally may be
used.
C - - (M) Associated lavatory system(s)

may be inoperative provided:
deactivated or isolated to
prevent leaks, and
secured CLOSED and
placarded “INOPERATIVE -
DO NOT ENTER”.
NOTE: These provisos are not

intended to prohibit
inspections by crewmembers.
3. Lavatory Dump/Drain C - - (M) May be inoperative provided: |

System a) Dump valve is secured in the
CLOSED and LOCKED
position, and
b) System is checked for leaks
before every flight.
4. Vacuum Toilet Holding D 1 0 May be inoperative provided:

Tank Indicator a) Tank is verified to be serviced
before first flight of the day,
and
b) Tank is serviced after the last
flight of the day.
DATE: 02/04/2010
TABLE KEY
45. Central Maintenance System
Change
1) Maintenance Data D 1 0
Acquisition Unit (MDAU)
(GV)
2) Central Maintenance C 1 0 May be inoperative provided all faults

Computer (CMC) are recorded after each flight.
(GV-SP, GIV-X)
C 1 0 May be inoperative or missing

provided:
a) All faults are recorded after
each flight, and
b) The CMC module is replaced
with an Airflow Blockage
Module (ABM) if the CMC
module is removed from the
MAU.
DATE: 02/04/2010
TABLE KEY
46. Information Systems
Change
1. Electronic Flight Bag

*** System (EFB)
1) Class 3 EFB C - - (O) May be inoperative provided

and used.
NOTE: Any function, program, or

document which operates
normally may be used.

2) Data Connectivity C - - (O) May be inoperative provided

*** (Class 2) alternate procedures are established
and used.

3. Power Connection C - - (O) May be inoperative provided

*** (Class 1 & 2) alternate procedures are established
and used.
D - - May be inoperative provided

4. Mounting Device C - 0 (M)(O) May be inoperative provided:

*** (Class 2) a) Associated EFB and
hardware is secured by an
alternate means or removed
from airplane, and
D - 0 (M) May be inoperative provided:

a) Associated EFB and
hardware is secured by an
alternate means or removed
from airplane, and
b) Procedures do not require its
use.
DATE: 07/05/2018
TABLE KEY
49. Airborne Auxiliary Power
Change
1. Auxiliary Power Unit C 1 0 (O) Except for ER operations, may be |

(APU) inoperative provided:
a) Both Engine Driven
generators are operative,
operative,
c) APU air inlet door is verified
fully CLOSED, and
2. APU EGT Indicator C 2 1

(EICAS and Overhead)
C 2 0 (O) Except for ER operations, may be |

inoperative, |
b) Both Engine Driven
operative, and
3. APU Tachometer C 2 1
(EICAS and Overhead)
C 2 0 (O) Except for ER operations, may be |

inoperative, |
operative, and
4. APU “READY” Light C 1 0 May be inoperative provided the APU

System is operated in accordance with
AFM Limitations.
DATE: 02/04/2010
TABLE KEY
Change
5. APU Remote Oil C 1 0 May be inoperative provided oil is

Quantity/Servicing checked before every flight.
System
6. APU Oil Pressure Gauge D - 0

***
7. APU Oil Temperature D - 0

*** Gauge
8. APU Fuel Pressure D - 0

*** Gauge
9. APU Start Indicator Light C 1 0
10. APU Air Load Control C 1 0 (M) May be inoperative provided

Valve valve is verified in CLOSED position.
11. APU External Fire C 1 0 May be inoperative provided an APU

Warning Alarm operation is monitored in cockpit.
(Fire Warning Bell)
12. APU Air Inlet Door C 1 0 (M) Except for ER operations, may be
a) APU Air inlet door is secured
fully CLOSED,
b) APU is not operated,
c) Both Engine Driven
generators are operative, and
d) Standby Electrical System is
operative.
DATE: 12/18/2017
TABLE KEY
Change
13. Bleed Air Augmentation C 1 0 (O) May be inoperative provided:

Valve a) APU starting is not attempted
(GV, GV-SP) above FL 350, and
b) APU is operated in
accordance with
AFM Limitations.
14. Surge Control Valve C 1 0 Except for ER operations, may be

(GV, GV-SP) inoperative provided:
a) APU is restricted to ground
use only at pressure altitude
of 8,000 feet or below,
generators are operative, and
operative.
15. Ignition System Channel C 2 1

(GV, GV-SP)
16. EGT Thermocouple C 2 1

System
(GV, GV-SP)
17. Temperature Resistance C 1 0

Bulb (T2)
18. Inlet Pressure C 1 0

Transmitter (P2)
(GV, GV-SP)
19. RPM Speed Sensor C 2 1

Channel
(GV, GV-SP)
20. APU Hour Meter C 1 0

DATE: 07/24/2007
TABLE KEY
Change
21. Oil Temperature C 1 0 May be inoperative provided airplane

(GV, GV-SP) is operated in accordance with
AFM Limitations.
22. Deprime Solenoid C 1 0 (M) May be inoperative provided

(GV, GV-SP) airplane is operated in accordance
23. Oil Heater C 1 0 May be inoperative provided airplane

(GV, GV-SP) is operated in accordance with
AFM Limitations.
24. APU Start/Engine Cowl D 1 0

*** Interrupt System
DATE: 07/05/2018
TABLE KEY
52. Doors
Change
1. Door Warning Light C 1 0 May be inoperative provided a

System crewmember verifies by visual
inspection before each departure that
the associated door is CLOSED and
LOCKED.
2. Cargo Door Operating C 1 0 May be inoperative provided a

*** System crewmember verifies by visual
LOCKED.
3 Cargo Door Warning C 1 0 May be inoperative provided a

*** Light System crewmember verifies by visual
LOCKED.
4. Door Seal Pressure D 1 0

*** Indicator
5. Main Entry Door Normal C 1 0 (O) May be inoperative provided:

Operating System a) Alternate system is operative,
and
b) Main door is not CLOSED
manually.
6. Main Entry Door D - -

Acoustic Curtain/Door
System
7. Lavatory Door D - - (M) May be inoperative provided the |

affected door is secured OPEN or
CLOSED for taxi, takeoff, and
landing.
NOTE: Includes pop-up panels,

latches, locks, and handles.
DATE: 07/05/2018
TABLE KEY
52. Doors
Change
8. Baggage Door Warning C 1 0 May be inoperative provided a

System crewmember verifies by visual
the baggage door is CLOSED and
LOCKED.
9. Main Entry Door C 1 0 May be inoperative provided a

Warning System crewmember verifies by visual
the Main Entry Door is CLOSED and
LOCKED.
10. Internal Baggage Door C 1 0 (O) May be inoperative provided: |

*** Warning System a) Door is verified to be |
(GV, GV-SP) CLOSED and LOCKED by a
crewmember after each use,
and
b) Door is placarded
“DO NOT ENTER at or above
40,000 feet”.
Internal Baggage Door C 1 0 (O) May be inoperative in the closed |

Warning System position provided the smoke detector
(GIV-X) is operative.
C 1 0 (O) May be inoperative in the open |

position provided baggage
compartment is empty.
11. Interior Pocket Door D - - (M) May be inoperative provided the |

affected door is secured OPEN for
taxi, takeoff, and landing.
NOTE: Includes pop-up panels,

latches, locks, and handles.
12. Cabin Over Wing Exit D 1 0 May be inoperative provided a

Window Warning System crewmember verifies by visual
the cabin exit window internal and
external locking (T) handles in the
over wing access panels are
engaged in their LOCKED position.
DATE: 02/04/2010
TABLE KEY
71. Powerplant
Change
1. EPA Tank Ejector Pump D 2 0 (M) May be inoperative provided

maintenance procedures are
established to drain tank:
a) Before the first flight of each
day,
b) After three normal shutdowns,
and
c) After two false (wet) starts.
DATE: 11/08/2010
TABLE KEY
73. Engine Fuel and Control
Change
1. Fuel Flow Indication

System
1) EICAS C 2 1 May be inoperative provided:

a) Associated EPR, LP, and HP
indicating systems are
operative, and
b) Fuel quantity indicating
systems are operative.
2) RFMU (GV) C 2 1 May be inoperative provided:

MCDU (GV-SP, GIV-X) a) Associated EPR, LP, and HP
indicating systems are
operative, and
b) Fuel quantity indicating
systems are operative.
2. Fuel Low Pressure C 2 1 May be inoperative provided:

Warning System a) Associated Fuel Boost Pumps
(EICAS) are operative, and
below FL 250.
DATE: 07/05/2018
TABLE KEY
73. Engine Fuel and Control
Change
3. Engine FADEC System A 2 0 (M)(O) Airplane may be dispatched

(GV, GV-SP) with Blue “Engine Maintenance STD
(###)” and/or “Engine Maintenance
LTD” messages displayed on EICAS
provided:
a) Repairs are made in
accordance with times (hours)
established by the BR 710-A1
Time Limits Manual (GV),
chapter 5 or BR 710-C4 Time
Limits Manual (GV-SP),
chapter 5 (no extensions are
authorized), and
b) FADEC faults are reviewed by
flightcrew before each takeoff.
|
Engine FADEC System A 2 0 (M)(O) Airplane may be dispatched
(GIV-X) with Blue “Engine Maintenance STD
(###)” and/or “Engine Maintenance
LTD” messages displayed on EICAS
provided:
a) Repairs are made in
accordance with times (hours)
established by the
Tay 611-8C Time Limits
Manual, chapter 5
(no extensions are
authorized), and
b) FADEC faults are reviewed by
flightcrew before each takeoff.
|
DATE: 07/05/2018
TABLE KEY
74. Ignition
Change
1. Ignition System A 4 3 May be inoperative provided:

(includes igniter and/or a) All 3 remaining ignition
ignition exciter) systems are operative,
b) Takeoff runway does not have
standing water, slush, or
snow, and
150 flight-hours.

a) Each engine has an operative |
ignition system,
b) Takeoff runway does not have
standing water, slush, or
snow, and
10 flight days.
2. Ignition ON Indicator C 2 0 (M) May be inoperative provided both

System airstart ignition systems are verified
to be operative before each flight.
DATE: 11/07/2014
TABLE KEY
77. Engine Indicating
Change
1. HP Tachometer C 2 1 May be inoperative on either engine

Indication EICAS provided associated LP, EPR, and
Fuel Flow Indicating Systems (EICAS
or Standby) are operative for affected
engine.
NOTE: Standby HP Indication may

also be inoperative on both
engines.
2. Engine Vibration Monitor

System Sensor
1) Primary Sensor C 2 0 May be inoperative provided

associated secondary sensor system
is operative.
2) Secondary Sensor C 2 0 May be inoperative provided

associated primary sensor system is
operative.
3. Standby Engine C 1 0 May be inoperative provided:

Instruments Indicating a) Associated EICAS indication
System (RFMU) is operative, and
(GV) b) All channels of both DAUs are
operative.
4. Standby Engine C 1 0 May be inoperative provided

Instruments on associated EICAS indication is
Multifunction Control operative.
Display (MCDU)
(GV-SP, GIV-X)
5. Engine Vibration Monitor B 1 0 May be inoperative provided:

System a) Both Ice Detection Systems
are operative,
in known or forecast icing
conditions, and
c) Crew reviews the Abnormal
Procedures for engine
vibration before each takeoff.
DATE: 07/05/2018
TABLE KEY
78. Engine Exhaust
Change
1. Thrust Reverser C 2 0 (M)(O) May be inoperative provided: |

a) Affected Thrust Reverser is
deactivated, stowed, and
LOCKED in forward thrust
position, and
accordance with
AFM Limitation and
Procedures.
DATE: 07/05/2018
TABLE KEY
79. Engine Oil
Change
1. Low Oil Pressure C 2 1 May be inoperative provided oil

Warning System pressure indications for both engines
are operative.
2. Engine Oil D 1 0
Replenishment System
3. Impending Oil Filter A 2 1 (M) May be inoperative provided: |

Bypass Indication a) Associated oil filter bypass
pop up indicator is verified in
normal (recessed) position
before each engine start,
b) The oil filter is changed every
flight day or
every15 flight-hours,
whichever occurs first,
c) The Magnetic Chip Detectors
are checked and verified to be
free of all debris,
d) Procedures are in place to
ensure all other DND
(Do Not Dispatch) messages
are addressed before
dispatch, and
e) Repairs are made within
3 flight days.
NOTE: An amber “Engine

Maintenance” message will
still be displayed on the Crew
Alerting System.
DATE: 07/05/2018
TABLE KEY
79. Engine Oil
Change
4. Oil Quantity Indication C 2 0 May be inoperative provided the

System (EICAS/Ground engine oil quantity is verified on the |
Service Control Panel) engine oil quantity gauge before each
engine start.
5. Oil Filter Pressure C 2 0 (M) May be inoperative provided: |

Switch Fault Indication a) Associated oil filter bypass
pop up indicator is verified in
normal (recessed) position
before each engine start,
b) Oil filter fault is not displayed
in MDAU (GV) or CMC
(GV-SP, GIV-X),
c) Fault is confirmed to be on the
indication system, and
d) Procedures are in place to
ensure all other DND
(Do Not Dispatch) messages
are addressed before
dispatch.
NOTE: An amber “Engine

Maintenance” message will
still be displayed on the Crew
Alerting System.
DATE: 07/05/2018
TABLE KEY
80. Starting
Change
1. Engine Starting System C 2 0 (M)(O) May be inoperative provided: |

a) Airstart Ignition System is
operative,
b) Start Valve has not failed in
OPEN position,
c) Start Valve is manually
OPENED and CLOSED for
engine starting,
d) Airstart Ignition, Engine
Selector, and Start Switches
are switched to OFF when
engine has reached
self-sustaining speed, and
e) Engine start is accomplished
in accordance with AFM
Engine Start Valve Fails To
Open Procedure.
2. Auto Start System C 2 0 May be inoperative provided:

a) Alternate start system is
operative, and
b) AFM procedures for alternate
engine start are used to start
engines.
DATE: 07/05/2018
TABLE KEY
80. Starting
Change
3. Start Valve Position C 2 0 (M)(O) May be inoperative provided: |

Indication a) Start Valve has not failed in
OPEN position as verified by
visual means through an
access panel,
b) Ignition ON indication is
operative during engine start,
and
c) Start Valve is verified
CLOSED following engine
start by visual means.
C 2 0 (M)(O) May be inoperative provided: |

a) Airstart Ignition System is
operative,
b) Start Valve has not failed in
OPEN position,
c) Start Valve is manually
engine starting,
d) Airstart Ignition, Engine
Selector, and Start Switches
are switched to OFF when
engine has reached
self-sustaining speed, and
e) Engine start is accomplished
in accordance with AFM -
ENGINE START VALVE
FAILS TO OPEN
PROCEDURE.
DATE: 07/05/2018
TABLE KEY
80. Starting
Change
4. Start Valve Position C 2 0 (M)(O) May be inoperative provided: |

*** Indicator Light a) Start valve has not failed in
OPEN position as verified by
visual means through an
access panel,
b) Start valve is manually |
engine starting in accordance
with AFM Start Valve Failure
procedure, and
c) Airstart Ignition, Engine
Selector, and Start switches
are switched to the OFF
position when engine has
reached self-sustaining
speed.
DATE: 11/07/2014
AIRCRAFT: CAS MESSAGE RELIEF
GIV-X (G450/G350), GV, GV-SP (G550/G500
5000 SERIES)
SECTION TWO
CREW ALERTING
SYSTEM (CAS)
MESSAGE RELIEF
DATE: 07/05/2018
AIRCRAFT: STATEMENT PAGE
GIV-X (G450/G350), GV, GV-SP (G550/G500
5000 SERIES)
1. Section Two of the MMEL will list only Crew Alerting system (CAS) Messages meeting the
following requirements:
a) Equipment failure indications(s) that can be used to determine the airworthiness status of
the airplane.
b) Messages that the crew can act upon from the cockpit with simple troubleshooting
procedures without the assistance of a mechanic, and for which the crew has been trained.
c) Messages using the new self-diagnostic technology (virtual) actions for which the crew has
been trained.
2. CAS message relief items not meeting these requirements will be listed in Section One of the
MMEL.
Please refer to Policy Letter 119 for further guidance.

DATE: 12/18/2017
AIRCRAFT: TABLE KEY
GIV-X (G450/G350), GV, GV-SP (G550/G500 1. REPAIR CATEGORY
5000 SERIES) 2. DISPATCH CONSIDERATION
CAS Messages
Change
Item 1 2 Bar
A/P TRIM PWR FAIL B (O) Airplane may be dispatched with one elevator trim
(Blue – Advisory) servo inoperative provided the inoperative trim servo
(GV) circuit breaker(s) is pulled and collared:
 A/P SERVO #1: POP, D-4, or
 A/P SERVO #2: CPOP, D-4.
A/T 1-2 FAIL B (O) Airplane may be dispatched provided affected

(Blue – Advisory) A/T system is confirmed disengaged.
A/T 1-2 TQA Power Fail B (O) Airplane may be dispatched provided affected
(Blue – Advisory) A/T system is confirmed disengaged.
(GV-SP, GIV-X)
ACS Default Mode, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
ACS DEFLT MODE, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV)
ACS Fail, L-R B Except for ER operations, airplane may be dispatched

(Amber – Caution) in the pressurized configuration with a single pack
(GV-SP, GIV-X) inoperative provided:
a) Inoperative ECS Pack is selected OFF,
b) Bleed Air Isolation Valve is CLOSED and
OPERATIVE,
d) Airplane is operated in accordance with
AFM Limitations,
e) Airplane is operated at or below FL 410, and
f) Autothrottles must be operative and engaged at
or above FL 400.
B Except for ER operations, airplane may be dispatched

in the pressurized configuration with both packs
inoperative provided the outflow valve is operative.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
ACS FAIL, L-R B Except for ER operations, airplane may be dispatched

(Amber – Caution) in the pressurized configuration with a single pack
(GV) inoperative provided:
a) Inoperative ECS Pack is selected OFF,
b) Bleed Air Isolation Valve is CLOSED and
OPERATIVE,
AFM Limitations,
e) Airplane is operated at or below FL 410, and
f) Autothrottles must be operative and engaged at
or above FL 400.
B Except for ER operations, airplane may be dispatched

in the unpressurized configuration with both packs
inoperative provided the outflow valve is operative.
ACS Maintenance, L-R C (O) Except for ER operations, airplane may be

(Blue – Advisory) dispatched provided:
(GV-SP, GIV-X) a) Manual Pressurization Control System is
operative,
b) Cabin Altitude and Differential Pressure
Indicators are operative,
c) Cabin Rate of Climb Indicator is operative, and
d) Autopilot is operative.
ACS MAINT REQD, L-R C (O) Except for ER operations, airplane may be
(GV) a) Manual Pressurization Control System is
operative,
c) Cabin Rate of Climb Indicator is operative, and
d) Autopilot is operative.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
ADF 1-2 Fail B Airplane may be dispatched provided system is not

(Blue – Advisory) required by 14 CFR.
(GV-SP, GIV-X)
ADM1-3 Probe Heat Fail A (O) Except for ER operations, airplane may be
(Blue – Advisory) dispatched with one probe heater inoperative provided:
(GV-SP) a) Airplane is not operated in visible moisture or
known or forecast icing conditions,
b) Flightcrew select ADS sources that are different
and not associated with failed pitot heater
element, and
c) Repairs are made within 2 flight days.
ADM2 Stby Probe Heat Fail A (O) Except for ER operations, airplane may be
(GV-SP) a) Airplane is not operated in visible moisture or
element, and
ADS 1-2 Probe Heat Fail A (O) Except for ER operations, airplane may be
(GIV-X) a) Airplane is not operated in visible moisture or
element, and
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
ADS 1-2-3 Fail B (O) Airplane may be dispatched with a single air data
(Blue – Advisory) system inoperative provided:
operative,
c) Cabin Rate of Climb Indicator is operative,
d) Autopilot is operative,
e) Airplane is operated in accordance with
AFM Limitations,
f) ADM #1: POP B-8, ADM #2: CPOP B-8, and
ADM #3: POP B-9 circuit breakers associated
with ADS failure is pulled and collared, and
g) Flightcrew selects operative and different ADS
sources prior to departure.
NOTE 1: Two systems are required for operation in

RVSM airspace.
NOTE 2: Transponder and Flight Director/Autopilot

must use same ADC data for RVSM.
NOTE 3: For ADS 1 Fail, expect the L Engine Backup

Air Data advisory, associated Engine
Maintenance LTD and SSEC 1 Disabled
(Amber) message to post.
NOTE 4: For ADS 2 Fail, expect the R Engine Backup

Air Data advisory, associated Engine
NOTE 5: For ADS 3 Fail, expect the associated Engine

