A319 / A320 / A321 : QUICK REFERENCE HANDBOOK : REV 40B PDF Free Download

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QTR ALL

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-2288 3071

QTR MSN 0928

QTR MSN 1566-2341

QTR MSN 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928

QTR MSN 1566-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 0928

QTR MSN 1656 2341

QTR MSN 1566

QTR MSN 1648 1773-2288 3071

QTR ALL

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288

QTR MSN 3071

QTR MSN 0928-1895 1957

QTR MSN 3071

QTR MSN 1928 2097-2341

QTR MSN 3071

QTR MSN 0928

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 1566-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 0928

QTR MSN 1656 2341

QTR MSN 1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1566

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 0928

QTR MSN 1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1566

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 0928

QTR MSN 1566

QTR MSN 1648-3071

QTR ALL

QTR MSN 0928

QTR MSN 1566-1648 1773-1895 1957-2097 2121-2288

QTR MSN 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR ALL

QTR MSN 0928

QTR MSN 1566-3071

QTR MSN 0928

QTR MSN 1566-1895 1957

QTR MSN 1928 2097-3071

QTR MSN 0928-1895 1957-2097 2121-3071

QTR MSN 1928 2107

QTR MSN 0928

QTR MSN 1566-1895 1957-2097 2121-3071

QTR MSN 1928 2107

QTR MSN 0928

QTR MSN 1566-1895 1957-2097 2121-3071

QTR MSN 1928 2107

QTR MSN 0928-1895 1957-2097 2121-3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928

QTR MSN 1566-3071

QTR ALL

QTR MSN 0928

QTR MSN 1566-2341

QTR MSN 3071

QTR MSN 0928

QTR MSN 1566-3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1928 2107

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 0928

QTR MSN 1566-1648 1773-2288

QTR MSN 1656 2341

QTR MSN 3071

QTR MSN 0928

QTR MSN 1566-3071

QTR ALL

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR ALL

QTR MSN 0928

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 1566-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288

QTR MSN 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR ALL

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 3071

QTR MSN 0928

QTR MSN 1656

QTR MSN 1566-1648 1773-1895 1957-2097 2121-2341

QTR MSN 1928 2107

QTR MSN 3071

QTR ALL

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR ALL

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1928 2107

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288 3071

QTR MSN 1656 2341

QTR MSN 1928 2107

QTR ALL

QTR MSN 1928 2107

QTR MSN 0928-1648 1773-1895 1957-2097 2121-2288

QTR MSN 3071

QTR MSN 1656 2341

QTR ALL

A319 QUICK REFERENCE CHECK LISTREV. 06ENGINE TAILPIPE FIREInternal 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 theMASTER switch is turned off.CAUTIONExternal fire agents can cause severe corrosive damage and should, therefore,only be considered after having applied the following procedure: MAN START (if manual start performed) . OFFENG MASTER (affected) . OFFNote: Do not press the engine fire pushbutton, since this would cut off theFADEC power supply, which would prevent motoring sequence. AIR BLEED PRESS . ESTABLISHSelect the APU, or opposite BLEED, to motor the engine.If APU BLEED is not available, and the opposite engine is shut down,connect external pneumatic power (if readily available). BEACON . ONENG MODE SEL.CRANK MAN START . ONThe start valve automatically reopens, when N2 is below 10 %. When burning has stopped: MAN START . OFF ENG START SEL . NORM Maintenance action is due.(AIRBUS QRH 2.23 : REV 37 / SEQ 035)RVSM CONTINGENCYATC. INFORMATC must be informed of any of the following equipment failures: All Altitude Control Systems Loss of redundancy of altimeter systems Loss of thrust on an engine requiring descent Any piece of equipment that affects the ability of the aircraft to maintain the FL.ATC will take immediate action to provide a minimum of 2000 ft vertical separationfrom all other aircraft.During severe turbulence encounters ATC must be informed.ON GROUND EMER EVACUATION AIRCRAFT / PARKING BRK . STOP/ ON ATC (VHF 1) . NOTIFY CABIN CREW (PA) .ALERT P (only if MAN CAB PR has been used). CHECK ZEROIf not zero, MODE SEL on MAN, V/S CTL FULL UP.ENG MASTERS 1 and 2. OFF FIRE P/Bs (ENG and APU) . PUSH AGENTS (ENG and APU).AS RQRD IF EVACUATION REQUIRED : EVACUATION. INITIATEIF EVACUATION NOT REQUIRED : CABIN CREW and PASSENGERS (PA) . NOTIFY(AIRBUS QRH 7.00 : REV 40 / SEQ 001)(AIRBUS QRH 7.01 : REV 40 / SEQ 320)QTR/FO/062

