a340-600 quick reference handbook - aviation for · pdf filewhen the failure occurs, and after...

340-600QRH/GEN.PM6/2

A340-600REV 19

SEQ 001GENERAL 0.00

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VIRGIN 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

R

RRRRR

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.

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346QRH-ch0.PM6/4

A340-600 AWOPS / AUTOLAND 0.00BREV 00

SEQ VAA

SUMMARY

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 0.00C

OM 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 00

SEQ VAA

Initial 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 00

SEQ 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 00

SEQ VAA

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

A340-600 QRH INDEX 0.00GREV 00

SEQ VAA

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

340-600QRH/CON.PM6/LM

A340-600

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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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RRR

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 Norm

MAN PRESS CTL inop inop inop Norm

RAM AIR Norm Norm Norm Norm

PACK VALVE Norm Norm Norm Norm

AVIONIC VENT OVBD only OVBD only OVBD only OVBD only

CARGO VENT ISOL valve only inop inop inop

MCDU 1 only inop inop 3 only

FCU 1 only 1 only 1 only 1 only

VHF 1 Norm Norm Norm Norm

RMP 1 Norm Norm Norm Norm

ACP (CAPT., F/O) Norm Norm Norm Norm

CIDS Norm Norm Norm Norm

INTERPHONE Norm Norm Norm Norm

CVR Norm inop inop inop

LOUDSPEAKER 1 + 2 Norm Norm Norm Norm

PFD 1 Norm Norm Norm Norm

ECAM upper DU Norm Norm Norm Norm

DMC 1 or 3 Norm Norm Norm Norm

SDAC 1, FWC 1 Norm Norm Norm Norm

ECP Norm Norm Norm Norm

CREW OXY valve ctl Norm inop inop inop

PAX OXY Norm Norm Norm Norm

SLIDES ARM/WARN Norm Norm Norm Norm

CLOCK Norm Norm Norm Norm

ENG LOOPS A only A only A only A only

APU LOOP A only A only A only Norm

CARGO SMOKE DET 1 only inop inop inop

ENG FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1

APU FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1

CARGO FIRE EXT. Bottle 1 Bottle 1 Bottle 1 Bottle 1

APU AUTO EXT. - - - Norm

PRIM 1 Norm Norm Norm Norm

SEC 1 Norm Norm Norm Norm

FCDC Norm inop inop inop

SFCC SLATS 1 only * 1 only * 1 only * 1 only *

SFCC FLAPS 1 only * inop inop inop

PITCH TRIM 1 only inop inop inop

RUDD 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 PUMPS

SUPPLIEDBY RAT

IN FLT ON 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 inopLT.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 inop

FIRE SOV Norm Norm Norm Norm

RAT CTL Norm Norm Norm Norm

ENG A. ICE Open Open Open Open

CAPT PITOT Norm Norm Norm Norm

RAIN REPEL Capt Capt Capt Capt

LGCIU 1 only * 1 only * 1 only * 1 only *

GRVTY EXT Norm Norm Norm Norm

IND. PANEL Norm Norm Norm Norm

AUTO BRK/ANTI SKID inop inop inop inop

PARK BRK Norm Norm Norm Norm

IR 1 and 3 Norm Norm Norm Norm

IR 2 5 min 5 min 5 min 5 min

ADR 1 or 3 Norm Norm Norm Norm

** VOR or ADF 1 only 1 only 1 only 1 only

MMR 1 only 1 only 1 only 1 only

DDRMI Norm Norm Norm Norm

ATC 1 only Inop Inop Inop

ISIS Norm Norm Norm Norm

Crew Oxy valve ctl Norm inop inop inop

Pax Oxy Norm Norm Norm Norm

ENG BLEED BMC 1 + 4 BMC 1 + 4 BMC 1 + 4 BMC 1 + 4inop inop inop inop

X BLEED man only man only man only man only

Norm Norm Norm Norm

SLIDES ARMWARN Norm Norm Norm Norm

FADEC A only A only A only A only

IGNITION A only A only A only A only

REV inop inop inop inop

HP 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 PUMPS

SUPPLIEDBY RAT

IN FLT ON 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

***** *****

RR

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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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A340-600

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346QRH-ch1.PM6/5


VI6 ALL

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

<APPR

FLARE : Only one ELEV and 2 spoilers per wing.A/C slightly sluggish - Direct law

SPOILERS : Only 2 per wing REVERSERS : Only N° 2

BRAKING : ALTERNATE

NO NOSEWHEEL STEERING

LANDING

NO GEAR RETRACTION. INCREASED FUEL CONSUMPTIONFor circuit : MAINTAIN SLATS/FLAPS CONFIGURATION

Recommended speed : MAX SPD - 10 KT/250 KTFor diversion :

If Flaps at zero : SELECT CLEAN CONFIGURATIONNormal operating speeds (MAX SPD 250 KT)If Flaps not at zero : MAINTAIN SLATS/FLAPS CONFIGRecommended speed : MAX SPD - 10 KT/250 KT

GO

AROUND

ACTUAL LANDING DISTANCES (feet) (for contaminated runways, refer to 4.03)

WEIGHT (1000 KG) 180 205 230 255 280 305 330 355 380DRY runway 3320 3420 3720 4080 4470 4900 5400 6050 6740WET runway 4690 4920 5500 6120 6690 7330 7960 8600 9220

CORRECTIONS + 1000 ft above SL + 10 Kt tailwindDRY runway + 4 % + 16 %WET runway + 23 %

The method for approach speed computation is given in the QRH 2.40.

<

<

RRRRRRR

R

R

R

W (1000 KG)VREF = VLSCONF FULL

180 200 220 240 260 280 300 320 340 360 380132 133 139 146 151 157 163 168 173 178 183132 133 135 142 147 153 159 164 169 174 179

13% CG35% CG

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


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 Vα 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.PM6/14


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

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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

VI6 ALL

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


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

VI6 ALL

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.

VI6 ALL

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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLYMultiply 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTRALIZECheck 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

VI6 ALL

VI6 ALL

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.



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 UNUSABLE

T 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 TEMP

NOTE: Before carrying out this drill refer to the Tech Log to checkon the fuel uplifted and its freezing point. (NB: JET A (Fpoint -40°C) is normally only uplifted in USA.

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

IF JET A FUEL:— DELAY T.O

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

If outer tank temp <-40° C (automatic recall at -47°C)IF JET A FUELMAX SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 305 KT— OUTR TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN

If trim tank temp <-40° C (automatic recall at -47°C)IF JET A FUEL— T TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FWD

Fuel consumption increases by approximately 2%.Note: If the trim tank pumps are failed, this part of the procedure will

be replaced by:WHEN SPD >270KT AND NOT IN CLIMB:— T TK XFR . . . . . . FWD

If inner tank temp <-40° C (automatic recall at -47°C)IF JET A FUEL— CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN

IF NECESSARY:— TAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE

Consider descending to a lower altitude and/or increasing Mach toincrease TAT.

Note: 1. The caution is automatically recalled, when:Any tank temperature is below - 47°C. In this case, " IF JET A" is notdisplayed in the procedure.

2. If a fuel type, other than Jet A is used, see 3.01.28 page 1 for theappropriate limits, and apply the procedure according to those limits.

STATUSAPPR PROC

AT SLATS EXTENSION:— T TK XFR . . . . . . . . . . . . AUTO

Manual trim tank transfer must be stopped at slats'extension, to avoid CG changes during approach.

If both trim tank transfer pumps have failed:LVL OFF FOR MAN FWD XFR


SEQ VAAA340-600

VI6 ALL

VI6 MSN 0371-0615

VI6 MSN 0622-0765

346QRH-ch2.PM6/13

A340-600

ECAM SINGLE DISPLAY

Only 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.

