PDP Abnormal Procedures

A330/340 AFR-TR-334-B-BAP-2a-1503
PDP
ABNORMAL
PROCEDURES
LIVRET INSTRUCTEUR
& STAGIAIRE
PDP ABNORMAL PROCEDURES
ABNORMAL PROCEDURES
Rédacteur Hervé GALY

Vérificateur Thierry PIGAGLIO
Approbateur Stéphane LARROQUE
AFR-TR-334-B-BAP-2a-1503
DOCUMENT DESTINE A LA QT A334
PDP ABNORMAL PROCEDURES
ABNORMAL
PROCEDURES
USE OF
TUTORAL
Mise à jour
Rev 11
REV11
PDP ABNORMAL PROCEDURES 1/2
ECAM
MANAGEMENT
EMERGENCY ELEC EMER

SMOKE
DESCENT CONFIGURATION
G+B DUAL HYD REJECTED TO

SYS LO PRESS FAILURE G+Y EVACUATION
WINDSHEAR EGPWS TCAS
UNERELIABLE STALL TWO ENGINES ALL ENGINES

SPEED INDICATION RECOVERY INOP LANDING FLAME OUT
REV11
PDP ABNORMAL PROCEDURES 2/2
ECAM
MANAGEMENT
DUAL FM TOTAL LOSS LOW ENERGIE

FAULT FCU AURAL ALERT
FLAPS LOCKED SLATS FAULT

ELEV REDUN
DURING DURING FAULT
RETRACTION EXTENSION
EIS DUAL RADIO FLIGHT CREW

FUEL LEAK
FAILURE ALTI FAILURE INCAPACITATION
ENG FAILURE ENG FAILURE

ENG START ENG FAILURE
IN CRUISE IN CRUISE
FAULT AT TO
(STANDARD) (OBSTACLE)
REV11
Modifications done to the A330/A340 Family Procedure Data Package
REV 11
PDP Modification Done
USE OF PDP New presentation
FMGS preparation: ALL ENTERED DATA CHECKED by PNF
COCKPIT PREPARATION
added New IRS (RE) ALIGNEMENT conditions
BEFORE START - ENGINE START - AFTER START NIL
TAXI - BEFORE TAKEOFF Before TAKEOFF: note for EXT lights added
TAKE OFF NIL
CLIMB NIL
CRUISE NAV ACCURACY....CHECK revised
FMGS preparation: PROG page modified
FMGS preparation: QNH misinput risk (PSC 193)
Low OAT effect: revision
SET QNH modified by SET QNH___
DESCENT
APPROACH briefing upgraded
Passing 10 000 ft: NAV ACCUR... CHECK revised
SEAT BELTS....ON iso ON/AUTO
ALTITUDE CHECK: reference to FCOM added
SOPs revision
APPR p/b to be pressed on intercept trajectory for LOC in addition of
ILS APPROACH cleared for approach
PNF callouts at landing explained
ECAM WHEEL page explained (OEAP29)
GO AROUND High energy go around: minor corrections
GROUND SPEED MINI Minor corrections
VOR/NDB USING TRK/FPA SOPs revision
VOR/NDB USING FINAL APP SOPs revision
RNAV (GNSS) USING LNAV/VNAV MINIMUM SOPs revision - PDP fully revised
AFTER LANDING - PARKING - SECURING THE A/C SECURING the A/C C/L: Consider COLD weather added
FIRST FFS SESSION NIL
NORMAL LAW PROTECTIONS New overspeed procedures
Wind correction on downwind leg
PNF callouts at landing added PF
VISUAL PATTERN
callout: CHECKED added at 70kt
Some FMA added
TCAS NIL
USE OF FPV - ILS RAW DATA NIL
LOW ENERGY AURAL ALERT NIL
MMEL/MEL USE Minor corrections
MODE REVERSIONS NIL
EGPWS Minor corrections
FCU flow added
G/S FROM ABOVE
SELECT V/S MODE modified for V/S MODE: PULL AND SET
Corrections on PFD (Altitude, RA..)
WINDSHEAR
Note for W/S at takeoff (before V1) added
CIRCLING NIL
Minor corrections (e.g. Communicate)
ECAM MANAGEMENT
Computer reset to be crosschecked
VAPP computation slide removed
FLAPS LOCKED DURING RETRACTION
APPR synthesis: VAPP set in FINAL
VAPP computation slide removed
SLATS FAULT DURING EXTENSION
APPR synthesis: VAPP set in FINAL
ENGINE START FAULT Minor corrections
SMOKE NIL
APPROACH summary: Decelerate to VAPP in Final Approach
DUAL HYDRAULIC FAILURE G+B
added STATUS page revised
EMERGENCY DESCENT MSA replaced by MEA as per ECAM
EIS FAILURE SWITCHING NIL
ELECTRICAL EMERGENCY CONFIGURATION NIL
ELEVATOR REDUNDANCY LOST - MECHANICAL B/UPNIL
FUEL LEAK NIL
EO landing remark added (rudder reset)
ENGINE FAILURE AT TAKEOFF
TOGA limitation (5 min for FAA) removed
REV11 MAR 2014 A330/A340 FAMILY PDP

Modifications done to the A330/A340 Family Procedure Data Package
REV 11
and A/THR OFF is now part of FLY
ENGINE FAILURE IN CRUISE - STANDARD STRATEGYMCT
Performance check revised
and A/THR OFF is now part of FLY
ENGINE FAILURE IN CRUISE - OBSTACLE STRATEGYMCT
Performance check revised
DUAL FMGC FAILURE Minor corrections
RECONFIGURATION LAW Low energy warning modified for aural alert
New standard callout
Speed scale revised
STALL RECOVERY Resume flight path is now part ot recovery
New: Rely on STALL warning even if Normal law
Step FLAPS 1 modified
PFD: STD flashes when below TRANS
TOTAL LOSS OF FCU
ALT BARO 996 on PFD removed
ALL ENGINE FLAME OUT NIL
CREW INCAPACITATION Minor corrections
APPROACH summary revised
DUAL HYDRAULIC FAILURE G+Y
STATUS page revised
UNRELIABLE SPEED INDICATIONS Pitch/Thrust adjustment while climbing
Guard of EMER EVAC p/b is black
REJECTED TAKEOFF - EMERGENCY EVACUATION DECEL callout linked to PFD and not on AUTO BRK panel
ENG FIRE ON GROUND: new remark for A320
DUAL RADIO ALTIMETER FAILURE Flare law information added
A340: TWO ENGINES INOPERATIVE LANDING NIL
Cockpit preparation: FMGS: PNF: Check all entered
FLOW PATTERNS data Descent: FMGS preparation: PROG page modified
Approach briefing upgraded
LOW VISIBILTY OPERATIONS Revision
REV11 MAR 2014 A330/A340 FAMILY PDP

ECAM MANAGEMENT
PF PNF
DETECTION
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
SITUATION ASSESSMENT
DECISION
SYNTHESIS
REV 11
PF DETECTION PNF
First pilot who notices an ADVISORY:
ANNOUNCE………………………………..”ADVISORY ON “TITLE” system”
First pilot who notices MASTER WARNING / MASTER CAUTION:

MASTER WARNING / MASTER CAUTION……..………………….………RESET
ANNOUNCE……………………………….…...…..”TITLE OF FAILURE”
FLY THE AIRCRAFT
NAVIGATE
 CONSIDER AUTOMATION USE: A/THR, AP
 If failure at takeoff:
NO ACTION until 400ft AGL , with safe flight path established.

PF ECAM PROCEDURE PNF
PF SYSTEM DISPLAY PNF
If a SYSTEM page is displayed on the ECAM SD page:
SYSTEM PAGE DISPLAYED……….ANALYSE

REQUEST…………...CLEAR “name of SYS”?
CONFIRM………… CLEAR “name of SYS”
SYSTEM DISPLAY…………….………..CLEAR
This is to be repeated for each failure displayed on the ECAM SD page.

PF STATUS PNF
ANNOUNCE….…………….………………….”STATUS?”
ANNOUNCE……………….……………“STOP ECAM”
Or
CONFIRM………….…………………“READ STATUS” STATUS ……………………………………..…….. READ
• LIMITATIONS
• DEFERRED PROC
• INFOS
• INOP SYS
REQUEST………………………”REMOVE STATUS ?”
CONFIRM………………………….”REMOVE STATUS”
STATUS…………………………………………REMOVE
ANNOUNCE…………”ECAM ACTIONS COMPLETE”
Return to normal task sharing:
COMMUNICATE
 Review FCOM procedure if time permits:

Applying ECAM procedure ensures flight safety.
However, referring to FCOM, if time permits, may provide useful additional information.
When necessary:
STATUS……………….………….RECALL AND ANALYSE
 For complex procedures (Dual hydraulic failure or Electrical emergency configuration): Refer also to the QRH SUMMARY.
In case of failures affecting Flight control surfaces (inc. Slats and Flaps ), Landing gear or Landing gear doors:
INCREASED FUEL CONSUMP…………….. EVALUATE
Check weather reports and airfield data at any considered airports:
WEATHER AND LANDING INFORMATION.................OBTAIN
When requested by ECAM:
LANDING DISTANCE PROCEDURE …...…..….……APPLY
or:
LANDING PERFORMANCE…………CONFIRM
 Use the FMS for situation assessment:

• Estimation of the Landing Weight (LW)
• Determination of the nearest suitable airport
DECISION
Taking into account:
Limitations - Performance
Weather
Operational & Commercial

considerations
DECISION NOTIFY
ATC
PURSER / PAX
OPS …
SYNTHESIS
Review of OEBs during preliminary cockpit preparation
IN CASE OF FAILURE
FLY / NAV MONITOR
COM
ORDER ECAM ACTION ECAM ACTION/OEB
T (until STATUS page)
E
A CONSIDER:
M NORMAL C/L
COMPUTER RESETS
CONTINUE ECAM
(STATUS page)
ECAM ACTIONS COMPLETED

COM
SITUATION ASSESSMENT /FORDEC/ DECISION
APPROACH W
PREPARATION O
APPROACH R APPROACH C/L
BRIEFING K
ECAM DEFERRED PROC
(if any)
THE END...
PF DETECTION PNF
ANNOUNCE………………………………..”ADVISORY ON “TITLE” system”

ADVISORY
First pilot who notices MASTER WARNING / MASTER CAUTION:

PF PNF
MASTER WARNING / MASTER CAUTION……..………………….………RESET
ANNOUNCE……………………………….…...…..”TITLE OF FAILURE”
SYSTEM PAGE DISPLAYED………...……….…....ANALYSE
PF
 If failure at takeoff: ECAM ADVISORY CONDITIONS……..………..……..CHECK
COMMUNICATE QRH
FLY THE AIRCRAFT
CONSIDER AUTOMATION USE: A/THR, AP
NAVIGATE
 CONSIDER AUTOMATION USE: A/THR, AP
 If failure at takeoff:
NO ACTION until 400ft AGL , with safe flight path established.

If the aircraft is not equipped with the OEB reminder function ( for more information, refer to FCOM-OEB and FCOM-DSC-31-27),
the flight crew should apply any OEB reviewed during the preliminary cockpit preparation instead of performing the ECAM actions.
COMMUNICATE ECAM……..CONFIRM using SD page and OVHD panel

ORDER………………………….…”ECAM ACTIONS”
ECAM ACTIONS / OEB…………...………PERFORM

REQUEST……………………CLEAR “name of SYS”?
ECAM ACTIONS COMPLETE……………..….CHECK
CONFIRM…………….….….. CLEAR “name of SYS”
ECAM……………………….……………………..CLEAR
This is to be repeated for each failure displayed on the EWD:
“ECAM
As he announces “ECAM ACTIONS”,
ACTIONS” Depending on the failure, LAND ASAP,the
orPF
LAND ASAP,of communications,
is in charge
until all the ECAM actions have been
may be displayed, in the right column
PF ofcompleted.
the ECAM procedure.
COMMUNICATE
“CLEAR RED LAND ASAP Land at the next suitable airport.
HYDRAULIC”
AMBER LAND ASAPActions

Assesstothe
be seriousness
confirmed byof both pilots: and
the situation
consider the selection of a suitable airport.

