A346QRH

340-600QRH/GEN.PM6/2

A340-600REV 19SEQ 001

GENERAL 0.00

VI6 ALLVIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002

IMPORTANT

SCOPE

The QRH contains some specific procedures which are not displayed on ECAM.As a general rule, procedures displayed on the ECAM are not provided in the QRH(refer to FCOM 3.02).

TASK SHARING FOR ABN/EMER PROC

For all abnormal/emergency procedures the task sharing is as follows:-

PF - Pilot Flying - responsible for:-

Thrust levers Flight path and airspeed control Aircraft configuration (Request configuration change) Navigation Communications

PNF - Pilot Non-Flying - responsible for:-

ECAM or checklist reading Execution of required actions on PF request Engine master switches, ENG FIRE pb (with consent of PF)

ECAM CLEAR

DO NOT CLEAR ECAM WITHOUT CROSS-CONFIRMATION OF BOTH PILOTS.

ABN/EMER PROC INITIATION

Procedures are initiated on pilot flying command.

No action will be taken (apart from audio warning cancel through MASTER WARNlight) until:-

The appropriate flight path is established and, The aircraft is at least 400 feet above the runway, if a failure occurs during takeoff,

approach, or go-around.(In some emergency cases, provided the appropriate flight path is established, thepilot flying may initiate actions before this height).

NORMAL CHECKLIST

The Before Start, After Start, Parking and Securing Aircraft checklists will beinitiated by the CM1 and read by the CM2. Other Normal checklists are initiatedby the PF and read by the PNF.

The Before T.O. checks, below the line, and after landing checks, when requested,should be actioned silently by the PNF as listed in the FCOM 3, SOPs. Aftercompletion of the actions, the Table or QRH checklist should be read aloudconfirming the actions and the appropriate "........ checklist complete" announced bythe PNF.The appropriate crew member shall respond after having checked the existingconfiguration. When both pilots have to respond, "BOTH" is indicated.The sign or indicates the specific VIRGIN ATLANTIC AIRWAYS requirements.

R

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346/QRH/GEN.PM6/3

REV 23SEQ 001

GENERALA340-600 0.00A USE OF SUMMARIES

GENERAL

In case of an electrical emergency configuration, or a dual hydraulic failure:The ECAM should be applied first.This includes both the procedure, and the STATUS section.

Only after announcing "ECAM ACTIONS COMPLETED", should the PNF refer to thecorresponding QRH summary.

When the failure occurs, and after performing the ECAM actions, the PNF shouldrefer to the "CRUISE" portion of the summary, in order to determine the landingdistance coefficient.Since normal landing distances are also given on this page, the PNF will be able tocompute the landing distance taking failure(s) into account, in order for the pilot todecide whether to divert or not.

APPROACH PREPARATION

As always, approach preparation includes a review of the ECAM STATUS.After reviewing the STATUS, the PNF should refer to the "CRUISE" portion of thesummary, to determine the VREF correction, and compute the VAPP.

A VREF table is provided in the summary, for failure cases leading to the loss of theMCDU.

The LANDING and GO-AROUND portions of the summary should be used for theapproach briefing.

APPROACH

The APPR PROC actions should be performed by reading the APPROACH portionof the summary.

The PNF should then review the ECAM STATUS, and check that all the APPRPROC actions have been completed.

VI6 ALL

346QRH-ch0.PM6/4

A340-600 AWOPS / AUTOLAND 0.00BREV 00SEQ VAASUMMARY

NB: This is a summary of the A340 AWOPS procedures to be used when Low VisibilityOperations are announced - for the full text please refer to the the FCOM and Ops Manual.

LOW VISIBILITY TAKE-OFF

1. Return Alternate required within 2 hours, Cat 1 or above.2. Check H.I. edge and C/L lighting available.3. Check threshold and R/W end lighting available.4. Check T/O minima.5. All relevant RVR's at or above minima.6. Maximum crosswind 10 kts.7. TOGA thrust to be used.8. Verify ILS tuned on RAD NAV page (LS pb ON).

9. Check lights visible 9/5 for spacing 15 m / 30 m with RVR 125 m.

RTO

- Max autobrake.- Maintain C/L.- Call ATC.- 900 m to go : C/L lights to alternating red/white.- 300 m to go : C/L lights on red.

LANDING IN CAT 2/3

1. A/C autoland operative. Check Tech Log and QRH page.2. Airfield equipment to Cat 2/3 standard (FCOM 2 + NOTAMS/ATIS).3. (a) Both pilots to hold valid LVO certificates.

(b) Capt. as PF.4. Confirm runway approved for autoland (No Cat 3B on L status runways).5. Minima checked.6. Two alternates required Cat 1 and above.7. Extra fuel for holding/approach delays (normally > 45 mins).8. Autoland wind limits (30 kt HWC, 10 kt TWC, 20 kt XWC).9. Use config "full" (config 3 - one engine inoperative).

10. Approach briefing to include:(a) Callouts on approach.(b) Different PF/PNF duties.(c) R/W and approach lighting expected.(d) Visual cues at DH.(e) Procedures for Rollout, R/W clearance and taxi.( f) GA procedure.(g) Alternates and fuel state.(h) Seat position.(j) Aircraft external lighting.(k) Autobrake 3 unless runway length or surface conditions warrant 4.

APPROACH

- APPR selected - select second A/P, check category.- TD or mid-point RVR below minima - continue to OM or equivalent.

VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006

346QRH-ch0.PM6/5

A340-600


AWOPS / AUTOLAND 0.00COM OR EQUIVALENT- RVR's must be at or above minima.- MID PT RVR may be substituted if T/D RVR is not available.- STOP END RVR is advisory.

1000' AAL- PNF calls "1000 ft G/A ALT set".-PF calls "Check".

500' RADIO- PNF calls "500 feet radio".-PF calls "Check".

350' RADIO / LAND GREEN ANNUNCIATED- PF and PNF check ILS course on PFD- PNF calls "LAND green".-PF calls "Course checked".

DH + 100'- Autocall - PNF calls "One hundread above"- PF responds "Check".

DH-Auto Call-PNF calls "Minimum"-PF responds "Landing" or "G/A Flap".

If visual reference lost below DH - Go-Around.

40'RPNF check 'FLARE' annunciated - call "NO FLARE" if not.

10'RAutocall "RETARD". PF closes thrust levers.

GO-AROUNDThrust levers to 'TO GA' - A/P commands G/A.

AFTER LANDINGReport 'runway vacated' when the entire aircraft is clear of CAT 3 protected area.

NON-NORMAL PROCEDURES

- Carry out a GA if following occurs:

Below 1000 ft and 200 ft:

Capability decrease (click, click, click).Amber Caution plus single chime.No 'LAND' green by 350 ft / incorrect RWY course.Engine failure.AP off (cavalry charge).

200ft or below

Red autoland light.

REV 00

SEQ VAA

346QRH-ch0.PM6/6

A340-600 PRM BREAKOUT MANOEUVRE 0.00DREV 00SEQ VAAInitial Actions

PF1) Disengage A/P2) Looking through F/D, turn immediatly towards cleared heading then

initiate climb/descent if or as required.

PNF1) Acknowledge2) Select cleared heading/ALT and pull.

Subsequent actions

When appropriate, clean up as required. eg a standard G/A procedure canbe initiated by PF selecting TOGA then back to CL, then calling G/A Flaps.

CAUTIONS

1) Do not overbank. The necessity to immediately respond is addressed by disconnecting A/P then smoothly applying bank, lookingthrough F/D.

2) Beware of high ROD beyond 1000 fpm in event of descendingbreakout. Consider that ROD will already be approx 800 fpm, ifestablished on G/S.

3) Do not descend below cleared altitude.

Notes

1) It is recommended to initially target the following pitch altitudesClimbing +12 deg.Descending +2 deg. (or current attitude if stablised on G/S.)Then adjust as required.

2) A/THR will maintain SPEED mode. brief accordingly if A/THR U/S.

3) If simultaneous TCAS RA, turn with ATC, climb/descend with TCAS.


