8 7 6 5 4 3 2 1

REVISIONS

GENERAL NOTES: UNLESS OTHERWISE SPECIFIED REV. DESCRIPTION CHECKED DATE

11. GROUNDING - RELEASED PER ECO 23881 J. WHITE 3-7-18

1. ALL WIRING TO COMPLY WITH AIRCRAFT MANUFACTURER'S
MAINTENANCE / WIRING MANUAL STANDARD PRACTICES. IN ALL A. INSTALL SHIELDED WIRE WHERE INDICATED AND GROUND A REVISED PER ECO 24039 J. WHITE 8-07-18
AREAS NOT DEFINED BY PRECEDING REFERENCE, ALL WIRING TO ONLY WHERE INDICATED. ALL GROUND WIRES SHALL BE
CONNECTED TO AIRFRAME GROUND. GROUND WIRE LENGTH NOT B REVISED PER ECO 24082 J. WHITE 9-04-18
COMPLY WITH AC 43.13-1B, CHAPTER 11 & AC 43.13-2B.
D
TO EXCEED 8" FOR SHIELD TERMINATIONS. ALL OTHER GROUND C REVISED PER ECO 24151 J. WHITE 12-04-18 D
TERMINATIONS MAY BE TAKEN TO THE NEAREST VERIFIABLE (2.5
MILI-OHM RESISTANCE BETWEEN GROUNDING DEVICE AND D REVISED PER ECO 24317 J. WHITE 2-28-19
2. ALL WIRE TO BE IN ACCORDANCE WITH; ANSI/NEMA
WC27500-2000 STANDARD FOR AEROSPACE AND INDUSTRIAL ADJACENT AIRFRAME STRUCTURE) GROUNDING DEVICE BUT MAY E REVISED PER ECO 24364 J. WHITE 4-8-19
ELECTRICAL CABLE, ANSI APPROVAL DATE: JANUARY 4, 2002 OR NOT EXCEED 24 INCHES. MINIMUM WIRE GAUGE ON GROUNDS
IN EXCESS OF 14 INCHES SHALL BE 20 AWG. ALL GROUND F REVISED PER ECO 24398 J. WHITE 5-14-19
LATER APPROVED REVISION. UNSHIELDED WIRE TO BE
M22759/16 OR /34, SHIELDED WIRE TO BE M27500-(XX)TG OR WIRES TO BE KEPT AS SHORT AS POSSIBLE. G REVISED PER ECO 24559 J. WHITE 8-9-19
SD (X)T14 OR 23 (XX = CONDUCTOR SIZE) (X = NO. WIRES IN B. AIRFRAME TERMINATIONS SHALL BE SEPARATED BY TYPE
H REVISED PER ECO 24713 J. WHITE 11-15-19
CABLE), ALL SHIELDS TYPE (T) AND JACKETS TYPE (14). OF GROUND AND SIGNAL CATEGORIES. EACH GROUNDING DEVICE
(STUD, MODULE, ETC.) SHALL BE IDENTIFIED AS TO TYPE (CHAS, J REVISED PER ECO 24878 J. WHITE 5-18-20
INDICATES EXISTING WIRE OR COMPONENT. SHLD AND DC). THERE SHALL BE A MINIMUM OF 1" SEPARATION
3.
BETWEEN EACH NEWLY INSTALLED GROUNDING DEVICE. IT IS
INDICATES EQUIPMENT OR WIRES TO BE DELETED. PERMISSIBLE TO RE-USE EXISTING GROUNDING DEVICES WITH
INDICATES NEW OR REROUTED WIRING.
VERIFICATION OF 2.5 MILI-OHM RESISTANCE BETWEEN
OR INDICATES CAP AND STOW WIRE. GROUNDING DEVICE AND ADJACENT AIRFRAME STRUCTURE.
X C. COMPONENTS MOUNTED IN RELAY BOXES, CB PANELS AND
INDICATES WIRES CONNECTED BETWEEN LIKE SYMBOLS.
SWITCH PANELS DO NOT REQUIRE GROUNDING UNLESS
SPECIFICALLY REQUIRED ON THE INDIVIDUAL WIRING DIAGRAM.
ALL INSTALLED WIRES TO BE 22 AWG UNLESS OTHERWISE D. ONLY THE MINIMUM AMOUNT OF SHIELD SHALL BE
4.
SPECIFIED. REMOVED FROM CABLES. CABLES WHICH REQUIRE SPECIAL
TREATMENT OF THE SHIELDS SHALL BE ADDRESSED ON EACH
C 5. IDENTIFY UNSHIELDED WIRES WITH WIRE NUMBER SHOWN WITHIN WIRING DIAGRAM. C
6" OF EACH END AND AT APPROXIMATELY 12" INTERVALS,
CONTINUING FOR LENGTH OF WIRES.
12. WIRE ROUTING
6. IDENTIFY CONNECTOR(S) WITH REFERENCE DESIGNATOR(S) SHOWN A. A PHYSICAL SEPARATION SHALL BE MAINTAINED BY ALL
IN PERMANENT INK. SYSTEM #1 (PRIMARY) FROM SYSTEM #2 (SECONDARY) AVIONICS.
B. EXPANDABLE SLEEVING MAY BE USED FOR ALL ADDED
BRANCH CABLES FROM THE POINT AT WHICH THE CABLES LEAVE
7. TYPICAL LENGTH OF EXPOSED WIRING AT SHIELD TERMINATIONS THE MAIN BUNDLE TO THE ADDED CONNECTION. BOTH ENDS OF
NOT TO EXCEED 6". THE EXPANDABLE SLEEVING SHALL BE SECURED BY AN
APPROPRIATE MEANS (CABLE TIES, STRAIN RELIEF, ETC). CABLES IN
8. STRIP ALL WIRING, INSTALL CONTACTS & CONNECTORS IN OTHER AREAS MAY USE THIS METHOD OF SECURING CABLING.
ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. C. A 2ND ID BAND SHALL BE PLACED ON OR NEAR ALL
ROUTE ALL NEW WIRING AWAY FROM EXISTING AIRCRAFT FUEL PRODUCTION CONNECTORS, WHICH ARE FREQUENTLY HANDLED, AND
9.
QUANTITY INDICATION AND OTHER FUEL SYSTEM WIRING. MAINTAIN WHICH MAY BE MISCONNECTED. THESE CONNECTIONS INCLUDE
A MINIMUM OF 2" SEPARATION. INSTRUMENT CONNECTORS AT THE INSTRUMENT PANEL AND
CONTROL PANEL CONNECTORS IN THE PEDESTAL AND SIDE
10. BONDING CONSOLES. ADDITIONALLY, ALL CONNECTORS ADDED BY THIS
MODIFICATION SHALL HAVE THE SAME TYPE OF I.D. BAND ADDED IN
A. ALL ELECTRICAL COMPONENTS SHALL BE INSTALLED ON
B ADDITION TO THE STANDARD NUMBERING SYSTEM. THE I.D. BANDS
B
METAL SHELVES, FLOORBOARDS, BRACKETS, ETC., WHERE SHALL IDENTIFY THE UNIT OR ITS FUNCTION AND ITS RELATIVE
PRACTICAL. NUMBER.
D. WHERE POSSIBLE, CABLE ROUTING SHOULD BE ACCOMPLISHED
B. ALUMINUM SURFACES THAT WILL BE USED AS BONDING
TO ENSURE MAXIMUM SEPARATION; FOR EXAMPLE, ONE SYSTEM
SURFACES (SHELF TO AIRFRAME) OR GROUNDING SURFACES ROUTED ON ONE SIDE OF THE AIRCRAFT AND THE OTHER SYSTEM
(STUDS, TJ MODULES, MOUNTED CONNECTORS, ETC.) SHALL BE ON THE OPPOSITE SIDE. SOME AREAS, SUCH AS PEDESTAL,
TREATED AS FOLLOWS: BEHIND INSTRUMENT PANELS, JUNCTION BOXES AND EQUIPMENT
RACKS BRING SYSTEMS CLOSE TOGETHER, AND IN THESE
1. REMOVE NONCONDUCTING FINISHES, SUCH AS PAINT OR
CONFINED AREAS PHYSICAL SEPARATION MAY NOT BE POSSIBLE.
ANODIZING FILM. IN THESE CASES, CABLES SHOULD BE TIED TOGETHER FOR THE
2. ON ALUMINUM SURFACES, APPLY A SUITABLE CONDUCTIVE SHORTEST POSSIBLE DISTANCES REQUIRED FOR INSTALLATION AND
CHEMICAL SURFACE TREATMENT TO MEET THEN SEPARATED.
MIL-DTL-81706.