A320 QUICK REFERENCE CHECK LISTREV. 07ENGINE TAILPIPE FIREInternal 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 theMASTER switch is turned off.CAUTIONExternal fire agents can cause severe corrosive damage and should, therefore,only be considered after having applied the following procedure: MAN START (if manual start performed) .OFFENG MASTER (affected) .OFFNote: Do not press the engine fire pushbutton, since this would cut off theFADEC power supply, which would prevent motoring sequence. AIR BLEED PRESS . ESTABLISHSelect the APU, or opposite BLEED, to motor the engine.If APU BLEED is not available, and the opposite engine is shut down,connect external pneumatic power (if readily available). BEACON .ONENG MODE SEL . CRANK MAN START .ONThe start valve automatically reopens, when N2 is below 10 %. When burning has stopped: MAN START .OFF ENG START SEL. NORM Maintenance action is due.(AIRBUS QRH 2.23 : REV 37 / SEQ 035)RVSM CONTINGENCYATC . INFORMATC must be informed of any of the following equipment failures: All Altitude Control Systems Loss of redundancy of altimeter systems Loss of thrust on an engine requiring descent Any piece of equipment that affects the ability of the aircraft to maintain the FL.ATC will take immediate action to provide a minimum of 2000 ft vertical separationfrom all other aircraft.During severe turbulence encounters ATC must be informed.ON GROUND EMER EVACUATION AIRCRAFT / PARKING BRK.STOP/ ON ATC (VHF 1) .NOTIFY CABIN CREW (PA) . ALERT P (only if MAN CAB PR has been used). CHECK ZEROIf not zero, MODE SEL on MAN, V/S CTL FULL UP.ENG MASTERS 1 and 2 .OFF FIRE P/Bs (ENG and APU) . PUSH AGENTS (ENG and APU) .AS RQRD IF EVACUATION REQUIRED : EVACUATION. INITIATEIF EVACUATION NOT REQUIRED : CABIN CREW and PASSENGERS (PA) .NOTIFY(AIRBUS QRH 7.00 : REV 40 / SEQ 001)(AIRBUS QRH 7.01 : REV 40 / SEQ 105)QTR/FO/063

A321 QUICK REFERENCE CHECK LISTREV. 06ENGINE TAILPIPE FIREInternal 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 theMASTER switch is turned off.CAUTIONExternal fire agents can cause severe corrosive damage and should, therefore,only be considered after having applied the following procedure: MAN START (if manual start performed) .OFFENG MASTER (affected) .OFFNote: Do not press the engine fire pushbutton, since this would cut off theFADEC power supply, which would prevent motoring sequence. AIR BLEED PRESS . ESTABLISHSelect the APU, or opposite BLEED, to motor the engine.If APU BLEED is not available, and the opposite engine is shut down,connect external pneumatic power (if readily available) BEACON .ONENG MODE SEL . CRANK MAN START .ONThe start valve automatically reopens, when N2 is below 10 %. When burning has stopped: MAN START .OFF ENG START SEL. NORM Maintenance action is due.(AIRBUS QRH 2.23 : REV 37 / SEQ 035)RVSM CONTINGENCYATC . INFORMATC must be informed of any of the following equipment failures: All Altitude Control Systems Loss of redundancy of altimeter systems Loss of thrust on an engine requiring descent Any piece of equipment that affects the ability of the aircraft to maintain the FL.ATC will take immediate action to provide a minimum of 2000 ft vertical separationfrom all other aircraft.During severe turbulence encounters ATC must be informed.ON GROUND EMER EVACUATION AIRCRAFT / PARKING BRK.STOP/ ON ATC (VHF 1) .NOTIFY CABIN CREW (PA) . ALERT P (only if MAN CAB PR has been used). CHECK ZEROIf not zero, MODE SEL on MAN, V/S CTL FULL UP.ENG MASTERS 1 and 2 .OFF FIRE P/Bs (ENG and APU) . PUSH AGENTS (ENG and APU) .AS RQRD IF EVACUATION REQUIRED : EVACUATION. INITIATEIF EVACUATION NOT REQUIRED : CABIN CREW and PASSENGERS (PA) .NOTIFY(AIRBUS QRH 7.00 : REV 40 / SEQ 001)(AIRBUS QRH 7.01 : REV 40 / SEQ 212)QTR/FO/064