PF STATUS PNF
ANNOUNCE….…………….………………….. STATUS?
ANNOUNCE……………….…………… STOP ECAM
Or
CONFIRM………….………………… READ STATUS STATUS ……………………………………..…….. READ
• LIMITATIONS
The PNF should not start reading the STATUS before confirmation from the PF.
• DEFERRED PROC
For any priority reason, STATUS analysis can be postponed by PF. • INFOS
• INOP SYS
Before reading the STATUS, specific actions must be considered:
REQUEST…………………………REMOVE STATUS ?
 NORMAL C/L
CONFIRM……………………………REMOVE STATUS
 Computer resets (Refer to QRH)
STATUS…………………………………………REMOVE
ANNOUNCE……………ECAM ACTIONS COMPLETE

When the actions are completed, PF must call out: “CONTINUE ECAM”.
RETURN TO NORMAL TASK SHARING
COMMUNICATE
 Review FCOM procedure if time permits:

Applying ECAM procedure ensures flight safety.
However, referring to FCOM, if time permits, may provide useful additional information.
If the aircraft is not equipped with the OEB reminder function ( for more information, refer to FCOM-OEB and FCOM-DSC-31-27),
the flight crew should apply any OEB reviewed during the preliminary cockpit preparation instead of performing the ECAM actions.
COMMUNICATE ECAM……..CONFIRM using SD page and OVHD panel

ORDER………………………….…”ECAM ACTIONS”
ECAM ACTIONS / OEB…………...………PERFORM

When ECAM actions request:
REQUEST……………………CLEAR “name of SYS”?
ECAM ACTIONS COMPLETE……………..….CHECK
“X” PROC …..…. APPLY
CONFIRM…………….….….. CLEAR “name of SYS”
ECAM……………………….……………………..CLEAR
Stop ECAM actions, refer to the QRH, and perform the related paper
procedure. This procedure will mention when to come back on the ECAM.
This is to be repeated for each failure displayed on the EWD:
“ECAM
As he announces “ECAM ACTIONS”,
ACTIONS”
the PF is in charge of communications,
until all the ECAM actions have been
PF completed.
COMMUNICATE
“CLEAR
HYDRAULIC”
Actions to be confirmed by both pilots:
STATUS page
Limitations
Deferred PROC
INOP systems
corrections to apply for landing
Infos
When the STATUS page mentions:

“X” PROC . . . . . . APPLY
or
INCREASED FUEL CONSUMP
… continue reading all the STATUS page, and when ECAM actions are
completed, refer to the QRH, and perform the related or appropriate procedure.
INCREASED FUEL CONSUMP…. EVALUATE
 Refer to the QRH FPE-FPF.
 For more, review the Performance course: FUEL PENALTY FACTOR module:
• FMS TRIP FUEL= FOB – FMS EFOB at DEST
• If only one Fuel Penalty Factor (FPF) is applicable:

TRIP FUEL PENALTY = FMS TRIP FUEL x FPF
• If two or more Fuel Penalty Factor (FPF) are applicable:

TRIP FUEL PENALTY = FMS TRIP FUEL x (FPF1 + FPF2 + …)
• The flight crew must manually calculate the Fuel Predictions to

take into account the Trip Fuel Penalty :
ACTUAL TRIP FUEL= FMS TRIP FUEL+ TRIP FUEL PENALTY
LDG DIST PROCEDURE …..…APPLY
 Refer to QRH FPE-IFL.
 For more information , review the Performance course: APPROACH AND LANDING module:
LANDING PERFORMANCE......CONFIRM
 A diversion or other event could lead to a landing performance confirmation, especially

when the fuel consumption is affected.
Estimation of the Landing Weight (LW)
 Provided the F-PLN page is completed (including ARRIVAL page, without any F-PLN DISCONTINUITY, etc…),
use the EFOB at DEST to calculate the LW.
 Consider any fuel consumption increment. (refer to QRH FPE-FPF).
 The LW is the entry point of the VAPP Determination and In-Flight Landing Distance tables (refer to QRH FPE-
VAPP and FPE-IFL).
 EFOB is displayed on the F-PLN page and on the FUEL PRED page.
Determination of the nearest suitable airport
 Use the CLOSEST AIRPORTS page. This page displays the four nearest airports,
sorted according to their distance.
 BRG, DIST, ETA and EFOB (second page) are provided for each airport.
 A fifth airport can be manually inserted.

LAST CHANGE
01 JUL 2012 ECAM PROCEDURE UPDATED

SITUATION ASSESSMENT UPDATED IAW IFLD
REV10
EMERGENCY DESCENT
DECOMPRESSION
or
PRESSURIZATION LOST
INTRODUCTION
DESCENT / TARGET ADJUSTMENTS ECAM ACTIONS
REACHING
FL100 / MEA or MORA
1st Loop 2nd Loop
ACTION FLOW
• Structural damage
• No structural damage
FL100 /
MEA or MORA
REV 11
PF DECOMPRESSION PNF
DETECTION
ANNOUNCE (INT) ......…...”EMERGENCY DESCENT”
CREW OXY MASK……….………..………….ON
ANNOUNCE (PA) ......….”ACCORDANCE WITH THE MSS” SIGNS……………………………………...……ON
INTERPHONE………………………………….ON
INTERPHONE VOLUME…..………………….ON
COMMUNICATION………………....ESTABLISH
 Use the headsets
 Interphone setting:
 When communication is established, avoid the continuous

use of the interphone to minimize the noise of the O2 masks
PF DESCENT PNF
1st loop
1. ALT……………………..…………….…TURN then PULL 1. ENG MODE SEL……………………………………..IGN
2. HDG……………………………TURN off airway & PULL 2. ATC…………………………………………….….NOTIFY
3. SPEED……………….………………………………..PULL 3. ATC XPDR…………………………………...CONSIDER
FMA
if Cab Alt > 14000 ft :

4. SPD BRK……………………………………………..FULL 4. PAX OXY Masks……………………………….MAN ON
PF TARGET ADJUSTMENTS PNF
2nd loop
ALT FL 100 or MORA or MSA…….……………....SET

HDG……………………………………….………...…SET
STRUCTURAL DAMAGE ?
YES, or suspected :
Loud bang, high NO
cabin v/s, air flow
SPD/MACH p/b…..PRESS VMO/MMO...…….SET
FMA
MORA is displayed if :
 CSTR selected
 range > 40 nm 150
PF ECAM ACTIONS PNF
ECAM ACTIONS
ECAM PROCEDURE
PF
SYSTEM DISPLAY
COMMUNICATE
STATUS
SITUATION ASSESSMENT STATUS, or

SUMMARY WEATHER
WEATHER
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
DECISION
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
Review FCOM procedure (If time permits)
QRH
 If ECAM warning
QRH MISCELLANEOUS
 If No ECAM warning
. EMER DESCENT
REACHING
PF FL100 / MEA or MORA PNF
When ALT* engages :
SPD BRK………………………………...………..…..RETRACT
SPEED…………………………………...……………..MANAGE
 For further descent :
V/S = - 1000ft/min 10
MAX
 Reminder: when CABIN PRESSURE is controlled manually, the V/S target is - 300 ft/min to
ensure passengers comfort.
……………..
THE END...
PF DECOMPRESSION PNF
DETECTION
ANNOUNCE (INT) ......…...”EMERGENCY DESCENT”
CREW OXY MASK……….………..………….ON
ANNOUNCE
ANNOUNCE (PA)
(PA) ......…....”EMERGENCY
.......”ACCORDANCE WITHDESCENT”
THE MSS” SIGNS……………………………………...……ON
INTERPHONE………………………………….ON
Inform the cabin crew of emergency descent on the PA system.
Turn on theINTERPHONE VOLUME…..………………….ON
SEAT BELTS lights before initiating the emergency descent.
COMMUNICATION………………....ESTABLISH
 Use the headsets
 Interphone and interphone volume….ON
 When communication is established, avoid the continuous

use of the interphone to minimize the noise of the O2 masks
PF DESCENT PNF
1st loop
2. ATC…………………………………………….….NOTIFY
Action on the altitude knob is TURN, then PULL .
If you PULL first, then TURN the altitude knob, 3. ATC XPDR…………………………………...CONSIDER
the aircraft will not descent.
FMA

PF DESCENT PNF
1st loop
 MAYDAY, MAYDAY, MAYDAY on current frequency. If no

FMA
contact with ATC, use the frequencies: (VHF) 121.5 MHz, or (HF)
2182 kHz or 8364 kHz.
 Squawk 7700 unless otherwise specified by ATC.

PF DESCENT PNF
1st loop
FMA
Reading FMA, you will confirm that the descent is engaged.

Delayed descent leads to limited oxygen for passengers, increasing hypoxia risk.

PF DESCENT PNF
1st loop
FMA

4. SPD BRK……………………………………………..FULL 4.
3. PAX OXY Masks……………………………….MAN ON
Contact the cabin crew to confirm that the passengers oxygen masks are released.
PF TARGET ADJUSTMENTS PNF
2nd loop
ALT FL 100 or MORA..……….…….……………....SET

HDG……………………………………….………...…SET
STRUCTURAL DAMAGE ?
YES, or suspected :
Loud bang, high NO
cabin v/s, air flow
SPD/MACH pb…..PRESS
p/b…..PRESS MMO...……..……SET
When in MACH target, pressing the SPD/MACH p/b will revert to SPD target, allowing IAS to be maintained.
FMA
MORA is displayed if :
 CSTR selected
 range > 40 nm 150
ACTION FLOW :
NO STRUCTURAL DAMAGE
PAX OXY
SPD
3 2 1 MASKS 4
HDG
ALT
4
FMA
1st loop “MAYDAY

ATC MAYDAY
MAYDAY”
2
SPD
BRK 5 3
ENG MODE 1 ATC XPDR
SEL
No Damage
Set speed target to

VMO/MMO 2nd loop
SPD
ALT
HDG
3 2 1
ACTION FLOW :
STRUCTURAL DAMAGE
SPD
3 2 1
HDG PAX OXY
ALT MASKS 4
4
FMA
1st loop
“MAYDAY
ATC MAYDAY
MAYDAY”
2
SPD
BRK 5
3
ENG MODE 1 ATC XPDR
SEL
Damage suspected
Maintain current IAS by 2nd loop
pressing SPD/MACH pb
SPD/MACH
3
1
2
LAST CHANGE
01 JULY 2012 USE OF INTERPHONE ENHANCED
REV10
ELEC EMER CONFIG
A330 A340-300
REV 11
A330 ELEC EMER CONFIG
APPROACH
ELEC EMER CONFIG APPROACH LANDING
PREPARATION
Approach Synthesis
LOSS OF ALL AC BUSES
ELEC EMER CONFIG
LAND ASAP
CONFIGURATION
FINAL APPR
LANDING GEAR
EXTENSION
REV10
LANDING & DECELERATION
A340-300 ELEC EMER CONFIG
APPROACH
PREPARATION
Approach Synthesis
ELEC EMER CONFIG
LAND ASAP
CONFIGURATION
FINAL APPR
LANDING GEAR
EXTENSION
REV10
A340-600 ELEC EMER CONFIG
APPROACH
PREPARATION
Approach Synthesis
ELEC EMER CONFIG
LAND ASAP
CONFIGURATION
FINAL APPR
LANDING GEAR
EXTENSION
REV10
PF ELEC EMER CONFIG PNF
DETECTION
CM1 CM2
FLY THE AIRCRAFT  LOSS OF AP and A/THR (THRUST LOCKED)
CONSIDER AUTOMATION USE
NAVIGATE  LAND ASAP…Short term decision
PF ECAM ACTIONS
COMMUNICATE
MAYDAY
ECAM PROCEDURE GE :
SYSTEM DISPLAY
STATUS
SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
DETECTION
CM1 CM2
PF ECAM ACTIONS
COMMUNICATE
MAYDAY
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
DETECTION
CM1 CM2
PF ECAM ACTIONS
COMMUNICATE
MAYDAY
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
PF APPROACH PREPARATION PNF
ECAM STATUS………………………….…….....REVIEW
SUMMARY…………..………………….…………..….USE
FMGS…………………………………….…..….PREPARE
Done upon PF request

using MCDU1
STANDARD
+
MANUAL INSERTION OF VAPP
APPR BRIEFING ............………………...…..PERFORM
APPROACH BRIEFING : STANDARD + STATUS + SUMMARY

SUMMARY…………..………………….…………..….USE
FMGS…………………………………….…..….PREPARE
Done upon PF request MCDU MENU:

using MCDU1 NAV BACK-UP MODE FOR FLIGHT PLANNING ONLY.

SUMMARY…………..………………….…………..….USE
FMGS…………………………………….…..….PREPARE
Done upon PF request MCDU MENU:

using MCDU1 NAV BACK-UP MODE FOR FLIGHT PLANNING ONLY.

PF APPROACH PNF
For slats extension :
LAND RECOVERY……………………………………..…..ON SUMMARY…………………………………….USE
FLY THE AIRCRAFT  LOSS OF AP/FD

NAVIGATE  USE RAW DATA
The Land recovery p/b:
 Removes non necessary loads (AP1, remaining fuel pump, ADR3)

 Restores equipment required for landing (SFCC 1, LGCIU 1, BSCU 1, WHC1, L LDG lights)
When L/G down : F/CTL DIRECT LAW
FLY THE AIRCRAFT  USE MAN PITCH TRIM
ECAM ACTIONS
PF APPROACH PNF

 Removes non necessary loads (Remaining fuel pump)

 Restores equipment required for landing (SFCC 1, LGCIU 1)
ECAM ACTIONS
PF APPROACH PNF


ECAM ACTIONS
PF LANDING PNF
FLY THE AIRCRAFT  NO AP, NO FD, NO A/THR, DIRECT LAW
USE MAN PITCH TRIM
 No Auto callouts (no RA avail)
 No REVERSER
 No NWS, no L/G retraction (L/G GRAVITY EXTENSION)
 Only 3 SPOILERS per wing
 NORMAL brake with ANTISKID

PF LANDING PNF
USE MAN PITCH TRIM
 No REVERSER
 ALTERNATE brake, NO ANTISKID
 MAX BRK PR: 1000 PSI (Monitored by PNF)

PF LANDING PNF
USE MAN PITCH TRIM
 No REVERSER
 ALTERNATE brake, NO ANTISKID
 MAX BRK PR: 1000 PSI ( Automatically limited, however monitored by PNF)
……………..
THE END...
ELEC EMER CONFIG
Electrical Emergency Configuration = Loss of all AC buses
It may be caused by:

 the loss of all AC bus bars, or
 the loss of all engines, or
 the loss of all generators, or
 combination of different failures.
Note: In case of simultaneous loss of all GEN, suspect a short-circuit: the probability of a
successful APU GEN coupling is low.
Remaining equipments depend on Green HYD pressure availability.