ACFT MODEL(S): INT. NEXT ASSY: DRAWN

THIRD ANGLE TOLERANCES
PROJECTION (UNLESS OTHERWISE SPECIFIED) M. CHRISTIANSON 11-08-17 One S-TEC Way
+.006
A
ENGINEER
Mineral Wells, TX
A
HOLE: -.001
M. CHRISTIANSON 11-08-17
DECIMAL: .XXX: ±.010
03-07-18 TITLE:
APPROVED
DECIMAL: .XX: ±.03
FORM (SWorks) 86359 REV -

DECIMAL: .X: ±.1 S. JOSEPH

ALL SHEETS MAINTAIN THE SAME REVISION LEVEL.
ANGLES:
SURFACE
±1°
125
W/D 01326 DFCS
ROUGHNESS: DIMENSIONING AND TOLERANCING
SHALL BE IAW ASME Y14.5M-1994.
EXPORT COMPLIANCE: TRANSFER OF S-TEC DATA (DOCUMENTS, SOFTWARE, DRAWINGS,
SPECS, ETC) BY ANY MEANS TO A FOREIGN PERSON OR ENTITY, WHETHER IN THE UNLESS OTHERWISE SPECIFIED
UNITED STATES OR ABROAD, MAY REQUIRE U.S. GOVERNMENT AUTHORIZATION. REMOVE ALL BURRS, ALL DIMENSIONS ARE IN INCHES,
BREAK SHARP EDGES
MILLIMETERS IN BRACKETS. SIZE CAGE CODE Drawing No.:
NOTICE: THE INFORMATION CONTAINED HEREIN IS CONFIDENTIAL AND PROPRIETARY R.015 MAX. INSIDE
INFORMATION, AND AS SUCH, CANNOT BE COPIED OR DISCLOSED TO OTHERS WITHOUT
THE PRIOR WRITTEN CONSENT OF THE S-TEC CORPORATION.
CORNER RADII .015 MAX.
DIMENSIONAL LIMITS APPLY B NA 10245
AFTER FINISH/PLATING. SCALE: 1:1 DO NOT SCALE DRAWING SHEET 1 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