Backup Air Data advisory, associated Engine
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
ADS 3 Stby Probe Heat Fail A (O) Except for ER operations, airplane may be
(GIV-X) a) Airplane is not operated in visible moisture or
b) Flightcrew selects ADS sources that are
different and not associated with failed pitot
heater element, and
NOTE: Standby instruments and ADS 3 may be

unreliable.
ADS-B Fail C (O) Airplane may be dispatched provided: |

(Blue – Advisory) a) Alternate procedures are established and used, |
(GV-SP, GIV-X) and |
NOTE: Any ADS-B function that operates normally may |

be used. |
Aft Cabin Temp Fan Fail C (O) Airplane may be dispatched provided:
(Blue – Advisory) a) None of the following CAS messages are also
(GV-SP, GIV-X) posted:
 Forward Cabin Temp Fan Fail, and
 Cockpit Temp Fan Fail,
b) Aft Cabin Temperature Manual mode is
operative,
c) Associated temperature indicator is operative,
d) AFT CABIN SENSOR FAN, LEER E-9, is pulled
and collared, and
e) Flightcrew monitors aft cabin temperature and
aft cabin duct temperature.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
AFT CABIN TMP FAN FL C (O) Airplane may be dispatched provided:

(GV) posted:
 Forward Cabin Temp Fan Fail, and
 Cockpit Temp Fan Fail,
b) Aft Cabin Temperature Manual mode is
operative,
d) AFT CABIN SENSOR FAN, LEER E-9, is pulled
and collared, and
e) Flightcrew monitor aft cabin temperature and aft
cabin duct temperature.
AGM 1-2-3-4 DMU Charts Fail C Airplane may be dispatched provided:

(Blue – Advisory) a) Current aeronautical charts are carried onboard
(GV-SP, GIV-X) the airplane and available to the flightcrew, and
b) Airplane is operated in accordance with
AFM Limitations.
AGM 1-2-3-4 Fail B (O) Airplane may be dispatched with one AGM
(Blue – Advisory) inoperative provided:
(GV-SP, GIV-X) a) The inoperative AGM is electronically switched
to the AGM 3 position resulting in DU3 red Xing,
b) DU3 is dimmed to eliminate the Red X, and
c) Crew actions for subsequent failures are
established.
AIU 1-2 FAIL A Airplane may be dispatched with one AIU inoperative
(Blue – Advisory) provided:
(GV) a) Operations do not require use of HF radio, and
b) Repairs are made within 2 flight days.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Alternate Pump Fail, L-R B (O) Except for ER operations, airplane may be
(Amber – Caution) dispatched with a single pump inoperative provided:
(GV-SP) a) Fuel Crossflow Valve is operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning Systems are
operative,
d) Flightcrew comply with AFM, Section 3,
Abnormal Procedures, Fuel Boost Pump Failure,
and
AFM Limitations.
Alt FuelPump Fail, L-R B (O) Except for ER operations, airplane may be
(GIV-X) a) Fuel Crossflow Valve is operative,
operative,
and
AFM Limitations.
ALT PUMP FAIL, L-R B (O) Except for ER operations, airplane may be
(GV) a) Fuel Crossflow Valve is operative,
operative,
and
AFM Limitations.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Antiskid Fail B (O) Airplane may be dispatched provided:

(Amber – Caution) a) ANTI-SKID is selected “OFF”,
(GV-SP, GIV-X) b) Anti-skid off braking procedures, AFM Section 3,
Abnormal Procedures, Anti-Skid Failure are
followed,
c) No WOW Power Faults exist,
d) If Auto mode of the AUX Hydraulic Pump is
inoperative, AUX pump is selected ON for
takeoff and landing, and
AFM Limitations.
NOTE: Anti-Skid inoperative AFM performance

penalties must be applied. Refer to AFM,
Section 5, Performance, Reference
Accelerate-Stop Distance.
ANTISKID FAIL B (O) Airplane may be dispatched provided:

(Amber – Caution) a) ANTI-SKID is selected “OFF”,
(GV) b) Anti-skid off braking procedures, AFM Section 3,
Abnormal Procedures, Anti-Skid Failure are
followed,
c) No WOW Power Faults exist,
d) If Auto mode of the AUX Hydraulic Pump is
inoperative, AUX pump is selected ON for
takeoff and landing, and
AFM Limitations.
NOTE: Anti-Skid inoperative AFM performance

penalties must be applied. Refer to AFM,
Section 5, Performance, Reference
Accelerate-Stop Distance.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
AP 1-2 Fail B (O) Except for ER operations or where enroute

(Amber – Caution) operations or approach minimums require its use,
(GV-SP, GIV-X) Airplane may be dispatched with one Autopilot
inoperative provided the airplane is operated in
accordance with AFM Limitations in the event operative
FGC fails and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP, and

PRNAV operations.
AP 1-2 Power Fail B (O) Except for ER operations or where enroute

(Blue – Advisory) operations or approach minimums require its use,
(GV-SP, GIV-X) Airplane may be dispatched with one inoperative
provided airplane is operated in accordance with AFM
Limitations in the event operative FGC fails and Yaw
Damper is inoperative.

PRNAV operations.
AP/Trim Fail B (O) Airplane may be dispatched with one elevator trim
(Blue – Advisory) servo inoperative provided the inoperative PITCH TRIM
(GV-SP, GIV-X) SERVO #1: POP, E-2 or PITCH TRIM SERVO #2:
CPOP, E-1 trim servo circuit breaker is pulled and
collared.
APM 1-2-3-4 Fail B Airplane may be dispatched with one APM inoperative.
(Blue – Advisory)
(GV-SP, GIV-X)
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
APU Fail B (O) Except for ER operations, airplane may be

(Amber – Caution) dispatched provided:
(GV-SP, GIV-X) a) Both Engine Driven generators are operative,
b) Standby Electrical System is operative, and
c) APU Air inlet door is verified fully CLOSED.
APU FAIL B (O) Except for ER operations, airplane may be

(GV) a) Both Engine Driven generators are operative,
c) APU Air inlet door is verified fully CLOSED.
***APU Fire Bottle Discharge B (O) Except for ER operations, airplane may be
a) APU is considered inoperative,
b) Both engine driven generators are operative,
c) Standby electrical system is operative, and
d) APU CONT #1 LEER C-13, and APU CONT #2
REER C-11 circuit breakers are pulled and
collared.
APU Fire Detector Fail B (O) Except for ER operations, airplane may be
(GV-SP, GIV-X) a) APU is considered inoperative, and |
b) APU CONT #1 LEER C-13, and APU CONT #2
collared.
APU FIRE DET FAIL B (O) Except for ER operations, airplane may be
(GV) a) APU is considered inoperative, and |
b) APU CONT #1 LEER C-13, and APU CONT #2
collared.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
APU GCU Fail A (O) Except for ER operations, airplane may be

(GV-SP, GIV-X) a) APU GCU PWR circuit breaker on left EER,
G-11 is pulled and collared,
b) Both Engine Driven generators are operative as
verified by reference to the AC synoptic and the
absence of failure messages on CAS,
c) Standby Electrical System is operative, and
d) Repairs are made within 2 flight days.
APU GCU FAIL A (O) Except for ER operations, airplane may be

(GV) a) APU GCU PWR circuit breaker on left EER,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
APU Generator Fail A (O) Except for ER operations, airplane may be

(GV-SP, GIV-X) a) APU GCU PWR circuit breaker on left EER,
APU Generator Maint Reqd C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
APU GEN FAIL A (O) Except for ER operations, airplane may be

(GV) a) APU GCU PWR circuit breaker on left EER,
APU GEN MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
APU Maintenance Required C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
APU MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
APU Shutoff Valve Fail B (O) Except for ER operations, may be inoperative
(Amber – Caution) provided:
(GV-SP, GIV-X) a) Both Engine Driven generators are operative,
c) APU is not used.
ATC 1-2 Fail C Airplane may be dispatched with any in excess of those
(Blue – Advisory) required by 14 CFR inoperative.
(GV-SP, GIV-X)
NOTE 1: Flight Director, Autopilot, and Transponder
must use the same Air Data source for flight
into RVSM airspace.
NOTE 2: Transponder and altitude reporting capability

must be operative for flight into RVSM
airspace.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
BAROSET 1 Fail C (O) Airplane may be dispatched provided:

1. ADS 2 Fail,
2. ADS 3 Fail,
3. BAROSET 2 Fail, and
4. BAROSET 3 Fail.
b) Manual Pressurization Control System is
operative,
c) Cabin Altitude and Differential Pressure
d) Cabin Rate of Climb Indicator is operative,
e) Flightcrew select ADS sources that are
independent and not associated with the
BAROSET failure,
f) Autopilot is operative, and
g) Airplane is operated in accordance with
AFM Limitations.

RVSM airspace.

must use same ADC data for RVSM.
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

1. ADS 1 Fail,
2. ADS 3 Fail,
4. BAROSET 3 Fail.
operative,
BAROSET failure,
AFM Limitations.

RVSM airspace.

must use same ADC data for RVSM. |
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

1. ADS 1 Fail,
2. ADS 2 Fail,
4. BAROSET 2 Fail.
operative,
BAROSET failure,
g) Airplane is operated in accordance with AFM
Limitations.

RVSM airspace.
NOTE 2: Transponder and Flight Director/Autopilotmust

use same ADC data for RVSM. |
BAS Default Mode, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
BAS DEFLT MODE, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
BAS Fail, L-R B (O) Except for ER operations, airplane may be

(Amber – Caution) dispatched in the pressurized configuration with one
(GV-SP, GIV-X) Bleed Air System inoperative provided (GV-SP):
a) Inoperative Bleed Control Valve is CLOSED and
deactivated electrically when associated Engine
Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF,
and
2. Affected R BLEED AIR CONT: REER, E-9
and R WING ANTI-ICE: REER, D-13 or
L BLEED AIR CONT: LEER, E-10 and
L WING ANTI-ICE: LEER, D-4 circuit
b) Opposite Engine Bleed Air System is operative,
c) Isolation Valve is verified to be operative and
selected OPEN, and
AFM Limitations.
NOTE: Autothrottle will be inoperative with Isolation

Valve OPEN.
(Continued)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

(GV-SP, GIV-X) Bleed Air System inoperative provided(GIV-X):
and
and R WING ANTI-ICE: REER,D-13 or
selected OPEN,
d) Airplane is not operated in forecast or known
icing conditions, and
AFM Limitations.

Valve OPEN.
(Continued)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

(Amber – Caution) dispatched in the unpressurized configuration with both
(GV-SP, GIV-X) Bleed Air Systems inoperative provided (GV-SP):
and
b) Manual pressurization control is selected,
c) Outflow valve is slewed to the full OPEN
position,
d) RAM Air is selected ON,
e) Cabin differential pressure is monitored to be
nominally zero psid during the flight,
f) Airplane is not operated in known or forecast
AFM Limitations.
(Continued)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

(GV-SP, GIV-X) Bleed Air Systems inoperative provided (GIV-X):
a) Affected Valve(s) is verified CLOSED,
position,
f) Airplane is not operated in forecast or known
AFM Limitations.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

(GV) Bleed Air System inoperative provided (GV):
and
selected OPEN, and
AFM Limitations.