The Green HYD can pressurized either:
 by ENG driven pumps (all GEN failure ), or
 by RAT driven pump (all ENG failure).
As a consequence, EMER GEN can supply:

 high power (more equipment ETOPS REQ)
 low power (supplied by RAT and speed below 260knots, minimum equipment ).
Note: In this presentation, the Green HYD system, which is driving the EMER GEN, is
powered by the Engine Driven Pump.
ELECELEC
EMER CONFIG
EMER CONFIG



ELECELEC
EMER CONFIG
EMER CONFIG



FLY THE AIRCRAFT  LOSS OF AP andA330 A/THR
DETECTION
 AP1, FD1 can be re-engaged after the failure occurred
Single Chime
(every 5 sec)
•••
 THR LK: Read N1, then move the thrust levers (O) accordingly
FLY THE AIRCRAFT  LOSS OF AP, A/THR PF

SYSTEMS REMAINING (Refer to QRH)
NAVIGATE  LAND ASAP…Short term decision COMMUNICATE
CM1  PF
CONSIDERFLT CTL: ALTN USE
AUTOMATION LAW until
(for L/G AP1/FD1
A330 down are available, and can be re-engaged) MAYDAY
FLT INS: PFD1, ND1, ECAM Upper DU, ISIS
A340
ENG: THR in manual control, FADEC, ENG A.ICE, L FUEL PUMP 2 and XFEED (auto open)
A340
ECAM ACTIONS
ECAM PROCEDURE A330
RR & PW
USE OF
SYSTEM SUMMARY
DISPLAY :
GE
:
STATUS
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
FLY THE AIRCRAFT  LOSS OF AP andA330
A/THR
DETECTION
 Remove FD flag ( FDs…..OFF)
 Use the bird (FPV) (TRK/FPA….SELECT)
Single Chime
(every 5 sec)
•••
NAVIGATE  LANDASAP…Short
THR LK: Read then move the thrust levers (O) accordingly
N1,decision
term COMMUNICATE
CONSIDER AUTOMATION
SYSTEMS USE(Refer
REMAINING (for A330 AP1/FD1 are available, and can be re-engaged)
to QRH) MAYDAY
A340 CM1  PF
FLT CTL: ALTN LAW until L/G down
FLT INS: PFD1, ECAM Upper DU, ISIS
ENG: THR in manual control, FADEC, ENG A.ICE, FUEL PUMP 1 and all XFEED (auto open) A340
USE OF SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
FLY THE AIRCRAFT  LOSS OF AP andA330
A/THR
DETECTION
 Remove FD flag (FDs…..OFF)
 Use the bird (FPV) (TRK/FPA…..SELECT)
Single Chime
(every 5 sec)
NAVIGATE  LANDASAP…Short
THR LK: Read or EPR, then move the thrust levers (O) accordingly
N1 decision
term
•••
COMMUNICATE
CONSIDER AUTOMATION
A340 USE (for A330AP1/FD1 arePF
CM1 available, and can be re-engaged) MAYDAY
FLT CTL: ALTN LAW until L/G down

FLT INS: PFD1, ECAM Upper DU, ISIS
A340
ENG: THR in manual control, FADEC, ENG A.ICE, FUEL MAIN 2 and all XFEED (auto open)
USE OF SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
A330
DETECTION
AUTO FLT: FMGC1, MCDU1

CM1  PF
NAV: ADR1+3, IR1+3, VOR1 or ADF1 (only one at a time), DME1, ILS1, DDRMI, RDR1 PF
FLY THE AIRCRAFT  LOSS OF AP, A/THR
AIR COND/PRESS/VENT: CPC1 and PACKS
NAVIGATE  LAND ASAP…Short term decision A340 COMMUNICATE
PNEU: BMC1 and X BLEED man only
CONSIDER AUTOMATION USE (for A330 AP1/FD1 are available, and can be re-engaged) MAYDAY
ETOPS: Windshield Heat, Pitot Heat, Wing Anti Ice, BSCU1 (and so, Anti Skid)
Oxygen
A340
USE OF SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
A330
DETECTION
AUTO FLT: MCDU1 with NAV B/UP

CM1  PF
NAV: ADR1 or 3, IR1+3, VOR1 or ADF1 (only one at a time), DME1, ILS1, DDRMI PF
PNEU: BMC1+4 and X BLEED man only
Oxygen
A340
USE OF SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
A330
DETECTION
AUTO FLT: MCDU1 with NAV B/UP

CM1  PF
NAV: ADR1 or 3, IR1+3, VOR1 or ADF1 (only one at a time), DME1, ILS1, DDRMI PF
PNEU: BMC1+4 and X BLEED man only
Oxygen
A340
USE OF SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
COMMUNICATE
A330
DETECTION
COM: RMP1, ACP1+2, VHF1, HF1, ATC1

CM1  PF

USE OF SUMMARY
ELEC EMER CONFIG
COMMUNICATE
A330
DETECTION
COM: RMP1, ACP1+2, VHF1, ATC1

CM1  PF

ELEC EMER CONFIG
COMMUNICATE
A330
DETECTION
COM: RMP1, ACP1+2, VHF1, ATC1

CM1  PF
NAVIGATE  LAND ASAP…Short term decision COMMUNICATE

ELEC EMER CONFIG
PF ECAM PROCEDURE A330 RR & PW PNF
DETECTION
ECAM: FWC1, SDAC1, ECP
CM1  PF
A330 A340
A340
MONITOR FUEL FEEDING
Fuel is fed from one side only

ECAM ACTIONS
(L PUMP 2 or R PUMP 2, if L PUMP 2 inop)
ECAM PROCEDURE FUEL
page
SYSTEM DISPLAY
THRUST CONTROL
STATUS
Overhead EPR mode
panel (normal situation)
USE SUMMARY…………..….……..CRUISE part
SUMMARY
RR &A330
STATUS, or
WEATHER
WEATHER
DECISION PW :
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
COMMERCIAL
AND
COMMERCIAL
GE
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
The N1 DEGRADED MODE is an N1 UNRATED MODE. :

NOTIFY
NOTIFY OPS
OPS …
…
Refer to FCOM PER-THR –N1: N1 MODE THRUST CONTROL:

Power management control tables
ELEC EMER CONFIG
PF ECAM PROCEDURE A330 GE PNF
DETECTION
ECAM: FWC1, SDAC1,

ECP
CM1 PF
A330 A340 A340
ECAM ACTIONS
ECAM PROCEDURE
Fuel is fed from one side only: SYSTEM DISPLAY
L PUMP 2, or R PUMP 2, if L PUMP 2STATUSis
inoperative, or set to OFF for fuel balancing. FUEL
page
USE SUMMARY…………..….……..CRUISE part
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
COMMERCIAL
AND
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ELEC EMER CONFIG
DETECTION
CM1 
PF
A340
A340
ECAM ACTIONS
Monitor
ECAM PROCEDURE
SYSTEM DISPLAY
Fuel is fed from one side only: FUEL
STATUS USE SUMMARY…………..….……..CRUISE part
PUMP 1, or STBY PUMP 4, if PUMP 1 is page
inoperative, or set to OFF for fuel balancing.
FLT CTL STATUS, or

GE :
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DECISION
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
The rudder trim remains operative, but position indicator is lost on center pedestal
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ELEC EMER CONFIG
ECAM PROCEDURE PNF
SYSTEMS REMAINING (Refer to QRH) DETECTION
CM1  PF
A340
ECAM ACTIONSMonitor
ECAM PROCEDURE
SYSTEM DISPLAY FUEL
Fuel is fed from one side only:
MAIN PUMP 2, or MAIN PUMP 3, if MAIN PUMP page
2 SUMMARY…………..….……..CRUISE
STATUS USE part
is inoperative, or set to OFF for fuel balancing.
FLT CTL
The rudder trim remains operative, but position indicator is lost on center pedestal
THRUST CONTROL
The N1 DEGRADED MODE is an N1 UNRATED MODE.
Refer to FCOM PER-THR-N1: N1 MODE THRUST CONTROL:
Power management control tables
SYSTEM DISPLAY
Only EWD available :
If needed, analyse SYSTEM page displayed on the upper ECAM screen:
OTHER SYSTEM PAGES
FUEL FUEL key on ECP……………...…PRESS and HOLD

PAGE DISPLAYED.…………….……..…....ANALYSE
REQUEST…………………………..”CLEAR FUEL ?”
CONFIRM……………………….…...”CLEAR FUEL”
FUEL key on ECP..…….……….………...RELEASE
SYSTEM DISPLAY
OTHER SYSTEM PAGES

SYSTEM DISPLAY
OTHER SYSTEM PAGES

STATUS
To display the STATUS page :
ANNOUNCE………………………..……..…..……”STATUS ?”
CONFIRM………………………….…………”READ STATUS” STATUS key on ECP…………….……….PRESS and HOLD
STATUS overflow :
… release the STATUS key on ECP and push it again within

2 sec to display the next STATUS page
Observe the ECAM MEMO:
Review FCOM procedure (If time permits)

Important note regarding
speed indication reliability
STATUS
ANNOUNCE………………………..……..…..……”STATUS ?”


STATUS
ANNOUNCE………………………..……..…..……”STATUS ?”


SITUATION ASSESSMENT USING SUMMARY
The summaries consist of QRH procedures.

They have been created to help the flight crew to handle the actions in the event of multiple failures.
The ECAM should be applied first (procedure and STATUS page review).
The CRUISE section highlights:

SUMMARY - the remaining systems,
- the main limitations,
3 CRUISE - the flight capability of the
ECAM aircraft.
1
ACTIONS
APPROACH
This section may help you to
LANDING assess the situation and to
2 STATUS choose an appropriate landing
runway.
GO AROUND
Refer, in the meantime, to the

QRH for :
- the evaluation of an increased
4 QRH: FPE
fuel consumption (FPE-FPF)
- the VAPP computation at the
selected airport (FPE-IFL),
5 DECISION - the In-Flight Landing Distance
computation (FPE-IFL).


ECAM aircraft.
1
ACTIONS
APPROACH
runway.
GO AROUND

QRH for :
4 QRH: FPE


ECAM aircraft.
1
ACTIONS
APPROACH
runway.
GO AROUND

QRH for :
4 QRH: FPE
APPROACH PREPARATION USING SUMMARY
SUMMARY
As always, the approach
CRUISE preparation begins by the review
ECAM of the STATUS page.
ACTIONS
APPROACH
Then, the sections APPROACH,

7 LANDING LANDING and GO AROUND
STATUS
may be used to prepare the
approach.
6 GO AROUND
When appropriate, these sections

may include, among others, the
LANDING WITH SLATS or
8 FMGS PREPARATION
FLAPS JAMMED procedure
and/or the L/G GRAVITY
EXTENSION procedure.
SUMMARY
ACTIONS
APPROACH

STATUS
approach.
6 GO AROUND

8 FMGS PREPARATION
SUMMARY
ACTIONS
APPROACH

STATUS
approach.
6 GO AROUND

8 FMGS PREPARATION
APPROACH BRIEFING USING SUMMARY
SUMMARY
CRUISE
ECAM
ACTIONS The sections APPROACH,
APPROACH
LANDING and GO AROUND
should be used to conduct the
STATUS
LANDING approach briefing, cross-
checking, as usual, the
9
10 associated FMS pages.
GO AROUND
A final review of the STATUS

FMGS pages review page is always necessary.
SUMMARY
CRUISE
ECAM
APPROACH
STATUS
9
GO AROUND

SUMMARY
CRUISE
ECAM
APPROACH
STATUS
9
GO AROUND

APPROACH USING SUMMARY
SUMMARY The APPR PROC of the STATUS

page should be performed by
reading the APPROACH section
CRUISE
ECAM of the summary (PNF), avoiding
ACTIONS to refer to others paper
11 APPROACH procedures.
Before the final approach, the

LANDING
STATUS PNF should review the STATUS
page and check that all the
12 GO AROUND APPR PROC have been
completed.
The LANDING and the GO

AROUND sections may be then
shortly commented (braking,
NWS, reversers and L/G
retraction in case of go-around).

CRUISE

LANDING
completed.


CRUISE

LANDING
completed.

PF APPROACH PNF



The Land
Use the recovery (TRK/FPA…..SELECT)
p/b:
bird (FPV)
 When in CONF2, L/G not downlocked warning (no RA avail).
Stops when L/G is DN.

ECAM ACTIONS
PF APPROACH PNF



The Land
Use the recovery (TRK/FPA…..SELECT)
p/b:
bird (FPV)
 When in CONF2, L/G not downlocked warning (no RA avail).
Stops when L/G is DN.

ECAM ACTIONS
PF APPROACH PNF

LAND RECOVERY……………………………………..…..ON
When in CONF2, L/G not downlocked warning (no RA avail).

Stops when
The Land L/G is DN.
recovery p/b:

ECAM ACTIONS
PF APPROACH PNF

LAND RECOVERY……………………………………..…..ON
When in CONF2, L/G not downlocked warning (no RA avail).