346QRH-ch0.PM6/7

A340-600 AWOPS / AUTOLAND 0.00EREV 00SEQ VAA


1 EMERGENCY PROCEDURES

ELEC ELEC EMER CONFIG-SYS REMAINING ................................................ 1.01

ELEC EMER CONFIG Summary ............................................................ 1.03

FIRE SMOKE/FUMES REMOVAL..................................................................... 1.04 SMOKE/FUMES/AVNCS SMOKE ............................................................ 1.05

HYDRAULIC HYD B+Y SYS LO PR Summary ............................................................. 1.07 HYD G+B SYS LO PR Summary ............................................................ 1.08 HYD G+Y SYS LO PR Summary ............................................................ 1.09

LANDING GEAR LOSS OF BRAKING ................................................................................ 1.10

NAVIGATION GPWS/EGPWS ALERTS ....................................................................1.11 TCAS WARNINGS .............................................................................1.12

POWER PLANT ALL-ENGINE FLAMEOUT-FUEL REMAINING ........................................ 1.13 ALL-ENGINE FLAMEOUT-NO FUEL REMAINING ................................. 1.17 TWO ENGINE INOP LANDING ............................................................... 1.20

MISCELLANEOUS DITCHING ............................................................................................... 1.21 FORCED LANDING ................................................................................ 1.23 EMER DESCENT.................................................................................... 1.25 CABIN FIXED OXYGEN SYSTEM............................................................ 1.26 ON GROUND EMER/EVACUATION ....................................................... 7.01

2 ABNORMAL PROCEDURES

AUTO FLT LOSS OF FMS DATA IN DESCENT/APPROACH

(SEVERE RESET) ................................................................................ 2.00B MCDU FAILURE ..................................................................................... 2.01

EQUIPMENT COCKPIT DOOR FAULT ........................................................................ 2.01

F/CTL RUDDER JAM/RUDDER PEDAL JAM .................................................... 2.02 RUDDER TRIM RUNAWAY .................................................................... 2.03 LDG WITH FLAPS/SLATS JAMMED ...................................................... 2.05 NO FLAPS NO SLATS LANDING.......................................................... 2.06A LOW ENERGY WARNING ...................................................................... 2.06

FUEL FUEL LEAK ............................................................................................. 2.07 GRAVITY FUEL FEEDING .................................................................... 2.08A WING TK IMBALANCE ............................................................................ 2.08 FUEL JETTISON ..................................................................................... 2.09 TRIM TANK FUEL UNUSABLE ............................................................... 2.10 FUEL LO TEMP..................................................................................... 2.10A

continued/ICE AND RAIN PROTECTION

346QRH-ch0.PM6/8

2 ABNORMAL PROCEDURES (continued)

ICE AND RAIN PROTECTION DOUBLE STAT (AOA) HEAT FAILURE ................................................... 2.11

INDICATING/RECORDING DISPLAY UNIT FAILURE ........................................................................ 2.11 ECAM SINGLE DISPLAY ........................................................................ 2.11 TAILSTRIKE .......................................................................................... 2.11A DISPLAY DISCREPANCY ....................................................................... 2.12

LANDING GEAR L/G GRAVITY EXTENSION ..................................................................... 2.13 LDG WITH ABNORMAL CENTER L/G .................................................... 2.14 LDG WITH ABNORMAL NOSE/MAIN L/G ............................................... 2.15 RESIDUAL BRAKING PROC .................................................................. 2.17

NAV FM/GPS POS DISAGREE ............................................................................... 2.18 ADR 1+2+3 FAULT ................................................................................. 2.19 ADR DISAGREE ..................................................................................... 2.20 ADR CHECK PROC ........................................................................................ 2.20A UNRELIABLE SPEED INDICATION ....................................................... 2.21 IR ALIGNMENT IN ATT MODE ................................................................ 2.24

POWER PLANT ENG RELIGHT IN FLIGHT ...................................................................... 2.26 ENG STALL ............................................................................................. 2.27 HIGH ENGINE VIBRATION ..................................................................... 2.28 ENGINE TAILPIPE FIRE ......................................................................... 2.28

MISCELLANEOUS OVERWEIGHT LANDING ...................................................................... 2.29 COCKPIT WINDSHIELD/WINDOW CRACKED ..................................... 2.30 COCKPIT WINDSHIELD/WINDOW ARCING ......................................... 2.30 VOLCANIC ASH ENCOUNTER .............................................................. 2.30 BOMB ON BOARD .................................................................................. 2.31 RESET OF COMPUTERS ....................................................................... 2.35 ECAM ADVISORY CONDITIONS ............................................................ 2.38 VAPP DETERMINATION ............................................................................ 2.40 LDG CONF/APP SPD/LDG DIST FOLLOWING FAILURES ................... 2.41

3 NORMAL PROCEDURES

SAFETY EXTERIOR INSPECTION ......................................................... 3.01 PRELIMINARY COCKPIT PREPARATION ............................................ 3.01 AFTER LANDING .................................................................................... 3.02 PARKING ................................................................................................ 3.02 SECURING THE AIRCRAFT .................................................................. 3.02

continued/4


A340-600 QRH INDEX 0.00FREV 00SEQ VAA

346QRH-ch0.PM6/9VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006

A340-600 QRH INDEX 0.00GREV 00SEQ VAA4 IN-FLIGHT PERFORMANCE

SPEEDS ................................................................................................. 4.01 LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3 ..................... 4.02 LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL .............. 4.03 AUTOLAND LANDING DISTANCE WITH AUTOBRAKE ......................... 4.04 ENG OUT

MAX ALTITUDE (ONE or TWO or THREE ENGINES OUT) .................... 4.05GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED ................. 4.06LONG RANGE CRUISE .......................................................................... 4.07IN CRUISE QUICK CHECK .................................................................... 4.08

ALL ENGINES:CLIMB CEILING ...................................................................................... 4.09MAX/OPT ALTITUDE ............................................................................... 4.10IN CRUISE QUICK CHECK ................................................................... 4.11COST INDEX .......................................................................................... 4.12DESCENT .............................................................................................. 4.13DIVERSION............................................................................................ 4.14

FLIGHT WITHOUT CAB PRESS ............................................................. 4.15 GROUND DISTANCE/AIR DISTANCE CONVERSION........................... 4.16 IAS MACH CONVERSION ....................................................................... 4.17

5 OPS DATA

SEVERE TURBULENCE ........................................................................ 5.01 HYD ARCHITECTURE ........................................................................... 5.02 FLT CTL ARCHITECTURE ..................................................................... 5.03 REQUIRED EQUIPMENT FOR CAT 2 AND CAT 3 ................................. 5.04

6 OEB

7 NORMAL CHECKLIST

340-600QRH/CON.PM6/LM

A340-600

VI6 ALL

4 IN-FLIGHT PERFORMANCE

SPEEDS .................................................................................................. 4.01 LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3 ........................ 4.02 LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL ................. 4.03 AUTOLAND LANDING DISTANCE WITH AUTOBRAKE ............................ 4.04 ENG OUT

MAX ALTITUDE (ONE or TWO or THREE ENGINES OUT) ...................... 4.05GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED................... 4.06LONG RANGE CRUISE ............................................................................ 4.07IN CRUISE QUICK CHECK ...................................................................... 4.08

ALL ENGINES:CLIMB CEILING ........................................................................................ 4.09MAX/OPT ALTITUDE ................................................................................ 4.10IN CRUISE QUICK CHECK ..................................................................... 4.11COST INDEX ............................................................................................ 4.12DESCENT ............................................................................................... 4.13DIVERSION ............................................................................................. 4.14

FLIGHT WITHOUT CAB PRESS .............................................................. 4.15 GROUND DISTANCE/AIR DISTANCE CONVERSION.............................. 4.16 IAS MACH CONVERSION......................................................................... 4.17

5 OPS DATA

SEVERE TURBULENCE .......................................................................... 5.01 HYD ARCHITECTURE.............................................................................. 5.02 FLT CTL ARCHITECTURE ....................................................................... 5.03 REQUIRED EQUIPMENT FOR CAT 2 AND CAT 3 ................................... 5.04