GENERAL NOTES: UNLESS OTHERWISE SPECIFIED FOR REVISION HISTORY SEE SHEET 1

13 IF THERE IS NO SOURCE SELECTION CAPABILITY IDENTIFYING GPS 2 AS

THE PRIMARY SOURCE OF DATA WHEN SELECTED ON THE PFD, A SWITCH 27 ANALOG INTERFACE REQUIREMENTS:
AND ANNUNCIATOR MUST BE INSTALLED SO THAT PIN 58 IS GROUNDED
WHEN GPS 2 IS SELECTED AS THE PRIMARY NAV SOURCE. DC COURSE ERROR
D USE WHEN NO DIGITAL COURSE (ARINC LABEL 100) IS D
14. CIRCUIT BREAKERS AND SWITCHES SHALL BE SUITABLY LABELED AVAILABLE AND CONFIGURED FOR AND INTERFACED TO A DC
BY OPERATION & CONTROLLED CIRCUIT AS IDENTIFIED IN THIS
WIRING DIAGRAM. MARKINGS SHALL BE LEGIBLE AND NOT EASILY HEADING SOURCE.
ERASED. LETTERS MUST BE AT LEAST .06" IN HEIGHT. LOCATION RANGE (± 12.5 VDC)
AND METHOD OF MARKING SHALL BE CONSISTENT WITH EXISTING MAX VOLTAGE +12.5 VDC MIN VOLTAGE -12.5 VDC
AIRCRAFT MARKINGS.
SCALING
210 mVDC/DEG
EXAMPLE ON
0 TO +12.5 VDC COMMAND TURN RIGHT
SWITCH 0 TO -12.5 VDC COMMAND TURN LEFT
DC HEADING ERROR
CB
OFF USED WHEN CONFIGURED FOR AND INTERFACED TO A DC
HEADING SOURCE.
RANGE (± 12.5 VDC)
15 CONNECT TO EXISTING AUDIO CONTROL PANEL AS REQUIRED. IF MORE MAX VOLTAGE +12.5 VDC MIN VOLTAGE -12.5 VDC
THAN ONE DEVICE IS TIED TO THE SAME AUDIO INPUT PIN OF THE AUDIO
AMP A RESISTOR MAY BE REQUIRED IN SERIES WITH MULTIPLE AUDIO 29 1 20600A RESISTOR, METAL FILM - - -
SCALING
C INPUTS TO PREVENT LOADING DOWN THE AUDIO (LOW VOLUME). 28 2 M83536/2-015M RELAY, DPDT, 5 AMP TE CONNECTIVITY - - C
550 mVDC/DEG
16 AUDIO WIRE MUST BE TERMINATED TO AN UNMUTED AUDIO INPUT OF 0 TO +12.5 VDC COMMAND TURN RIGHT 27 1 61282-08 DIODE MODULE, DOUBLE - - -
THE EXISTING AUDIO CONTROL PANEL. REFER TO APPLICABLE 0 TO -12.5 VDC COMMAND TURN LEFT 26 3 M12883/45-01S RELAY SOCKET - - -
MANUFACTURER'S INSTALLATION MANUAL TO ENSURE LOCALIZER / GPS APPROACH ENABLE
COMPATIBILITY WITH EQUIPMENT. 25 3 M83536/2-024M RELAY - - -
NORMALLY OPEN INPUT (OPEN OR GROUND OPERATION).
17 REFER TO MANUFACTURERS INSTALLATION MANUAL OR INSTALLATION 24 REF 3595 SWITCH, PUSHBUTTON, N.O. - - -
DOCUMENTATION FOR FURTHER INTERCONNECT INFORMATION. INPUT ACTION
GROUND APPROACH ACTIVE 23 REF 03112 SWITCH, TRIM COMMAND - - -
18 AP COMPUTER POWER MAY BE 28VDC OR 14VDC DEPENDING ON THE OPEN (10V PULL-UP) APPROACH NOT ACTIVE
22 REF 3519 SWITCH, DPDT, MOM - - -
AIRCRAFT'S GENERATED VOLTAGE. IF THE SYSTEM INSTALLATION
REQUIRES 14 VDC OPERATION, CONNECTOR P1 PIN 75 MUST BE GROUNDED. TWO WIRE DIFFERENTIAL ANALOG INPUTS
21 REF 3934 COIL CORD - - -
LEFT/RIGHT (CROSS TRACK) DEVIATION
19 CAN BUSES AND ASSOCIATED MAINTENANCE SWITCH MUST BE 20 REF 2111031001 POT, 1 TURN, 10K OHM, 2W, LINEAR - - -
INSTALLED AND ACCESSIBLE FOR AUTOPILOT CONFIGURATION AND INPUT ACTION
MAINTENANCE. 150m VDC 100% RIGHT DEVIATION 19 2 30D88 ANNUNCIATOR LIGHT, LED - - -
-150m VDC 100% LEFT DEVIATION
18 1 3520 SWITCH, TOGGLE SPDT - - -
20. INDIVIDUAL SHIELDS FOR ALL CONNECTORS WILL BE DAISY CHAINED UP/DOWN (GLIDE SLOPE) DEVIATION
TOGETHER AND TERMINATED TO 3100P1 PIN 78 AND 3100P2 PIN 77 17 11 52133-02 TERMINATOR, SOLDER SLEEVE - - -
RESPECTIVELY. INPUT ACTION
B
16 6 6104 SLIDE LOCK - - -
21. WIRES NOT INCLUDED IN KIT TO BE PROVIDED BY INSTALLER. 150m VDC 100% UP DEVIATION B
-150m VDC 100% DOWN DEVIATION 15 6 5508 CONNECTOR HOOD - - -