Stops when
The Land L/G is DN.
recovery p/b:

ECAM ACTIONS
APPROACH SYNTHESIS
ALTERNATE LAW
Approach flown manually

with raw data : no AP CONF 1
FD
A/THR CONF 2
LANDING GEAR GRAVITY

CONF 3 EXTENSION
GO AROUND FINAL APPR
 NO GEAR RETRACTION  NO AUTO CALLOUTS
 DIRECT LAW
 USE MAN PITCH TRIM

BE AWARE OF :
 NO REVERSER
 NO NWS
 NO AUTO BRK
 PARTIAL LOSS OF GRND SPOILERS
APPROACH SYNTHESIS
ALTERNATE LAW

FD
A/THR CONF 2

CONF 3 EXTENSION
NO GEAR RETRACTION NO AUTO CALLOUTS
 DIRECT LAW

BE AWARE OF :
NO REVERSER
NO NWS
NO AUTO BRK
PARTIAL LOSS OF GRND SPOILERS
NO ANTI SKID (1000 PSI MAX)
APPROACH SYNTHESIS
ALTERNATE LAW

FD
A/THR CONF 2

CONF 3 EXTENSION
NO GEAR RETRACTION NO AUTO CALLOUTS
 DIRECT LAW

BE AWARE OF :
NO REVERSER
NO NWS
NO AUTO BRK
PARTIAL LOSS OF GRND SPOILERS
NO ANTI SKID (1000 PSI MAX)
LAST CHANGE
01 JULY 2012 SUMMARY MODIFIED

FOR RR and PW engines: N1 UNRATED MODE
RMK ADDED
REV10
SMOKE/FUMES/AVNCS SMOKE
AIR COND SMOKE
SMOKE
IMMEDIATE CABIN EQUIPMENT
FUMES TO SET ELEC
ACTIONS SMOKE REMOVAL OF SMOKE
AVNCS SMOKE EMER CONFIG
SMOKE SOURCE NOT

DETERMINED OR
AVNCS/ELECTRICAL
SMOKE
SMOKE !!!
LAND ASAP
REV 11
PF DETECTION PNF
FLY THE AIRCRAFT
NAVIGATE
QRH
ORDER……..….” SMOKE/FUMES/AVNCS SMOKE ” SMOKE/FUMES/AVNCS SMOKE.………...APPLY
PF Procedure Layout
COMMUNICATE
Immediate actions
Actions considered if, during the procedure :

- Smoke becomes the greatest threat:
- SMOKE/FUMES REMOVAL QRH
- ELEC EMER CONFIG
- Situation becomes critical and can no longer
be controlled:
- DIVERSION
Actions specific to
each smoke source
PF IMMEDIATE ACTIONS PNF
QRH
SMOKE/FUMES/AVNCS SMOKE.…….……...APPLY
Apply:
APPLY IMMEDIATELY:
With or without ECAM activations, these immediate actions correspond to the

most common steps to be taken in smoke cases:
 Avoid any further contamination
 Communication with cabin crew
 Flight crew protection
QRH
1.00
PF IF AIR COND SMOKE SUSPECTED PNF
Moderate smoke persists. You suspect AIR COND SMOKE:
QRH
SMOKE/FUMES/AVNCS SMOKE.…….……...APPLY
Keep in mind:
At ANY TIME of the procedure, if smoke/fumes Apply:

becomes the GREATEST THREAT:
IF AIR COND SMOKE SUSPECTED:
At ANY TIME of the procedure, if situation
becomes UNMANAGEABLE:
QRH
1.00 In this case, try to identify the smoke
source by isolating the packs, one by
one.
PF IF CABIN EQUIPMENT SMOKE SUSPECTED
PNF
Moderate smoke persists. You suspect CABIN EQUIPMENT SMOKE:
QRH
SMOKE/FUMES/AVNCS SMOKE.…………..APPLY
Keep in mind:
At ANY TIME of the procedure, if smoke/fumes

becomes the GREATEST THREAT: Apply:
At ANY TIME of the procedure, if situation IF CAB EQUIPMENT SMOKE SUSPECTED:

QRH In this case, try to identify the smoke

source by isolating the different
electrical equipments.
IF SMOKE SOURCE NOT DETERMINED
PF AND STILL CONTINUES
OR AVNCS/ELECTRICAL SMOKE SUSPECTED
PNF
Moderate smoke persists. You cannot determine the source,

or, the smoke still continues after the application of others specific actions,
QRH
or, you suspect AVIONICS or ELECTRICAL SMOKE :
SMOKE/FUMES/AVNCS SMOKE.…….…....APPLY
Keep in mind: Apply:
IF SMOKE SOURCE CANNOT BE DETERMINED

At ANY TIME of the procedure, if smoke/fumes
AND STILL CONTINUES OR AVNCS/ELECTRICAL
becomes the GREATEST THREAT:
SMOKE SUSPECTED:
At ANY TIME of the procedure, if situation
QRH This part of the procedure consists of

shedding the different AC buses.
PF REMOVAL OF SMOKE / FUMES PNF
Smoke is dense, and becomes the greatest threat:
QRH
ORDER……..….” SMOKE/FUMES REMOVAL ” SMOKE/FUMES REMOVAL ...........………...APPLY
Procedure Layout
Smoke Removal above FL100

or MEA Smoke Removal without
window opening
Smoke Removal at or below

FL100 or MEA
If cockpit window
opening required …
Dense smoke still continues, being the greatest threat
or, when all the specific actions have been unsuccessful:
QRH
ORDER……..….” SET ELEC EMER CONFIG ” Refer to the end of the SMOKE/FUMES/AVNCS
SMOKE procedure to set ELEC EMER CONFIG
1.00
QRH
THE END...
SMOKE FUMES AVNCS SMOKE
General guidelines to determine the smoke source:

(available in FCOM but not in QRH)
VARIOUS SMOKE SOURCES
EXISTING PROCEDURES
VARIOUS SMOKE SOURCES
 CARGO Easy to Identify
 LAVATORY
 CREW REST COMPARTMENT
(A330/A340)
 AVIONICS Hard to Identify

 AIR COND
 CABIN EQUIPMENT
EXISTING PROCEDURES
Hard to Identify
Supported by ECAM Procedure Supported by ECAM or Paper procedures

Always the same process: More difficult to locate and to treat
Isolate (close door / hatch, close isolation valve…) Process depends on the situation
Extinguish (automatic system or manual)
When ECAM supported : Carry out ECAM actions
Note: In the event of not readable ECAM, QRH procedure has to be applied.
When not ECAM supported :

QRH
FIRE
. SMOKE /FUMES/AVNCS SMOKE
Note: This QRH procedure covers many cases of smoke sources (even all steps of the AVIONICS SMOKE ECAM procedure).
SMOKE PROCEDURE LAYOUT
General guidelines to determine the smoke source:

(available in FCOM PRO-ABN-26 but not in QRH)
LAST CHANGE
01 JULY 2012 - MINOR CHANGES
REV10
HYD: G+B SYS LO PR
APPROACH
HYD G SYS LO PR HYD G+B SYS LO PR PREPARATION APPROACH
HYD G SYS LO PR
HYD G+B SYS LO PR
LAND ASAP
FMGS PREP
APPROACH BRIEFING
GO AROUND
USE OF SUMMARY
REV 11
PF HYD G SYS LO PR PNF
DETECTION
FLY THE AIRCRAFT

NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF SYSTEM DISPLAY
COMMUNICATE
STATUS
MASTER CAUTION: No immediate action required,

However, execute the ECAM actions as soon as possible.
NOTE: As a general rule, do not manually select an HYD ELEC PUMP ON, except
temporarily, to retract the spoilers if they remain out after an hydraulic failure.
PF HYD G+B SYS LO PR PNF
DETECTION
FLY THE AIRCRAFT  LOSS OF AP + ALTN LAW
ECAM ACTIONS
PF
COMMUNICATE ECAM PROCEDURE RAT
MAYDAY Message
SYSTEM DISPLAY
STATUS
SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DIST
DECISION
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ANNOUNCE……………”YOU HAVE CONTROL ?” ANNOUNCE…………………….”I HAVE CONTROL”

ECAM STATUS………………………………REVIEW
SUMMARY…………..…………………………….USE
FMGS……………………………………….PREPARE
APPR BRIEFING .......….………………..PERFORM
FMGS PREPARATION:
STANDARD
+
APPR BRIEFING .......….………………..PERFORM

PF APPROACH PNF
FLAPS EXTENSION (SLATS JAMMED)....USE SUMMARY
ALTN LAW
CONFIGURATION
NO AP
FLY A STABILIZED APPROACH
 LDG WITH SLATS JAMMED: USE THE SUMMARY
GO AROUND
LDG CANNOT BE RETRACTED LANDING GEAR EXTENSION

 DOORS WILL REMAIN OPEN
 L/G GRAVITY EXTENSION
 DOORS REMAIN OPEN
BE AWARE OF:
 NO ANTISKID (B BRK PRESSURE MONITORED BY PNF)
 ONE REVERSER AVAIL ( FOR A340 and A330 PW AND RR ENG ONLY)
 PARTIAL LOSS OF GRND SPOILERS
 NO N/W STRG (except on A340-600)
……………..
THE END...
USE OF SUMMARY

 SITUATION ASSESSMENT USING SUMMARY
 APPROACH PREPARATION USING SUMMARY
 APPROACH BRIEFING USING SUMMARY
 APPROACH USING SUMMARY

PF HYD G+B SYS LO PR PNF
DETECTION
FLY THE AIRCRAFT  LOSS OF AP + ALTN LAW
 When flaps/slats are faulty, if speed is not selected at actual speed, the aircraft will continue to decelerate down to
a speed inconsistent with the actual aircraft configuration, or accelerate and possibly exceed Max Speed.
Slats are lost Flaps are slow

ECAM ACTIONS
PF
COMMUNICATE ECAM PROCEDURE
MAYDAY Message
 The loss of some FLT CTL components makes the aircraft handling more demanding:
SYSTEM DISPLAY
STATUS
SUMMARY
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DIST
DECISION
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
RAM AIR TURBINE
 The RAT automatically extends in flight, if:

- All engines fail
- GREEN + BLUE LO LVL (A340-600: GREEN + BLEU LO LVL + Engine burst detected)
- GREEN + YELLOW LO LVL (A330 only).
 - RAT…….……MAN ON is displayed on ECAM after an automatic deployment of the RAT for confirmation.
 With the RAT extended, the green system could be recovered. This would permit slat extension recovery.
 With the RAT extended, the fuel consumption increases by approx 1 %.
 - CONSIDER RAT MAN USE is not triggered in case of GREEN RSVR OVERHEAT, or GREEN LO LVL.
STATUS

CRUISE
- the flight capability of the
3
ECAM aircraft.
1
ACTIONS
APPROACH
assess the situation and to
LANDING
runway.
GO AROUND

QRH for :
4 QRH: FPE fuel consumption (FPE-FPF)


CRUISE - the flight capability of the
3
ECAM aircraft.
1
ACTIONS
APPROACH
assess the situation and to
LANDING
runway.
GO AROUND

QRH for :
4 QRH: FPE-IFL fuel consumption (FPE-FPF)
SUMMARY
ACTIONS
APPROACH

STATUS
approach.
6 GO AROUND

8 FMGS PREPARATION
SUMMARY
ACTIONS
APPROACH

STATUS
approach.
6 GO AROUND

8 FMGS PREPARATION
SUMMARY
CRUISE
ECAM
APPROACH
STATUS
9
GO AROUND

SUMMARY
CRUISE
ECAM
APPROACH
STATUS
9
GO AROUND


CRUISE

LANDING
completed.


CRUISE

LANDING
completed.

LAST CHANGE
01 JULY 2012 SUMMARY MODIFIED
REV10
HYD: G+Y SYS LO PR
REV 11
REJECTED TAKEOFF AND EVACUATION
REV 11
WINDSHEAR
REV 11
EGPWS
REV 11
TCAS
REV 11
UNRELIABLE SPEED INDICATION
REV 11
STALL RECOVERY
REV 11
TWO ENGINES INOPERATIVE LANDING
Rev 11
ALL ENGINE FLAME OUT
REV 11
DUAL FMGC FAULT
AUTO FLT FM 1 FAULT AUTO FLT FM 1 + 2 FAULT NAV B/UP
NORMAL mode :
REV 11
PF AUTO FLT FM 1 FAULT PNF
FMGC AUTO-RESET
DETECTION
FLY THE AIRCRAFT  LOSS OF AP1 / FD1
CONSIDER AUTOMATION USE  AP2
NAVIGATE
PF
COMMUNICATE
ECAM ACTIONS
ECAM PROCEDURE MCDU Menu
SYSTEM DISPLAY
STATUS Manual Reset
SINGLE mode :
PF AUTO FLT FM 1+2 FAULT PNF
DETECTION
FLY THE AIRCRAFT  Loss of AP/FD and A/THR
NAVIGATE  NAVAIDs tuned via RMP
PF
COMMUNICATE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS Manual Reset
PF NAV B/UP MODE PNF
If the resets of both FMGCs are unsuccessful, use the back-up navigation degraded mode:
NAV B/UP…………..……………………..…SELECT on both MCDU MENU pages
- The MCDU continuously memorizes the active F-PLN in its internal memory
- The pilot recovers the navigation function through the MCDU and ADIRS
- The MCDU 3 is not able to operate as back up navigation
- F-PLN display on ND
- No AP / FD NAV mode
- The MCDU’s NAV B/UP mode provides the following functions :
 B/UP F-PLN with auto-sequencing and limited lateral revision
 B/UP F-PLN for DIR TO
 B/UP PROG page
 B/UP IRS (aircraft position using onside IRS or IRS 3)
 B/UP GPS page (option)
FMGC1 FMGC2
MCDU 1 MCDU 2
MCDU 3 BACK UP
BACK UP
NAV NAV
……………..
THE END...
NORMAL MODE
FMGC 1 FMGC 2
FADEC
MCDU 1 MCDU 2
THRUST
LEVERS
MCDU 3
STBY
FMGC AUTO-RESET
DETECTION
NAVIGATE
PF
COMMUNICATE
ECAM ACTIONS
SYSTEM DISPLAY
STATUS Manual Reset
Engage AP2
SINGLE mode :
ECAM PROCEDURE
ND1 ND1
Select the same range and mode on both NDs……
FMGC 2
MCDU MENU
DETECTION
Select FM2
CONSIDER AUTOMATION USE  USE AP2
NAVIGATE
ECAM ACTIONS
PF
ECAM PROCEDURE
COMMUNICATE
SYSTEM DISPLAY
STATUS Manual Reset