6 OEB

7 NORMAL CHECKLIST


QRH INDEXVAA

PAGE VS 0.00H

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346QRH-ch1.PM6/1

REV 24SEQ 001 1.00EMERGENCY PROCEDURES

ELEC ELEC EMER CONFIG-SYS REMAINING . . . . . . . . . . . . . . . . 1.01 ELEC EMER CONFIG Summary . . . . . . . . . . . . . . . . . . . . . . 1.03

FIRE SMOKE /FUMES REMOVAL . . . . . . . . . . . . . . . . . . . . . . . . 1.04 SMOKE/FUMES/AVNCS SMOKE . . . . . . . . . . . . . . . . . . . . . 1.05

HYDRAULIC HYD B+Y SYS LO PR Summary . . . . . . . . . . . . . . . . . . . . . . 1.07 HYD G+B SYS LO PR Summary. . . . . . . . . . . . . . . . . . . . . . 1.08 HYD G+Y SYS LO PR Summary. . . . . . . . . . . . . . . . . . . . . . 1.09

LANDING GEAR LOSS OF BRAKING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10

NAVIGATION GPWS/EGPWS ALERTS . . . . . . . . . . . . . . . . . . . . . . . . 1.11 TCAS WARNINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.12

POWER PLANT ALL ENG FLAMEOUT-FUEL REMAINING . . . . . . . . . . . . . . . 1.13 ALL ENG FLAMEOUT-NO FUEL REMAINING . . . . . . . . . . . . 1.17 TWO ENGINES INOP LANDING . . . . . . . . . . . . . . . . . . . . . . 1.20

MISCELLANEOUS DITCHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.21 FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.23 EMER DESCENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.25 CABIN FIXED OXYGEN SYSTEM . . . . . . . . . . . . . . . . . . . . . 1.26 ON GROUND EMER/EVACUATION . . . . . . . . . . . . . . . . . . . 7.01

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A340-600

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VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005

340-600/QRH/S1.PM6/3

PRESS AUTO SYS 1 Norm Norm Norm NormMAN PRESS CTL inop inop inop NormRAM AIR Norm Norm Norm NormPACK VALVE Norm Norm Norm NormAVIONIC VENT OVBD only OVBD only OVBD only OVBD onlyCARGO VENT ISOL valve only inop inop inopMCDU 1 only inop inop 3 onlyFCU 1 only 1 only 1 only 1 onlyVHF 1 Norm Norm Norm NormRMP 1 Norm Norm Norm NormACP (CAPT., F/O) Norm Norm Norm NormCIDS Norm Norm Norm NormINTERPHONE Norm Norm Norm NormCVR Norm inop inop inopLOUDSPEAKER 1 + 2 Norm Norm Norm NormPFD 1 Norm Norm Norm NormECAM upper DU Norm Norm Norm NormDMC 1 or 3 Norm Norm Norm NormSDAC 1, FWC 1 Norm Norm Norm NormECP Norm Norm Norm NormCREW OXY valve ctl Norm inop inop inopPAX OXY Norm Norm Norm NormSLIDES ARM/WARN Norm Norm Norm NormCLOCK Norm Norm Norm NormENG LOOPS A only A only A only A onlyAPU LOOP A only A only A only NormCARGO SMOKE DET 1 only inop inop inopENG FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1APU FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1CARGO FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1APU AUTO EXT. - - - NormPRIM 1 Norm Norm Norm NormSEC 1 Norm Norm Norm NormFCDC Norm inop inop inopSFCC SLATS 1 only * 1 only * 1 only * 1 only *SFCC FLAPS 1 only * inop inop inopPITCH TRIM 1 only inop inop inopRUDD TRIM 1 only **** inop inop inop

AIR CONDPRESSVENT

* Operative when LAND RECOVERY pushbutton is ON.**** RUDDER TRIM is operative, but position indicator is lost on center pedestal.

EMER GEN RUNNING BAT ONLYELEC EMER CONFIGSYS REMAINING

SUPPLIEDBY ENG

HYD PUMPSSUPPLIED

BY RAT IN FLTON GND

(IAS < 50 kt)

AUTO FLT

COM

EIS

EMEREQPT

FLT INS

FIRE

FLTCTL

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REV 19SEQ 100 1.01EMERGENCY PROCEDURESA340-600

340-600QRH/S1.PM6/4

FCMC 1 only Inop Inop 1 only FDC Norm Norm Norm Norm PUMPS PUMP 2 and PUMP 2 inop inop

LT.TK PUMP X FEED Mot 1 only Mot 1 only inop inop LP VALVES Mot 1 only Mot 1 only Mot 1 only Mot 1 only APU, ISOL VALVES Norm Norm Norm Norm APU PUMP Norm Norm Norm Norm APU LP VALVE Norm Norm Norm Norm JETTISON Inop inop inop inopFIRE SOV Norm Norm Norm NormRAT CTL Norm Norm Norm NormENG A. ICE Open Open Open OpenCAPT PITOT Norm Norm Norm NormRAIN REPEL Capt Capt Capt CaptLGCIU 1 only * 1 only * 1 only * 1 only *GRVTY EXT Norm Norm Norm NormIND. PANEL Norm Norm Norm NormAUTO BRK/ANTI SKID inop inop inop inopPARK BRK Norm Norm Norm NormIR 1 and 3 Norm Norm Norm NormIR 2 5 min 5 min 5 min 5 minADR 1 or 3 Norm Norm Norm Norm** VOR or ADF 1 only 1 only 1 only 1 onlyMMR 1 only 1 only 1 only 1 onlyDDRMI Norm Norm Norm NormATC 1 only Inop Inop InopISIS Norm Norm Norm NormCrew Oxy valve ctl Norm inop inop inopPax Oxy Norm Norm Norm NormENG BLEED BMC 1 + 4 BMC 1 + 4 BMC 1 + 4 BMC 1 + 4

inop inop inop inopX BLEED man only man only man only man only

Norm Norm Norm NormSLIDES ARMWARN Norm Norm Norm NormFADEC A only A only A only A onlyIGNITION A only A only A only A onlyREV inop inop inop inopHP VALVE closure Norm Norm Norm Norm

FUEL

* Operative when the LAND RECOVERY pushbutton is ON.** Only VOR1 or ADF1 (as selected on the DDRMI) is available at a time.

If the DDRMI is deactivated, only VOR1 is available on the ND (ADF1 will not be availableindependently of the selection performed on the DDRMI).

*** Shed when LAND RECOVERY ON.*****. All crossfeed valves automatically open.

. If Pump 1 is inoperative, Pump 4 STBY takes over.Remaining pump is lost, when the LAND RECOVERY pushbutton is ON.When supplied by the RAT only, the remaining pump is lost when speed is below 260 knots.

EMER GEN RUNNING BAT ONLYELEC EMER CONFIGSYS REMAINING

SUPPLIEDBY ENG

HYD PUMPSSUPPLIED

BY RAT IN FLTON GND

(IAS < 50 kt)

HYD

ICE &RAIN

L / G

NAV

OXYGEN

PNEU

APU

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REV 22SEQ 200 1.02EMERGENCY PROCEDURESA340-600

DOORS

PWRPLT

***** *****

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346QRH-ch1.PM6/3

EMERGENCY PROCEDURES REV 25SEQ 001 1.05

LAND ASAPAPPLY IMMEDIATELY- VENT EXTRACT . . . . . . . . . . . . . . . . . . . . . . . OVRD PNF- CAB FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF PNF- GALLEYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF PNF- SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON PNF- CKPT/CAB COM . . . . . . . . . . . . . . . . . . ESTABLISH PNF

IF REQUIRED :- CREW OXY MASKS . . . . . . . . . . ON/100%/EMERG BOTH

IF SMOKE SOURCE IMMEDIATELY OBVIOUS,ACCESSIBLE AND EXTINGUISHABLE :

- FAULTY EQUIPT. . . . . . . . . . . . . . . . . . . . . . ISOLATE PNF

IF SMOKE SOURCE NOT IMMEDIATELYISOLATED :

- DIVERSION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE- DESCENT (FL 100/MEA, min obstacle clearance

altitude) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE

At ANY TIME of the procedure, if smoke/fumesbecomes the GREATEST THREAT:- SMOKE/FUMES REMOVAL . . . . . . . . . . . . .CONSIDER- ELEC EMER CONFIG . . . . . . . . . . . . . . . . . .CONSIDER

Refer to the end of the procedure to set ELEC EMERCONFIG.