REV. 06A319/A320/A321 NORMAL CHECK LISTPAGE 1 OF 2BEFORE STARTDESCENTGEAR PINS and COVERS REMOVEDMOBILE PHONES OFF (B)COCKPIT PREP COMPLETED (B)ADIRS NAVBARO REF SET / X-CHECKED (B)BRIEFING CONFIRMEDSEAT BELTS ONECAM STATUS CHECKEDBRIEFING CONFIRMED-------------- CLEARED TO ALTITUDE -------------BARO REF QNH / X-CHECKED (B)---------------- LOADSHEET -----------------PARK BRAKE ONSIGNS ON / AUTOFUEL PUMPS ON / KGS CHECKEDT.O SPDS / FLEX TEMP SET (B)PUSH/ STARTWINDOWS AND DOORS CLOSED (B)BEACON ONTHR LEVERS IDLEA/SKID & NW STRG AS RQRDNW STRG DISC MSG AS RQRDAFTER STARTASKID & NW STRG ONANTI ICE AS RQRDECAM STATUS CHECKEDTRIMS % / ZEROGROUND CREW CLEARANCE RECEIVEDBEFORE TAKE OFFFLIGHT CONTROLS CHECKED (B)FLAP SETTING CONF (B)T.O. SPD / FLX TEMP SET (B)ATC SETECAM MEMO T/O NO BLUEAUTO BRK MAXSIGNS ONSPLRS ARMEDFLAPS T.O.T.O. CONFIG NORM--------------- ENTERING RUNWAY --------------CABIN SECURED / SIGNALLEDPACKS AS RQRDAFTER TAKE OFFLDG GEAR UPECAM MEMO CHECKED--------------- CLEARED TO FL -----------------LANDINGCABIN SECURED / SIGNALLEDA/THR SPEED / OFFECAM MEMO LDG NO BLUEL/G DOWNSIGNS ONSPLRS ARMEDFLAPS SETAFTER LANDINGWX RADAR . OFFPRED W/S . OFFSPOILERS. DISARMEDFLAPS . RETRACTEDTCAS .STBYAPU . STARTSHUTDOWNPARK BRAKE AS RQRDENGINES OFFSEAT BELTS OFFFUEL PUMPS OFFBEACON OFFSECURING THE AIRCRAFTOXYGEN . OFFADIRS. OFFNO SMOKING . OFFEMER EXIT LTS. OFFAPU BLEED.OFFEXT PWR .AS RQRDAPU MASTER SW.OFFBATTERIES.OFFBEFORE LEAVING THE AIRCRAFTLPC AS RQRD (B)TRIP KIT AS RQRD (B)NOTES:1) PNF reads PF replies2) . PNF reads PNF replies .BARO REF STD / X-CHECKED (B)3) (B) PNF Reads and both PF then PNF replies