TAILSTRIKE

When a tail strike is experienced apply the following procedureLAND 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 PROCEDURESREV 25

SEQ 100

VI6 ALL

346QRH-ch2.PM6/15


LDG WITH ABNORMAL NOSE/MAIN L/G

PREPARATION

— 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) STALL

A 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) . . . . . . . . . . . . . . . . . . . . . . . . . OFF

If 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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Operation 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 VIBRATION

The 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 FIRE

Internal engine fire may be encountered during engine start, or engine shutdown.It may be seen by the ground crew, or the EGT may fail to decrease after the MASTERswitch is turned off.

CAUTIONExternal fire agents can cause severe corrosive damage and should,therefore, only be considered after having applied the following procedure :

— ENG MASTER (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFNote : Do not press the engine fire pushbutton, since this would cut off the

FADEC power supply, which would prevent motoring sequence.— AIR BLEED PRESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH

. Select the APU, or the opposite ENG BLEED, to motor the engine.

. If APU BLEED is not available, and the other engine is shut down, connect external pneumatic power (if readily available).

— BEACON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONWhen N3 < 30 %— ENG START SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRANK— MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONWhen burning has stopped :— MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF— ENG START SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM

Maintenance action is due.

R

VI6 ALL

VI6 MSN 0371-0449

VI6 MSN 0575-0765

VI6 ALL

340-600QRH/S3.PM6/1

A340-600NORMAL PROCEDURES

SEQ 001

REV 11 3.00

CONTENTS

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

VI6 ALLVIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002

346QRH-ch3.PM6/3

A340-600 NORMAL PROCEDURES REV 24SEQ 200 3.01

CM1 CM2

CM1 CM2

SAFETY EXTERIOR INSPECTION

PRELIMINARY COCKPIT PREP

NOSE WHEEL CHOCK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN PLACEL/G DOORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK POS.APU AREA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

VI6 ALL

EMER EQPTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKENG panel . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . .CHECKL/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWNWIPERS . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFBAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKEXT PWR . . . . . . . . . . . . . . . . . . . . . . . . . .ONBAT . . . . . . . . . . . . . . . . . . . . . . . .CHECK/.AUTOAPU FIRE . . . . . . . . . . . . . . . . . . .CHECK/TESTAPU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .STARTEXT PWR . . . . . .. . . . . . . . . . . . . . . . . . AS RQRDCOCKPIT LT . . . . . . . . . . . . . . . . . . . . .AS RQRDPARKING BRK .. . . . . . . . . . . . . . . . . . . . . . . . . ONACCU/BRAKE PRESS .. . . . . . . . . . . . . . . . . . . . . .CHECKFLAPS . . . . . . . . . . . . . . . . . . . . . . CHECK POSITIONSPEEDBRAKE .. . . . . . . . . . . . . . . .CHECK RETPROBES/WINDOW HEAT . . . . . . . . . . . . . . .AUTOAPU BLEED . . . . . . . . . . .. . . . . . . . . . . . . .ONAIR COND panel . . . . . .. . . . . . . . . . . . . . . .SETELEC panel . . . . . . . . . . . . . . . . . . . . . . . . .CHECKVENT panel . . . . . . . . . . . . . . . . . . . . . . . . .CHECKECAM RECALL .. . . . . . . . . . . . . . . . . . . . . DEPRESSECAM HYD QTY, ENG OIL QTY . . . . . . . . . CHECK


EXT WALK ROUND . . . . . . . . . . . . .PERFORM PNF

SECURITY CHECK

FLIGHT DECK & FLIGHT CREW REST AREA . . . . . . . . . . . . . . PERFORM CM2

ENTER FLIGHT NUMBER IN INIT PAGE 'A'

COMPLETE AND SEND LOAD SHEET PAGE 1

INCLUDING RTOW

(IF ACARS STBY, PERFORM IRS ALIGNMENTFOR SATELLITE COMMUNICATION)

346QRH-ch3.PM6/4

A340-600

ADIRS (1 + 2 + 3) . . . . . . . . . . . . . . . . . . . . . . . .OFFCMS POST FLT REPORT . . . . . . . . . . . . . . . AS RQRDDUs . . . . . . . . . . . . . . . . . . . . . . . . . . . .DIM or OFFTECH LOG . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETED

SECURING THE A/C C/L

CM1 CM2

SECURING THE A/C

FMGS POSTFLIGHT REPORT . . . . . . . . . . . PRINTOXY CREW SUPPLY . . . . . . . . . . . . . . . . . . . . . .OFFEXT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAPU BLEED . . . . . . . . . . . . . . . . . . . . . . . . AS RQRDEXT PWR . . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRDAPU MASTER SW . . . . . . . . . . . . . . . . . . . . AS RQRDEMER EXIT LT . . . . . . . . . . . . . . . . . .. . . . . . . . .OFFNO SMOKING . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFBAT 1 + 2 + APU . . . . . . . . . . . . . . . . . . . . . .AS REQDDU's . . . . . . . . . . . . . . . . . . . . . . . . . . . DIM or OFF

NORMAL PROCEDURES

VI6 ALL

3.02

PF PNF

AFTER LANDING

GRND SPLRS . . . . . . . . . . . . . . . . . . . . . . . . . . .DISARM(signal for PNF to commence after landing items)NOSE LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TAXI

AFTER LDG C/L

RADAR . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF/STBYFLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RETRACTTCAS (as installed) . . . . . . . . . . . . . . . . . . . . . . .STBYENG START sel . . . . . . . . . . . . . . . . . . . . . . . . . .NORMEXT LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . .AS RQRDANTI ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRDAPU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .STARTBRAKES TEMP . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

CM1 CM2

PARKING

PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . .ONAPU BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . .ONENG MASTER 1, 2, 3, 4 . . . . . . . . . . . . . . . . . . . .OFFSLIDE DISARMED . . . . . . . . . . . . . . . . . . . . . . .CHECKBEACON LT . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFEXT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AS RQRDSEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFGROUND CONTACT . . . . . . . . . . . . . . . . . . . ESTABLISHPARKING BRK . . . . . . . . . . . . . . . . . . . . . . .AS RQRDPARKING C/L

ELAPSED TIME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .STOPFUEL PUMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFSTATUS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKIRU DRIFT RATE . . . . . . . . . . . . . . . . . . . . . . . .CHECK


REV 00SEQ VAA

340-600QRH/S4.PM6/1

VI6 ALL

IN FLIGHT PERFORMANCE REV 10

SEQ 001 4.00

CONTENTS

• 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 ENGINESCLIMB CEILING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.09MAX/OPT ALTITUDES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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