FM
F MG
GCC 11 FMGC2
The FMGC software automatically resets itself.
FM
F MG
GCC 11 FMGC2
MCDU 1 MCDU 2
OPP FMGC IN PROCESS OPP FMGCGC IN PROCESS
MCDU 1 MCDU 2
SINGLE MODE
FMGC1 FMGC 2
FADEC
MCDU 1 MCDU 2
THRUST
LEVERS
MCDU 3
STBY
DETECTION
 Remove
NAVIGATE  NAVAIDs (FDs…..OFF)
FD flag tuned via RMP
 Use the bird (FPV) (TRK/FPA…. SELECT)
PF Single Chime
THR LK (every 5 sec)
COMMUNICATE
ECAM ACTIONS
 THR LK: Read N1 or EPR, then move the thrust levers ( ) accordingly
ECAM PROCEDURE •••
ECAM SYSTEM DISPLAY

ACTIONS
ECAM PROCEDURE
Note: STATUS
AP may be available if Flight GuidanceManual
is not lost.Reset
SYSTEM DISPLAY
STATUS Manual Reset
DETECTION
PF
COMMUNICATE
Both NDs display:

ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS Manual Reset
ECAM PROCEDURE
 Switching panel:
 Adjust the landing elevation of the destination on the overhead panel

 Observe MCDU 1 menu:
FMGC AUTO-RESET
An resynchronization with the other FM always occurs after an FM reset
 Minor RESET (the system will recover by itself) :

3 sec max + resynchronization(s) with the other FM ( one resynch lasts 25 sec)
 Major RESET :
Several recurrent resets during 2 or 3 min
Memories are cleared  loss of F-PLN, GW, CI, CRZ FL, MCDU-entered speeds and navaids
 While RESET / RESYNCH occurs:
MAP NOT AVAIL
MAP NOT AVAIL
MCDU reverts to
A/C STATUS page.
Autotuning of
NAVAIDS is lost PLEASE WAIT
PLEASE WAIT
After 4 resets without auto-recovery SINGLE mode operation
If several resynch occurs within 5 min INDEPENDENT mode operation

DETECTION
PF
COMMUNICATE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS Manual Reset
Successively reset both FMGCs, with the FMGEC reset breakers
FOR TRAINING PURPOSE : DELAY MANUAL RESET

FMGC AUTO-RESET
DETECTION
NAVIGATE
PF
COMMUNICATE
ECAM ACTIONS
SYSTEM DISPLAY
STATUS Manual Reset
Reset FMGC with the FMGEC reset breaker
FOR TRAINING PURPOSE : DELAY MANUAL RESET

SINGLE mode :
MANUAL RESET
 Reset only one FMGC at a time
DETECTION
 Resynchronization of both FMs will occur after a dual successful reset with messages:
MAP NOT AVAIL
MAP NOT AVAIL
MCDU reverts to
PF A/C STATUS page. PLEASE WAIT
COMMUNICATE Autotuning of NAVAIDS

is lost on failed side
ECAM ACTIONS
PLEASE WAIT
 Three successive dual resets without result erase all pilot-entered data (F-PLN, GW, CRZ FL,
ECAM
CI…). In that case, refer to FCOM: DUAL RESETPROCEDURE
WITH LOSS OF DATA AND AUTORECOVERY
SYSTEM DISPLAY
 Deselect standby NAV on RMPs (but ILS and ADF must be tuned manually)
 Select the initial databaseSTATUS Manual Reset
 Select DIR TO and define DESTINATION
 Enter GW and CG (FUEL page)
 Enter CRZ FL (PROG page)
 Enter CI (PERF page)
 Set Landing Elevation selector to AUTO
 Set switching panel to NORM, if applicable
LAST CHANGE
01 JULY 2012 -
REV10
TOTAL LOSS OF FCU
REV 11
LOW ENERGY AURAL ALERT
REV 11
FLAPS LOCKED during retraction
APPROACH
F/CTL FLAPS LOCKED APPROACH
PREPARATION
-F Flaps 1
F/CTL FLAPS LOCKED
L/G UP
REV11
PF F/CTL FLAPS LOCKED PNF
At F speed with positive speed trend
ORDER……………………………...…”FLAPS 1” ANNOUNCE…………..”SPEED CHECKED”

FLAPS 1………………………………SELECT
DETECTION
SPEED……………………………….PULL & SELECT A330 / A340-300
FLY THE AIRCRAFT

NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
COMMUNICATE SYSTEM DISPLAY
STATUS A330 / A340-300
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ANNOUNCE……………….....”YOU HAVE CONTROL ?” ANNOUNCE…………………………...”I HAVE CONTROL”
FMGS……………………………………………..PREPARE
APPR BRIEFING ......………….....……………PERFORM
FMGS PREPARATION:
STANDARD
+
QRH
APP BRIEFING:
STANDARD
+
STATUS
+
QRH LANDING WITH SLATS OR FLAPS JAMMED
+
OVERWEIGHT LANDING (if required)
PF APPROACH PNF
For Slats extension:

QRH
LANDING WITH SLATS OR
FLAPS JAMMED PROC………………………….….APPLY
Before 500 ft:

AP………………………..………………………….…OFF
 MONITOR AP behaviour (not tuned for abnormal configuration)
 FLY a stabilized approach
 USE selected speed to avoid deceleration to S and F
QRH Second approach maintain configuration

 In case of go around:
Diversion - Maintain configuration if
FLAPS jammed >0
 APPROACH SYNTHESIS: A330 / A 340-300 - Select clean configuration

if FLAPS jammed at 0

DETECTION
SPEED……………………………….PULL & SELECT A330 / A340-300 A340-600
FLY THE AIRCRAFT

When flaps/slats are faulty or locked, if speed is not selected at actual speed,
the aircraft will continue to accelerate and possibly exceed Max Speed.
NAVIGATE
At take off ECAM ACTIONS At go around

250 227
ECAM PROCEDURE
PF
STATUS A330 / A340-300 A340-600
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…

DETECTION
SPEED……………………………….PULL & SELECT A330 / A340-300 A340-600
FLY THE AIRCRAFT

When flaps/slats are faulty or locked, if speed is not selected at actual speed,
the aircraft will continue to accelerate and possibly exceed Max Speed.
NAVIGATE
At take off At go around
ECAM ACTIONS
250
ECAM PROCEDURE
PF
STATUS A330 / A340-300 A340-600
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
STOP ECAM
Some actions may have to be performed before reading the status:
 NORMAL C/L QRH
 Computer resets
In this exercise:
ANNOUNCE…………………………….…..”STATUS ?”
ORDER……………………………”STOP ECAM”
AFTER TAKEOFF/CLIMB C/L

STATUS
A330 / A340-300
 Flaps locked = Flaps wing tip brakes are applied
 Slats are available
 Evaluate increased fuel consumption
 Compute VAPP & LDG distance
 Speed displayed on PFD:
• VFE
• VFE NEXT Computed according to
• S speed the flaps’ lever position.
• F speed
• Overspeed warning
Computed according to the actual
• VLS flaps/slats position.
Flaps
Slats in locked in
CONF 1 CONF 2
STATUS
A340-600
 Flaps locked = Flaps wing tip brakes are applied
 Slats are available
 Compute VAPP & LDG distance
 Speed displayed on PFD:
• VFE
• VFE NEXT Computed according to
• S speed the flaps’ lever position.
• F speed
• Overspeed warning
Computed according to the actual
• VLS flaps/slats position.
Flaps
Slats in locked in
CONF 1 CONF 2
SLATS FAULT during extension
F/CTL SLATS SYS 1 FAULT F/CTL SLATS FAULT APPROACH

APPROACH
PREPARATION
F/CTL SLATS SYS 1 FAULT F/CTL SLATS FAULT -F Flaps 1
REV11
PF F/CTL SLATS SYS 1 FAULT PNF
DETECTION
FLY THE AIRCRAFT
NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
STATUS
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
PF F/CTL SLATS FAULT PNF
DETECTION
SPEED……………………………..…….PULL & SELECT
FLY THE AIRCRAFT  ALTN LAW with AP

NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
STATUS
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ANNOUNCE………..………..”YOU HAVE CONTROL ?” ANNOUNCE………………..……...”I HAVE CONTROL”
FMGS……………………..……………………...PREPARE
APPR BRIEFING .........……….…………….…PERFORM
FMGS PREPARATION:
STANDARD
+ QRH
APP BRIEFING:
STANDARD
+
STATUS
+
QRH
LANDING WITH SLATS OR FLAPS JAMMED
PF APPROACH PNF
QRH For Flaps extension:

LANDING WITH SLATS OR
FLAPS JAMMED PROC…………….……………….APPLY
Before 500 ft:
AP……………………………………………..……………OFF
 Monitor AP behaviour (not tuned for abnormal configuration)
 Fly a stabilized approach
QRH
Second approach maintain configuration
 In case of go around
Diversion clean the A/C
 APPROACH SYNTHESIS A330 / A 340-300

PF F/CTL SLATS SYS 1 FAULT PNF
DETECTION
FLY THE AIRCRAFT
NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
STATUS
 Single SFCC Slats channels fault

STATUS, or
 Flaps are available

WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
 SLATS SLOW: Slats operate at half speed.

DETECTION

NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
STATUS
 Slats fault = Both SFCC slats channels are failed
 ALTN LAW: PROT LOST
 Flaps are available
A330 – A340-300:
STATUS, or
SUMMARY WEATHER
WEATHER

LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
STATUS, or ATC
ATC
WEATHER
WEATHER
SUMMARY DECISION
DECISION PURSER
PURSER // PAX
PAX
DECISION
LDG
LDGDIST
DIST
NOTIFY
NOTIFY AND
OPERATIONAL
OPERATIONAL AND OPS
OPS …
…
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
 Compute the VAPP & LDG distance.

ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
Approach flown with AP APPROACH SYNTHESIS
FD
ALTN LAW A/THR
To reach next configuration:
Decelerate towards VFE NEXT – 5kt
280 Use placard’s speeds, as VFE next
SPD
220 and VLS are not displayed.
LIM FLAPS 1
FLAPS 2
L/G DOWN
VAPP at FCU
GO AROUND
FINAL APPR
DETECTION

 When flaps/slats are faulty or locked, if speed is not selected at actual
speed, theUSE
CONSIDER AUTOMATION aircraft will continue to decelerate down to a speed
inconsistent with the actual aircraft configuration
NAVIGATE
ECAM ACTIONS
 No characteristic speed available: VLS, S,
ECAM SPD
PROCEDURE
F, VFE next, VSW, Vmax
LIM
PF
STATUS
 SLATS position isRETURN
unknown. TO NORMAL
S TASK SHARING
F
XX
XX
STATUS, or
WEATHER
WEATHER
SUMMARY
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
ELEV REDUND LOST – PITCH MECH BACKUP
A330
A340-300
REV 11
A330
A340-300 ELEV REDUND LOST – PITCH MECH BACKUP
F/CTL SEC 2 FAULT

F/CTL PRIM 2 FAULT
HYD G SYS LO PR
ELEV REDUND LOST
F/CTL L+R ELEV FAULT
PITCH MECH BACK UP
G B G B
Y G P1 P2 P1 P2 Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 REV10
S1 S2
Successive failures affecting F/CTL computers (PRIM, SEC) and/or HYD supply and/or Servojacks
may lead to the loss of flight controls redundancy. The case studied here is: HYD G + PRIM 2 + SEC2 failures
DETECTION
FLY THE AIRCRAFT
NAVIGATE
PF ECAM ACTIONS
COMMUNICATE
ECAM PROCEDURE
SYSTEM DISPLAY FLT CLT Architecture
STATUS
F/CTL PRIM 2 FAULT
PF ELEV REDUND LOST PNF
DETECTION
FLY THE AIRCRAFT  LOSS OF AP
NAVIGATE
ECAM ACTIONS
PF ECAM PROCEDURE
COMMUNICATE
STATUS Why ailerons preset ?

SUMMARY WEATHER
WEATHER
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
COMMERCIAL
COMMERCIAL
AND
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
PF PITCH MECH BACK UP PNF
DETECTION
FLY THE AIRCRAFT  MAN PITCH TRIM ONLY
NAVIGATE
ECAM ACTIONS
PF ECAM PROCEDURE
COMMUNICATE
SYSTEM DISPLAY
STATUS
Reset F/CTL computers for recovery.