22 PIN 57 OF CONNECTOR P1 MUST BE GROUNDED WHEN ST-360 LATERAL FLAG (NAV FLAG) 14 4 3406 CONNECTOR RECEPTACLE - - -
PRESELECTOR ALERTER IS INTERFACED TO THE AP COMPUTER.
INPUT ACTION 13 18 52119-02 SPLICE, IN-LINE CRIMP - - --
23. DELETED > 220mVDC VALID
12 2 4906 CIRCUIT BREAKER, 5 AMP - - -
< 180mVDC INVALID
24 NAV SOURCE SELECTION: 11 1 3551 TOGGLE SWITCH, LOCKING - - -
VERTICAL FLAG (G/S FLAG)
CUSTOM DDW LABEL: 10 3 33190 CONNECTOR, PLUG, 15 PIN - - -
ARINC 429 LABEL THAT CONTAINS UNIQUE BIT SETS FOR INPUT ACTION
ILS, VOR, GPS, (BC OPTIONAL), AND FMS-APR. THIS CAN BE SET > 220mVDC VALID 9 3 34136 CONNECTOR, RECEPTACLE, 15 PIN - - -
AS ONE BIT FOR EACH
- APR/LOC BIT SET = ILS < 180mVDC INVALID
8 33 5210 CRIMP CONTACT,PIN,D-SUB, 20-24 AWG, -- - -
- FMS(GPSS) BIT SET = GPSS (FP, DIRECT-T, ETC)
- FMS-APR BIT SET = FMS APR 7 56 5208 CRIMP CONTACT,RECPT,D-SUB, 20-28 AWG, - - -
- VOR BIT SET = VOR
OR JUST TWO BITS 28 WHEN NO HSI READY INPUT IS PROVIDED FROM AN INTERFACED 6 86 5279 CONTACT, FEMALE, CRIMP - - -
- APR/LOC BIT SET ALONE = ILS NAVIGATION SOURCE P1 PIN 70 OF THE AP COMPUTER MUST BE
- FMS(GPSS) BIT SET ALONE = GPSS GROUNDED. 5 2 3415 CONNECTOR, RECEPTACLE, 78 PIN - - -
- APR/LOC AND FMS BIT SET = FMS APPROACH
- NO BITS SET = VOR 4 2 5504 HOOD CONNECTOR RECEPTACLE, 50 PIN - - -
29 SEE INSTALLATION INSTRUCTIONS TO DETERMINE IF
OR APPROACH AND MODE SELECT DISCRETES MAY BE USED FLAP COMPENSATION IS REQUIRED.
A FROM AN INTERFACED NAVIGATION SOURCE AS REQUIRED.
3 2 205203-8 CONNECTOR, 9 PIN - - - A
2 63 52133-03 TERMINATOR SHIELD, SOLDER SLEEVE - - -
30 AP100A22 WILL TERMINATE TO CONNECTOR P2 PINS
25 DELETED 25, 30, OR 31 IN ACCORDANCE WITH AIRCRAFT 1 2 35146-01 SWITCH, TOGGLE - - -
LIGHTING BUS VOLTAGE REQUIREMENTS. REFERENCE
FORM 86359 REV -

AIRCRAFT LIGHTING WIRING DIAGRAMS FOR CORRECT ITEM QTY PART NUMBER DESRIPTION VENDOR/SPEC ALTERNATE PART NOTES
26 DELETED NO.
VOLTAGE INPUT.
SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 2 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS
31 INTERFACE TO THE 01326 AUTOPILOT COMPUTER IS FOR REVISION HISTORY SEE SHEET 1
CONFIGURED BASED ON INSTALLED EQUIPMENT AS SHOWN ON
CONFIG DOCUMENT 87338.

32 IF ADDITIONAL AIR DATA SOURCE IS ADDED/INSTALLED,

REMOVE SPLICED CONNECTION FROM RX1A AND RX1B
D PINS 44 AND 45 OF CONNECTOR P2 AND REPLACE WITH D
STANDBY WIRING AS SHOWN ON SHEET 10.

33 DELETED

34 OPTIONAL INPUT FOR AIR DATA SOURCE ARINC LABEL 206

(INDICATED AIRSPEED) REQUIRED TO ENABLE IAS MODE AND
ENVELOPE PROTECTION FUNCTIONALITY.

35 OPTIONAL INPUT TO ADD ARINC LABEL 204 (BARO-CORRECTED

ALTITUDE) TO ENABLE ALTITUDE PRESELECT FUNCTIONALITY.
INPUT MUST ALSO PROVIDE ARINC LABELS 203, 206, 212 AND 320.

36 OPTIONAL INTERFACE TO THE EXISTING AIRCRAFT PROP DE-

ICE ON/OFF SWITCH TO PROVIDE AN ADDITIONAL LEVEL OF
UNDERSPEED THRESHOLD VALUE FOR FLIGHT-INTO-KNOWN-
ICING (FIKI) APPROVED AIRCRAFT. WITH THE DE-ICE SYSTEM
ON, THE UNDERSPEED THRESHOLD IS SET TO A HIGHER
VALUE THAN WITH THE DE-ICE SYSTEM OFF TO ACCOUNT FOR
C THE CHANGE IN STALL SPEED. REFER TO AFMS FOR C
UNDERSPEED VALUES.
P1.11 CAN BE JUMPERED TO GROUND TO PERMANENTLY
FORCE THE UNDERSPEED THRESHOLD TO THE LOWER VALUE.
NOTE THAT THE AUTOPILOT IS NOT APPROVED FOR FIKI IF
P1.11 IS GROUNDED.

37 28VDC/14VDC SUPPLIED WHEN PROP DE-ICE SYSTEM IS SWITCHED

ON AND OPERATING.

38 DO NOT INSTALL RESISTOR (ITEM 29), ON 14VDC SUPPLY.

B B

A A
FORM 86359 REV -

SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 3 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS
AUTOPILOT COMPUTER
P1 4 5 6 47X [REQUIRED] POWER, LIGHTING, CONTROL WHEEL, AUDIO AND MAINTENANCE
FOR REVISION HISTORY SEE SHEET 1
K2
A3 [OPTIONAL]
2X
36 ICEPRTCT 11 AP103C22 A2 A1 AP102D22
13 29 38
25 26 X2 AP102C22
D X1
19
13 3X D
AP POWER 28/14 VDC + 1 AP103B22
AP102B22 AP102B22 37 AP
18 MASTER SWITCH AUTOPILOT
K1 A3
AP DISC 10 AP103A22 A2 AP102A22 AP102A22 AP100A20 5 28VDC/14VDC BUS
A1 13 2X AP101A22
28 OR 25 12 2X
1 2X 18
X1 AP202A22
POWER GND 3 AP111A22N 26 AP202A22 AP200A20 5 28VDC/14VDC BUS
X2 AP110A22N DC
AP201A22 TRIM
MASTER SWITCH TRIM
P2 4 5 6 39X
18
28/14 VDC TRIM POWER IN 78 AP202B22