A340-600

VI6 ALL

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 ALL

340-600QRH/S5.PM6/1

VI6 ALL

OPS DATA REV 21

SEQ 001 5.00

CONTENTS

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

A340-600

VI6 MSN 0371-0622

VI6 MSN 0639-0765

VI6 ALL

346QRH-appendices.PM6/1

VI6 ALL

SUPPLEMENTARY INFORMATION

CONVERSIONSREV 00SEQ VAA

KPH

259

314

333

390

450

500

593

834

1019

1112

M

30

40

50

60

100

200

KTS

140

170

180

210

243

270

320

450

550

600

FT

100

130

160

200

330

660

AIRSPEED

CLOUD CEILING

M/SECFT/MIN

200

400

600

800

1000

1400

1600

2000

2400

3000

3400

4000

1

2

3

4

5

7

8

10

12

15

17

20

50

60

70

80

90

100

KTS

2

4

6

8

10

14

16

20

24

29

33

39

97

117

136

155

175

195

VERTSPD

WINDSPD

AppendixA


A340-600


VI6 ALL

REV 00SEQ VAA

MM

630

1

2

3

4

5

6

7

8

9

640

1

2

3

4

5

6

7

8

9

650

1

2

3

4

5

6

7

8

9

660

1

2

3

4

5

6

7

8

9

MBS

839.9

841.2

842.6

843.9

845.2

846.6

847.9

849.2

850.5

851.9

853.2

854.5

855.9

857.2

858.5

859.9

861.2

862.5

863.9

865.2

866.5

867.9

869.2

870.5

871.9

873.2

874.5

875.9

877.2

878.5

879.9

881.2

882.5

883.9

885.2

886.5

887.9

889.2

890.5

891.9

MM

670

1

2

3

4

5

6

7

8

9

680

1

2

3

4

5

6

7

8

9

690

1

2

3

4

5

6

7

8

9

700

1

2

3

4

5

6

7

8

9

MBS

893.2

894.5

895.9

897.2

898.5

899.9

901.2

902.5

903.9

905.2

906.5

907.9

909.2

910.5

911.9

913.2

914.5

915.9

917.2

918.5

919.9

921.2

922.5

923.9

925.2

926.6

927.9

929.2

930.5

931.9

933.2

934.5

935.8

937.2

938.5

939.9

941.2

942.5

943.8

945.2

MM

710

1

2

3

4

5

6

7

8

9

720

1

2

3

4

5

6

7

8

9

730

1

2

3

4

5

6

7

8

9

740

1

2

3

4

5

6

7

8

9

MBS

946.5

947.9

949.2

950.5

951.8

953.2

954.5

955.9

957.2

958.5

959.9

961.2

962.5

963.9

965.2

966.5

967.9

969.2

970.5

971.9

973.2

974.5

975.9

977.2

978.5

979.9

981.2

982.5

983.9

985.2

986.5

987.9

989.2

990.5

991.9

993.2

994.5

995.9

997.2

998.5

MM

750

1

2

3

4

5

6

7

8

9

760

1

2

3

4

5

6

7

8

9

770

1

2

3

4

5

6

7

8

9

780

1

2

3

4

5

6

7

8

9

MM

590

1

2

3

4

5

6

7

8

9

600

1

2

3

4

5

6

7

8

9

610

1

2

3

4

5

6

7

8

9

620

1

2

3

4

5

6

7

8

9

MBS

786.6

787.9

789.2

790.6

791.9

793.2

794.6

795.9

797.2

798.6

799.9

801.2

802.6

803.9

805.2

806.6

807.9

809.2

810.6

811.9

813.2

814.6

814.9

817.2

818.6

819.9

821.2

822.6

823.9

825.2

826.6

827.9

829.2

830.6

831.9

833.2

834.6

835.9

837.2

838.6

MBS

999.9

1001.2

1002.5

1003.9

1005.2

1006.5

1007.9

1009.2

1010.5

1011.9

1013.2

1014.5

1015.9

1017.2

1018.5

1019.9

1021.2

1022.5

1023.9

1025.2

1026.5

1027.9

1029.2

1030.5

1031.9

1033.2

1034.5

1035.9

1037.2

1038.5

1039.9

1041.2

1042.5

1043.9

1045.2

1046.5

1047.9

1049.2

1050.5

1051.9


ALTIMETER SETTING CONVERSION

AppendixB


A340-600


VI6 ALL

REV 00SEQ VAA


FREQUENCIES

AppendixC

Virgin Ground Callsign NotesCompany HandlingFreq Freq(MHz) (MHz)

AMS EHAM 131.625 KLM OPS

ANU TAPA 130.050

BGI TBPB 130.200

BOM VABB 131.150 CAMBATA

BOS KBOS 131.250

CPT FACT 129.870

DEL VIDP 131.150 CAMBATA

DUB EIDW 131.500 AER LINGUS

DXB OMDB 131.600

EWR KEWR 131.250

GND TGPY 131.625 Aviation Services of Grenada

HAV MUHA 126.900

HKG VHHH 131.150 HIAS HIAS FLIGHT OPERATIONS

IAD KIAD 130.075

JFK KJFK 131.250

JNB FAJS 131.240

LAS KLAS 129.775 SWISSPORT

LAX KLAX 129.000 129.150ANZ Eng. 129.600 N/W

LGW EGKK 131.425 122.050 GROUNDSTAR

LHR EGLL 131.425

LOS DNMM 118.300

MAN EGCC 131.425

MCO KMCO 130.275 131.850 DELTA TOWER

MIA KMIA 130.275 129.150 BA Eng.

NAS MYNN 129.800 NAS FLT SERVICES

NRT RJAA 130.900 UNITED

PVG ZSPD 129.800 DONG HAI 130.500 as alternate

SFO KSFO 130.275 130.850 SWISSPORT 129.700 BA Engineering

SYD YSSY 129.600 MENZIES

TAB TTCP 130.700 SERVISAIR PENAUILLE SERVISAIR

UVF TLPL 131.400 CARRIBEAN DISPATCH


A340-600


VI6 ALL

REV 00SEQ VAA


CRUISING LEVELS

U.S.S.R. CRUISING LEVELS< WEST

900 m1,500 m2,100 m2,700 m3,300 m3,900 m4,500 m5,100 m

5,700 m6,300 m6,900 m7,500 m8,100 m9,100 m

10,100 m11,100 m12,100 m

EAST >

CHINA CRUISING LEVELS< WEST EAST >

1,200 m1,800 m2,400 m3,000 m3,600 m4,200 m4,800 m5,400 m6,000 m6,600 m7,200 m7,800 m8,600 m9,600 m

10,600 m11,600 m13,100 m

3,900 ft5,900 ft7,900 ft9,800 ft

11,800 ft13,800 ft15,700 ft17,700 ft19,700 ft21,700 ft23,600 ft25,600 ft28,200 ft31,500 ft34,800 ft38,100 ft43,000 ft

3,000 ft4,900 ft6,900 ft8,900 ft


3,000 ft4,900 ft6,900 ft8,900 ft


900 m1,500 m2,100 m2,700 m3,300 m3,900 m4,500 m5,100 m5,700 m6,300 m6,900 m7,500 m8,100 m9,000 m

10,200 m11,400 m12,600 m

2,000 ft3,900 ft5,900 ft7,900 ft9,800 ft

11,800 ft13,800 ft15,700 ft17,700 ft19,700 ft21,700 ft23,600 ft25,600 ft27,600 ft31,500 ft35,400 ft39,400 ft

600 m1,200 m1,800 m2,400 m3,000 m3,600 m4,200 m4,800 m5,400 m6,000 m6,600 m7,200 m7,800 m8,400 m9,600 m

10,800 m12,000 m

AppendixD


A340-600


VI6 ALL


AIRCRAFT INFORMATIONREV 00SEQ VAA

AppendixE

Applicable to ALL A340-642G-VGOA (371 G-VATL (376) G-VSHY (383) G-VMEG (391)

G-VOGE (416) G-VFOX (449) G-VEIL (575) G-VSSH (615)

G-VNAP (622) G-VGAS (639) G-VWKD (706) G-VBLU (723)

G-VWIN (736) G-VFIT (753) G-VFIZ (764) G-VYOU (765)


Max

imum

Tax

y W

eigh

t

369

,200

kgs

Max

imum

Tak

e-O

ff W

eigh

t

368

,000

kgs

Max

imum

Lan

ding

Wei

ght

2

59,0

00 k

g

Max

imum

Zer

o Fu

el W

eigh

t

2

45,0

00 k

gs

Fuel

Cap

acity

*

152

,400

kgs

Max

imum

Tai

lwin

d (T

ake-

Off

and

Land

ing)

10 k

ts

Max

imum

Cro

ssw

ind

Dem

onst

rate

d (T

ake-

Off)

3

5 kt

s gu

st in

clud

ed

Max

imum

Cro

ssw

ind

Dem

onst

rate

d (L

andi

ng)

37

kts

gus

t inc

lude

d

* Bas

ed o

n a

fuel

den

sity

of 0

.785

kgs

per

litre

.