A340-600 F/CTL ELEV REDUND LOST
HYD G SYS LO PR
HYD Y SYS LO PR
HYD G SYS LO PR F/CTL ELEV SERVO FAULT

PITCH MECH BACK UP
F/CTL L ELEV FAULT
G B G B
Y G P1 P2 P1 P2 Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 REV10
S1 S2
Successive failures affecting F/CTL computers (PRIM, SEC) and/or HYD supply and/or Servojacks
may lead to the loss of flight controls redundancy. The case studied here is: HYD G + ELEV SERVO + Y HYD failures
DETECTION
FLY THE AIRCRAFT
NAVIGATE
PF ECAM ACTIONS
COMMUNICATE
ECAM PROCEDURE
STATUS
PF F/CTL L ELEV FAULT
PNF
DETECTION
FLY THE AIRCRAFT  LOSS OF AP + ALTN LAW (PROT LOST)
NAVIGATE
ECAM ACTIONS
PF ECAM PROCEDURE
COMMUNICATE
STATUS Why ailerons preset ?

SUMMARY WEATHER
WEATHER
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
COMMERCIAL
COMMERCIAL
AND
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
PF PITCH MECH BACK UP PNF
DETECTION
NAVIGATE
ECAM ACTIONS
PF ECAM PROCEDURE
COMMUNICATE
SYSTEM DISPLAY
STATUS
Reset F/CTL computers for L ELEV SERVO FAULT recovery (PRIM2 and SEC2).
……………..
THE END...
HYD G SYS LO PR
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
F/CTL PRIM 2 FAULT
ELEV REDUND LOST
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
Ailerons and elevators are still available, but redundancy is lost.

Look what would happen in case of a third failure affecting flight controls (SEC 2 FAULT):
F/CTL SEC 2 FAULT

PITCH MECH BACK UP
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
Both elevators are lost. Pitch mechanical control is available through the THS, using the trim wheel.
Why ailerons preset ?
.
 When lost, the ailerons go to a zero hinge moment (14° up), causing a pitch up effect:
 The elevators and the THS, when available, are able to compensate this effect (FBW).
 After a total loss of elevator, pitch is manually controlled by the trim wheel (MECHANICAL BACKUP). The
efficiency, in this case, would not be sufficient to counteract the pitch up effect.
 As a precautionary measure, when 2 of 3 failures, leading to the loss of both elevators, have occurred :
- ECAM F/CTL ELEV REDUND LOST is triggered,
- The ailerons are preset close to the zero hinge position (12° up), causing voluntarily a pitch up effect,
- The auto pitch trim (which is available at this stage) counters immediately this pitch up effect through the THS.
F/CTL PRIM 2 FAULT

HYD G SYS LO PR HYD G SYS LO PR + ELEV REDUND LOST
SYSTEM DISPLAY
HYD G SYS LO PR
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
F/CTL ELEV SERVO FAULT
F/CTL L ELEV FAULT
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
Ailerons are still available. Left elevator is lost.

Look what would happen in case of a third failure affecting the yellow hydraulic system
HYD Y SYS LO PR

PITCH MECH BACK UP
G B G B
P1 P2 P1 P2
Y G Y G
P3 S1 S2 P3
S1 S2 S1 S2
B G G Y
P2 P1 P1 P2
S2 S1 S1 S2
Both elevators are lost. Pitch mechanical control is available through the THS, using the trim wheel.
Why ailerons preset ?
.
 When lost, the ailerons go to a zero hinge moment (14° up), causing a pitch up effect:
 The elevators and the THS, when available, compensate this effect (FBW).
 After a total loss of elevator, pitch is manually controlled by the trim wheel (MECHANICAL BACKUP). The efficiency
is not sufficient to counteract the pitch up effect.
 As a precautionary measure, when 2 of 3 failures, leading to the loss of both elevators, have occurred :
- ECAM F/CTL ELEV REDUND LOST is triggered,
- The ailerons are preset close to the zero hinge position (13° up), causing voluntarily a pitch up effect,
- The auto pitch trim (which is available at this stage) counters immediately this pitch up effect through the THS.
F/CTL L ELEV SERVO FAULT

HYD G SYS LO PR HYD G SYS LO PR + ELEV REDUND LOST
STATUS
ELEV REDUNDANCY LOST is not always associated to aileron preset
 Ailerons are preset upwards ~12° with  Ailerons are not preset upwards.
high fuel consumption & AP disconnection AP is available
The altitude is limited to FL 350 The altitude is limited to FL 300

The speed is limited to M.80 The speed is limited to M.75
STATUS
ELEV REDUNDANCY LOST is not always associated to aileron preset
 Ailerons are preset upwards ~13° with  Ailerons are not preset upwards.
high fuel consumption & AP disconnection AP is available
The altitude is limited to FL 350 The altitude is limited to FL 300

The speed is limited to M.80 The speed is limited to M.75
SYSTEM DISPLAY
In our case:
 Pitch is mechanically controlled by the trim wheel through the THS
 Roll is slowly controlled by side stick (1aileron + some spoilers)
 Rudder is controlled by the PRIM 3 and the yellow hydraulic jack
Recommendations for aircraft stabilization:
 Disconnect A/THR
 PNF may set thrust on PF request
 PF uses pitch trim wheel, sidestick for the remaing aileron and rudder
(if necessary)
 Try not to exceed 15 degrees bank angle

In our case:
 Pitch is mechanically controlled by the trim wheel through the THS
 Roll is slowly controlled by side stick (1aileron + some spoilers)
 Rudder is controlled by the PRIM 3 and the yellow hydraulic jack
Recommendations for aircraft stabilization:
 Disconnect A/THR
 PNF may set thrust on PF request
 PF uses pitch trim wheel, sidestick for the remaing aileron and rudder
(if necessary)
 Try not to exceed 15 degrees bank angle

LAST CHANGE
01 JULY 2012 MINOR CORRECTIONS ON A346
REV10
FUEL LEAK
A330 A340-300
REV 11
A330 - FUEL LEAK
FUEL MONITORING FUEL LEAK SUSPECTED FUEL L WING TK LO LVL LANDING
ADVISORY
Kg Kg
REV10
A340-300 - FUEL LEAK
ADVISORY
Kg Kg
REV10
FUEL LEAK
FUEL MONITORING FUEL WING TK IMBALANCE FUEL INR 2 LO LVL LANDING
SUSPECTED
Kg Kg
REV10
PF ADVISORY PNF
ANNOUNCE………………………………..”ADVISORY ON “FUEL” SYSTEM”
PF
COMMUNICATE FUEL PAGE DISPLAYED………...……….…....ANALYSE
ECAM ADVISORY CONDITIONS……..…………..CHECK
QRH
PF ADVISORY PNF
ANNOUNCE………………………………..”ADVISORY ON “FUEL” SYSTEM”
PF
COMMUNICATE FUEL PAGE DISPLAYED………...……….…....ANALYSE
ECAM ADVISORY CONDITIONS……..…………..CHECK
QRH
PF FUEL WING TK IMBALANCE PNF
ECAM ACTIONS
FUEL WING TK IMBALANCE

. IF NO FUEL LEAK:
-…
Do not apply the ECAM procedure

if a fuel leak is suspected.
QRH
Refer to the FUEL LEAK procedure.
PF FUEL L WING TK LO LVL PNF
Remember FUEL LEAK PROC recommendations:
If
FUEL X FEED.………USE AS RQRD
has not been mentioned, disregard any:
FUEL L(R) WING TK LO LVL
FUEL IMBALANCE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
QRH
PF FUEL L WING TK LO LVL PNF
If
FUEL X FEED 1+2+3+4 …… USE AS RQRD
has not been mentioned, disregard any:
FUEL L(R) WING TK LO LVL
FUEL IMBALANCE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
QRH
PF FUEL INR 2 LO LVL PNF
If
FUEL X FEED 1+2+3+4………USE AS RQRD
has not been mentioned, disregard any
FUEL INR 1 (2) (3) (4) LO LVL
FUEL WING TK IMBALANCE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
QRH
A330 - FUEL LEAK
ADVISORY
Approach and landing can be done, even
with one full wing/one empty wing but,
DO NOT USE THE REVERSERS.
Kg Kg
REV10

ADVISORY
Kg Kg
REV10
FUEL LEAK
FUEL MONITORING FUEL WING TK IMBALANCE FUEL INR 2 LO LVL LANDING
SUSPECTED

Kg Kg
REV10
PF FUEL LEAK SUSPECTED PNF
When fuel leak is suspected:
QRH
ORDER………………………………….…” FUEL LEAK proc”
FUEL LEAK PROC……..…..………….……....APPLY
DECISION
The QRH procedure

gives some cues to
confirm the leak and
to help to locate it To be applied when the leak is confirmed
■ LEAK FROM ENGINE/PYLON CONFIRMED
■ LEAK NOT LOCATED


QRH
ORDER………………………………….…” FUEL LEAK proc” FUEL LEAK PROC……..…..………….……....APPLY
DECISION
The QRH procedure

gives some cues to
■ LEAK AFTER ENG FAIL
■ OTHER CASES
QRH
DECISION
The QRH procedure

gives some cues to

PF FUEL MONITORING PNF
FLIGHT PROGRESS……..…..………….…….........CHECK
FUEL………………………………………………...MONITOR
In flight, carry out periodical fuel checks (WPT, or at least every 30 min) using:
FOB and EFOB comparisons
CHECK FUEL AT DEST, ALTN and EXTRA
FOB, FU and FOB at departure comparisons
Fuel Flow and Fuel Imbalance.

FOB and EFOB comparaisons
At any waypoint,
or every 30 min,
COMPARE
If FOB < EFOB:
VALUES
Suspect an increased
fuel consumption
or a fuel leak
F-PLN B PAGE
CHECK FUEL AT
DEST, ALTN and
EXTRA F-PLN A PAGE
FUEL PRED PAGE

FOB
FU FOB at
departure
Every 30 min,
If FOB + FU < FOB at departure or,

if the sum decreases:
Suspect a fuel leak
FUEL FLOW / FUEL IMBALANCE
COMPARE FUEL FLOW BETWEEN ENGs MONITOR FUEL IMBALANCE

FUEL………………………………………………...MONITOR

At any waypoint,
or every 30 min,
COMPARE If FOB < EFOB:

VALUES
fuel consumption
or a fuel leak
F-PLN B PAGE
CHECK FUEL AT
DEST, ALTN and
EXTRA F-PLN A PAGE
FUEL PRED PAGE

FOB
FU FOB at
departure
Every 30 min,

Suspect a fuel leak

FUEL………………………………………………...MONITOR

At any waypoint,
or every 30 min,
COMPARE
If FOB < EFOB:
VALUES
fuel consumption
or a fuel leak
F-PLN B PAGE
CHECK FUEL AT
DEST, ALTN and
EXTRA F-PLN A PAGE
FUEL PRED PAGE

FOB
FU FOB at
departure
Every 30 min,

Suspect a fuel leak

QRH
ORDER………………………………….…” FUEL LEAK proc”
FUEL LEAK PROC……..…..………….……....APPLY
DECISION
The QRH procedure

gives some cues to
QRH
Follow QRH to shut down affected engine.
If the leak stops:
DO NOT RESTART THE ENGINE


QRH
QRH
DECISION
The QRH procedure

gives some cues to
Follow QRH to shut down affected

■ LEAK engine.
AFTER ENG FAIL QRH
If the leak stops: ■ OTHER CASES

QRH
DECISION
The QRH procedure

gives some cues to
QRH
Follow QRH to shut down affected engine.
If the leak stops:


QRH
QRH
DECISION
The QRH procedure

gives some cues to
■ LEAK AFTER ENG FAIL QRH
FUEL X FEED 1+2+3+4…………….…MAINTAIN CLOSED

■ OTHER CASES
FUEL LOSS REDUCTION procedure…………. CONSIDER
CAUTION:
Do not apply the FUEL IMBALANCE procedure.
■ OTHER CASES QRH
CLICK TO MOVE FORWARD

QRH
Feed each engine 2.00
by a single wing tank
No DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Gravity Fuel Feeding proc
No Yes
Fuel smell ?
No Engine Yes
Flameout?
Consider FUEL LOSS Switch OFF APU Use Fuel X feed

REDUCTION proc Maintain T TK isolated Consider FUEL LOSS as rqrd
REDUCTION proc
Apply LEAK FROM
DO NOT APPLY ENG/PYLON
FUEL IMBALANCE PROC CONFIRMED proc
Maintain Fuel X feed
CLOSED
■ OTHER CASES QRH

QRH
No DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Gravity Fuel Feeding proc
No Yes
Fuel smell ?
No Engine Yes
Flameout?
Consider FUEL LOSS Switch OFF APU Use Fuel X feed

REDUCTION proc
Apply LEAK FROM
DO NOT APPLY ENG/PYLON
FUEL IMBALANCE PROC CONFIRMED proc
Maintain Fuel X feed
CLOSED
QRH
QRH
No
DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Shutdown the engine
No Yes
Fuel smell ?
No Yes
Leak stops ?
Consider FUEL LOSS Switch OFF APU Consider ENG restart Use Fuel X feed
REDUCTION proc
DO NOT RESTART
DO NOT APPLY FUEL THE ENGINE
IMBALANCE PROC
Maintain Fuel X feed CLOSED
QRH
QRH
No
DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Shutdown the engine
No Yes
Fuel smell ?
No Yes
Leak stops ?
REDUCTION proc
DO NOT RESTART
DO NOT APPLY FUEL THE ENGINE
IMBALANCE PROC
Maintain Fuel X feed CLOSED
QRH
QRH
No
DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Shutdown the engine
No Yes
Fuel smell ?
No Yes
Leak stops ?
REDUCTION proc
DO NOT
Maintain Fuel X feed RESTART THE
CLOSED ENGINE
QRH
QRH
No
DECISION
One tk depletes Yes
Case 2 Case 1
faster ?
Shutdown the engine
No Yes
Fuel smell ?
No Yes
Leak stops ?
REDUCTION proc
DO NOT
Maintain Fuel X feed RESTART THE
CLOSED ENGINE
LAST CHANGE
01 JULY 2012 - MINOR CHANGES
REV10
EIS FAILURE - SWITCHING
EIS DMC 2 FAULT EIS DMC 3 FAULT EIS DMC 1 FAULT EIS DMC 3 FAULT
E EFIS E
EFIS C
C DMC 3
DMC 3 A A
M M
DMC 2 DMC 1
ND UNIT 1 FAILURE PFD UNIT 2 FAILURE
REV 11
PF EIS DMC 2 FAULT PNF
DETECTION
CM1  PF
FLY THE AIRCRAFT
NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
PF
STATUS