28 VDC 25 LP100A22
LIGHTING BUS 5 VDC 29 LP100A22 LP100A22 TO AIRCRAFT LIGHTING BUS 11X 7 9 10 8 11X PILOT'S CONTROL WHEEL
14 VDC 31 LP100A22
30 3
J157 P157
RD GY 2 UP L TRIM SW
AP201A22 14
C P1 2 4X
13 WH
BR 1
DN C
AP101A22
AP205A22N 1 BK 23 REF
CWS 38 WH WH 4 YL 3
BL AP314A22 AP314A22 BL 3 OR 2 UP
GND 31 R TRIM SW
52 BL BL 7 WH/RD BK DN
GND 1
AP315A22 AP315A22
GO AROUND 39 WH WH 6 VI
TRIM INTERUPT 36 AP204A22 AP204A22 15 GN NC 1 22 REF
GN 5
9 BL 21 RD
AP DISCONNECT IN 35 AP104A22 AP104A22 NO 3
WH WH 2 NC 4 AP/TRIM
PITCH MANUAL TRIM UP 18 BR REF BL DISCONNECT
AP316A22 AP316A22 2
PITCH MANUAL TRIM DN 19 BL BL 5 GY WH 6
NO
17 2X 17 2X
2 3X
AUDIO OUT + 8 WH 24 REF
AP155A22 TO AUDIO PANEL
AUDIO OUT - 9 BL 15 16 17 NO CWS
YL
OR
P2 24 REF
11 ON
WH MAINTENANCE NO
MAINT MODE 26 19 GO AROUND
AP159A22 SWITCH VI
GROUND 27 BL WH/RD (BLACK)
B OFF B
2 2X 15 16 3 7 2X

CAN BUS 1 + 62 WH 7 MAINTENANCE

AP157A22
CAN BUS 1 - 63 BL 2 CONNECTOR 19
SHIELD GROUND 77
EXTERNAL CAN BUS
P1 2 15 16 3 7 2X

CAN BUS 2 + 29 WH 7 MAINTENANCE

AP158A22 19
CAN BUS 2 - 30 BL 2 CONNECTOR
SHIELD GROUND 78
INTERNAL CAN BUS
18 14VDC ENABLE 75 AP320A22

P2
13 AP182A22 REF NAV 1 DISPLAY [OPTIONAL]
5 VDC OUT 14 17 REF FLAP COMPENSATOR 29
A A
17
P1
AP330A22 AP330A22 1
FORM 86359 REV -

FLAP POT WIPER 72 WH WH 2 20 REF

AP329A22 AP329A22
GND 73 BL BL 3
2 SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 4 OF 11
29
8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

[OPTIONAL] FOR REVISION HISTORY SEE SHEET 1

DUAL CONTROL WHEEL SWITCHING
PLT CTRL WHL
CO-PLT CTRL WHL
PILOT'S CONTROL WHEEL CO-PLT'S CONTROL WHEEL
7 9 10 8
11X 7 9 10 8 11X
D PITCH TRIM SW 11 REF REF REF 11 REF
PITCH TRIM SW D
2200S2 J158 P158 2200S3
P157 J157
UP 3 3 UP
2 2
L TRIM SW GY GY 9 TM310B22 TM320B22 9 GY GY L TRIM SW
1 1
DN DN
23 REF
UP 3 3 UP
2 2
R TRIM SW BR BR 5 TM312B22 TM322B22 5 BR BR R TRIM SW
1 1
DN DN
BK BK

AP/TRIM DISC SW
AP/TRIM DISC SW
2200S5
NC GN BK 3 WH WH 3 BK GN NC 22 REF
C GN 8 BL 1AP332A22 2AP332A22 BL 8 GN C
NO RD RD 4 OR OR 4 RD RD NO
C NC BL BL 11 WH WH 11 BL BL NC C
DISCONNECT
DISCONNECT C WH WH 7 BL 1AP333A22 2AP333A22 BL 7 WH WH C
NO YL 6 OR OR 6 YL NO
21 21
OR 2 WH WH 2 OR
CTRL WHEEL STEERING REF 2AP331A22 REF
VI 1 BL 1AP331A22 BL 1 VI
W/R 10 OR OR 10 W/R REF 24 CTRL WHEEL STEERING
YL
CWS OR YL
GO AROUND OR
2 3X CWS
2 3X REF 24 GO AROUND
VI
GA
W/R VI
11X 7 9 10 8 11X W/R GA

2 3X J159 P159
2 3X
15 CHASIS AUTOPILOT COMPUTER
2205K1
TRIM XFER RELAY 2AP333A22 BL P1
B 1AP333A22 WH B
25 26 2205XK1
A3 TM320B22 2AP331A22 OR 1 39 GO AROUND IN
OR AP315A22 52 GND
A2 TM331A22 1AP331A22 OR
28 A1 TM310B22 2AP331A22 BL 10
B3 TM322B22 1AP331A22 BL
B2 TM330A22 2AP331A22 WH 2 WH 31 GND
B1 TM312B22 1AP331A22 WH AP314A22
X1 C A 2AP333A22 OR 6 BL 38 CWS IN
27 D B 1AP333A22 OR
2205CR1 2AP333A22 WH 11 AP104A22 35 AP DISC IN
2AP332A22 WH
X2 TM307A20N DC
1AP332A22 WH 3 AP205A22N DC

LOC. BEHIND INSTR PANEL

1AP332A22 OR 4 RD AP201A22
2AP332A22 OR 8 WH AP204A22 36 TRIM INTERUPT
19 TRIM DOWN
TM331A22 9 BL
AP316A22 18 TRIM UP
A TM330A22 5 WH A
1AP333A22 BL 7 RD AP101A22
14
1AP332A22 BL
FORM 86359 REV -