At ANY TIME of the procedure, if situationbecomes UNMANAGEABLE:- IMMEDIATE LANDING . . . . . . . . . . . . . . . . . .CONSIDER

VI6 ALL VIRGIN ATLANTIC AIRWAYS REVISION 07 / 26 July 2004

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A340-600

SMOKE/FUMES/AVNCS SMOKE

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346QRH-ch1.PM6/4

SMOKE/FUMES/AVNCS SMOKE (CONT'D)


If AIR COND SMOKE SUSPECTED:- APU BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF- VENT EXTRACT . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO- PACK 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

If smoke continues:- PACK 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON- PACK 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

If smoke still continues:- PACK 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON- VENT EXTRACT. . . . . . . . . . . . . . . . . . . . . . . . . OVRD

- SMOKE/FUMES REMOVAL . . . . . . . . . . . . CONSIDER

IF CAB EQUIPMENT SMOKE SUSPECTED :- PAX SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

If smoke continues- EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . .ON- COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . .OFF- SMOKE DISSIPATION . . . . . . . . . . . . . . . . .CHECK- FAULTY EQPT . . . . . . . . . . . . .SEARCH/ISOLATE

If smoke still continues or when faultyequipment confirmed isolated :- COMMERCIAL . . . . . . . . . . . . . . . . . . . . . .NORM- PAX SYSTEM . . . . . . . . . . . . . . . . . . .NORM

- SMOKE/FUMES REMOVAL . . . . . CONSIDER

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346QRH-ch1.PM6/5


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A340-600HYD G + Y SYS LO PR Summary

SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USEMAX SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 305/.82MANEUVER WITH CAREALTN LAW : PROT LOSTFUEL : Increased fuel comsumption LANDING CONF APPROACH SPEED LANDING DIST MULTILY BY DRY WET CONTAIf flaps < 1+F : Use FLAP 2 VAPP = VREF+40 1.65 2.15 2.30If 1+F Flaps < 2 : Use FLAP 2 VAPP = VREF+15 1.40 1.75 1.95If Flaps = 2 : Use FLAP 3 VAPP = VREF+10 1.35 1.70 1.85If 2 < Flaps 3 : Use FLAP 3 VAPP = VREF+10 1.35 1.70 1.85If Flaps > 3 : Use FLAP FULL VAPP = VREF+10 1.35 1.70 1.85

CRU ISE

SLATS SLOW / FLAPS JAMMED CAT 1 ONLY

GPWS SLAT MODE (If Flaps 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

For Slat extension : SPD SEL . . . . . . . . . . . . . . . . . . . . . . . . . . VFE NEXT - 5 KTWhen in landing CONF : DECELERATE TO CALCULATED VAPPL/G GRAVITY EXTENSION :MAX SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 250 KT

346QRH-ch1.PM6/6

LOSS OF BRAKING

EMERGENCY PROCEDURES REV 21SEQ 100

IF AUTOBRAKE IS SELECTED: BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . PRESS

IF NO BRAKING AVAILABLE: REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . RELEASE A/SKID . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . PRESS MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 PSI

IF STILL NO BRAKING PARKING BRAKE . . . . . . . . . . . . . . . . . . SHORT AND

SUCCESSIVE APPLICATION

VIRGIN ATLANTIC AIRWAYS REVISION 03 / 22 May 2003VI6 ALL

1.10A340-600

346QRH-ch1.PM6/7


CAUTIONDuring night or IMC conditions, immediately apply the procedure. Do notdelay reaction for diagnosis.During daylight VMC conditions, with terrain and obstacles clearly in sight,the alert may be considered cautionary. Take positive correction action,until the alert ceases or a safe trajectory is ensured.

"PULL UP" - "TERRAIN TERRAIN PULL UP"- "TERRAIN AHEADPULL UP" - "OBSTACLE AHEAD PULL UP":Simultaneously:

A/P . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF PITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP

Pull up to full backstick and maintain. THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA SPEED BRAKE LEVER . . . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED BANK . . . . . . . . . . . . . . . . . . .WINGS LEVEL TO INITIATE PULL UP THEN ADJUST AS RQRD

When the flight path is safe, and the GPWS warning ceases:Decrease pitch attitude and accelerate.

When speed is above VLS, and vertical speed is positive :Clean up aircraft, as required.

"TERRAIN TERRAIN" - "TOO LOW TERRAIN" :Adjust the flight path, or initiate a go-around.

"TERRAIN AHEAD" - "OBSTACLE AHEAD" - "CAUTIONOBSTACLE":Adjust the flight path. Stop descent. Climb and/or turn, as necessary,based on analysis of all available instruments and information.

"SINK RATE" "DON'T SINK" :Adjust pitch attitude and thrust to silence the alert.

"TOO LOW GEAR" - "TOO LOW FLAPS" :Correct the configuration, or perform a go-around.

"GLIDESLOPE" :Establish the airplane on the glideslope, or switch OFF the G/S modepushbutton, if flight below the glideslope is intentional (non-precisionapproach).

EGPWS ALERT

VIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002

A340-600

VI6 ALL

R

RR

346QRH-ch1.PM6/8

NAV TCAS WARNINGS


1.12

VI6 ALL VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005

A340-600

Traffic Advisory: "TRAFFIC" messages: Do not manoeuvre based on a TA alone. Attempt to see the reported traffic.

Preventive Resolution Advisory: "MONITOR VERTICAL SPEED"messages: Maintain or adjust the vertical speed, as required, to avoid the red area

of the vertical speed scale.

Notify ATC. When "CLEAR OF CONFLICT" is announced:

Resume normal navigation, in accordance with ATC clearance.

Corrective Resolution advisory: All "CLIMB" and "DESCEND" or"MAINTAIN VERTICAL SPEED MAINTAIN" or "ADJUST VERTICALSPEED ADJUST" type messages: Respond promptly and smoothly to an RA. A/P (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF BOTH FDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAdjust the vertical speed, as required, to that indicated on the green areaof the vertical speed scale.NOTE: Avoid excessive manoeuvres while aiming to keep the vertical

speed just outside the red area of the VSI and within the greenarea. If necessary, use the full speed range between V maxand Vmax.

Respect stall, GPWS or windshear warning.

Notify ATC. When "CLEAR OF CONFLICT" is announced:

Resume normal navigation in accordance with ATC clearance. A/P/FD can be re-engaged as desired.

GO-AROUND procedure must be performed when an RA "CLIMB"or "INCREASE CLIMB" is triggered on final approach

NOTE : Resolution Advisories (RA) are inhibited below 900 feet

VI6 ALL

346QRH-ch1.PM6/9



A340-600

VI6 ALL

IF FORCED LANDING ANTICIPATED APPROACH

MIN RAT SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 KTAt a suitable altitude (not below 3000 feet AGL), configure the

aircraft for landing (CONF 1; L/G DOWN) LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT

EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only.

At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

MAX SPEED for GRAVITY EXTENSION . . . . . . . . . . . . . . . .250 KT L/G GRAVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN

Disregard "USE MAN PITCH TRIM" on the PFD, because the stabilizer is frozen in theposition it was at, when the windmilling was insufficient to provide hydraulic power.When L/G downlocked L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . 190 KTAdjust the speed to the Vapp given above. However, to reach the landing field/runway,the approach speed may be adjusted up to 250 knots (max speed with landing gearextended) GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI

AT 1000 FEET AGL CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"

AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF BRAKES ON ACCU ONLYAFTER LANDINGWhen the aircraft has stopped : PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING

If not, switch on the transmitter

ENG ALL ENG FLAMEOUT - FUEL REMAINING Cont'd

346QRH-ch1.PM6/10


1.16

VI6 ALL VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006

A340-600

IF DITCHING ANTICIPATED APPROACH


aircraft for ditching (CONF 1, L/G UP)

LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT


At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK UP APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . .190 KT

AT 1000 FEET AGL CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS" DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON

In case of strong crosswind, ditch face to the wind.In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdownwith approximately 11 degrees of pitch and minimum aircraft vertical speed.

AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAFTER DITCHING ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING


ENG ALL ENG FLAMEOUT- FUEL REMAINING Cont'd

R

R

R

346QRH-ch1.PM6/11

EMERGENCY PROCEDURES REV 25SEQ 104 1.17A340-600

VI6 ALL

This paper procedure is applicable in the case of an all engine flameout, if no fuelremains on board. It includes all the necessary and sufficient ECAM steps and additionalinformation to manage the situation. Therefore, the flight crw should apply this paperprocedure and then, if time permits, clear ECAM warnings and check the ECAM STATUSpage.

RAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAN ON THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE OPTIMUM SPEED . . . . . . . . . . . . . . . . . . . 220 KT/GREEN DOT

Initially, fly 220 knots, because the Captain's PFD does not display the green dot speed.When time permits, check the green dot value in the following table :

GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)Weight At or below FL 200 FL 300 FL 400

(1000 kg) FL 100 280 232 247 260 246 260 224 238 252 245 240 216 230 243 241 220 208 221 234 233 200 200 211 223 221 180 190 199 210 208

At green dot speed, the aircraft can fly up to approximately 3 NM per1000 feet (with no wind).Average rate of descent is approximately 1500 feet/min.

LANDING STRATEGY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DETERMINEDetermine if a runway can be reached, or determine the most appropriate place for aforced landing/ditching.

EMER ELEC POWER if not automatically coupled) . . . . . MAN ON VHF 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .USE

Only VHF1 is always supplied. Notify ATC of the nature of the emergency and stateintentions. If there is no contact with the ATC, transmit a distress message on VHFfrequency 121.5 MHz.

CREW OXY MASKS (Above FL 100) . . . . . . . . . . . . . . . . . . . .ONCabin altitude will increase due to the lack of engine bleed : The EXCESS CAB ALTECAM warning could be triggered. Depending on the situation, to gain gliding distance,the flight crew may disregard the ECAM emergency descent requirement, becausepassengers will be provided with oxygen for a sufficient period of time.

CABIN AND COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE Loose equipment secured Survival equipment prepared Belts and shoulder harnesses locked

SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF USE RUDDER WITH CAREWHEN BELOW FL 150 : RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON

Switch ON the RAM AIR to ensure complete depressurization.

APPROACH PREPARATION BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . .OFFNOTE : Final descent slope, when configured (CONF 1 ; L/G DOWN), will be approximately

650 feet/NM (with no wind),

ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Cont'd

R

346QRH-ch1.PM6/12


1.18


A340-600

IF FORCED LANDING ANTICIPATED APPROACH


aircraft for landing (CONF 1; L/G DOWN) LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT

EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only. MAX SPEED for GRAVITY EXTENSION . . . . . . . . . . . . . . . .250 KT L/G GRAVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN

Disregard "USE MAN PITCH TRIM" on the PFD, because the stabilizer is frozen in theposition it was at, when the windmilling was insufficient to provide hydraulic power.When L/G downlocked L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . 190 KTAdjust the speed to the Vapp given above. However, to reach the landing field/runway,the approach speed may be adjusted up to 250 knots (max speed with landing gearextended) GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI

AT 1000 FEET AGL CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"

AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF BRAKES ON ACCU ONLYAFTER LANDINGWhen the aircraft has stopped : PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING


ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Cont'd

346QRH-ch1.PM6/13

REV 25SEQ 205 1.19

IF DITCHING ANTICIPATED APPROACH


aircraft for ditching (CONF 1, L/G UP)

LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT


L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK UP APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . .190 KT

AT 1000 FEET AGL CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS" DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON


AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAFTER DITCHING ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING


ENG ALL ENG FLAMEOUT-NO FUEL REMAINING Cont'd

VI6 ALL

EMERGENCY PROCEDURESA340-600

R

R

R

R


346QRH-ch1.PM6/14VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005

REV 24SEQ 001

1.20EMERGENCY PROCEDURES

TWO ENGINE INOP LANDING

VI6 ALL

A340-600

GREE

N DO

T

ONE

DOT

BELO

WGS

OR

2000

FT A

BV G

RND

SPD

SEL:

F OR

VLS

*,W

HICH

EVER

IS H

IGHE

R

FLAP

S 2

STAB

ILISE

DFI

NAL A

PPR

FLAP

S 2

STAR

T TIM

E

TURN

ING

BASE

SPD

SEL:

F OR

VLS

*,W

HICH

EVER

IS H

IGHE

R

ABM

THRE

SHOL

DDO

WNW

IND

LEG

SHOR

T FI

NAL

FUEL

JETT

ISON

TIM

E PE

RMIT

TING

COM

MIT

ALT

ITUD

E50

0 Ft A

GL

IN C

ASE

OF 2

ENGI

NES

OUT

ON T

HE S

AME

WIN

G:RE

DUCE

SPD

TO

NORM

Vap

p(B

ASED

ON

MCDU

VLS

) DIS

REGA

RD V

LS O

N PF

D

ACCE

L ALT

ITUD

E15

00 F

t AGL

CAUT

ION:

IF G

EAR

RETR

ACTI

ON IS

NOT

POSS

IBLE

, DO

NOT A

TTEM

PT A

GO-A

ROUN

D AF

TER

LAND

ING

GEAR

EXT

ENSI

ON.

NOTE

:

FOR

2 ENG

INES

OUT

ON

THE

SAM

E W

ING,

VLS

SHOW

N ON

PFD

IS LI

MIT

ED TO

VM

CL-2

. (15

7kts)

FOR

2 ENG

INES

OUT

ON

OPPO

SITE

WIN

GS, T

HE V

LSSH

OWN

ON TH

E PF

D, A

S W

ELL A

S ON

MCD

U, IS

LIMIT

ED TO

VMC

L. (1

32kts

)

FCOM

3/340

6003

0210

.cdr

PNF A

NNOU

NCES

"FIN

AL F

LAP

SETT

ING"

, DU

E TO

NON

STA

NDAR

D CO

NFIG

URAT

ION.

(T

HE S

AME

APPL

IES

TO O

NE E

NGIN

E IN

OP LA

NDIN

G).

FLAP

S 1

PACK

S OF

F (O

R BY

APU

)

SET

GA T

HRUS

TRO

TATE

TO S

RSRE

TRAC

T FL

APS

TO 1+

FL/G

UP

*

FLAP

S 1

PACK

S OF

F (O

R BY

APU

)

L/G: D

OWN

FLAP

S 3 (

OR, A

S IN

STRU

CTED

BY

ECAM

)

LDG

C/L

A/TH

R DI

SCON

NECT

SPD

SEL:

VLS

*

SET

CAT

1MD

A IN

MCD

U

346QRH-ch1.PM6/15

REV 25SEQ 100 1.21

This procdure applies when engines are running. If engines are not running, refer to the QRH"ALL ENGINE FLAME OUT" (with or without fuel remaining) procedures, which has beenamended to include the ditching procedure, when the engines are running.

PREPARATION ATC/TRANSPONDER (if available) . . . . . . . . . . .NOTIFY/AS RQRDNotify ATC of the nature of the emergency encountered, and state intentions. If not in contactwith ATC, select transponder code A7700, or transmit the distress message on :(VHF) 121.5 MHZ or (HF) 2182 KHZ or 8364 KHZ.

CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE Loose equipment secured. Survival equipment prepared. Belts and shoulder harnesses locked.

JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON GPWS SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF GPWS TERR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF LDG ELEV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT 00 BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET

Omit the normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . . .OFFAPPROACH L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP SLATS and FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX AVAIL JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

DITCHING

VI6 ALL


R

346QRH-ch1.PM6/16


1.22


A340-600

AT 1000 FEET AGL CAB PRESS MODE SEL . . . . . . . . . . . . . . . . . . .CHECK AUTO BLEED (ENGs and APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS" DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON


AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAFTER DITCHING ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING


DITCHING (Cont'd)

346QRH-ch1.PM6/17

REV 25SEQ 100 1.23

This procedure applies when engines are running. If engines are not running, refer to theQRH "ALL ENG FLAME OUT" (with or without fuel remaining) procedure, which has beenamended to include the forced landing procedure, when the engines are not running.

PREPARATION ATC/TRANSPONDER (if available) . . . . . . . . . . .NOTIFY/AS RQRDNotify ATC of the nature of the emergency encountered, and state intentions. If not in contactwith ATC, select transponder code A7700, or transmit the distress message on :(VHF) 121.5 MHZ or (HF) 2182 KHZ or 8364 KHZ.

CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE Loose equipment secured. Survival equipment prepared. Belts and shoulder harnesses locked.

JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON GPWS SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF GPWS TERR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF LDG ELEV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT 00 BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET

Omit normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . . .OFFAPPROACH RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN SLATS and FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX AVAIL GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARM JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI

FORCED LANDING

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346QRH-ch1.PM6/18


1.24


A340-600

AT 1000 FEET AGL CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"AT 200 FEET BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"AT TOUCHDOWN ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF BRAKES ON ACCU ONLYAFTER LANDINGWhen the aircraft has stopped : PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING


FORCED LANDING (Cont'd)

346QRH-ch1.PM6/19

EMER DESCENTIMMEDIATE ACTIONS- CREW OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . .ON BOTH

Set the oxygen diluter selector to the N position.NOTE: With the oxygen diluter selector left at 100%, oxygen quantity

may not be sufficient for the entire emergency descent profile.

The recommendation is to descend with the A/P engaged : Turn the ALT selector knob and pull. Turn the HDG selector knob and pull. Adjust target SPD/MACH.

- THRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLE PF If autothrust is engaged, check IDLE on the UPPER ECAM. If not engaged, retard the thrust levers.

- SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FULL PF

WHEN DESCENT ESTABLISHEDEMER DESCENT FL 100, or MEA (whichever is higher)- SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX/APPROPRIATE

CAUTIONDescend at the maximum appropriate speed. If structural damage issuspected, use the flight controls with care and reduce speed as appropriate.

Landing gear may be extended below 21,000 feet. Speed must be reduced to VLO.- SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON- ENG START SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IGN- ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY

IF CAB ALT > 14,000 feet:- PAX OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAN ON

. Confirm passenger oxygen masks released.

Note: Notify the cabin crew, when a safe flight level has been reachedand oxygen mask use can be terminated.



A340-600

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346QRH-ch1.PM6/20

CABIN FIXED OXYGEN SYSTEM

CABIN OXYGEN ENVELOPE

Any emergency descent profile with passengers supplied by chemical oxygen generators must beexecuted below boundary given in the figure.

NOTE: 30 minutes now allowed (JAR's) at FL 140 prior to descent to FL 100.

400

300250200

100

00 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 TIME (MIN)

290

FLIGHTLEVEL

EMERGENCY PROCEDURES 1.26


A340-600

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REV 00SEQ VAA

346QRH-ch2.PM6/1

VI6 MSN 0371-0615

ABNORMAL PROCEDURES REV 25SEQ 402 2.00

CONTENTS


(SEVERE RESET) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.00B MCDU FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.01

EQUIPMENT COCKPIT DOOR FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.01

F/CTL RUDDER JAM/RUDDER PEDAL JAM . . . . . . . . . . . . . . . . . . 2.02 RUDDER TRIM RUNAWAY . . . . . . . . . . . . . . . . . . . . . . . . . . 2.03 LDG WITH FLAPS/SLATS JAMMED . . . . . . . . . . . . . . . . . . 2.05 NO FLAPS NO SLATS LANDING . . . . . . . . . . . . . . . . . . . . . 2.06A LOW ENERGY WARNING . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.06

FUEL GRVTY FUEL FEEDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.07 WING TK IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.07 FUEL LEAK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.08 FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND

TANKS 3 & 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.08B FUEL JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.09 FUEL LOSS REDUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.09 TRIM TANK FUEL UNUSABLE . . . . . . . . . . . . . . . . . . . . . . . 2.10 FUEL LO TEMP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10A

ICE AND RAIN PROTECTION DOUBLE STAT (AOA) HEAT FAILURE. . . . . . . . . . . . . . . . . 2.11

INDICATING/RECORDING DISPLAY UNIT FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11 ECAM SINGLE DISPLAY . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11A TAILSTRIKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11A DISPLAY DISCREPANCY . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.12

LANDING GEAR L/G GRAVITY EXTENSION . . . . . . . . . . . . . . . . . . . . . . . . . 2.13 LDG WITH ABNORMAL CENTER L/G . . . . . . . . . . . . . . . . . 2.14 LDG WITH ABNORMAL NOSE/MAIN L/G . . . . . . . . . . . . . . . 2.15 RESIDUAL BRAKING PROC . . . . . . . . . . . . . . . . . . . . . . . . . 2.17

NAV FM/GPS POS DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . 2.18 ADR 1+2+3 FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.19 ADR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20 ADR CHECK PROC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20A UNRELIABLE SPEED INDICATION . . . . . . . . . . . . . . . . . . . 2.21 IR ALIGNMENT IN ATT MOD . . . . . . . . . . . . . . . . . . . . . . . . 2.24

A340-600

RRR

R

VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005

R

346QRH-ch2.PM6/3

VI6 MSN 0622-0765


CONTENTS


(SEVERE RESET) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.00B MCDU FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.01

EQUIPMENT COCKPIT DOOR FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.01

F/CTL RUDDER JAM/RUDDER PEDAL JAM . . . . . . . . . . . . . . . . . . 2.02 RUDDER TRIM RUNAWAY . . . . . . . . . . . . . . . . . . . . . . . . . . 2.03 LDG WITH FLAPS/SLATS JAMMED . . . . . . . . . . . . . . . . . . 2.05 NO FLAPS NO SLATS LANDING . . . . . . . . . . . . . . . . . . . . . 2.06A LOW ENERGY WARNING . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.06

FUEL GRVTY FUEL FEEDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.07 WING TK IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.07 FUEL LEAK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.08 FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND

TANKS 3 & 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.08B FUEL JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.09 FUEL LOSS REDUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.09 TRIM TANK FUEL UNUSABLE . . . . . . . . . . . . . . . . . . . . . . . 2.10 FUEL LO TEMP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10A

ICE AND RAIN PROTECTION DOUBLE STAT (AOA) HEAT FAILURE. . . . . . . . . . . . . . . . . 2.11

INDICATING/RECORDING DISPLAY UNIT FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11 ECAM SINGLE DISPLAY . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11A TAILSTRIKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.11A DISPLAY DISCREPANCY . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.12

LANDING GEAR L/G GRAVITY EXTENSION . . . . . . . . . . . . . . . . . . . . . . . . . 2.13 LDG WITH ABNORMAL CENTER L/G . . . . . . . . . . . . . . . . . 2.14

NAV FM/GPS POS DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . 2.18 ADR 1+2+3 FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.19 ADR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20 ADR CHECK PROC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20A UNRELIABLE SPEED INDICATION . . . . . . . . . . . . . . . . . . . 2.21 IR ALIGNMENT IN ATT MOD . . . . . . . . . . . . . . . . . . . . . . . . 2.24

A340-600

RRR

R

VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005

R

346QRH-ch2.PM6/5

ABNORMAL PROCEDURES REV 25SEQ 100 2.00A

POWER PLANT ENG RELIGHT IN FLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . 2.26 ENG STALL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.27 HIGH ENGINE VIBRATION . . . . . . . . . . . . . . . . . . . . . . . . . . 2.28 ENG TAILPIPE FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.28

MISCELLANEOUS OVERWEIGHT LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.29 COCKPIT WINDSHIELD/WINDOW CRACKED . . . . . . . . . . . 2.30 COCKPIT WINDSHIELD/WINDOW ARCING . . . . . . . . . . . . . 2.30 VOLCANIC ASH ENCOUNTER . . . . . . . . . . . . . . . . . . . . . . . 2.30 BOMB ON BOARD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.31 RESET OF COMPUTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.35 ECAM ADVISORY CONDITIONS . . . . . . . . . . . . . . . . . . . . . 2.38 VAPP DETERMINATION . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.40 LDG CONF/APP SPD/LDG DIST FOLLOWING FAILURES. . 2.41

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A340-600

R

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340-600QRH/S2.PM6/5

MCDU 1 (2) (3) FAILURE

ABNORMAL PROCEDURES REV 22SEQ 102 2.01A340-600

BRT KNOB (on affected MCDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMCDU 3 automatically replaces MCDU 1 or 2.