PF EIS DMC 3 FAULT PNF
DETECTION
CM1  PF
FLY THE AIRCRAFT
NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS

EIS DMC 1 FAULT
PF PNF
DETECTION
CM2  PF
FLY THE AIRCRAFT
NAVIGATE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS

EIS DMC 3 FAULT
PF PNF
DETECTION
CM2  PF
FLY THE AIRCRAFT
NAVIGATE
QRH
DISPLAY UNIT FAILURE PROC………..APPLY

Then ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS

ND UNIT 1 FAILURE
PF PNF
CM1 QRH
DISPLAY UNIT FAILURE PROC……….….APPLY
NO AUTO SWITCHING
ND 1 Unit Blank
PFD UNIT 2 FAILURE
PF PNF
CM2 QRH
DISPLAY UNIT FAILURE PROC……….….APPLY
PFD AUTO SWITCHING

(PFD has priority over ND)
……………..
THE END...
ECAM PROCEDURE
INVALID DATA
EFIS DMC SWITCHING
E E E E E E E E E E E E
F C F C F C F C F C F C
I A I A I A I A I A I A
S M S M S M S M S M S M
DMC1 DMC3 DMC2 DMC1 DMC3 DMC2

ECAM PROCEDURE
During 1 sec … EFIS SINGLE SOURCE 1 EFIS SINGLE SOURCE 1

INVALID DATA INVALID DATA
ECAM AUTO
SWITCHING TO DMC 1
+
PFD/ND MANUAL
SWITCHING E E E E E E
E E E E E E F C F C F C
F C F C F C I A I A I A
I A I A I A S M S M S M
S M S M S M
DMC1 DMC3 DMC2

DMC1 DMC3 DMC2
Manual confirmation
of ECAM auto
switching
QRH PROCEDURE then ECAM PROCEDURE
DISPLAY UNIT FAILURE

INVALID DATA on EWD and SD
QRH
NO ECAM AUTO
SWITCHING
EFIS SINGLE SOURCE 2 EFIS SINGLE SOURCE 2
INVALID DATA
INVALID DATA
MANUAL SWITCHINGs
E E E E E
E E E E E E
F C F F E
C C F C F F
I I C C
A I A A I I
S A I A A
M S M S M S M S M S M
DMC1 DMC3 DMC2

DMC1 DMC3 DMC2
LAST CHANGE
01 JULY 2012 -
REV10
DUAL RADIO ALTIMETER FAILURE
REV 11
CREW INCAPACITATION
REV 11
« ICI LE POSTE DE PILOTAGE, PNC A VOS POSTE »
ENG START FAULT
ENG 1 START FAULT
A330 GE STALL
A340 CFM EGT OVERLIMIT
REV11
ENG 1 START FAULT
PF PNF
…Apply before start procedure

…Start engine 1
DETECTION
ECAM ACTIONS
ECAM PROCEDURE A330 A340
SYSTEM DISPLAY
STATUS
STATUS, or
SUMMARY WEATHER
WEATHER
A330 GE
DECISION
LDG
LDGDIST
DIST
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
OPS
OPS …
A340 CFM
NOTIFY
NOTIFY …
PF
COMMUNICATE
ACTIONS PERFORMED BY THE FADEC (A330 RR)
The FADEC automatically:

 Shuts off the fuel
 Turns off the ignition
 Closes the start valve.
After 30 sec. of auto crank, the FADEC

automatically performs a new start.
Both igniters are powered.
If the engine doesn’t start, the ECAM

asks the pilot to confirm the automatic
start abort by setting ENG MASTER 1
to OFF.
ACTIONS PERFORMED BY THE FADEC (A330 PW)

 Adjust the fuel flow.
As adjustment of the fuel flow has not

been successful, the FADEC:
 Turns off the ignition.
Note: The FADEC

performs an auto crank
After 30 sec. of dry crank, the FADEC

If the engine doesn’t start, the ECAM

to OFF.
ACTIONS PERFORMED BY THE FADEC (A330 GE)

Automatic new start: the FADEC

reduces the start fuel schedule
down to 14% in steps of 7%.
If engine doesn’t start, the ECAM asks

the pilot to confirm the automatic start
abort by setting ENG MASTER 1 to
OFF.
ACTIONS PERFORMED BY THE FADEC (A340 CFM)

Automatic new start : the FADEC

reduces the start fuel schedule
down to 21% in steps of 7%.
If the engine doesn’t start, the FADEC

to OFF.
ACTIONS PERFORMED BY THE FADEC (A340 RR)

 Turns off the ignition
 Closes the start valve.
After 30 sec. of dry crank, the FADEC

If the engine doesn’t start, the FADEC

to OFF.
ECAM PROCEDURE (A330)
 Do not interrupt the FADEC protective actions.
The FADEC automatically The fault light turns off when the
abort the start sequence. engine master switch is set to OFF.
ECAM PROCEDURE (A340)
 Do not interrupt the FADEC protective actions.
The FADEC automatically The fault light turns off when the
abort the start sequence. engine master switch is set to OFF.
DECISION (A330 RR)
Then, 2 options:
 Ask for appropriate maintenance actions
 Perform a new start attempt (prefer manual start procedure).
Starter engagement is limited in time and in number of successive attempts:

Note: Run down to zero N3 between each cycle.
Start cycle
3 min 3 min 1 min Starter cool down

30 min
 Starter maximum continuous operation is 5 minutes

 No engagement of the starter when the N3 is above 10%.
DECISION (A330 PW)
Then, 2 options:

Start cycle
5 min 5 min 5 min Starter cool down 5 min Starter cool down

30 min 30 min

DECISION (A340 RR)
Then, 2 options:
3 min 3 min 1 min

Run down Run down Starter cool down

to zero N3 to zero N3
30 min
OR
Start cycle
5 min Starter cool down
30 min

DECISION (A330 GE)
Then, 2 options:

Start cycle
5 min 5 min Starter cool down 5 min Starter cool down

Pause 10 min 10 min
30’’ per min
of operation
Starter maximum continuous operation is 5 minutes
No engagement of the starter when the N2 is above 30%.
DECISION (A340 CFM)
Then, 2 options:
Start cycle
2 min 2 min 2 min 2 min Starter cool down 2 min

20’’ 20’’ 20’’ 15 min
Pause

LAST CHANGE
01 JULY 2012 -
REV10
ENG FAILURE AFTER TAKEOFF
At Green Dot
At EO ACCEL ALT
CONTINUE
ECAM
ENG FAIL EO ACC ALT APPROACH
PREPARATION
DECISION
APPROACH BRIEFING
PRESS
ALT P/B to…
FMGS PREP
OP CLB MCT
PITCH : 12,5° Green dot
LEVEL OFF -F Flaps 1 -S Flaps 0 -
L/G up °
Beta target EO ACCELERATION
ALTITUDE
ENGINE
FAILURE
400 ft mini
V1
REV11
PF ENG FAIL PNF
DETECTION
The first who detects :
ANNOUNCE .………………………..……”ENGINE FAILURE”
FLY THE AIRCRAFT NO ACTION until 400 ft AGL

NAVIGATE  LAND ASAP
Above 400 ft and established on appropriate flight path :

PF
COMMUNICATE ECAM ACTIONS
ECAM PROCEDURE DAMAGE ?
NO DAMAGE ?
ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...
PF EO ACC ALT PNF
Before EO ACC ALT
ORDER…………….………………………..……”STOP ECAM” ECAM ACTIONS………………….…………………....STOP
At EO ACC ALT
ALT P/B on FCU………………………………….PRESS
FMA
CLEAN UP THE A/C

At GREEN DOT
1. ALT SELECTOR knob……..…………………..…PULL

2. THR LEVERS……..……………...………..…..…….MCT
FMA
For T/O in FLEX : FLEX MCT
THR LEVERS……..….MCT
CLB
PF CONTINUE ECAM PNF
ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
DECISION
 If an ELEC PUMP is running after an ENG failure, the MEMO display presents:
SWITCH OFF the electric pump when in clean configuration. After flight control surfaces retraction, the
ELEC PUMPs should not be used to replace the ENG driven pumps
PERF
 After a succesful engine relight, if EO CLR is still displayed, press on the prompt 
 Pressing EO CLR prompt restores predictions and performances for ALL ENGINES OPERATIVE.
Once pressed : Reverting to ONE ENGINE OUT conditions is not possible
ANNOUNCE………………..”YOU HAVE CONTROL ?” ANNOUNCE………………………...”I HAVE CONTROL”
FMS………………………….…………………PREPARE
APPR BRIEFING .........……….……………PERFORM

………………
THE END...
PF ENG FAIL PNF
DETECTION

NAVIGATE  LANDUp
- Gear ASAP
- Consider TOGA
- Pitch adjust 12.5º

- Beta
PF target Conditions
- Consider A/P
NO DAMAGE ?
PF ENG FAIL PNF
DETECTION

In such situation, stabilizing the flight path is number one priority.

Performing
Above 400 ftECAM actions before
and established stabilization reduces
on appropriate efficiency
flight path : due to PF high workload.
PF
NO DAMAGE ?
PF ENG FAIL PNF
DETECTION

If applicable, consider EOSID for TAKEOFF RWY.

PF
NO DAMAGE ?
PF NO DAMAGE ?
PNF
DETECTION
NO ACTION until 400 ft AGL
FLY THE AIRCRAFT

According to the situation, the crew may decide to attempt an engine relight in flight at
this step,
PF but it is recommended:
- To perform all ECAM actions andECAM PROCEDURE DAMAGE ?
NO DAMAGE ?
- To consider engine relight when reaching the STATUS page.
ENG FAIL
PF DAMAGE ?
PNF
DETECTION
NO ACTION until 400 ft AGL

CONSIDER ENGINE DAMAGE IF YOU NOTICE :
FLY THE AIRCRAFT

 High vibration prior to flame out
 Loud noise,
Aboveexplosion
400 ft and established on appropriate flight path :
PF
 Repeated and uncontrollable engine stalls
 Abnormal engine indications on ECAM (such as N1 orNO
N2DAMAGE
~ 0) ?
No attempt of RELIGHT
PF EO ACC ALT PNF
Before EO ACC ALT
ORDER…………….………………………..……”STOP
You should delay the ECAM” ECAM
acceleration for ACTIONS………………….…………………....STOP
SECURING the engine.
An engine is considered SECURED when:
 ENG MASTER…OFF At forEO
an ACC
engine failure without damage
ALT
 AGENT 1…DISCH for an engine failure with damage
 Fire extinguished or AGENT 2…DISCH for an engine fire.
ALT P/B on FCU………………………………….PRESS
CAUTION: DO NOT EXCEED THE MAXIMUM EO ACC ALT
FMA
PRESS OP CLB MCT
ALT P/B to… Green dot
-F Flaps 1 -S Flaps 0 -
CLEAN UP THE A/C°
LEVEL OFF MAX EO ACC ALT:
At GREEN DOT
1. ALT SELECTOR knob……..…………………..…PULL

2. THR LEVERS……..……………...………..…..…….MCT
ECAM
ACTIONS
FMA
ENGINE
FAILURE
400 ft mini
V1
For T/O in FLEX : FLEX MCT

THR LEVERS……..….MCT
CLB 10 MIN
CHRONO
MAX
FLY THE AIRCRAFT
PF PNF
Beta target and rudder trim
- “Engine failure”
- “Engine failure”
- Reset MASTER CAUTION
- Cancel -warning
Gear Up
Beta target
- Consider TOGA
- Gear Up
- Consider TOGA
- Beta target
Once centered :
Moves at 1 deg/s,
Appropriate sideslip
for optimum - Consider
A/P and, after 1.5 seconds,
at 3 deg/s
aircraft performance
- Beta target
- Consider A/P
PF ENG FAIL PNF
DETECTION

NAVIGATE  LANDUp
- Gear ASAP
- Consider TOGA

 T/O thrust (FLEX or TOGA) must
Above 400be keptestablished
ft and until GREEN DOT speedflight
on appropriate is reached,
path : limited to 10 min
- Beta
PFFAAtarget Conditions
(5 min under rules) ECAM ACTIONS
COMMUNICATE
- Consider
 TOGA thrust A/P more rudder input
requires ECAM PROCEDURE DAMAGE ?
 Setting TOGA when out of SRS mode with slats extended, triggers GO AROUND mode
NO DAMAGE ?
 On DERATED takeoff (option), DO NOT USE TOGA thrust if speed is below F in CONF 2 or 3
PF ENG FAIL PNF
Beta target conditions
DETECTION
A330