Valve OPEN.
(Continued)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar

(GV) Bleed Air Systems inoperative provided (GV):
and
position,
f) Airplane is not operated in known or forecast
AFM Limitations.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
BAS Maintenance Reqd, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
BAS MAINT REQD, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV)
BATT CHGR FAIL, L-R A (O) Airplane may be dispatched with one inoperative
(Amber – Caution) battery charger provided:
(GV) a) Both Engine Generators are operative,
c) Associated L BATT CHGR: Left PDB, Left Main
AC section or R BATT CHGR: Right PDB, Right
Main AC section circuit breaker on the Power
Distribution Box is pulled and collared,
d) Standby Electrical System is operative,
e) Affected Battery is selected OFF, and
f) Repairs are made within 2 flight days.
DATE: 08/24/2015
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Battery Charger Fail, L-R A (O) Airplane may be dispatched with one inoperative
(Amber – Caution) battery charger provided:
(GV-SP, GIV-X) a) Both Engine Generators are operative,
c) Associated L BATT CHGR: Left PDB, Left Main
AC section or R BATT CHGR: Right PDB, Right
Main AC section circuit breaker on the Power
Distribution Box is pulled and collared,
d) Standby Electrical System is operative,
e) Affected Battery is selected OFF, and
Brake Maintenance Reqd C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
BRAKE MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CAB PRESS SEMIAUTO C Airplane may be dispatched provided airplane is

(Blue – Advisory) operated in accordance with AFM Limitations.
(GV)
Cabin Pressure Semi-auto C Airplane may be dispatched provided airplane is

(Blue – Advisory) operated in accordance with AFM Limitations.
(GV-SP, GIV-X)
CCD 1-2 Fail B (O) Airplane may be dispatched provided:

(Blue – Advisory) a) Both Display Controllers, Weather Radar
(GV-SP, GIV-X) Controllers, and 2 MCDUs are operative, and
b) Current terminal charts for the origin, destination
and alternate airports are carried, or EFBs are
carried, onboard the airplane and available to
the flightcrew.
CDU 1-2-3 FAIL A Except where enroute operations or approach

(Blue – Advisory) minimums require its use, airplane may be dispatched
(GV) provided:
a) Affected system is not required for IRS
alignment,
b) Long Range Navigation is not dependent on its
use,
c) Procedures do not require its use,
d) Both RFMUs are operative, and
e) Repairs are made within 2 flight days.
NOTE: Two systems are required for dispatch into

MNPS or RNP-10 airspace. One system is
required in PRNAV, BRNAV, RNAV 1, and
RNAV 2 airspace.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CHECKLIST MISMATCH B (O) Airplane may be dispatched provided:

(Blue – Advisory) a) The checklist module in Fault Warning
(GV) Computer (FWC) one is operative, and
b) Current paper checklists are utilized.
CKPT TEMP FAN FAIL C (O) Airplane may be dispatched provided:

(GV) posted:
 Aft Cabin Temp Fan Fail.
 Forward Cabin Temp Fan Fail.
b) Cockpit Temperature Manual mode is operative,
d) CKPT SENSOR FAN, REER D-10, is pulled and
collared, and
e) Flightcrew monitor cockpit temperature and
cockpit duct temperature.
CMC Fail B Airplane may be dispatched provided all faults are

(Blue – Advisory) recorded after each flight.
(GV-SP, GIV-X)
CMF 1-2 Fail B (O) Airplane may be dispatched provided:

(Blue – Advisory) a) Alternate procedures are established and used,
(GV-SP, GIV-X) and
b) Flightcrew utilizes voice over VHF/HF to relay
pertinent information to the air traffic
management system.
B (O) Airplane may be dispatched provided routine

CMS 1-2 Fail B Airplane may be dispatched with one system

(Blue – Advisory) inoperative.
(GV-SP, GIV-X)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Cockpit Temp Fan Fail C (O) Airplane may be dispatched provided:

 Forward Cabin Temp Fan Fail.
b) Cockpit Temperature Manual mode is operative,
d) CKPT SENSOR FAN, REER D-10, is pulled and
collared, and
e) Flightcrew monitor cockpit temperature and
cockpit duct temperature.
Cockpit Voice Recorder Fail A Airplane may be dispatched provided:

(Blue – Advisory) a) Flight Data Recorder (FDR) is operative, and
(GV-SP, GIV-X) b) Repairs are made within 3 flight days.
without FDR installed A Airplane may be dispatched provided repairs are made
within 3 flight days.
not Air Carrier or Commercial A Airplane may be dispatched provided repairs are made
in accordance with applicable 14 CFRs.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Cowl Valve Fail Open, L-R B (O) Airplane may be dispatched with 1 inoperative
(GV-SP, GIV-X) a) Affected Valve is verified OPEN,
b) All components of both HP Bleed Air Systems
are operative,
c) Both Environmental Control Systems (ECS)
Packs are operative,
d) Affected Cowl Anti-Ice switch is ON,
e) Affected L COWL ANTI-ICE: LEER, D-3, or
R COWL ANTI-ICE: REER, D-14 valve circuit
breaker is pulled or in the OPEN position,
f) Performance Computer is initialized with COWL
ANTI-ICE selected ON for either takeoff or
landing when COWL ANTI-ICE valve is
pressurized, and
AFM Limitations and Performance.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
COWL VLV FL OP, L-R B (O) Airplane may be dispatched with one inoperative
(GV) a) Affected Valve is verified OPEN,
b) All components of both HP Bleed Air Systems
are operative,
c) Both Environmental Control Systems (ECS)
d) Affected Cowl Anti-Ice switch is ON,
e) Affected L COWL ANTI-ICE: LEER, D-3, or
R COWL ANTI-ICE: REER, D-14 valve circuit
breaker is pulled or in the OPEN position,
f) Performance Computer is initialized with COWL
ANTI-ICE selected ON for either takeoff or
landing when COWL ANTI-ICE valve is
pressurized, and
AFM Limitations and Performance.
CPAM Fail B Airplane may be dispatched provided both auto systems

(Amber – Caution) are operative.
(GV-SP, GIV-X)
CPAM FAIL B Airplane may be dispatched provided both auto systems

(Amber – Caution) are operative.
(GV)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS 1-2 Fail A (O) Except for ER operations, airplane may be

operative,
AFM Limitations and Abnormal Procedures
(for Taxi, Takeoffs, and Landings – Max Cabin
Pressure Differential 0.3 psi), and
A (O) Except for ER operations, airplane may be

dispatched in unpressurized configuration provided:
a) Manual pressurization is selected,
b) The outflow valve is slewed to the full open
position,
c) Both engine bleeds and air conditioning packs
are selected ON if available, or RAM Air is
selected ON,
d) Cabin pressure is monitored to be nominally
zero psid during the flight, and
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS 1-2 FAIL A (O) Except for ER operations, airplane may be

operative,

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS Channel 1-2 Fail A (O) Except for ER operations, airplane may be
operative,

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS CHNL 1-2 FAIL A (O) Except for ER operations, airplane may be
operative,

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS Control Panel Fail A (O) Except for ER operations, airplane may be
operative,
AFM Limitations (for Taxi, Takeoffs, and
Landings – Max Cabin Pressure Differential
0.3 psi), and

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS CONT PNL FAIL A (O) Except for ER operations, airplane may be
operative,
0.3 psi), and

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS Fail - Select Manual A (O) Except for ER operations, airplane may be
operative,
0.3 psi), and

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS FAIL-SEL MAN A (O) Except for ER operations, airplane may be

operative,
0.3 psi), and

position,
selected ON,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CPCS LAND ELEV FL B Airplane may be dispatched provided pressurization

(Blue – Advisory) system is operated in the Semi mode.
(GV)
CPCS Landing Elevation Fail B Airplane may be dispatched provided pressurization

(Blue – Advisory) system is operated in the Semi mode.
(GV-SP, GIV-X)
CPCS Maintenance Required C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
CPCS MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
CPCS Select Panel Fault A Airplane may be dispatched provided:

(Blue – Advisory) a) Auto system (Cabin Pressure Control Panel) is
(GV-SP, GIV-X) operative,
b) Semi-auto mode is considered inoperative, and
CPCS SEL PNL FAULT A Airplane may be dispatched provided:

(Blue – Advisory) a) Auto system (Cabin Pressure Control Panel) is
(GV) operative,
b) Semi-auto mode is considered inoperative, and
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
CVR FAIL A Airplane may be dispatched provided:

(Blue – Advisory) a) Flight Data Recorder (FDR) operates normally,
(GV) and
b) Repairs are made within 3 flight days.
without FDR installed A Airplane may be dispatched provided repairs are made
within 3 flight days.
not Air Carrier or Commercial A Airplane may be dispatched provided repairs are made
in accordance with applicable 14 CFRs.
Database Config A Airplane may be dispatched provided: |

(Blue – Advisory) a) Operations do not require its use,
(GV-SP, GIV-X) b) It is not used in a primary navigation system
required by 14 CFR,
c) Alternate procedures are developed and used,
d) The ICAO flight plan is updated (as required) to
notify ATC of the navigation equipment status of
the aircraft, and
NOTE: An out-of-currency or out-of-date navigation

database is not authorized MMEL relief per
14 CFR.
DAU 1A FL A (O) Airplane may be dispatched with one failed DAU

DAU 1B FL channel provided:
DAU 2A FL a) Flightcrew selects operative channel via the
DAU 2B FL display controller, and
(Blue – Advisory) b) Repairs are made within 2 flight days.
(GV)
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
DISP CTRL 2 FAIL A (O) Aircraft may be dispatched provided:

(Blue – Advisory) a) The weather at the destination is forecast to be
(GV) VFR (1,000 feet ceiling and 3 miles visibility),
b) An alternate airport is specified in the flight plan
which has VFR weather forecast (1,000 feet
ceiling and 3 miles visibility),
c) Both VOR and ADF navigation receivers are
operative,
d) Flight is conducted based on short range
navigation sources only being available,
e) Navigation suffix in the IFR flight plan clearly
indicates that the airplane is not capable of any
RNP required navigation capability,
f) Flight is conducted in airspace where the
availability of navigation by short range
navigation receivers (VOR/ADF) is assured,
g) One DBDI or Standby RMI or Secondary
Navigation Display is operative,
h) Alternate procedures are established and used,
i) Flightcrew pull and collar DISP CONT #2:
REER, C-2 Display Controller circuit breaker,
j) Flightcrew prepare and display a TOLD (Takeoff
and Landing Data) card prior to takeoff and prior
to approach and landing (GV only),
k) Flightcrew verify required approaches are
available at the destination and alternate airports
without being NOTAMed out of service or
unusable,
l) Pilot-Not-Flying (PNF) is prepared to announce
approach minimums in the event the operative
Display Controller fails enroute, and
m) Repairs are made within 1 flight day.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Display Controller 2 Fail A (O) Aircraft may be dispatched provided:

(Blue – Advisory) a) FMS is the navigation source on both PFDs,
(GV-SP, GIV-X) b) Destination and alternate airports have either
LPV, GPS, or FMS overlay approaches
available without NOTAM restrictions for
airplanes not equipped with Enhanced
Navigation Package,
c) Destination and alternate airports have either
LPV, GPS, FMS overlay, or ILS approach
available without NOTAM restrictions for
airplanes equipped with Enhanced Navigation
Package,
d) No other display system failures exist,
e) Flightcrew pull and collar DISP CONT #2:
REER, C-2 Display Controller circuit breaker,
f) Alternate procedures are established and used,
g) Pilot-Not-Flying (PNF) is prepared to announce
approach minimums in the event the operative
Display Controller fails enroute, and
h) Repairs are made within 1 flight day.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
DME 1-2 Fail C Airplane may be dispatched except where enroute

(Blue – Advisory) operations or approach minimums require its use. Any
(GV-SP, GIV-X) in excess of those required by 14 CFR may be
inoperative.
EGPWM SYS 1-2 Fail B Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X) NOTE: Synthetic Vision PFD synthetic terrain will not be
available with dual Terrain Server failures, but
the full PFD may be used without restriction.
Elevator Trim 1-2 Fail B (O) Airplane may be dispatched with electric elevator
(Amber – Caution) trim inoperative provided:
(GV-SP, GIV-X) a) Electric Elevator Trim remains OFF,
b) Both Flap/Stabilizer Control Channels are
operative (no messages on CAS), and
c) Airplane is operated in accordance with
AFM Limitations (Maximum Operating Limit
Speed 0.80 Mach for GV-SP and Maximum
Operating Limit Speed 0.75 Mach for GIV-X).
ELEV TRIM INOP B (O) Airplane may be dispatched with electric elevator
(Amber – Caution) trim inoperative provided:
(GV) a) Electric Elevator Trim remains OFF,
b) Both Flap/Stabilizer Control Channels are
operative (no messages on CAS), and
c) Airplane is operated in accordance with
AFM Limitations (Maximum Operating Limit
Speed 0.80 Mach).
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Engine Maintenance ###, L-R A (O) Airplane may be dispatched with Blue “Engine
(Blue – Advisory) Maintenance STD (###)” and/or “Engine Maintenance
(GV-SP, GIV-X) LTD” messages displayed on EICAS provided:
a) Repairs are made in accordance with times
(hours) established by the BR 710-C4 Time
Limits Manual (GV-SP) Chapter 5, or
Tay 611-8C Time Limits Manual (GIV-X),
Chapter 5 (no extensions are authorized), and
b) FADEC faults are reviewed by flightcrew before
each takeoff.
NOTE: Blue “Engine Maintenance STD (###)”

messages require maintenance action within
150 hours and Blue “Engine Maintenance LTD”
messages required maintenance action within
500 hours.
Engine Maintenance LTD, L-R A (O) Airplane may be dispatched with Blue “Engine
(GV-SP, GIV-X) LTD” messages displayed on EICAS provided:
(hours) established by the BR 710-C4 Time
Limits Manual (GV-SP) Chapter 5, or
Tay 611-8C Time limits Manual (GIV-X),
Chapter 5 (no extensions are authorized), and
each takeoff.

500 hours.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
ENG MAINT ###, L-R A (O) Airplane may be dispatched with Blue “Engine
(GV) LTD” messages displayed on EICAS provided:
(hours) established by the BR 710-A1 Time
Limits Manual (GV), Chapter 5 (no extensions
are authorized), and
each takeoff.

500 hours.
ENG MAINT LTD, L-R A (O) Airplane may be dispatched with Blue “Engine
(GV) LTD” messages displayed on EICAS provided:
(hours) established by the BR 710-A1 Time
Limits Manual (GV), Chapter 5 (no extensions
are authorized), and
each takeoff.

500 hours.
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
EPS Maintenance Reqd, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP,GIV-X)
EPS MAINT REQD, L-R C Airplane may be dispatched.

(Blue – Advisory)
(GV)
EVS Fail C Airplane may be dispatched.

(Amber – Caution)
(GV-SP, GIV-X)
EVS FAIL C Airplane may be dispatched.

(Amber – Caution)
(GV)
EVS Maintenance Required C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
EVS MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
EVS Window Heat Fail C Airplane may be dispatched.

(Amber – Caution)
(GV-SP, GIV-X)
EVS WINDOW HEAT FAIL C Airplane may be dispatched.

(Amber – Caution)
(GV)
FDAU FAIL A Airplane may be dispatched provided:

(Blue – Advisory) a) Cockpit Voice Recorder (CVR) is operative,
(GV) b) Airplane is not dispatched from a designated
(Operator is a Holder of an Air airport as listed in the operator’s MEL unless the |
Carrier or Commercial Operator FDR failure occurs after pushback but before |
Certificate) takeoff, and |
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FDAU FAIL A Airplane may be dispatched provided repairs are made |

(Blue – Advisory) in accordance with applicable 14 CFRs. |
(GV) |
(Operator Other Than a Holder |
of an Air Carrier or Commercial |
Operator Certificate) |
FDR SYS FAIL A Airplane may be dispatched provided:

(Blue – Advisory) a) Cockpit Voice Recorder (CVR) operates
(GV) normally,
(Operator is a Holder of an Air b) Airplane is not dispatched from a designated |
Carrier or Commercial Operator airport as listed in the operator’s MEL unless: |
Certificate) 1. The FDR failure occurs after pushback but |
before takeoff, or
2. The FDR repair was attempted but was not
successful.
c) In those cases where repair is attempted but not
successful, the airplane may be dispatched on a
flight or series of flights until the next designated
airport where repair must be accomplished prior
to dispatch, and
(Operator Other Than a Holder A Airplane may be dispatched provided repairs are made |
of an Air Carrier or Commercial in accordance with applicable 14 CFRs. |
FDR System Fail A Airplane may be dispatched provided:

(Blue – Advisory) a) Cockpit Voice Recorder (CVR) operates
(GV-SP, GIV-X) normally,
(Operator is a Holder of an Air b) Airplane is not dispatched from a designated |
Carrier or Commercial Operator airport as listed in the operator’s MEL unless: |
Certificate) 1. The FDR failure occurs after pushback but |
before takeoff, or
2. The FDR repair was attempted but was not
successful.
c) In those cases where repair is attempted but not
successful, the airplane may be dispatched on a
flight or series of flights until the next designated
airport where repair must be accomplished prior
to dispatch, and
(Operator Other Than a Holder A Airplane may be dispatched provided repairs are made |
of an Air Carrier or Commercial in accordance with applicable 14 CFRs. |
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FGC 1-2 FAIL B (O) Except for ER operations or where enroute

(Amber – Caution) operations or approach minimums require its use,
(GV) airplane may be dispatched with one failed provided
airplane is operated in accordance with AFM Limitations
in the event the operative FGC fails and the Yaw
Damper is inoperative.

PRNAV operations.
Fire Detection Loop Fault B Except for ER operations, airplane may be dispatched
(Amber – Caution) with one complete loop (A or B) inoperative provided
(GV-SP, GIV-X) the Fault Switch/Light is pressed to isolate the faulty
loop and illuminate the OFF portion of the switch light.
FIRE DET LOOP FALT B Except for ER operations, airplane may be dispatched
(Amber – Caution) with one complete loop (A or B) inoperative provided
(GV) the Fault Switch/Light is pressed to isolate the faulty
loop and illuminate the OFF portion of the switch light.
Flap/Stab Maint Reqd A-B C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP)
Flap/Stab Maint Reqd C Airplane may be dispatched.

(Blue – Advisory)
(GIV-X)
Flap/Stab System Fail A-B A Airplane may be dispatched with one channel
(GV-SP) a) Electric Pitch Trim System is operative,
b) Alternate control is verified to be operative
before each departure, and
FLP/STB MX RQD A-B C Airplane may be dispatched.

(Blue – Advisory)
(GV)
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FLP/STB SYS FL A-B A Airplane may be dispatched with one channel

(GV) a) Electric Pitch Trim System is operative,
b) Alternate control is verified to be operative
before each departure, and
FMS/GPS Pos Monitor Unavail B (O) Airplane may be dispatched provided:

(Blue – Advisory) a) FMS position is checked against available
(GV-SP, GIV-X) sensors, and
b) If errors encountered, affected GPS is
de-selected as a position sensor and FMS
position is updated.
FMS 1-2-3 Fail A Airplane may be dispatched with two inoperative except
(Blue – Advisory) where enroute operations or approach minimums
(GV-SP, GIV-X) require its use provided:
alignment,
use,
c) Procedures do not require its use, and

MNPS or RNP-10 airspace. RNP RNAV
including PRNAV and BRNAV only require a
single FMS.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FMS 1-2 FAIL A Airplane may be dispatched with two inoperative except
(Blue – Advisory) where enroute operations or approach minimums
(GV) require its use provided:
alignment,
use,
d) Both RFMU’s are operative (GV), and

MNPS or RNP-10 airspace. RNP RNAV
including PRNAV and BRNAV only require a
single FMS.
Forward Cabin Temp Fan Fail C (O) Airplane may be dispatched provided:
 Cockpit Temp Fan Fail.
b) Forward Temperature Manual mode is
operative,
d) FWD CABIN SENSOR FAN, LEER D-9, is
pulled and collared, and
e) Flightcrew monitor forward cabin temperature
and forward cabin duct temperature.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FQMS Maintenance Required C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
FQMS MAINT REQD C Airplane may be dispatched.