2AP332A22 BL

TO AP MASTER SWITCH SHEET 4 AP101A22 SIZE CAGE CODE SWorks Drawing No.: REV

TO TRIM MASTER SWITCH SHEET 4 AP201A22 B NA 10245 J

SCALE: 1:1 DO NOT SCALE DRAWING SHEET 5 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS
ASPEN EFD 500/1000 (CONFIG 1_YD) FOR REVISION HISTORY SEE SHEET 1

AUTOPILOT COMPUTER [OPTIONAL] FLT DIRECTOR ANNUNCIATOR

13 REF 17 2X 17 REF 17 2X ST-670 ST-645
D P2 FLIGHT DIRECTOR 01180 01180-01 01188
D

FD LOGIC 18 AP180A22 AP180A22 12 12 20 FD LOGIC 17 31

[OPTIONAL] TO AP330A22 FLAP COMPENSATOR SEE SHEET 4 13
5 VDC OUT 14 AP182A22 AP182A22 14 7 13 5VDC SIGNAL REF

8 8 5VDC SIGNAL REF

ROLL STR SIGNAL 16 WH WH 7 14 14 ROLL STR SIGNAL

AP181A22 AP181A22
PITCH STR SIGNAL 17 BL BL 15 15 15 PITCH STR SIGNAL
2 2

P2
GPS_2 RX8A 70 WH
AP178A22 GPS 2
GPS_2 RX8B 71 BL
13 17 31
C GPS_1 RX7A 68 WH C
AP177A22 GPS 1
GPS_1 RX7B 69 BL

2 2X
GPS 2 ANNUNCIATOR
P2 13 31 REF 19

EFIS SEL 12 VDC OUT 20 AP324A22 AP324A22

GPS 1/2 SELECT SWITCH

REF 13
P1 GPS1

13 EFIS SELECT 58 AP325A22 AP325A22

GPS 2 13 31
AP179A22N
REF 18 INSTRUMENT PANEL

[OPTIONAL]
B AP COMPUTER B
P2 2 REF
AIR DATA SOURCE AIR DATA SOURCE
REF 2

ADC_1 RX2A 46 WH WH ARINC 429 TX A

AP151A22 AP151A22 34
ADC_1 RX2B 47 BL BL ARINC 429 TX B

AP COMPUTER 2 REF 2X ASPEN EFD 500/1000 INTERFACE 13 17 31

REF 2X 2
P2 P1 ASPEN EFD 500/1000

EFIS_1 RX5A 64 WH WH 26 ARINC 429 TX A

AP170A22 AP170A22
EFIS_1 RX5B 65 BL BL 27 ARINC 429 TX B
A A
EFIS_2 RX6A 66 WH
AP171A22 AP171A22
EFIS_2 RX6A 67 BL
13 2X
FORM 86359 REV -

SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 6 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

FOR REVISION HISTORY SEE SHEET 1

AP COMPUTER
P2 GARMIN GDU 620 INTERFACE GRS 77 GSU 75
2 4X
(POST GDU SOFTWARE 7.22) 17 31 (CONFIG 2_YD) P771 P751

AHRS_1 RX1A 44 WH WH 33 49 AHRS/ADAHRS 429 TX A

D AP150A22 AP150A22
19 50 AHRS/ADAHRS 429 TX B
D
AHRS_1 RX1B 45 BL BL
GDC 74 -
P741 -

ADC_1 RX2A 46 WH WH 44 3 ADC 429 TX A

AP151A22 AP151A22 ADC 429 TX B
ADC_1 RX2B 47 BL BL 45 23

P-6203 GDU 620 PFD

FLIGHT DIRECTOR_ TX1A 38 WH WH 4 ARINC 429 RX 7A
AP153A22 AP153A22
FLIGHT DIRECTOR_ TX1B 39 BL BL 26 ARINC 429 RX 7B

4X 2
EFIS_1 RX5A 64 WH WH 1 ARINC 429 TX 2A
AP152A22 AP152A22
EFIS_1 RX5B 65 BL BL 23 ARINC 429 TX 2B

C GARMIN TXi INTERFACE WITH J4 C

AP COMPUTER P2 TXI GDU 700/1060 PFD
2 4X REF INTEGRATED AHRS/ADC 17 31 (CONFIG 2_YD)
AHRS_1 RX1A 44 WH WH 54 AHRS 429 TX 2A
AP150A22 AP150A22
AHRS_1 RX1B 45 BL BL 74 AHRS 429 TX 2B

ADC_1 RX2A 46 WH WH 55 ADC 429 TX 3A

AP151A22 AP151A22
ADC_1 RX2B 47 BL BL 75 ADC 429 TX 3B

EFIS_1 RX5A 64 WH 53 ARINC 429 TX 1A

WH AP152A22 AP152A22
EFIS_1 RX5B 65 BL BL 73 ARINC 429 TX 1B
REF 4X 2
13 REF J3
FD LOGIC 18 AP180A22 AP180A22 57 FD ENABLE IN
ROLL STR SIGNAL 16 WH WH 20 FD ROLL RIGHT
AP181A22 AP181A22
BL
B PITCH STR SIGNAL 17 BL 42 FD PITCH UP B
5 VDC SIGNAL REF. 14 AP182A22 AP182A22 19 SIGNAL REF. (LEFT)
[OPTIONAL] TO AP330A22 FLAP COMPENSATOR SEE SHEET 4 REF 13 21 SIGNAL REF. (DWN)