- Slats/Flaps in CONF 1, 1+F, 2, 3 or FULL, and
NAVIGATE  LANDUp
- Gear ASAP
- one thrust lever > MCT ( > or = FLX, if FLX or DRT TO), and
- at least one ENG > 1.3 EPR (or 80% N1), and
- Consider TOGA
- thrust asymmetry > 0.25 EPR (or 30% N1).
A340-300Above 400 ft and established on appropriate flight path :
- Beta
PF target Conditions
- Slats/Flaps in CONF 1,ECAM ACTIONS
2, or 3, and
COMMUNICATE
- any ENG
- Consider A/P N1 > 80%, and
- the difference between the ENG N1’sECAM PROCEDURE
exceeds 30%. DAMAGE ?
NO DAMAGE ?
A340-600
- Slats/Flaps in CONF 1, 1+F, 2, 3 or FULL, and

- one thrsut lever > MCT ( > or = FLX, if FLX or DRT TO), and
ECAM actions
- thrust can be stopped
asymmetry > 30%at N1,
any time on PFENG
between request for trajectory,
2 and 3, or ENGconfiguration,
1 and 4. etc...
STOP ECAM
Before reading STATUS page :
 NORMAL C/L
 Computer reset
QRH
ENG RELIGHT (IN FLIGHT)

LAST CHANGE
01 JULY 2012 HYD ELEC PUMP MEMO ADDED
REV10
ENGINE FAILURE IN CRUISE (Standard strategy)
For descent
to Long Range Cruise Ceiling
DETECTION
STOP CONTINUE REACHING
ECAM ECAM ECAM LRC CEILING
ACTIONS
STRATEGY ?
ENGINE A330
LAND ASAP
FAILURE
A340
LRC CEILING
REV11
PF ENG 1 FAIL PNF
DETECTION
FLY THE AIRCRAFT
THRUST LEVERS………………………………..MCT
A/THR………………………………………………OFF
ECAM ACTIONS
ECAM PROCEDURE
STOP ECAM actions when:
PF
COMMUNICATE
And Or
Deceleration NOT below Green Dot

PF STANDARD STRATEGY PNF
For descent:
EO
M.82/300 KT.……………………….SET AND PULL
EO LRC CEILING ALT…………....SET AND PULL
On PROG page: REC MAX = EO LRC Ceiling
FMA:
When V/S < 500ft/min:

V/S – 500 FT/MIN.……………….….SET AND PULL
A/THR…………………..………………..………….ON
FMA:
PF ECAM ACTIONS PNF
ECAM ACTIONS
SYSTEM DISPLAY QRH
STATUS ENG RELIGHT
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DIST
DECISION
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
Consider APU Start DIST & FUEL computations to Landing

FCOM
APU normal flight envelope:
FCOM
OR
QRH
• •
•••• •••• •
PF REACHING LRC CEILING PNF
Reaching LRC ceiling:
FMA:
SPEED….……………………………...MANAGED
END...
STRATEGY (A330)
DESCENT TO
LONG RANGE STANDARD
CRUISE
No obstacle and time constraint

CONTINUE
DETECTION STOP ECAM RESUME
ECAM STANDARD
ECAM (ENG RELIGHT)
(STANDARD STRATEGY
ACTIONS STRATEGY)
DECISION
OBSTACLE
STRATEGY ?
ENGINE To ensure the margins over obstacles
FAILURE
A330
LAND ASAP
A340
FIXED SPEED
As established before
dispatch, use:
ETOPS constraint
M.82
LRC / 330
CEILING KT
Or
M.82 / 310 KT
ENGINE FAILURE STRATEGY
IN CRUISE(A340) (with no damage)
DESCENT TO
LONG RANGE STANDARD
CRUISE
DETECTION
CONTINUE
STOP ECAM RESUME
ECAM STANDARD
ECAM (ENG RELIGHT)
(STANDARD STRATEGY
ACTIONS STRATEGY)
DECISION
OBSTACLE
STRATEGY ?
ENGINE To ensure the margins over obstacles
FAILURE
A330
LAND ASAP
A340
LRC CEILING
REV10
LRC AND GREEN DOT GROSS
CEILING QUICK CHECK (A330)
QRH
 Speed controlled by the elevator
Green Dot
Gross
Check
CeilingLRC CEILING
LRC
REC MAX = EO LRC Ceiling
Ceiling External
Temperature
GW at ENG FAIL
LRC AND GREEN DOT GROSS
CEILING QUICK CHECK (A340)
QRH
Green Dot
Gross
Ceiling
LRC
Ceiling
External
Temperature
GW at ENG FAIL
For descent:
EO
During the first part of the descent…
M.82/300 KT.……………………….SET AND PULL
EO LRC CEILING ALT…………....SET ANDPULL
Thrust MCT
FMA:

A/THR…………………..………………..………….ON
FMA:
 Confirm the EO LRC Ceiling using QRH:  EO CLR Prompt
QRH A330
A340
For descent:
EO
M.82/300 KT.……………………….SET AND PULL
EO LRC CEILING ALT…………....SET AND PULL
FMA:

A/THR…………………..………………..………….ON
FMA:
Clearing EO on the MCDU is an irreversible action that will

lead to
 Confirm the EO LRC the loss
Ceiling of single
using  EO(discrepancy
QRH: engine computation CLR Prompt
between computation and real aircraft status).
QRH A330
A340
DAMAGE OR NO DAMAGE ?
CONSIDER ENGINE DAMAGE IF YOU NOTICE:
 Loud noise, explosion
 Abnormal engine indications on ECAM (such as N1 or N2 ~ 0)
Descent from LR CRZ ceiling (A330)
to landing computations
(A340)
Remaining distance to diversion airport

Fuel used in LRC FL Down to Landing
Time in LRC FL Down to Landing
Diversion Airport
LEVEL CHANGE
PF FCU ALTITUDE SELECTION PNF
CONSEQUENCES
LR
A/C at more than 200 NM from DEST
A/C at less than 200 NM from DEST

FMA
DESTINATION DESTINATION
Current CRZ FL
FCU FL selected above
CRZ FL
CRZ FLDESCENT New FCU FL
changes to
Phase has to be under changes to
the new the new
FCU FL selected below FCU FLActivation REC MAX alt
FCU FL
Page
Page Page
Current CRZ FL
ENGINE FAILURE IN CRUISE (Obstacle strategy)
Descent to Descent to
Drift Down Ceiling Long Range Cruise Ceiling
DETECTION CONTINUE
STOP ECAM
ECAM WHEN OBSTACLES
ECAM
ACTIONS ARE CLEARED
DECISION
STRATEGY ?
A330
ENGINE
FAILURE LAND ASAP
A340
DRIFT DOWN CEILING
LRC CEILING
OBSTACLES
REV11
PF ENG 1 FAIL PNF
DETECTION
FLY THE AIRCRAFT
THRUST LEVERS……………………………….MCT
A/THR……………………………………………..OFF
ECAM ACTIONS
ECAM PROCEDURE
STOP ECAM actions when:
PF
COMMUNICATE
And Or
Deceleration NOT below Green Dot

PF OBSTACLE STRATEGY PNF
For descent:
GREEN DOT……………………….SET AND PULL
DRIFT DOWN CEILING ALT…….SET AND PULL
FMA:
During descent to Drift Down Ceiling ...

 EO CLR Prompt
 Thrust MCT
Check GREEN DOT GROSS CEILING
QRH A330
A340
PF ECAM ACTIONS PNF
ECAM ACTIONS
SYSTEM DISPLAY QRH
STATUS ENG RELIGHT
STATUS, or
WEATHER
WEATHER
SUMMARY
LDG
LDGDIST
DIST
DECISION
OPERATIONAL
OPERATIONAL AND
AND
COMMERCIAL
COMMERCIAL
CONSIDERATIONS
CONSIDERATIONS
ATC
ATC
DECISION
DECISION PURSER
PURSER // PAX
PAX
NOTIFY
NOTIFY OPS
OPS …
…
 Consider APU Start  DIST & FUEL computations to Landing

FCOM
APU normal flight envelope:
FCOM
OR
QRH
• •
•••• •••• •
PF WHEN OBSTACLES ARE CLEARED PNF
EO
When obstacles are cleared:
EO LR CEILING ALT……………...….….SET AND PULL
QRH FCOM FCOM PER-OEI-CRT

QRH FPE-OEI CRUISE
LONG RANGE CRUISE LONG RANGE
EO LR CRZ SPEED…………………….CHECK AND SET or CRUISE
SPEED
FMA:
A/THR…………………..………………..………….ON
FMA:
Reaching LRC ceiling:
FMA:
SPEED….……………………………...MANAGED
END...
ENGINE FAILURE IN CRUISE
STRATEGY (A330) (with damage)
DESCENT TO DESCENT TO
DRIFT DOWN STANDARDLONG RANGE
CEILING CRUISE
DETECTION STOP CONTINUE DIVERSION
ECAM ECAM AND
ECAM
LANDING
ACTIONS
DECISION
OBSTACLE
OBSTACLE
ENGINE
FAILURE
To ensure
STRATEGY the margins over obstacles
A330
LAND ASAP
A340
FIXED
DRIFT DOWN SPEED
CEILING
As established before
dispatch, use:
ETOPS constraint
M.82
LRC / 330
CEILING KT
Or
M.82 / 310 KT
OBSTACLES
ENGINE FAILURE IN CRUISE
STRATEGY (A340) (with damage)
DESCENT TO DESCENT TO
DRIFT DOWN STANDARDLONG RANGE
CEILING CRUISE

DETECTION STOP CONTINUE DIVERSION
ECAM ECAM AND
ECAM
LANDING
ACTIONS
DECISION
OBSTACLE
OBSTACLE
ENGINE
FAILURE
To ensure
STRATEGY the margins over obstacles
A330
LAND ASAP
A340
DRIFT DOWN CEILING
LRC CEILING
OBSTACLES
REV10
DAMAGE OR NO DAMAGE ?
CONSIDER ENGINE DAMAGE IF YOU NOTICE:
 Loud noise, explosion
 Abnormal engine indications on ECAM (such as N1 or N2 ~ 0)
LEVEL CHANGE
CONSEQUENCES
LR

FMA
Current CRZ FL
CRZ FL
changes to
the new the new
FCU FL
Page
Page Page
Current CRZ FL
LEVEL CHANGE
CONSEQUENCES
LR

FMA
Current CRZ FL
CRZ FL
changes to
the new the new
FCU FL
Page
Page Page
Current CRZ FL
LAST CHANGE
01 JULY 2012 -
REV10
MAIN SLIDE
DETAILED SLIDES
RECOMMENDATIONS
RISK SYMBOLS

PDP Abnormal Procedures

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A330/340 AFR-TR-334-B-BAP-2a-1503

Rédacteur Hervé GALY

EMERGENCY ELEC EMER

G+B DUAL HYD REJECTED TO

WINDSHEAR EGPWS TCAS

UNERELIABLE STALL TWO ENGINES ALL ENGINES

DUAL FM TOTAL LOSS LOW ENERGIE

FLAPS LOCKED SLATS FAULT

EIS DUAL RADIO FLIGHT CREW

ENG FAILURE ENG FAILURE

REV11 MAR 2014 A330/A340 FAMILY PDP

REV11 MAR 2014 A330/A340 FAMILY PDP

First pilot who notices an ADVISORY:

ANNOUNCE………………………………..”ADVISORY ON “TITLE” system”

First pilot who notices MASTER WARNING / MASTER CAUTION:

FLY THE AIRCRAFT

 CONSIDER AUTOMATION USE: A/THR, AP

NO ACTION until 400ft AGL , with safe flight path established.

If a SYSTEM page is displayed on the ECAM SD page:

SYSTEM PAGE DISPLAYED……….ANALYSE

This is to be repeated for each failure displayed on the ECAM SD page.

ANNOUNCE…………”ECAM ACTIONS COMPLETE”

Return to normal task sharing:

 Review FCOM procedure if time permits:

STATUS……………….………….RECALL AND ANALYSE

INCREASED FUEL CONSUMP…………….. EVALUATE

Check weather reports and airfield data at any considered airports:

WEATHER AND LANDING INFORMATION.................OBTAIN

When requested by ECAM:

LANDING DISTANCE PROCEDURE …...…..….……APPLY

 Use the FMS for situation assessment:

Taking into account:

Operational & Commercial

ECAM ACTIONS COMPLETED

First pilot who notices an ADVISORY:

ANNOUNCE………………………………..”ADVISORY ON “TITLE” system”

First pilot who notices MASTER WARNING / MASTER CAUTION:

 CONSIDER AUTOMATION USE: A/THR, AP

NO ACTION until 400ft AGL , with safe flight path established.

COMMUNICATE ECAM……..CONFIRM using SD page and OVHD panel

ECAM ACTIONS / OEB…………...………PERFORM

This is to be repeated for each failure displayed on the EWD:

AMBER LAND ASAPActions

consider the selection of a suitable airport.

ANNOUNCE……………ECAM ACTIONS COMPLETE

RETURN TO NORMAL TASK SHARING

 Review FCOM procedure if time permits:

COMMUNICATE ECAM……..CONFIRM using SD page and OVHD panel

ECAM ACTIONS / OEB…………...………PERFORM

corrections to apply for landing

When the STATUS page mentions:

 Refer to the QRH FPE-FPF.

• FMS TRIP FUEL= FOB – FMS EFOB at DEST

• If only one Fuel Penalty Factor (FPF) is applicable:

• If two or more Fuel Penalty Factor (FPF) are applicable:

• The flight crew must manually calculate the Fuel Predictions to

 Refer to QRH FPE-IFL.

 A diversion or other event could lead to a landing performance confirmation, especially

 Consider any fuel consumption increment. (refer to QRH FPE-FPF).