A340-600


VI6 ALL


STANDARD FUELLINGREV 00SEQ VAA

AppendixF

FUEL TANK QUANTITY (Kgs)Valid for all fuel SGs between 0.74 and 0.88 kgs/litre

TOTALFUEL81800820008300084000850008600087000880008900090000910009200093000940009500096000970009800099000100000101000102000103000104000105000106000107000108000109000110000111000112000113000114000115000116000116200117000118000119000120000121000122000123000124000125000

TRIM

01484153223293363433502572642712781851921991106011301200127013401409147915491619168817581828189819672037210721772247231623862400250626382770290230343166329834303562

TOTALFUEL126000127000128000129000130000131000132000133000134000135000136000137000138000139000140000141000142000142700143000144000145000146000147000148000149000150000151000152000153000154000155000156000157000158000159000160000161000162000163000164000165000166000167000168000169000169700

TRIM

3694382639584091422343554487461947514883501551475279541155435675580859005912595259926032607261126152619262326271631163516391643164716511655165916631667167116751679168316871691169516978

VIRGIN ATLANTIC AIRWAYS REVISION 05 / 05 December 2003

A340-600


VI6 ALL

Ground OAT D1 D2<ISA +10° <360T <340T

<ISA +15° <355T <335T

<ISA +20° <350T <330T


DERATE CLIMBREV 00SEQ VAA

AppendixG

There are two initial thrust reductions, De-rate 1 and De-rate 2.De-rate 1 is a 10% reduction of full climb thrust and De-rate 2 is a 15%reduction. At altitudes (above 30,000 ft) the de-rate climb is identicalto the max climb rating. For temperatures below ISA +10° there is aprogressive transition from De-rate climb to max climb between26,000 ft and 30,000 ft for DCLB 1 and between 24,000 ft and 30,000ft for DCLB2. With Ambient temps >ISA +10° the altitudes are lower.

De-rate climb can be selected on the PERF CLB Page, by inserting'D1' or 'D2' in position (1R) on the CLB Page.

After analysis of the data the following is a guide to the use of De-rateClimb.


A340-600


VI6 ALL


REDUCED TAKE-OFF THRUST

REV 00SEQ VAA

AppendixH

Reduced Take-Off Thrust may be used at the Captain's discretionand is referred to as Flexible Take-Off Thrust. Flexible Thrust may beused when the actual take-off weight is lower than the RTOW, exceptwhen prohibited by the exceptions listed below. Thrust reduction mustnot exceed 40% of the full rated take-off thrust. Use of reduced thrust,where possible, will assist engine condition and make a significantcontribution to reducing the rate of engine failure. The engines may beopened up to full 'Go-around thrust at any time after V1 is attainedshould the need arise.

Reduced Take-Off Thrust (Flexible Trust) must not be used when:

(a) The corrected 'FLEX' temperature (CT) is higher than ISA+60°C or lower than 'TREF' (Reference Temperature) or lowerthan ambient temperature.

(b) The runway is affected by snow, slush, standing water or ice, orsuspected of having a marginal braking capability.

(c) Significant windshear conditions are anticipated.

(d) Operating with landing gear extended.

(e) One or more brake(s) inoperative.

(f) One or more thrust reversers are inoperative.

(g) Ground spoilers inoperative.

(h) One tachometer inoperative.

(i) Generalised or non specific RTOW tables are used.

A calculated RTOW of more than maximum structural can be used forFlexible Thrust calculations.

VIRGIN ATLANTIC AIRWAYS REVISION 05 / 05 December 2003

A340-600


VI6 ALL

SUPPLEMENTARY INFORMATIONTAKE-OFF DATA CALCULATION

(TODC)

REV 00SEQ VAA

AppendixI

Item Definition Example

AIRPORT * Airport ICAO code KBOS

RUNWAY * Runway 22LNote:- For Taxyway/Holding Point start of roll positions,

suffix the Runway designator Taxyway/HoldingPoint designator. (e.g. 21LN3).

DIRECTION * Wind Direction (°) 190

SPEED * Wind Speed (kts) 009

OAT * Outside Air Temp = -50 to 55 12

QNH * QNH 1020Note:- Range 0920 to 1070 implies hPa.

Range 2700 to 3200 implies Hg.i.e. “2745” = 27.45 Hg.

%MAC % Mean Aerodynamic Chord 170Note:- 170 = %MAC 17.0.

170 is the Standard CG position for Take-Offcalculations for the A340-600.Default = 170.

AZFW * Actual Zero Fuel Weight (kg) 245000

ATOW * Actual Take-Off Weight (kg) 308500

CONDTN Runway Condition 00 = Dry1 = Wet2 = Standing Water3 = Slush4 = Compact Snow5 = Wet Snow6 = Dry Snow7 = Dry Ice8 = Wet Ice9 = Very Dry SnowDefault = 0.When selecting options 2 to 9,REVERS must be set to 0.

SHORTENING Shortened Runway (metres) B0800“B” prefix denotes the runway has beenshortened at the Beginning/Start of Roll endof the runway. “E” suffix denotes the runwayhas been shortened at the Lift-Off End of therunway. Range – 0001 to 2000 metres.Default = Blank spaces.

DEPTH Contaminant Depth (mm) 05Depth not required for items 0, 1, 4, 7 or 8 above.Default N/A (see above).


A340-600


VI6 ALL


BRK ACTION Runway Braking Action 1Note:- 0 = Friction Coefficient

1 = GOOD2 = MEDIUM to GOOD3 = MEDIUM4 = MEDIUM to POOR5 = POOREnter “0” if Friction Coefficient reported.Then enter Friction Coefficient (see below).Default = 1.

FC Friction Coefficient 21Note:- Range from 16 to 70. e.g 21 = FC 0.21.

Default = Blank spaces.

FLAPS * Take-Off Flaps/Configuration 3Note:- 1 = Conf 1+F, 2 = Conf 2, 3 = Conf 3.

Default = 3.

AIR COND Air Conditioning 0Note:- 0 = Off. 1 = On.

Default = 0.

REVERS Reverse Thrust considered 3Note:- 0 = ALL OK. 1 = 1 Inboard Inop.

2 = 1 Outboard Inop. 3 = All InopDefault = 3.When CONDTN is set to 2 to 9, REVERSmust be set to 0.

ANT ICE Anti-Ice considered 0Note:- 0 = Off. 1 = Engine AI On. 2 = Engine & Wing AI On.

Default = 0.

BRAKES Brakes 0Note:- 0 = OK. 1 = 1 Inop. 2 = 2 Inop.

Default = 0.

L/GEAR Landing Gear 0Note:- 0 = OK. 1 = Extended

Default = 0.

WHEEL TACHO Wheel Tachometer 0Note:- 0 = OK. 1 = 1 Inop.

Default = 0.

GRND IDLE Ground Idle 0Note:- 0 = OK. 1 = Inop.

Default = 0.


(TODC)

REV 00SEQ VAA

AppendixJ


A340-600


VI6 ALL


ENG ANT-ICE Engine Anti-Ice Valve Position 0VALVE POSN

Note:- 0 = OK. 1 = Open.Default = 0.

ENGINES Engines Inop 0Note:- 0 = None. 1 = 3 Engine Ferry

Default = 0.

ALT RUNWAY Alternate Runways 0Note:- 0 = No. 1 = Yes.

If “1” is inserted a calculation will be done for allrunways for the specified airport held in theTODC database.Default = 0.

GROUND Ground Spoilers 0SPOILER

Note:- 0 = OK. 1 = 1 Pair Inop.2 = 2 Pairs Inop. 3 = All Inop.Default = 0.

* Mandatory Input.