(Blue – Advisory)
(GV)
FQSC Channel Fail, L-R B (O) Except for ER operations, airplane may be
(Blue – Advisory) dispatched with one channel inoperative provided:
(GV-SP, GIV-X) a) Both tanks are completely filled using overwing
refueling,
b) Both Fuel Flow Indicating Systems are
operative,
c) After takeoff, power is set by matching fuel flow
indications on both engines, and
d) Flightcrew maintains a log of fuel burned.
NOTE 1: Do not pull Fuel Qty circuit breakers as this

disables Fuel Level Low caution message.
NOTE 2: Total Fuel indications will be INVALID with

inoperative indicator.
B (O) Except for ER operations, airplane may be

dispatched with one channel inoperative provided:
a) Affected tank is defueled before each refueling,
b) Affected tank is fueled with a known quantity of
fuel,
c) Both fuel flow meters are operative,
d) After takeoff, power is set by matching fuel flow
e) Flightcrew maintains a log of fuel burned.
NOTE: Total Fuel indications will be INVALID with

DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FQSC CH FAIL, L-R B (O) Except for ER operations, airplane may be

(Blue – Advisory) dispatched with one channel inoperative provided:
(GV) a) Both tanks are completely filled using overwing
refueling,
b) Both Fuel Flow Indicating Systems are
operative,
c) After takeoff, power is set by matching fuel flow
d) Flightcrew maintains a log of fuel burned.

B (O) Except for ER operations, airplane may be

dispatched with one channel inoperative provided:
a) Affected tank is defueled before each refueling,
b) Affected tank is fueled with a known quantity of
fuel,
c) Both fuel flow meters are operative,
d) After takeoff, power is set by matching fuel flow
e) Flightcrew maintains a log of fuel burned.

DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Front Windshield Fail, L-R B Except for ER operations, airplane may be dispatched
(Amber – Caution) with one inoperative provided airplane is not operated in
(GV-SP, GIV-X) known or forecast icing conditions.
Front Windshield Fault, L-R C Airplane may be dispatched with one inoperative sensor
(Blue – Advisory) in each Windshield Heat System.
(GV-SP, GIV-X)
Fuel Crossflow Valve Open B (O) Except for ER operations, airplane may be
(Amber – Caution) dispatched with inoperative crossflow valve provided:
(GV-SP, GIV-X) a) All Fuel Boost Pumps are operative,
c) Fuel Quantity Indicating System is operative,
d) Fuel Tank Temperature System is operative,
and
AFM Limitations.
NOTE: Avoid uncoordinated maneuvers when Fuel

Fuel Return Fail, L-R B Airplane may be dispatched provided:

(Blue – Advisory) a) Flightcrew monitors fuel tank temperature, and
(GV-SP) b) Airplane is operated in accordance with
AFM Limitations.
FUEL RETURN FL, L-R B Airplane may be dispatched provided:

(Blue – Advisory) a) Flightcrew monitors fuel tank temperature, and
(GV) b) Airplane is operated in accordance with
AFM Limitations.
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
FWD CAB TMP FAN FL C (O) Airplane may be dispatched provided:

(GV) posted:
 Cockpit Temp Fan Fail.
b) Forward Temperature Manual mode is
operative,
d) FWD CABIN SENSOR FAN, LEER D-9, is
pulled and collared, and
e) Flightcrew monitor forward cabin temperature
and forward cabin duct temperature.
F WSHLD FAIL, L-R B Except for ER operations, airplane may be dispatched

(Amber – Caution) with one inoperative provided airplane is not operated in
(GV) known or forecast icing conditions.
GCU Fail, L-R A Except for ER Operations, airplane may be dispatched

(Blue – Advisory) with one Engine Generator Control Unit (GCU)
(GV-SP, GIV-X) inoperative provided:
a) APU Generator is used for all phases of flight,
b) Airplane is operated at or below FL 450,
NOTE 1: This relief only applies to airplanes not |

affected by AD 2017-20-08. |
NOTE 2: Crew must verify and abide by AD and AFM |

APU limitations. |
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
GCU FAIL, L-R A Except for ER Operations, airplane may be dispatched



APU limitations. |
Generator Fail, L-R A (O) Except for ER Operations, airplane may be

(Blue – Advisory) dispatched with one Engine Generator Control Unit
(GV-SP, GIV-X) (GCU) inoperative provided:
b) Airplane is operated at or below FL 450 (GV-SP)
or FL 370 (GIV-X),


APU limitations. |
GEN FAIL, L-R A Except for ER Operations, airplane may be dispatched



APU limitations. |
GPS 1-2 Fail B Airplane may be dispatched except where enroute

(Blue – Advisory) operations or approach minimums require the use of
(GV-SP, GIV-X) GPS or GNSSU.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
GPS 1-2 FAIL B Airplane may be dispatched except where enroute

(Blue – Advisory) operations or approach minimums require the use of
(GV) GPS or GNSSU.
GPWS 1-2 Fail A (O) Airplane may be dispatched provided:

(GV-SP, GIV-X) b) Pilot-Not-Flying (PNF) monitors flight progress
with reference to radio altimeter data and
situational awareness,
c) PNF advises Pilot-Flying (PF) of adverse
situations,
GPWS FAIL A (O) Airplane may be dispatched provided:

(GV) b) Pilot-Not-Flying (PNF) monitors flight progress
with reference to radio altimeter data and
situational awareness,
c) PNF advises Pilot-Flying (PF) of adverse
situations,
HUD COMP Fan Fail C Airplane may be dispatched provided extended ground
(Blue – Advisory) operations are avoided.
(GV-SP, GIV-X)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
HUD OHU Fan Fail C Airplane may be dispatched, provided:

(Blue – Advisory) a) Extended ground operations are avoided, and
(GV-SP, GIV-X) b) Pilot selected HUD brightness is reduced.
Hydraulic Temp Sen Fail, L-R B Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X) NOTE: Accuracy of hydraulic quantity indication will be
degraded during long flights in cold soak
conditions. If Right Hydraulic System (R SYS)
sensor has failed in flight, there is no protection
against overheating R SYS pumps during Power
Transfer Unit (PTU) operation. In flight, with
either or both sensors failed, there is no warning
of hot hydraulic system temperatures.
HYD TMP SEN FL, L-R B Airplane may be dispatched.

(Blue – Advisory)
(GV) NOTE: Accuracy of hydraulic quantity indication will be
degraded during long flights in cold soak
conditions. If Right Hydraulic System (R SYS)
sensor has failed in flight, there is no protection
against overheating R SYS pumps during Power
Transfer Unit (PTU) operation. In flight, with
either or both sensors failed, there is no warning
of hot hydraulic system temperatures.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Ice Detect Fail, L-R B (O) Airplane may be dispatched provided:

(Amber – Caution) a) Airplane is operated in accordance with
(GV-SP, GIV-X) alternate AFM procedures,
b) Cowl Anti-Ice shall be selected ON manually any
time visible moisture is present and SAT is
+10 degrees C or less, and
c) Wing Anti-Ice should be selected ON manually if
icing conditions are imminent or immediately
upon detection of ice formation on the wings,
winglets, or windshield edges.
NOTE: With Ice Detection Systems inoperative,

automatic anti-ice is not available.
ICE DETECT FL, L-R B (O) Airplane may be dispatched provided:

(Amber – Caution) a) Airplane is operated in accordance with
(GV) alternate AFM procedures,
b) Cowl Anti-Ice shall be selected ON manually any
time visible moisture is present and SAT is
+10 degrees C or less, and
c) Wing Anti-Ice should be selected ON manually if
icing conditions are imminent or immediately
upon detection of ice formation on the wings,
winglets, or windshield edges.
NOTE: With Ice Detection Systems inoperative,

automatic anti-ice is not available.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
IRS 1-2-3 Fail A (O) Airplane may be dispatched with one IRS
(GV-SP, GIV-X) a) Both PFD attitude indicating systems operate
independently,
b) Flightcrew ensure same IRS is NOT used as
attitude source for both pilots,
c) Standby Attitude Indicator is operative, and
IRS 1-2-3 FAIL A (O) Airplane may be dispatched with one IRS
(GV) a) Both PFD attitude indicating systems operate
independently,
b) Flightcrew ensure same IRS is NOT used as
attitude source for both pilots,
c) Standby Attitude Indicator is operative, and
IRS 1-2-3 ON DC A Airplane may be dispatched provided:

(Blue – Advisory) a) Only one IRU/IRS is on Secondary Power, and
(GV) b) Repairs are made within 1 flight day.
IRU On Sec Pwr A Airplane may be dispatched provided:

(Blue – Advisory) a) Only one IRU/IRS is on Secondary Power, and
(GV-SP, GIV-X) b) Repairs are made within 1 flight day.
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
IRU Sec Pwr 1-2-3 Fail A Airplane may be dispatched with one back-up battery
(GV-SP, GIV-X) a) The affected battery is located in the #2 and |
#3 IRU back up battery position, and
b) Repairs are made within 1 flight day.
A Airplane may be dispatched with one back-up battery |

a) Airplane is operated in Day VMC conditions, and
A Airplane may be dispatched with one back-up battery |

a) All other components of the Electrical Power
system are operative, and
LASERTRAK FAIL B Airplane may be dispatched provided at least one flight

(Blue – Advisory) Management System is operative.
(GV)
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
L PSU Fan Fail B (O) Airplane may be dispatched provided:

(Blue – Advisory) a) Ambient Temperature is 95 degrees F
(GV-SP, GIV-X) (35 degrees C) or cooler,
b) TRU electrical loads are 50 percent or less,
c) Right main TRU is operative,
d) Both Environmental Control System (ECS)
e) Flightcrew minimize ground operation time, and
f) For ground operations longer than 15 minutes,
flightcrew ensure main and baggage doors are
closed, APU air is selected “ON” and outflow
valve is fully OPEN.
LX Fail C Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X)
Mach Trim 1-2 Fail B Airplane may be dispatched with one Mach Trim
(Blue – Advisory) System inoperative.
(GV-SP, GIV-X)
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
MADC 1-2-3 FAIL B (O) Airplane may be dispatched with one micro air data
(Blue – Advisory) computer inoperative provided:
operative,
AFM Limitations in Section 01-03-30, 01-03-40,
and 01-21-10,
f) MADC 1: POP A-9, MADC 2: CPOP A-9, and
MADC 3: POP A-10 circuit breakers associated
with the failed Micro Air Data Computer (MADC)
are pulled and collared, and
g) Flightcrew selects operative and different MADC
sources prior to departure.