COCKPIT DOOR FAULTThis procedure should be applied, if the Cockpit Door Locking System (CDLS) fails. This Failureis indicated when the FAULT light on the center pedestal's CKPT DOOR panel comes on.

CKPT DOOR CONT PANEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThis panel is located on the overhead panel. It is used to identify the faulty CDLS item, and toverify the status of the pressure sensors and the three electrical latches (referred to as strikes).

If two or more electrical latches (strikes) are faulty :The cockpit door is not intrusion-proof.

If two pressure sensors are faulty :Automatic latch release is unavailable, in case of cockpit decompression.

If no LED on the CKPT DOOR CONT panel is on :The CDLS control unit is faulty; therefore, the cockpit door might unlock automatically. Ifit does not, consider using the mechanical override system to unlock the door.

NOTE: In case of a DC BUS 2 fault, no FAULT indication appears on the center pedestal's CKPTDOOR panel. The CDLS is not electrically-supplied, and is inoperative.

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340-600QRH/S2.PM6/6

A340-600REV 23SEQ 102 2.02ABNORMAL PROCEDURES

F / CTL RUDDER JAM/RUDDER PEDAL JAMRudder jam :In case of a rudder jam, the rudder pedals are not jammed. If the rudder is jameed in the 0 position :

The RUDDER FAULT ECAM warning will automatically be triggered. Refer to thisprocedure.

If the rudder is jammed in a position other than 0 :Unusual pedal movement or position, which corresponds to the computed rudder trimvalue, may indicate a rudder jam.AP can be used. However, automatic landing is not authorized.When engaged, the autopilot introduces rudder trim, and so, pedal deflection.When the rudder trim reaches 25, the indication is dashed on the RUDDER TRIM panel.At autopilot disengagement, this pedal deflection remains.Use the ECAM F/CTL page for a visual check of the rudder position.

BEFORE FINAL APPROACH

AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGE RUDDER TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET

Rudder pedal jam :The rudder operates normally, and automatic landing is recommended.If an autoland is performed, do not apply the following approach procedure.

FOR APPROACH

AVOID LANDING WITH CROSSWIND from the side where the rudder isdeflected.

FOR LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE FLAP 2 GPWS FLAP MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF SPEED and TRAJECTORY . . . . . . . . . . . . . . . . . . STABILIZE ASAP LDG DIST PROC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY

Multiply the landing distance by 1.1 on dry runway or by 1.15 on wet or contaminatedrunway.

ON GROUND

DIFFERENTIAL BRAKING . . . . . . . . . . . . . . . . . . . . . . . USE ASAPDo not use asymmetrical thrust reverse.Use nosewheel steering handle below 100 knots.

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RR

340-600QRH/S2.PM6/7


F / CTL RUDDER TRIM RUNAWAY LATERAL CONTROL . . . . . . . . . . . . . . . . . . . . USE TO LEVEL WINGS RUDDER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTRALIZE

Check the rudder position on the ECAM F/CTL page.

Note : This failure will be seen mainly as uncommanded roll (induced by yaw). In mostconditions, the aircraft will self stabilize in a steady heading sideslip.For continued flight, either maintain rudder central or leave the aircraft in a steadystabilized heading sideslip, but ensure that all changes between rudder centralizedand steady heading sideslip are made smoothly. As speed is reduced, the RudderTravel Limit may gradually open to allow more rudder to be applied by the trim runaway.

FOR LDG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE NORMAL CONFR

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340-600QRH/S2.PM6/8


LEFT INTENTIONALLY BLANK

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346QRH-ch2.PM6/5

FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND TANKS 3 & 4

Note: DO NOT BALANCE INNER TANKS (1 and 2) + (3 and 4) AT THESAME TIME.

If significant imbalance between Inner Tanks 1 and 2:

X-FEED 1 + 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON STBY 1 (2) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF MAIN 1 (2) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

When tanks are balanced, recover normal configuration by,

MAIN and STBY pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON X-FEEDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSE

If significant imbalance between Inner Tanks 3 and 4:

X-FEED 3 + 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON STBY 3 (4) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF MAIN 3 (4) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

When tanks are balanced, recover normal configuration by,

MAIN and STBY pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON X-FEEDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSE

Note: Do not exceed 2500 kg between inner tanks 1 and 4, 3000 kg betweeninner tanks 2 and 3, in order to avoid the FUEL WING TK IMBALANCEECAM caution to be triggered.

ABNORMAL PROCEDURES REV 00SEQ VAA 2.08BA340-600

VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005VI6 ALL

346QRH-ch2.PM6/9

FUEL JETTISONWARNING

If the jettison procedure is applied following the "FUEL LEAK" or "ENG FAIL"with tank damage procedure, the flight crew must comply with the followingrequirements: If a fuel leak is present, and weight reduction is essential for landing, once

close to the landing airfield, adopt the following procedure for fuel jettison.

It is possible to jettison in any convenient configuration and at any speed.When practicable, the height should be sufficient to avoid contamination onthe ground (5,000 feet is considered adequate).Do not jettison in a thunderstorm.When jettisoning is performed, avoid flying into the jettisoned flow (which isdescending at about 500 ft/min).Average weight reduction (by jettison only) is 1600 kg/min.On the MCDU: FUEL PRED key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT JET GW . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENTER THE FINAL GWOn the OVERHEAD panel: JETTISON ARM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON JETTISON ACTIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ONCAUTION: During jettison operation, monitor the CG. If either the forward

or aft takeoff and landing limit is reached, stop jettison.When jettisoning in clean configuration, do not usespeedbrakes.

When JETTISON is completed, or to manually stop the JETTISONoperation:JETTISON ACTIVE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFJETTISON ARM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Notes: Jettison operation is automatically stopped when:-- Fuel WING TK LO LVL warning threshold is reached.- Actual GW reaches the value inserted in the MCDU.


VIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002

A340-600

VI6 ALL

FUEL LOSS REDUCTIONApply this procedure only if suggested by the FUEL LEAK procedure, and ifthe flight crew needs to minimize the fuel loss. It covers two type of leak :- A leak from wing : a manual Trim tank transfer (via the Center tank) and/or

manual Center tank transfer can be done, to symmetrically transfer thefuel to all inner tanks, and avoid automatic transfer to only the least fullinner tank.

- A leak from the Center tank, or the Trim tank : a manual Trim and/orCenter tank transfer to the inner tanks can be done to save some Trim orCenter tank fuel.

If Center Tank or Trim Tank not empty : CTR TO INR L + R PUMPS . . . . . . . . . . . . . . . . . . . . . . . , . . . . . .ON CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN T TK FEED (if not empty) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO T TK XFR (if not empty) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FWDWhen Trim Tank empty : T TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO T TK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ISOLWhen Center Tank empty : CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO

RRRRRRRRRRRRRRRRRRRR

346QRH-ch2.PM6/10


TRIM TANK FUEL UNUSABLET TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FWDT TK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

If TRIM TANK FUEL still unusable OUTR TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON CTR TO INR L and R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF CTR AFT XFR L and R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMAXIMUM FLIGHT TIME . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 HOURSAfter 4 hours, depending on the fuel distribution, the aft CG limit may bereached.