GARMIN TXi WITH INDEPENDENT GRS 77 GRS 79 GSU 75

AP COMPUTER P2 2 4X REF
ADHRS/ADC OR ADAHRS INTERFACE 17 31 (CONFIG 2_YD) REF 2 P771 P791 P751

AHRS_1 RX1A 44 WH WH 33 27 49 AHRS/ADAHRS 429 TX A

AP150A22 AP150A22 19 7 50 AHRS/ADAHRS 429 TX B
AHRS_1 RX1B 45 BL BL
GDC 74 GDC 74 -
REF 2 P741 P741 -

ADC_1 RX2A 46 WH WH 44 44 3 ADC 429 TX A

AP151A22 AP151A22 45 45 23 ADC 429 TX B
ADC_1 RX2B 47 BL BL

J4 TXI GDU 700/1060 PFD

EFIS_1 RX5A 64 WH 53 ARINC 429 TX 1A
WH AP152A22 AP152A22
A EFIS_1 RX5B 65 BL BL 73 ARINC 429 TX 1B A
13 REF 2X REF 2 J3
FD LOGIC 18 AP180A22 AP180A22 57 FD ENABLE IN
ROLL STR SIGNAL 16 WH WH 20 FD ROLL RIGHT
AP181A22
FORM 86359 REV -

AP181A22
PITCH STR SIGNAL 17 BL BL 42 FD PITCH UP
5 VDC SIGNAL REF. 14 AP182A22 AP182A22 19 SIGNAL REF. (LEFT)
SIZE CAGE CODE SWorks Drawing No.: REV
[OPTIONAL] TO AP330A22 FLAP COMPENSATOR SEE SHEET 4 13 21 SIGNAL REF. (DWN)
B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 7 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

FOR REVISION HISTORY SEE SHEET 1

NON EFIS (CONFIG 3_YD)

KI-525A (REF)
2 6X
AUTOPILOT COMPUTER P2 6X 2

D b LAT DEV RIGHT D

LATERAL DEVIATION + (RT) 1 WH WH
AP163A22 AP163A22 LAT DEV LEFT
LATERAL DEVIATION - (LT) 2 BL BL V

LATERAL FLAG + 5 WH WH K NAV FLAG +

AP164A22 AP164A22
LATERAL FLAG - 6 BL BL F NAV FLAG -

HEADING + WH WH P HDG ERROR 31

40 AP165A22 AP165A22
HEADING - BL BL S HDG/CRS REF
41
27
COURSE - 43 BL BL
AP166A22 AP166A22
COURSE + 42 WH WH e CRS ERROR

VERTICAL FLAG - 8 BL BL W VERT FLAG -

AP161A22 AP161A22 13
VERTICAL FLAG + 7 WH WH J VERT FLAG +

VERTICAL DEVIATION DWN 3 WH WH B G/S DEV DWN

VERTICAL DEVIATION UP AP160A22 AP160A22 E G/S DEV UP
C 4 BL BL C

P1
28 HSI VALID 70 AP167A22 AP167A22 P HSI VALID

P2 2 2X REF
EFIS_1 RX5A 64 WH
AP183A22 TO NAV RECEIVER NO 1 31
EFIS_1 RX5B 65 BL

EFIS_2 RX6A 66 WH
AP184A22 TO NAV RECEIVER NO 2 31
EFIS_2 RX6B 67 BL

GPS_2 RX8A 70 WH GPS 2

AP178A22
GPS_2 RX8B 71 BL
13 17 31
GPS_1 RX7A 68 WH
GPS 1
B GPS_1 RX7B 69 BL
AP177A22 B
2 2X REF
P1
GPS ANNUNCIATE_1 74 AP317A22 GPS ANNUNCIATE NAV 1

APPROACH SELECT_1 AP318A22 ILS/GPS APPROACH NAV 1

37
13 24 31
GPS ANNUNCIATE_2 69 AP322A22 GPS ANNUNCIATE NAV 2

APPROACH SELECT_2 59 AP323A22 ILS/GPS APPROACH NAV 2

P2 [OPTIONAL] 19 GPS 2 ANNUNCIATOR

13 31
EFIS SEL 12 VDC OUT 20 AP324A22 AP324A22
GPS 1/2 SELECT SWITCH
P1 13
GPS1
13 EFIS SELECT 58 AP325A22 AP325A22

A AP179A22N 13 31 A
GPS 2
18 INSTRUMENT PANEL
[OPTIONAL] P3 SANDEL SN3500
P1 REF 13
FORM 86359 REV -

8 NAV 2 DISCRETE OUTPUT

13 EFIS SELECT 58 AP325A22
15 GPS 2 DISCRETE OUTPUT
SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 8 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

FOR REVISION HISTORY SEE SHEET 1

NON EFIS (CONFIG 4_YD)
CDI / GDI
2 4X REF
REF 4X 2
AUTOPILOT COMPUTER P2
D LATERAL DEVIATION + (RT) 1 WH WH LAT DEV RIGHT D
AP163A22 AP163A22
LATERAL DEVIATION - (LT) 2 BL BL LAT DEV LEFT

LATERAL FLAG + 5 WH WH NAV FLAG +

AP164A22 AP164A22
LATERAL FLAG - 6 BL BL NAV FLAG -

VERTICAL FLAG - 8 BL BL 31
AP161A22 VERT FLAG -
AP161A22
VERTICAL FLAG + 7 WH WH VERT FLAG +

VERTICAL DEVIATION DWN 3 WH WH G/S DEV DOWN

AP160A22 AP160A22
VERTICAL DEVIATION UP 4 BL BL G/S DEV UP

P1
28 HSI VALID 70 AP167A22 AP167A22 HSI VALID

2 2 X REF
C P2 C
EFIS_1 RX5A 64 WH
AP183A22 TO NAV RECEIVER NO 1 31
EFIS_1 RX5B 65 BL

EFIS_2 RX6A 66 WH
AP184A22 TO NAV RECEIVER NO 2 31
EFIS_2 RX6B 67 BL
03976 CONVERTER
P2
COURSE + 42 WH WH 13 COURSE +
HEADING + 40 BL AP165A22 AP165A22 BL 10 HEADING + 31
HEADING - 41 OR OR 11 5V REF OUT
COURSE - 43 13
GPS_2 RX8A 70 WH
AP178A22 GPS 2
GPS_2 RX8B 71 BL
13 17 31
GPS_1 RX7A 68 WH
GPS 1
B GPS_1 RX7B 69 BL
AP177A22 B
2 3X
P1
GPS ANNUNCIATE_1 74 AP317A22 GPS ANNUNCIATE NAV 1