RVSM airspace.
NOTE 2: For MADC 1 FAIL, expect the L Engine

Backup Air Data advisory and associated
Engine Maintenance message to post.
NOTE 3: For MADC 2 FAIL, expect the R Engine

Backup Air Data advisory and associated
Engine Maintenance message to post.
NOTE 4: For airplanes equipped with ADS-B, (ASC 192

or ASC 214) if MADC 1 is the failed MADC,
select ATC 2 and if MADC 2 is the failed
MADC select ATC 1.
(Continued)
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
MADC 1-2-3 FAIL B (O) Airplane may be dispatched with one micro air data
(Blue – Advisory) computer inoperative provided airplane is operated in
(GV) unpressurized configuration.
(Cont’d)
NOTE: For airplanes equipped with ADS-B, (ASC 192
or ASC 214) if MADC 1 is the failed MADC,
select ATC 2 and if MADC 2 is the failed MADC
select ATC 1.
MADC 1-3 PROBE FL A (O) Except for ER operations, airplane may be

(GV) a) Airplane is not operated in visible moisture or
b) L LWR PITOT HTR: POP A-5, and R LWR
PITOT HTR: CPOP A-5 circuit breakers are
pulled and collared,
c) Flightcrew select MADC sources that are
heater element, and
MADC 2-SBY PROBE FL A (O) Except for ER operations, airplane may be

(GV) a) Airplane is not operated in visible moisture or
b) L UPR PITOT HTR: POP A-6, and R UPR
PITOT HTR: CPOP A-4 circuit breakers are
pulled and collared,
c) Flightcrew select MADC sources that are
heater element, and
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Main Fuel Pump Fail, L-R B (O) Except for ER operations, airplane may be
(Amber – Caution) dispatched with one pump inoperative provided:
(GV-SP, GIV-X) a) Fuel Crossflow Valve is operative,
operative,
and
AFM Limitations.
MAIN PUMP FAIL, L-R B (O) Except for ER operations, airplane may be
(Amber – Caution) dispatched with one pump inoperative provided:
(GV) a) Fuel Crossflow Valve is operative,
operative,
and
AFM Limitations.
MAINT REQUIRED C Airplane may be dispatched.

(Blue – Advisory)
(GV)
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Main TRU Fault, L-R A (O) Airplane may be dispatched with one main TRU
(Amber – Caution) inoperative provided:
(GV-SP, GIV-X) a) Both Generators are operative,
b) Both essential TRUs are operative,
e) Both Battery chargers are operative,
f) Both Main Airplane Batteries are operative,
g) Inoperative L MAIN TRU: LPDB, Left Main AC
section or R MAIN TRU: RPDB, Right Main AC
section TRU circuit breaker on the Power
Distribution Box is pulled and collared, and
h) Repairs are made within 2 flight days.
MAU 1-2-3 Fan Fail B Airplane may be dispatched with one failed fan |
(Blue – Advisory) provided: |
(GV-SP, GIV-X) a) Performance of items affected by the indicated |
MAU are monitored during the flight, and
b) Flightcrew references the appropriate matrix in
AFM Section 03-16-80.
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
MAU 1B-2A-3A-3B Fail A (O) Airplane may be dispatched with one channel
(GV-SP, GIV-X) a) Failed channel is not MAU 1A or MAU 2B,
b) No other failures exist in the Avionics System,
c) Associated MAU circuit breakers:
 MAU 1B PRI: CPOP, A-9,
 MAU 1B SEC: POP, A-9,
 MAU 2A PRI: CPOP, A-8,
 MAU 2A SEC: POP, A-8,
 MAU 3A PRI: POP, A-6,
 MAU 3A SEC: CPOP, A-6,
 MAU 3B PRI: POP, A-5, and
 MAU 3B SEC: CPOP, A-5 are pulled and
collared.
d) Alternate procedures are established and used,
e) Flightcrew discusses contingency procedures for
next worse failures as described in GAC-OIS-09
Dispatch with MAU Channels Inoperative, and
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
MDAU FAIL B Airplane may be dispatched provided all faults are

(GV)
MDAU MEM 90% FULL B Airplane may be dispatched provided all faults are
(GV)
MN TRU FAULT, L-R A (O) Airplane may be dispatched with one main TRU
(GV) a) Both Generators are operative,
b) Both essential TRUs are operative,
e) Both Battery chargers are operative,
f) Both Main Airplane Batteries are operative,
g) Inoperative L MAIN TRU: LPDB, Left Main AC
section or R MAIN TRU: RPDB, Right Main AC
section TRU circuit breaker on the Power
Distribution Box is pulled and collared, and
MRC 1 Fail A Airplane may be dispatched with one MRC failed

(GV-SP, GIV-X) a) Associated Comm and Nav radios and opposite
ATC are operative, and
NOTE: EICAS blue messages “APM FAIL” and “ASCB

FAIL” displayed. “ASCB FAIL” is only displayed
in flight.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
MRC 2 Fail A Airplane may be dispatched provided:

(Blue – Advisory) a) Associated Comm and Nav radios and opposite
(GV-SP, GIV-X) ATC are operative, and
NOTE: With MRC 2 Fail, expect EICAS blue messages

“APM FAIL” and “ASCB FAIL” displayed.
“ASCB FAIL” will display inflight only.
NAV 2 Fail B Airplane may be dispatched as required by 14 CFR.

(Blue – Advisory)
(GV-SP, GIV-X)
NAVCOM Fail B Airplane may be dispatched provided operations do not

(Blue – Advisory) require its use.
(GV-SP, GIV-X)
NMS 1-2 FAIL A Except where enroute operations or approach

(GV) provided:
alignment,
use,

RNAV 2 airspace.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
NMS FAIL A Except where enroute operations or approach

(GV) provided:
alignment,
use,

RNAV 2 airspace.
NWS Fixed Gain B Airplane may be dispatched provided Nose Wheel Tiller
(Blue – Advisory) Steering System is operative.
(GV-SP, GIV-X)
NWS FIXED GAIN B Airplane may be dispatched provided Nose Wheel Tiller
(Blue – Advisory) Steering System is operative.
(GV)
Outflow Valve Fault B Airplane may be dispatched provided:

(Blue – Advisory) a) DC motor is operative, and
(GV-SP, GIV-X) b) Airplane is operated in accordance with
AFM Limitations.
OUTFLOW VLV FAULT B Airplane may be dispatched provided:

(Blue – Advisory) a) DC motor is operative, and
(GV) b) Airplane is operated in accordance with
AFM Limitations.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Pitch Trim 1-2 Power Fail B (O) Airplane may be dispatched with one inoperative
(Blue – Advisory) Autopilot Pitch Trim Servo provided PITCH TRIM
(GV-SP, GIV-X) SERVO #1: POP, E-2, or PITCH TRIM SERVO #2,
CPOP, E-1 circuit breaker is pulled and collared.
RAAS 1-2 Fail B

(Blue – Advisory)
(GV-SP, GIV-X)
RAD ALT 1-2 FAIL B Airplane may be dispatched provided:

(Blue – Advisory) a) Landing weather minimums or operating
(GV) procedures do not require its use, and
b) Other systems affected (E/GPWS, TCAS, Flight
Director, Autopilot, Autothrottle, Altimeter
Ground Awareness Display, Synthetic Vision
Primary Flight Display, HUD Flare Cue) are
considered.
Radio Altimeter 1-2 Fail B Airplane may be dispatched provided:

(Blue – Advisory) a) Landing weather minimums or operating
(GV-SP, GIV-X) procedures do not require its use, and
b) Other systems affected (E/GPWS, TCAS, Flight
Director, Autopilot, Autothrottle, Altimeter
Ground Awareness Display, Synthetic Vision
Primary Flight Display, HUD Flare Cue) are
considered.
Rudder Steering Fail B Airplane may be dispatched provided:

(Amber – Caution) a) Nose Wheel Tiller Steering System is operative,
(GV-SP, GIV-X) and
b) Left seat pilot performs the takeoff and landing
task.
DATE: 08/24/2015
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
RUDDER STRG FAIL B Airplane may be dispatched provided:

(Amber – Caution) a) Nose Wheel Tiller Steering System is operative,
(GV) and
b) Left seat pilot performs the takeoff and landing
task.
SATCOM Call C Airplane may be dispatched provided procedures do not

(Blue – Advisory) require their use.
(GV-SP, GIV-X)
Service Door B (O) Airplane may be dispatched provided a

(Blue – Advisory) crewmember verifies by visual inspection before each
(GV-SP, GIV-X) departure that the associated door is CLOSED and
LOCKED.
SERVICE DOOR B (O) Airplane may be dispatched provided a

(Blue – Advisory) crewmember verifies by visual inspection before each
(GV) departure that the associated door is CLOSED and
LOCKED.
Side Windshield Fail, L-R B Airplane may be dispatched.

(Amber – Caution)
(GV-SP, GIV-X)
Single Rudder B Airplane may be dispatched provided the Rudder

(Blue – Advisory) Limitation indication is operative.
(GV)
Single Speed Brake B Airplane may be dispatched provided the Single Rudder
(Blue – Advisory) indication is operative.
(GV-SP)
SINGLE SPEED BRAKE B Airplane may be dispatched provided the Single Rudder
(Blue – Advisory) indication is operative.
(GV)
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
STCK PUSH 1-2 FAULT A (O) Airplane may be dispatched with one system
(GV) a) Angle of Attack indication is available on both
PFDs,
b) Alternate procedures are established and used,
c) The inoperative stall barrier system is electrically
disabled by pulling and collaring the
SHAKER #1: POP E-6, SHAKER #2: CPOP E-6,
STALL BARR VALVE #1: POP E-5, STALL
BARR VALVE #2: CPOP E-5 Stall Barrier Valve
and Stick Shaker circuit breakers associated
with the failed system,
d) Crew procedures in the event the remaining stall
barrier fails are discussed,
e) If the remaining stall barrier fails the minimum
speed shall be no less than Vref (1.3 Vs) for all
phases of flight (this minimum speed shall be
cross referenced to a normalized AOA value of
0.59 as displayed on the PFD),
f) Weather at departure and destination is
considered,
g) Consideration is given to delaying takeoff or
approach and landing, if windshear is forecast
until such conditions cease, or consideration is
given to proceeding to alternate, and
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
STCK PUSH 1-2 FL A (O) Airplane may be dispatched with one system
PFDs,
considered,
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Stick Push 1-2 Fail A (O) Airplane may be dispatched with one system
(GV-SP, GIV-X) a) Angle of Attack indication is available on both
PFDs,
considered,
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Stick Push 1-2 Fault A (O) Airplane may be dispatched with one system
PFDs,
considered,
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
STICK PUSH UNAVAIL A (O) Airplane may be dispatched with one system
PFDs,
considered,
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Stick Push Unavailable A (O) Airplane may be dispatched with one system
PFDs,
considered,
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Stick Shake 1-2 Fail A Airplane may be dispatched with a single control
(Blue – Advisory) column shaker inoperative provided:
PFDs,
b) Both stall barrier systems are operative, and
STICK SHAKE 1-2 FL A Airplane may be dispatched with a single control

(Blue – Advisory) column shaker inoperative provided:
PFDs,
b) Both stall barrier systems are operative, and
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Stuck MIC ACP 3 A (O) Airplane may be dispatched with ACP 3 indicating
(Blue – Advisory) stuck MIC provided:
(GV-SP, GIV-X) a) Pilot and Copilot ACPs are operative,
b) OBSERVER ACP: REER, D-7 is pulled and
collared,
c) Affected ACP is not required as determined by
the Pilot-in-Command,
d) Flight Deck to cabin communication is operative,
e) A passenger seat in the passenger cabin is
made available to an FAA inspector for the
performance of official duties,
f) Alternate procedures are established and used,
g) Required minimum safety equipment (safety belt
and oxygen) is available,
h) Seat is acceptable to the FAA inspector for
performance of official duties, and
i) Repairs are made within 2 flight days.
NOTE 1: These provisos are intended to provide for

occupancy of the above seats by an
FAA inspector when the minimum safety
equipment (oxygen and safety belt) is
functional and the inspector determines the
condition to be acceptable.
NOTE 2: The pilot-in-command will determine if the

minimum safety equipment is functional for
other persons authorized to occupy any
observer seat(s).
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
S WSHLD FAIL, L-R B Airplane may be dispatched.