(TODC)

REV 00SEQ VAA

AppendixK


A340-600

346QRH-ch7.PM6/1

A340-600

VI6 ALL

REV 24SEQ 205

BEFORE STARTCOCKPIT PREP . . . . . . .COMPLETE (BOTH)GEAR PINS and COVERS . . . . . .REMOVEDSIGNS . . . . . . . . . . . . . . . . . . . . . . . . .ON / AUTOADIRS . . . . . . . . . . . . . . . . . . . . . . . . . . . .NAVFUEL QUANTITY . . . . . . . . . . _________ KGTO DATA / DCLB . . . . . . . _____SET (BOTH)BARO REF . . . . . . QNH_______SET (BOTH)WINDOWS/DOORS. . .CLOSED/ARMED (BOTH)BEACON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ONTHR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . .IDLEPARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . .SET

NORMAL CHECKLIST 7.01

VIRGIN ATLANTIC AIRWAYS REVISION 09 / 01 April 2005

APPROACHBRIEFING . . . . . . . . . . . . . . . . . . . . . . CONFIRMECAM STATUS . . . . . . . . . . . . . . . . . . . . CHECKSEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . ONMINIMUMS. . . . .__________ SET (BOTH)BARO . . . . . . QNH__________ SET (BOTH

LANDING

A/THR . . . . . . . . . . . . . . . . . . . . . .SPEED/OFFECAM MEMO . . . . . . . . . . . . . . .LDG NO BLUE

. L/G/ DOWN

. SIGNS ON

. SPLRS ARM

. FLAPS SETCABIN . . . . . . . . . . . . . . . . . . . . . . . . . . . . READY

AFTER STARTANTI ICE . . . . . . . . . . . . . . . . . . . . . . . .AS RQRDECAM STATUS . . . . . . . . . . . . . . . . . . . . CHECKTRIMS . . . . . . . . . . . . . . . . __________ SET

BEFORE T.O.FLIGHT CONTROLS . . . . CHECKED (BOTH)FLT INST . . . . . . . . . . . . . . . CHECKED (BOTH)BRIEFING/CLEARANCE . . . . . .CONFIRMFLAPS . . . . . . . . . . . . . . ________ SET (BOTHT.O. SPEEDS/ FLX TEMP . . . . .____ ____/____(BOTH)ECAM MEMO . . . . . . . . . . . . . . . .T/O NO BLUE

. AUTO BRK MAX

. SIGNS ON

. SPLRS ARM

. FLAPS TO

. TO CONFIG NORM

CABIN . . . . . . . . . . . . . . . . . . . . . . . READY/ADVISELIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPACKS . . . . . . . . . . . . . . . . . . . . . . ON APU/OFFRADAR/TCAS/PWS . . . . . AS RQRD/SET/AUTO

AFTER LANDINGSPOILERS . . . . . . . . . . . . . . . . . . . . DISARMEDFLAPS . . . . . . . . . . . . . . . . . . . . . . .RETRACTEDRADAR/PWS . . . . . . . . . . . . . . . . . . OFF/OFFAPU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .START

PARKINGAPU BLEED . . . . . . . . . . . . . . . . . . . . . . . . ONENGINES . . . . . . . . . . . . . . . . . . . . . . . . . OFFSEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . OFFEXT LT . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRDFUEL PUMPS . . . . . . . . . . . . . . . . . . . . . . OFFCHOCKS and PARK BRAKE . . . . AS RQRD

AFTER T.O./CLIMBLDG GEAR . . . . . . . . . . . . . . . . . . . . . . . . UPFLAPS . . . . . . . . . . . . . . . . . . . . . . .RETRACTEDPACKS / APU . . . . . . . . . . . . . . . . . . . . ON/OFFBARO REF . . . . . . . . . ________ SET (BOTH)

SECURING AIRCRAFTTCAS. . . . . . . . . . . . . . . . . . . . . . . . . . . STBYADIRS . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFOXYGEN . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAPU BLEED . . . . . . . . . . . . . . . . . . AS RQRDEMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . .OFFNO SMOKING . . . . . . . . . . . . . . . . . . . . . . .OFFBAT 1 + 2 + APU BAT . . . . . . . . . . . . .AS RQRDTECH LOG . . . . . . . . . . .. . . . . . . . COMPLETED

ON GROUND EMER / EVACUATION- AIRCRAFT/PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . STOP/ON CM1- ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY CM1- ∆∆∆∆∆P (only if MAN CAB PR has been used) . . . . . . . . . . . . . CHECK ZERO CM1

IF ∆P IS NOT ZERO SELECT MANUAL MODE AND V/S CTL FULL UP TO FULLY OPEN THE OUTFLOW VALVE.

- ALL ENG MASTER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF CM1- FIRE P/Bs (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH CM1- AGENTS (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . . . DISCHARGE CM1- EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE CM1- BAT 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

TAKEOFF CG

TRIM POS

13/16 20

6 5

24 28

4 3 2 1 0

32 36 40/44

A340 QRH VOL.3 REV025A CROSS REFERENCE TABLE

THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE

BETWEEN :

- THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES

- THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS INDUSTRIE.

----------------------------------------------------------------------------

MSN REGISTRATION

----------------------------------------------------------------------------

0371 G-VGOA

0376 G-VATL

0383 G-VSHY

0391 G-VMEG

0416 G-VOGE

0449 G-VFOX

0575 G-VEIL

0615 G-VSSH

0622 G-VNAP

0639 G-VGAS

0706 G-VWKD

0723 G-VBLU

0736 G-VWIN

0753 G-VFIT

0764 G-VFIZ

0765

VI6

0.04

06 MAR 2006 PAGE : CRT001

346QRH-TR'S.PM6/1

A340-600GENERAL INFORMATION

RECORD OF TEMPORARY REVISIONS20 MAR 06

SEQ VAA

MSN Nos: 0371 - G-VGOA 0376 - G-VATL 0383 - G-VSHY 0391 - G-VMEG

0416 - G-VOGE 0449 - G-VFOX 0575 - G-VEIL 0615 - G-VSSH

0622 - G-VNAP 0639 - G-VGAS 0706 - G-VWKD 0723 - G-VBLU

0736 - G-VWIN 0753 - G-VFIT 0764 - G-VFIZ 0765 - G-VYOU

No. Title ApplicableAircraft

183-1B COCKPIT DOOR LOCKING SYSTEM JAM 0371-0575

200-1H CDSS SMOKE FROM LCD MONITOR 0416

232-2B ENGINE FUEL FEED PIPE RUPTURE WITHIN FUEL TANK 0371-0639

234-1A "SMOKE CABVIDEO 1 (2)(3)(4) SMOKE" ECAM WARNING ALL

235-1A "SMOKE VIDEO 1 (2)(3)(4) DET FAULT" ECAM CAUTION ALL

236-1A "COND IFE BAY VENT FAULT" ECAM CAUTION, or "SMOKE ALLIFE BAY DET FAULT" ECAM CAUTION

243-1B FUEL 1 (2) FAULT/FUEL MONITORING 0371-0706

258-1A DISPLAY UNIT FAILURE - INVALID DISPLAY UNIT ALL

259-1A PERIODIC RESET OF ALL DISPLAY UNITS ALL

261-1A ABNORMAL PROCEDURES - FUEL WING TANK IMBALANCE ALL

New or revised Temporary Revisions included in this revision are highlighted in bold type.

TRs

VIRGIN ATLANTIC AIRWAYSVIR ALL

346QRH-prelims.PM6/1

VI6 ALL

QUICK REFERENCEHANDBOOK

VAA PAGE LEP


LIST OF EFFECTIVE PAGES AMENDEDOR ADDED BY VIRGIN ATLANTIC AIRWAYS

New or revised pages included in this revision are highlighted in bold text.