FOR LANDING

If CG > aft CG limit shown below : APPR SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VLS + 10 KT LDG DIST PROC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLYMultiply the landing distance by 1.20 on dry runway, or 1.20 on wet runway,or 1.20 on contaminated runway.

RR

A340-600

VI6 ALL

346QRH-ch2.PM6/11

ABNORMAL PROCEDURESREV 00 2.10A

FUEL LO TEMPNOTE: Before carrying out this drill refer to the Tech Log to check

on the fuel uplifted and its freezing point. (NB: JET A (Fpoint -40C) is normally only uplifted in USA.

Any fuel temperature below - 40COn ground, before takeoff:

IF JET A FUEL: DELAY T.O

Do not takeoff, until temperatures are within limits.In flight:

If outer tank temp

VI6 MSN 0371-0615

VI6 MSN 0622-0765

346QRH-ch2.PM6/13

A340-600

ECAM SINGLE DISPLAYOnly the EWD is available. No SD on the other DUs.

To call a SYS page: PRESS AND MAINTAIN the SYS page key on the ECP

OVERFLOW ON THE STATUS page: PRESS AND MAINTAIN the SYS key on the ECP

The first page of the STATUS is displayed. RELEASE IT, THEN PRESS IT AGAIN WITHIN 2 SECONDS

The second page of the STATUS is displayed. CONTINUE UNTIL THE OVERFLOW ARROW DISAPPEARS

When the STS key is released for more than 2 seconds, the EWD isdisplayed again.

TAILSTRIKEWhen a tail strike is experienced apply the following procedure

LAND ASAP MAX FL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 100 or MSA

500 feet/minute should be targeted for the climb, to minimise pressurechanges, for passenger and crew comfort. Similarly, the rate of descentmust be limited to about 1000 feet/minute, except for the final approach,that must be performed normally.Notify the ATC of the aircraft's rate of climb.

RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON PACK 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

VI6 ALL VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005

2.11AABNORMAL PROCEDURES REV 25SEQ 100

VI6 ALL

346QRH-ch2.PM6/15


LDG WITH ABNORMAL NOSE/MAIN L/GPREPARATION

CABIN CREW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONSIDER

If NOSE L/G abnormal CG location (if possible) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AFT

. 10 passengers from front to rear moves the CG roughly 2% aft.

If one MAIN L/G abnormal FUEL IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONSIDER

. Open all the fuel crossfeed valves, and switch off the pumps on the side with landing gear normally extended.

OXYGEN CREW SUPPLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PREPARE . Loose equipment secured.

. Survival equipment prepared.

. Belts and shoulder harness locked.

APPROACH

GPWS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF L / G GRVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN L/G LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN AUTOBRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT ARM EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF CABIN REPORT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OBTAIN JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISOL

If one MAIN L/G abnormal GROUND SPOILERS . . . . . . . . . . . . . . . . . . . . . . . . . .DO NOT ARM

APPROACH

RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . . ORDER

R

cont'd

A340-600

VI6 ALL

340-600QRH/S2.PM6/24


LDG WITH ABNORMAL NOSE/MAIN L/G (Cont'd)FLARE, TOUCHDOWN, AND ROLLOUT

Engines should be shut down sufficiently early to ensure fuel is shut off before thenacelles impact, but sufficiently late to ensure adequate hydraulic supplies for the flightcontrols. Hydraulic pressure for flight controls remains available for 30 seconds afterthe shut down of engines 1 and 4.

If NOSE L/G abnormal REVERSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE NOSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN UP

After touchdown, keep the nose off the runway by using the elevator.Then, lower the nose onto the runway before elevator control is lost.

BRAKES (compatible with elevator efficiency) . . . . . . . . . APPLY ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Shut down the engines before nose impact.If one MAIN L/G abnormal REVERSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE ENG MASTERS (in sequence) . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

After main gear touchdown, shut down the outboard engines first, then theinboard engines (failure side first) before nacelle touchdown.

FAILURE SIDE WING . . . . . . . . . . . . . . . . . . . . . . MAINTAIN UPUse roll control, as necessary, to keep the unsupported wing up as long aspossible.

DIRECTIONAL CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN Use rudder and brakes (maximum 1000 psi) to maintain runway axis as long

as possible.

WHEN A/C STOPPED

ENG (all) and APU FIRE pushbutton . . . . . . . . . . . . . . . . . . . . . . PUSHPressing the ENG FIRE pushbutton shuts off the related hydraulic pressurewithin a short time.

ENG (all) and APU AGENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCH

EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE Announce : "PASSENGER EVACUATION" over the PA. All emergency and

passenger doors may be used to evacuate the aircraft. If one main landinggear is not extended, the aircraft will rest on the nose gear and outer engine(s).

R

R


A340-600

VI6 ALL

VI6 MSN 0371-0615

VI6 MSN 0622-0765

VI6 MSN 0371-0615

VI6 MSN 0622-0765

VI6 ALL

346QRH-ch2.PM6/17


ENG 1(2)(3)(4) STALLA stall may be indicated by varying degrees of abnormal engine noises,accompanied by flame from the engine exhaust and possibly from engine inlet insevere cases, fluctuating parameters, sliggish or no thrust lever response, high EGTand/or a rapid EGT rise when thrust lever is advanced. Engine stalls must bereported for maintenance action.

Stall is detected by the FADEC :If on ground :

THR LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE ENG MASTER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . OFFIf the crew detects a stall before the ECAM activation :The following procedure may be applied : THR LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE ENG PARAMETERS (affected engine) . . . . . . . . . . . . . . . . . . . . . CHECK

If abnormal parameters : ENG MASTER (affected engine) . . . . . . . . . . . . . . . . . . . . OFF

ENG 1(2)(3)(4) SHUT DOWNApply ENG SHUT DOWN procedure.Engine restart at crew discretion.

If normal parameters : ENG A ICE (affected engine) . . . . . . . . . . . . . . . . . . . . . . . ON WING A ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONOperation of ENG and WING A ICE will increase the stall margin but EGTwill increase accordingly. THR LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . SLOWLY ADVANCE

if stall does not reoccur : Continue engine operation

cont'd

A340-600

VI6 ALL

346QRH-ch2.PM6/18


HIGH ENGINE VIBRATIONThe ECAM's VIB advisory mainly serves as a guideline to induce the crew to closelymonitor and crosscheck engine parameters.VIB detection alone does not require engine shutdown.NOTE : High engine vibrations may be accompanied by cockpit and cabin

smoke, and /or burning smells. This may be due only to compressorblade tip contact with associated abradable seals.High N1 vibrations are generally accompanied by perceivable airframevibrations.High N2/N3 vibrations can exist without perceivable airframe vibrations.

IF NO ICING CONDITIONS EXIST :ENG PARAMETERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCheck engine parameters and especially EGT ; crosscheck with the otherengines.Report in maintenance log.

If rapid increase above the advisory : THRUST LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . RETARDFlight conditions permitting reduce N1 to maintain the vibration level belowthe advisory threshold.NOTE : If the VIB indication does not decrease following thrust reduction,

this may indicate other engine problems. Apply the applicableprocedure.

IF NO ICING CONDITIONS EXIST :An increase of N1 vibration in icing conditions, with or without engine anti-ice,may be due to fan blades and /or spinner icing. A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF ENGINE ANTI ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKIf still OFF, ENG ANTI ICE should be switched ON at idle fan speed, one engineafter the other, at an approximate interval of 30 seconds. THRUST (one engine at a time). . . . . . . . . . . . . . . . . . . . . . . . INCREASEIncrease thrust with the power setting compatible with the flight phase. The VIBlevel will return to normal after ice shedding, despite a light increase duringacceleration.Resume normal operation.NOTE : If possible, shut down the engine after landing, for taxiing, when

vibrations above the advisory level have been experienced duringthe flight.

RR


A340-600

VI6 ALL

346QRH-ch2.PM6/19

ABNORMAL PROCEDURES REV 00SEQ VAA 2.28AA340-600


ENG TAILPIPE FIREInternal engine fire may be encountered during engine start, or engine shutdown.It may be seen by the groun

A346QRH

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