APPROACH SELECT_1 AP318A22 ILS/GPS APPROACH NAV 1

37
13 24 31
GPS ANNUNCIATE_2 69 AP322A22 GPS ANNUNCIATE NAV 2

APPROACH SELECT_2 AP323A22 ILS/GPS APPROACH NAV 2

59
GPS 2 ANNUNCIATOR
P2 13 31 REF 19

EFIS SEL 12 VDC OUT 20 AP324A22 AP324A22

GPS 1/2 SELECT SWITCH
P1 REF 13
GPS1
13 EFIS SELECT 58 AP325A22 AP325A22

A AP179A22N 13 31 A
GPS 2
REF 18
INSTRUMENT PANEL
FORM 86359 REV -

SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 9 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS
NON EFIS (CONFIG 3_YD AND CONFIG 4_YD)
FLIGHT DIRECTOR, AIR DATA AND PRESELECT FOR REVISION HISTORY SEE SHEET 1

[OPTIONAL] FLT DIRECTOR ANNUNCIATOR

AUTOPILOT COMPUTER
P2
ANALOG FLIGHT DIRECTOR 17 2X ST-670 ST-645
13 REF 17 3X REF D
D 01180 01180-01 01188
18 AP180A22 AP180A22 12 12 20 FD LOGIC 17 31
FD LOGIC
[OPTIONAL] TO AP330A22 FLAP COMPENSATOR SEE SHEET 4 13

5 VDC OUT 14 AP182A22 AP182A22 14 7 13 5VDC SIGNAL REF

8 8 5VDC SIGNAL REF

ROLL STR SIGNAL 16 WH WH 7 14 14 ROLL STR SIGNAL

AP181A22 AP181A22
PITCH STR SIGNAL 17 BL BL 15 15 15 PITCH STR SIGNAL
2 2

P2 2 REF
[OPTIONAL] FLIGHT DIRECTOR
FLIGHT DIRECTOR_ TX1A 38 WH
DIGITAL FLIGHT DIRECTOR WH ARINC RX A
AP153A22 AP153A22 31
FLIGHT DIRECTOR_ TX1B 39 BL BL ARINC RX B
C C

[OPTIONAL]
P1 2 ST-360 ALTITUDE PRE-SELECTOR ALERTER
ALT ENGAGE 77 WH WH 10
AP172A22 AP172A22
VS COMMAND 71 BL BL 17 17 22 31

22 ST-360 ENABLE 57 AP321A22

B SANDIA ADC INTERFACE REF 2 B

2 REF 17 31
AP COMPUTER P2 (USED IN ANALOG INTERFACE ONLY) J100 SANDIA ADC SAC 7-35
32
ADC_1 RX2A 46 WH WH 8 ARINC 429 TX A
AP154A22 AP154A22
ADC_1 RX2B 47 BL BL 7 ARINC 429 TX B

ADC/AHRS_1 RX1A 44 20 GND

ADC/AHRS_1 RX1A 45 13 2X

[OPTIONAL]
AIR DATA SOURCE 17 31 35
2 REF 2 P1 AIR DATA SOURCE
AP COMPUTER REF
32
P2

A ADC/AHRS_1 RX1A 44 WH WH ARINC 429 TX A A

AP148A22 AP148A22 35
ADC/AHRS_1 RX1B 45 BL BL ARINC 429 TX B
FORM 86359 REV -

SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 10 OF 11

8 7 6 5 4 3 2 1
 8 7 6 5 4 3 2 1

REVISIONS

FOR REVISION HISTORY SEE SHEET 1

D D

AUTOPILOT COMPUTER 7 14 15 16 PITCH SERVO

2 2X
7X P1
P1
2X 2
MOTOR 2 21 WH WH 4 MOTOR 2
MOTOR 1 22 BL BL 3 MOTOR 1
23 OR AP136A22 AP136A22 1
SOLENOID OR SOLENOID PITCH
GND 24 GN GN 2 GND
PITCH SERVO SERVO
17 WH WH 8 TRIM SW A
TRIM SW DN 42 BL AP137A22 AP137A22
TRIM SW COM BL 7 TRIM SW COM
TRIM SW UP 16 OR OR 6 TRIM SW B
AP135A22N

7 14 15 16
C 2
4X
ROLL SERVO C
2 P1
J1
MOTOR 2 4 WH WH 4
MOTOR 1 5 BL MOTOR 2
AP140A22 AP140A22 BL 3 MOTOR 1 ROLL
ROLL SERVO SOLENOID 6 OR OR 1 SOLENOID SERVO
GND 7 GN GN 2 GND

AP141A22N

7 14 15 16
2 4X YAW SERVO
2 P1
J1
YAW MOTOR 2 25 WH WH 4 MOTOR 2
MOTOR 1 26 BL AP138A22 AP138A22 BL 3 MOTOR 1 YAW
SERVO SOLENOID 27 OR OR 1 SOLENOID SERVO
GND 28 GN GN 2 GND
B B
AP138A22N

7 14 15 16
4X
2 PITCH TRIM SERVO
P2 2 P1
J1
PITCH TRIM MOTOR 2 52 WH WH 4 MOTOR 2
MOTOR 1 53 BL AP139A22 AP139A22 BL 3 MOTOR 1 PITCH TRIM
SERVO SOLENOID 54 OR OR 1 SOLENOID SERVO
GND 55 GN GN 2 GND

AP139A22N

A A
FORM 86359 REV -

SIZE CAGE CODE SWorks Drawing No.: REV

B NA 10245 J
SCALE: 1:1 DO NOT SCALE DRAWING SHEET 11 OF 11

8 7 6 5 4 3 2 1