Page MSN No. Effective Date

0.00 ALL 01 Jul 020.00B ALL 20 Mar 060.00C ALL 20 Mar 060.00D ALL 20 Mar 060.00E ALL 20 Mar 060.00F ALL 20 Mar 060.00G ALL 20 Mar 06

VSRecord of TR's ALL As dated1.00 ALL 01 May 051.05 ALL 26 Jul 041.10 ALL 22 May 031.11 ALL 01 Jul 021.12 ALL 15 Aug 051.15 ALL 20 Mar 061.16 ALL 20 Mar 061.18 ALL 20 Mar 061.19 ALL 20 Mar 061.20 ALL 01 May 051.22 ALL 20 Mar 061.24 ALL 20 Mar 061.25 ALL 01 May 051.26 ALL 01 May 052.00 ALL 15 Aug 052.08A ALL 15 Aug 052.09 ALL 01 Jul 022.10A ALL 26 Jul 042.11A ALL 15 Aug 053.00 ALL 01 Jul 023.01 ALL 15 Aug 053.02 ALL 01 May 05VS LEP ALL 20 Mar 06

VS Appendix A ALL 01 Jul 02 VS Appendix B ALL 01 Jul 02 VS Appendix C ALL 20 Mar 06 VS Appendix D ALL 22 May 03 VS Appendix E ALL 15 Aug 05 VS Appendix F ALL 05 Dec 03 VS Appendix G ALL 15 Aug 05 VS Appendix H ALL 05 Dec 03 VS Appendix I ALL 15 Aug 05 VS Appendix J ALL 01 May 05 VS Appendix K ALL 12 Mar 04 7.01 ALL 01 Apr 05

A340-600

A340 QUICK REFERENCE HANDBOOK REV025A LIST OF EFFECTIVE PAGES (LEP) M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----- M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----- -------------------EFFECTIVITY-------------------------------------------------------------------------------------------