(Amber – Caution)
(GV)
TCAS Fail A (O) Airplane may be dispatched provided:

(Blue – Advisory) a) System is deactivated and secured by pulling
(GV-SP, GIV-X) and collaring TCAS: POP, F-2 circuit breaker,
b) Enroute or approach procedures do not require
its use, and
TCAS FAIL A (O) Airplane may be dispatched provided:

(Blue – Advisory) a) System is deactivated and secured by pulling
(GV) and collaring TCAS: POP, F-2 circuit breaker,
b) Enroute or approach procedures do not require
its use, and
Terrain 1-2 Fail B Airplane may be dispatched.

(Blue – Advisory)
Terrain Bus Fail B Airplane may be dispatched.

(Blue – Advisory)
DATE: 07/05/2018
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
THROT QUAD 1-2 FL B Airplane may be dispatched.

(Blue – Advisory)
(GV) NOTE: With both Channel 1 and Channel 2 failed, the
autothrottle system will be inoperative.
Throttle Quadrant 1-2 Fail B Airplane may be dispatched.

(Blue – Advisory)
(GV-SP, GIV-X) NOTE: With both Channel 1 and Channel 2 failed, the
autothrottle system will be inoperative.
VHF COM 1-2 Fail C Airplane may be dispatched with any in excess of those
(Blue – Advisory) required by 14 CFR provided it is not powered by the |
(GV-SP, GIV-X) Emergency AC Bus, Emergency DC Bus, Battery Bus, |
Battery Direct Bus, or the DC Transfer Bus and not |
required for emergency procedures. |
NOTE: Comm 1 is powered by the Emergency Bus. |
VHF COMM 1-2 FAIL C Airplane may be dispatched with any in excess of those
(Blue – Advisory) required by 14 CFR provided it is not powered by the |
(GV) Emergency AC Bus, Emergency DC Bus, Battery Bus, |
Battery Direct Bus, or the DC Transfer Bus and not |
required for emergency procedures. |
NOTE: Comm 1 is powered by the Emergency Bus. |
WG A/I SYS FL, L-R B Except for ER operations, airplane may be dispatched
(Amber – Caution) with wing anti-ice system inoperative provided airplane
(GV) is not operated in known or forecast icing conditions.
NOTE: Do not select affected side Wing Anti-Ice to ON.

DATE: 08/24/2015
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Windshear 1-2 Fail A (O) Airplane may be dispatched provided:

(Blue – Advisory) a) At least one radio altimeter is operative,
(GV-SP, GIV-X) b) Alternate procedures are established and used,
c) Flightcrew comply with AFM/AOM guidance in
windshear situations and recommended
procedures when encountering windshear, and
NOTE: Operator’s alternate procedures should include

reviewing windshear avoidance and windshear
WINDSHEAR FAIL A (O) Airplane may be dispatched provided:

(Blue – Advisory) a) At least one radio altimeter is operative,
(GV) b) Alternate procedures are established and used,
c) Flightcrew comply with AFM/AOM guidance in
windshear situations and recommended
procedures when encountering windshear, and
NOTE: Operator’s alternate procedures should include

reviewing windshear avoidance and windshear
DATE: 12/18/2017
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
Wing Anti-Ice Sys Fail, L-R B Except for ER operations, airplane may be dispatched
(Amber – Caution) with wing anti-ice system inoperative provided airplane
(GV-SP, GIV-X) is not operated in known or forecast icing conditions.
NOTE: Do not select affected side Wing Anti-Ice to ON.
Yaw Damper 1-2 Fail B (O) Except for ER operations, airplane may be
(Amber – Caution) dispatched with one channel inoperative provided
(GV-SP, GIV-X) airplane is operated in accordance with AFM Limitations
in the event the operative Yaw Damper fails.
YD 1-2 FAIL B (O) Except for ER operations, airplane may be

(Amber – Caution) dispatched with one channel inoperative provided
(GV) airplane is operated in accordance with AFM Limitations
in the event the operative Yaw Damper fails.
YD 1-2 Power Fail B (O) Airplane may be dispatched with one inoperative
(Blue – Advisory) yaw damper system provided the inoperative
(GIV-X) YAW DAMPER SERVO #1: POP, D-6 or
YAW DAMPER SERVO #2: CPOP, D-6 circuit breaker
is pulled and collared.
YD 1-2 Fail B (O) Airplane may be dispatched with one inoperative

(Blue – Advisory) yaw damper system provided the inoperative
(GV-SP) YAW DAMPER SERVO #1: POP, D-6 or
YAW DAMPER SERVO #2: CPOP, D-6 circuit breaker
is pulled and collared.
DATE: 11/07/2014
AIRCRAFT: TABLE KEY
CAS Messages
Change
Item 1 2 Bar
50 HZ Power Fail, L-R C (O) Airplane may be dispatched provided:

(Blue – Advisory) a) L FREQ CONV: Left PDB or R FREQ CONV:
(GV-SP, GIV-X) Right PDB circuit breaker is pulled and collared,
b) Flightcrew brief passengers on items that are
inoperative with the failure of the power source
for cabin entertainment, and
c) Backup battery is available if EFB is used.
60 HZ Power Fail, L-R C (O) Airplane may be dispatched provided:

(Blue – Advisory) a) Affected L FREQ CONV: Left PDB or R FREQ
(GV-SP, GIV-X) CONV: Right PDB circuit breaker is pulled and
collared,
60HZ PWR FAIL, L-R C (O) Airplane may be dispatched provided:

(Blue – Advisory) a) Affected L FREQ CONV: Left PDB or R FREQ
(GV) CONV: Right PDB circuit breaker is pulled and
collared,

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U.S.

Master Minimum Equipment List (MMEL)

Troy A. Zwicke, Chair

Federal Aviation Administration (FAA)

Telephone: (562) 627-5317

2a 11/09/2001 HIGHLIGHTS OF REV., DEFINITIONS, 34-2, 34-3, 34-4, 34-5, 34-6, 34 7,

3 08/11/2003 HIGHLIGHTS OF REV., DEFINITIONS, 22-1, 23-1, 23-2, 23-3, 23-4, 23 5,

4 12/14/2004 HIGHLIGHTS OF REV., DEFINITIONS, 21-1, 21-2, 21-4, 21-5, 21-6, 22 1,

4a 06/02/2006 HIGHLIGHTS OF REV., DEFINITIONS, 23-2, 23-5, 23-6, 23-7, 23-8, 25 1,

4b 07/05/2006 HIGHLIGHTS OF REV., DEFINITIONS, 25-15, 25-16, 25-17.

5 06/18/2007 ISSUED IN ERROR, THEN RETRACTED.

7 02/04/2010 HIGHLIGHTS OF REV., DEFINITIONS, 21-3, 21-5, 21-6, 21-7, 21-8, 22 1,

7a 11/08/2010 HIGHLIGHTS OF REV., DEFINITIONS, 22-1, 23-8, 23-9, 23-10, 23-12,

Cover Page, TOC, Control Page, Log of Revisions,Highlights of Change,

PAGE NO. EXPLANATION OF CHANGE

21-3 Item 21-4, Removed Plural

21-4 Item 21-8. Capitalization correction.

21-5 Item 21-2. Capitalization correction.

Item 21-9-11. Removed Plurals

21-6 Item 21-12. Capitalization correction.

21-7 Item 21-15. Changed A/C to AC.

21-8 Item 21-17-02, Deleted item from MMEL.

22-2 Item 22-7-10, Remove plurals

23-3 Item 23-2-2 and 3, corrected numbering

Item 23-4-02, Updated per Policy Letter 120 r2.

Item 23-5, removed heading relief requirement.

Item 23-5 (a) updated relief category.

Item 23-5.2 – Updated title.

23-5 Item 23-8-1, Updated per Policy Letter 09.

23-8 Item 23-8 14.1(b) updated relief categories.

23-9 Item 23-15(b), remove invalid “B’ relief.

23-10 Item 23-17-02, Updated per Policy Letter 106 r5.

24-1 Item 24-1, Added 2 Notes.

Item 24-4, Inserted ‘and’ to proviso.

Item 24-5, Updated proviso.

25-1 Item 25-2-01, -2. Updated per Policy Letter 79 r9.

25-2 Item 25-2-03, -4. Updated per Policy Letter 79 r9.

25-3 Item 25-2-05, -6. Updated per Policy Letter 79 r9.

25-4 Item 25-3. Deleted relief for Crewmember Shoulder Harnesses.

25-5 Item 25-5, removed plural.

Item 26-6, updated note.

25-8 Item 25-10, updated proviso.

25-10 Item 25-15-1, -2, -3. Added (M) procedure.

Item 25-17. Deleted item and removed from MMEL.

25-12 Item 25-22-01. Deleted item and removed from MMEL.

25-13 Item 25-26 renumbered.

25-14 Item 25-27 renumbered.

26.3 Item 26-5 Added D proviso.

26-4 Item 26-6. Added (M) procedure and D proviso.

27-1 Item 27-7. Added (O) procedure.

28-2 Item 28-2. Added (O) procedure.

28-3 Item 28-2. Added (O) procedure.

29-1 Item 29-6, -7. Added (O) procedure.

31-1 Item 31-2, Updated proviso to Policy Letter 87 r10.

31-2 Item 31-2. Removed extra wording.

32-1 Item 32-3. Deleted Landing Gear Position Indicators.

33-1 Item 33-1. Removed NVG Note.

Item 33-3. Removed note below item title.

33-2 Item 33-3. Added (O) procedure requirement.