0 .00 001 REV019 ALL

0 .00A 001 REV023 ALL

0 .01 001 REV025 LIST OF CODES 0 .02 001 REV025 LIST OF CODES ALL

0 .02A 001 REV025 LIST OF CODES ALL

0 .03- 001 REV025 LIST OF TEMPORARY REVISIONS ALL

0 .04- 001 REV025 CROSS REFERENCE TABLE ALL

0 .06- 001 REV025 LIST OF EFFECTIVE PAGES ALL

0 .07- 001 REV025 LIST OF MOD/MP/SB ALL

1 .00 001 REV024 ALL

1 .01 100 REV019 47002 1 .02 200 REV022 CODE:0009 ALL

1 .03 302 REV025 40624+41300+47000 1 .04 100 REV025 47002 ALL

1 .05 001 REV025 1 .06 100 REV025 CODE 0080 ALL

1 .06A 001 REV025 ALL

1 .06B 001 REV025 ALL

1 .07 300 REV025 M:40624+41300+47000 1 .08 302 REV025 40624+41300+47000 ALL

1 .09 300 REV025 M:40624+41300+47000 1 .10 100 REV021 47002 ALL

1 .11 102 REV025 49026 1 .12 100 REV023 CODE 0008 ALL

1 .13 102 REV025 47000 1 .14 102 REV024 47002 ALL

1 .15 205 REV024 CODE 0066 1 .16 205 REV025 CODE 0066 ALL

1 .17 104 REV025 47002 1 .18 205 REV024 CODE 0066 ALL

1 .19 205 REV025 CODE 0066 1 .20 001 REV024 ALL

1 .21 100 REV025 46324=52992 1 .22 200 REV025 CODE 0066 ALL

1 .23 100 REV025 46324=52992 1 .24 200 REV024 CODE 0066 ALL

1 .25 001 REV024 STD=40257=40379 ALL

2 .00 402 REV025 46257+46290+47002+50014 0371-0615

2 .00 505 REV025 CODE 0078 0622-0765

2 .00A 100 REV025 47002 ALL

0.0606 MAR 2006 VI6 PAGE : LEP001


2 .00B 001 REV024 ALL

2 .01 102 REV022 50014 2 .02 102 REV025 M:47000 ALL

2 .03 100 REV019 M:47002=49144 2 .04 210 REV013 M:46257+46290 ALL

2 .05 100 REV022 47002 2 .06 102 REV022 47002 ALL

2 .06A 160 REV025 M:47002/RR ALL

2 .06B 060 REV022 RR 556-61 ALL

2 .07 100 REV025 47002 2 .08 100 REV025 47000 ALL

2 .08A 102 REV025 47000 ALL

2 .09 100 REV025 47002 2 .10 105 REV025 47000 ALL

2 .11 105 REV024 CODE 0075 0371-0615

2 .11 200 REV024 CODE 0076 0622-0765

2 .11A 001 REV025 ALL

2 .12 001 REV021 ALL

2 .13 100 REV021 M:47002 2 .14 100 REV022 47002 ALL

2 .15 100 REV025 47002 2 .16 100 REV021 47002 ALL

2 .17 100 REV023 49192=52306=47002+51913 2 .18 300 REV023 CODE 0048 0622-0765

2 .17 110 REV023 M:47002 2 .18 300 REV023 CODE 0048 0371-0615

2 .19 100 REV025 M:47002 2 .20 001 REV023 0371-0615

2 .19 100 REV025 M:47002 2 .20 100 REV023 CODE 0077 0622-0765

2 .20A 001 REV025 ALL

2 .20B 100 REV025 CODE 0058 ALL

2 .21 123 REV025 CODE 0069/ E556-61 2 .22 100 REV025 CODE 0069 ALL

2 .23 100 REV025 CODE 0069 ALL

2 .23A 043 REV025 556-61 ALL

2 .23B 043 REV025 556-61 ALL

2 .24 001 REV025 ALL

2 .25 100 REV021 46257 2 .26 150 REV025 M:50968/RR ALL

0.0606 MAR 2006 VI6 PAGE : LEP002


2 .27 050 REV021 RR 2 .28 050 REV023 RR ALL

2 .29 140 REV024 47000/RR556-61 ALL

2 .29A 160 REV022 M:47000/RR 556-61 ALL

2 .29B 160 REV022 M:47000/RR 556-61 ALL

2 .30 001 REV024 ALL

2 .31 001 REV021 2 .32 100 REV021 47002 ALL

2 .33 001 REV021 2 .34 001 REV021 ALL

2 .35 100 REV025 40259=40512 2 .36 200 REV025 43078+47002 ALL

2 .37 300 REV025 46742+47002+47921 2 .38 300 REV025 M:45748+47002+50616 ALL

2 .39 020 REV024 RR 2 .40 100 REV022 47000=44495+47000 0371-0449

2 .39 120 REV024 M:MP S17972/RR 2 .40 100 REV022 47000=44495+47000 0575-0765

2 .41 105 REV025 47000 2 .42 105 REV025 47000 ALL

2 .43 105 REV025 47000 2 .44 001 REV025 ALL

3 .00 001 REV011 ALL

3 .01 200 REV024 CODE 0125 3 .02 102 REV022 47244 0371-0376 0391-0416 0575-0765

3 .01 300 REV024 CODE 0126 3 .02 102 REV022 47244 0383 0449

3 .03 050 REV025 RR=SIA/RR 3 .04 100 REV025 46459 ALL

3 .05 001 REV025 3 .06 001 REV025 ALL

3 .07 001 REV025 3 .08 001 REV025 ALL

3 .09 100 REV025 47002=47002/ACA/SIA 3 .10 001 REV014 ALL

4 .00 001 REV010 ALL

4 .01 178 REV025 47000=44495+47000/RR556 4 .02 210 REV022 RR556/47000+40624 ALL

4 .03 210 REV022 RR556/47000+40624 4 .04 210 REV023 M:40624+47000/RR556 ALL

4 .05 140 REV021 RR556/47000 4 .06 140 REV021 RR556/47000 0371-0622

4 .05 240 REV024 47000+50655/RR 556 4 .06 240 REV024 47000+50655/RR 556 0639-0765

0.0606 MAR 2006 VI6 PAGE : LEP003


4 .07 140 REV021 RR556/47000 4 .08 140 REV023 RR556/47000 0371-0622

4 .07 240 REV024 47000+50655/RR 556 4 .08 240 REV024 47000+50655/RR 556 0639-0765

4 .09 140 REV022 RR556/47000 4 .10 140 REV023 M:47000/RR556 0371-0622

4 .09 140 REV022 RR556/47000 4 .10 240 REV024 47000+50655/RR 556 0639-0765

4 .11 120 REV023 47000/RR 556 4 .12 105 REV022 M:47002 0371-0622

4 .11 240 REV024 47000+50655/RR 556 4 .12 105 REV022 M:47002 0639-0765

4 .13 120 REV024 47000/RR 556 4 .14 120 REV023 47000/RR 556 0371-0622

4 .13 120 REV024 47000/RR 556 4 .14 240 REV024 47000+50655/RR 556 0639-0765

4 .15 120 REV023 47000/RR 556 4 .16 001 REV010 0371-0622

4 .15 240 REV024 47000+50655/RR 556 4 .16 001 REV010 0639-0765

4 .17 001 REV011 ALL

5 .00 001 REV021 ALL

5 .01 100 REV025 RR556/47000 5 .02 100 REV023 M:47002 0371-0622

5 .01 250 REV025 47000+50655/556-61 5 .02 100 REV023 M:47002 0639-0765

5 .03 100 REV022 47002 5 .04 102 REV024 47002 ALL

7 .01 205 REV024 CODE:0056 ALL

0.0606 MAR 2006 VI6 PAGE : LEP004

A340 QRH

VOLUME : 3 QUICK REFERENCE HANDBOOK

LIST OF MOD/MP/SB AFFECTING THE MANUAL REVISION : 025A

M

V REV MOD MP TITLE

T SB VALIDITY

. 023 ...... S17972 AIR-NACELLE TEMPERATURE INDICATING RELOCATE

........... RRT500 ENGINE FOR A3456-CNFRR26

G-VEIL G-VSSH G-VNAP

G-VGAS G-VWKD G-VBLU

G-VWIN G-VFIT G-VFIZ

MSN 0765

. 021 40259 ...... EQUIPMENT/FURNISHINGS-CREW REST

........... COMPARTMENT-INSTALL STRUCTURAL

PROVISIONS

ALL

. 020A 40624 ...... INDICATING/RECORDING SYSTEMS-FMGEC-

........... REPLACE METERS BY FEET

ALL

. 020A 41300 ...... WINGS-GENERAL-DEFINE A340 GROWTH

........... VERSION

ALL

. 020A 43078 ...... FLIGHT CONTROLS - CHANGE WIRING OF

........... FCPC1 AND FCSC1 FAULT INDICATOR LIGHTS

ALL

. 020A 44482 ...... ICE AND RAIN PROTECTION -

........... WINDSHIELD RAIN PROTECTION -

DEACTIVATE RAIN REPELLENT SYSTEM

ALL

. 020A 44495 ...... AUTO FLIGHT - FMGEC - INTRODUCE L6

........... STD FOR CFMI

ALL

. 020A 44575 ...... FUEL - FMCS - FIT FCMC (STAGE 7.1) WITH

........... CHANGES TO SOFTWARE FOR A330 AND A340

AIRCRAFT

ALL

. 020A 44604 ...... FUEL - APU FUEL PUMP SYSTEM - PREVENT

........... AN ELECTRICAL ESS NETWORK �OVERLOAD�

(A340)

ALL

VI6 0.07

06 MAR 2006 PAGE LOM001

A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

. 021 44754 ...... NAVIGATION - WEATHER RADAR SYSTEM -

........... ACTIVATE ALLIED SIGNAL PREDICTIVE

WINDSHEAR FUNCTION

ALL

. 020A 45057 ...... INDICATING/RECORDING SYSTEM - FWC -

........... DEFINE NEW OEB REMINDER FUNCTION

ALL

. 020A 45509 ...... NAVIGATION - MMR - INSTALL COLLINS

........... MULTI-MODE RECEIVERS PROVIDING ILS

(FM IMMUNE) AND GPS PRIMARY FUNCTION

ALL

. 023 45748 ...... OXYGEN - CREW OXYGEN - INSTALL A 115

........... CU.FT COMPOSITE OXYGEN CYLINDER

ALL

. 022 45897 ...... ICE AND RAIN PROTECTION - WINDSHIELD

........... RAIN PROTECTION - REACTIVATE THE RAIN

REPELLENT SYSTEM

ALL

. 020A 46257 ...... INDICATING/RECORDING SYSTEMS - FWC -

........... INSTALL NEW FWC STANDARD L7-0

ALL

. 020A 46290 ...... FLIGHT CONTROLS - FCDC - INSTALL FCDC

........... STANDARD L15/M12

ALL

. 020A 46324 ...... NAVIGATION - GPWS - ACTIVATE ENHANCED

........... GPWS

ALL

. 022 46459 ...... INDICATING/RECORDING SYSTEMS-CENTRAL

31-5011 02 WARNING SYSTEMS-PROVIDE NEW AUTO

CALL-OUT CALLED �V1�

ALL

. 020A 46532 ...... INDICATING/RECORDING SYSTEMS - EIS -

........... DISPLAY MANAGEMENT COMPUTER - INSTALL

NEW DMC SOFTWARE V110X

ALL

VI6 0.07


A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

. 020A 46728 ...... NAVIGATION-TCAS-INSTALL ALLIED SIGNAL

........... CHANGE 7 P/N 066-50000-2220

ALL

. 023 46742 ...... INFORMATION SYSTEMS - AIR TRAFFIC AND

........... INFORMATION MANAGEMENT SYSTEM -

ACTIVATE ATSU

ALL

. 020A 46893 ...... NAVIGATION - MMR - INSTALL COLLINS

........... MULTI-MODE RECEIVERS P/N 822-1152-121

ALL

. 022 46976 ...... ICE AND RAIN PROTECTION - WINDSHIELD

30-5001 RAIN PROTECTION - DE-ACTIVATE RAIN

REPELLENT SYSTEM

G-VGOA G-VATL G-VMEG

G-VOGE G-VEIL G-VSSH

G-VNAP G-VGAS G-VWKD

G-VBLU G-VWIN G-VFIT

G-VFIZ MSN 0765

. 020A 47000 ...... GENERAL - PROVIDE BASIC DEFINITION

........... FOR A340-600

ALL

. 020A 47002 ...... WINGS - GENERAL - DEFINE BASIC DESIGN

........... FOR A340-500/600

ALL

. 020A 47110 ...... COMMUNICATIONS-GENERAL-INSTALL CEIS

........... P/N 93N6035 EMERGENCY CONTROL PANEL IN

COCKPIT

ALL

. 022 47244 ...... NAVIGATION-STANDBY NAVIGATION SYSTEMS-

........... INSTALL SEXTANT AVIONICS INTEGRATED

STANDBY INSTRUMENT SYSTEM (ISIS)

ALL

. 020A 47524 ...... INDICATING/RECORDING SYSTEMS-ELECTRONIC

........... INSTRUMENT SYSTEM - INSTALL NEW DISPLAY

SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES)

ALL

VI6 0.07


A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

. 024 47921 ...... INFORMATION SYSTEMS - ATIMS - INSTALL

........... ATSU RESET PUSHBUTTON SWITCH FOR FANS

A CONFIGURATION

ALL

. 021 49026 ...... NAVIGATION - EGPWS - ACTIVATE

........... OBSTACLE FUNCTION

ALL

. 024 49101 ...... AIR CONDITIONING-DISTRIBUTION-INSTALL A

........... SMOKE DETECTION SYST. FOR VCC CONNECTED

TO THE AIR EXTRACTION SYST.IN DOOR 1 LH

ALL

. 022 50014 ...... EQUIPMENT/FURNISHINGS - COCKPIT -

........... INSTALL AN ARMOURED COCKPIT DOOR

ALL

. 024 50161 ...... INDICATING/RECORDING SYSTEM - EIS -

........... INSTALL NEW EIS2 STANDARD L3-1

(DMC, DU AND DISKS)

ALL

. 024 50242 ...... COMMUNICATIONS - VIDEO MONITORING -

23-5001 04 INSTALL A COCKPIT DOOR SURVEILLANCE

SYSTEM (CDSS)

ALL

. 022 50246 ...... FLIGHT CONTROLS - SLAT/FLAP CONTROL

........... COMPUTER - INTRODUCE SFCC STANDARD

-0508

ALL

. 024 50279 ...... ENGINE - GENERAL - DEFINE ENGINE

........... CONFIGURATION FOR A340-600 AIRCRAFT

TYPE CERTIFICATE

ALL

. 022 50321 ...... AUTO FLIGHT - FMGEC - INSTALL EIS STD

........... P2-E3 FOR A340-600

ALL

. 023 50616 ...... INDICATING/RECORDING SYSTEMS - EIS -

31-5001 INTALL NEW EIS2 STANDARD L4 ON

A330/A340 ENHANCED

ALL

VI6 0.07


A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

. 024 50655 ...... ENGINE - GENERAL - INTRODUCE ENHANCED

........... PERFORMANCE PACKAGE ON RR T500 ENGINES

G-VGAS G-VWKD G-VBLU

G-VWIN G-VFIT G-VFIZ

MSN 0765

. 022 50968 ...... ENGINE FUEL AND CONTROL- FADEC -

73-5001 INTRODUCE NEW EEC STD L4.1.3 ON RR

T500 ENGINES

ALL

. 024 51153 ...... INDICATING/RECORDING SYSTEMS - EIS -

31-5001 INSTALL NEW EIS2 STANDARD L4-1 CAPABLE

OF ALL LONG RANGE AIRCRAFT

ALL

. 024 51315 ...... AUTO FLIGHT - FMGEC - INSTALL NEW

22-5002 STANDARD FMGEC �P2E5�

ALL

. 023 51486 ...... LANDING GEAR - NORMAL BRAKING -

32-5018 01 INTRODUCE BSCU STANDARD S2K

ALL

. 023 51733 ...... FLIGHT CONTROL - FLIGHT CONTROL PRIMARY

27-5010 01 COMPUTER (FCPC) - INSTALL NEW FCPC

SOFTWARE STANDARD W8 ON A340/500-600

ALL

. 024A 51973 ...... INDICATING/RECORDING SYSTEMS - FWC -

........... INSTALL FWC W4-0 WITH 486 BASED CPU

BOARD ON A340/500-600

G-VNAP G-VGAS G-VWKD


G-VFIZ MSN 0765

. 024 51974 ...... INDICATING/RECORDING SYSTEMS - EIS

31-5012 01 - INSTALL NEW EIS2 STD L5 TO INCREASE

SYSTEM ROBUSTNESS AND MATURITY

ALL

. 024 52465 ...... LANDING GEAR - NORMAL BRAKING -

32-5029 INSTALL NEW BSCU WITH HARDWARE DD8 AND

SOFTWARE S3B

ALL

VI6 0.07


A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

. 024 52528 ...... LANDING GEAR-NORMAL BRAKING-

32-5037 INSTALL WIRING FOR FREEFALL SWITCH

MONITOR

ALL

. 025 52652 ...... EQUIPMENT/FURNISHINGS - CURTAINS AND

........... PARTITIONS - INSTALL A MAXIMUM NOISE

REDUCED COCKPIT DOOR LOCK SYSTEM (CDLS)

G-VSSH G-VNAP G-VGAS

G-VWKD G-VBLU G-VWIN

G-VFIT G-VFIZ MSN 0765

. 025 52845 ...... INFORMATION SYSTEMS-A/C INFORMATION

........... NETWORK SYSTEM - INSTALL AINS RESET

COMMAND



. 024A 52866 ...... COMMUNICATIONS - ANTI HIJACK SYSTEM -

23-5017 REPLACE HINGE ASSEMBLY FOR THE LCD

SYSTEM CONTROLLER OF THE CDSS

G-VGOA G-VATL G-VSHY

G-VMEG G-VFOX G-VEIL

G-VSSH G-VNAP G-VGAS



. 025 53389 ...... INFORMATION SYSTEMS -A/C INFO NETWORK

........... SYSTEM-INSTALL AINS RESET COMMAND

(SERIAL SOLUTION)



. 025 53923 ...... INDICATING/RECORDING SYSTEM - EIS:

31A5016 ACTIVATE CRC MONITORING ON EIS2

ALL

. 025 53951 ...... INFORMATIONS SYSTEMS - AIRCRAFT -

........... INFORMATION NETWORK SYSTEM - REMOVE

AINS/RESET SWITCH AND �INOP� PLACARD



VI6 0.07


A340 QRH



M

V REV MOD MP TITLE

T SB VALIDITY

N 025A 54201 ...... FUEL - MAIN FUEL PUMP SYSTEM- INTRODUCE

........... AN ADDITIONAL THERMAL RELIEF VALVE TO

EACH FUEL LINE



N 025A 54611 ...... INDICATING/RECORDING SYSTEMS - FWC -

........... INSTALL FWC STANDARD W4-1 ON A3456

(WITH 486 CPU BOARD)


G-VFIZ MSN 0765

N 025A 54624 ...... FUEL-FUEL CONTROL AND MONITORING SYSTEM

........... (FCMS)-AMEND WIRING BETWEEN FDC AND FWC


G-VFIZ MSN 0765

N 025A 54807 ...... FUEL-FUEL CONTROL AND MONITORING SYSTEM

28-5033 (FCMS) - UPDATE FCMC SOFTWARE STANDARD

TO FLIGHTLOAD 8.1

G-VGOA G-VATL G-VMEG

G-VOGE G-VEIL G-VGAS



VI6 0.07


346QRH-TR'S.PM6/3

A340-600 TEMPORARY REVISION No 183-1 JUN 03

ISS. B

TR No 183-1 PAGE 1 OF 2

0.0

This Temporary Revision has been issued after normal revision No 22.Do not remove it until instructed to do so.

VI6 MSN 0371-0575

346QRH-TR'S.PM6/5

A340-600 ABNORMAL PROCEDURES JUN 03 2.01

TR N° 183-1 PAGE 2 OF 2

VI6 MSN 0371-0575

346QRH-TR'S.PM6/7

A340-600 TEMPORARY REVISION No 200-1 FEB 04

ISS. H


0.0


VI6 MSN 0416

346QRH-TR'S.PM6/9

A340-600 EMERGENCY PROCEDURES FEB 04 1.04A

TR N° 200-1 PAGE 2 OF 2

VI6 MSN 0416

346QRH-TR'S.PM6/11

A340-600 TEMPORARY REVISION No 232-2 APR 05

ISS. B


0.0


VI6 MSN 0371-0639

346QRH-TR'S.PM6/13

A340-600 OEB APR 05 6.00

TR N° 232-2 PAGE 2 OF 3

VI6 MSN 0371-0639

346QRH-TR'S.PM6/15

A340-600 OEB APR 05 6.00

TR N° 232-2 PAGE 3 OF 3

VI6 MSN 0371-0639

346QRH-TR'S.PM6/17

A340-600 TEMPORARY REVISION No 234-1 JAN 05

ISS. A


0.0


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A340-600 OEB JAN 05 6.00

TR N° 234-1 PAGE 2 OF 2

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ISS. A


0.0


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A340-600 OEB JAN 05 6.00

TR N° 235-1 PAGE 2 OF 2

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ISS. A


0.0


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A340-600 OEB JAN 05 6.00

TR N° 236-1 PAGE 2 OF 2

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A340-600 TEMPORARY REVISION No 243-1 MAR 05

ISS. B


0.0


VI6 MSN 0371-0706

346QRH-TR'S.PM6/31

A340-600OEB MAR 05 6.00

TR N° 243-1 PAGE 2 OF 3

VI6 MSN 0371-0706

346QRH-TR'S.PM6/33

A340-600OEB MAR 05 6.00

TR N° 243-1 PAGE 3 OF 3

VI6 MSN 0371-0706

346QRH-TR'S.PM6/35

A340-600 TEMPORARY REVISION No 258-1 SEP 05

ISS. A


0.0

VI6 ALL


346QRH-TR'S.PM6/37

A340-600 ABNORMAL PROCEDURES SEP 05


2.11

VI6 ALL

346QRH-TR'S.PM6/39

A340-600

VI6 ALL

TEMPORARY REVISION No 259-1 OCT 05

ISS. A


0.0


346QRH-TR'S.PM6/41

A340-600OEB OCT 05


6.00

VI6 ALL

346QRH-TR'S.PM6/43

A340-600

VI6 ALL

TEMPORARY REVISION No 261-1 DEC 05

ISS. A


0.0


346QRH-TR'S.PM6/45

A340-600 ABNORMAL PROCEDURES DEC 05


2.07

VI6 ALL

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