REV. 06A319/A320/A321 NORMAL CHECK LISTPAGE 2 OF 2PRELIMINARY COCKPIT PREPARATIONGEAR PINS and COVERS . REMOVEDENGINE PANEL . CHECKLANDING GEAR LEVER . DOWNBATTERIES . 25.5V/ AUTODU’S. ONPARK BRAKE .CHECKED / AS RQRDFLAP LEVER . CHECKEDSPEED BRAKE LEVER.DISARMEDECAM. CHECKEDTURBULENCE SPEEDSBelow ----- Above20000 feetA319/A320A321250 --- 275 / M0.76270 --- 300 / M0.76TAKE-OFF BRIEFAPPROACH BRIEFAIRCRAFT TYPE / EMERGENCIES / MEL /NOTAMS / SIG. WEATHER/ RETURNALTERNATE / RUNWAY / FLAP / ACCEL ALT /TRANSITION ALT / TERRAIN / PERFORMANCERESTRICTIONS / MINIMUM SAFE ALTITUDE /SID / RADIO AIDS / FMGC / FD/ REVIEW.AIRCRAFT TYPE / CONFIGURATION /NOTAMS/ WEATHER / QNH / TRANSITIONLEVEL/ MINIMUM SAFE ALTITUDE/ STAR/APPROACH/ AIRFIELD ELEVATION/ GOAROUND/ RUNWAY/ STOPPING/ RADIO AIDS /ALTERNATE/ FUEL CAPABILITY/ REVIEW.ALL WEATHER OPERATIONS BRIEFING GUIDEIn addition to the normal approach briefing the following items should be covered:1) CREW QUALIFICATION – Both members qualified for approach type2) GROUND & AIRCRAFT EQUIPMENT STATUS – All equipment for approach is serviceable.3) ALTERNATE – Weather above minima required and fuel sufficient for diversion.4) DOWNGRADE OPTIONS – Options with regard to current RVR. Any downgrade option to be takenabove 1000 feet.5) FLIGHT DECK LIGHTING – Internal lights to be set to minimum brightness consistent with viewinginstruments.6) SEAT POSITION – Captain’s seat affords good view over a/c nose and F/O a clear view ofinstruments.WEIGHTS/KGMTOWMLWMZFWMAX FUEL*A31975 50062 50058 50020 900A32077 00066 00062 50018 600A32193 00077 80073 80020 800A7-ABR77 00064 50061 00018 600* Based on SG 0,780

ENGINE OUT MISSED APPROACH(EOMA) A319-133REV. 00PAGE 1 OF 2Published Missed Approach Vs Takeoff EOSIDThe flow chart details the process of determining whether an aircraft hasthe performance to meet the published missed approach procedure in theengine out scenario. If it does not, then the takeoff EOSID shall be flownas the EOMA.QTR/FO/105

ENGINE OUT MISSED APPROACH(EOMA) A319-133REV. 00PAGE 2 OF 2Maximum Structural Landing Mass (62,500kg)Approach Climb CONF 3PressureAltitude0 ft1000 ft2000 ft3000 ft4000 ft5000 ft6000 ft7000 ftISA 30and below4800 ft5600 ft6500 ft7400 ft8100 ft8900 ft9600 ft10300 ftISA 35ISA 404800 ft5600 ft6500 ft7200 ft7900 ft8600 ft9300 ft4600 ft4300 ft4000 ft6700 ft7400 ftTable 1: Maximum Level-off Altitude TableMaximum Structural Landing Mass (62,500kg)Approach Climb CONF 2PressureAltitude0 ft1000 ft2000 ft3000 ft4000 ft5000 ft6000 ft7000 ft8000 ft9000 ftISA 30And below6000 ft6800 ft7700 ft8500 ft9200 ft10000 ft10700 ft11400 ft12000 ft12600 ftISA 35ISA 406000 ft6800 ft7700 ft8400 ft9100 ft9800 ft10400 ft11100 ft11700 ft12200 ft5800 ft6400 ft5100 ft7800 ft8500 ft9200 ft9800 ft10400 ftTable 2: Maximum Level-off Altitude TableBased on:Climbing on Runway heading followed by a 180 turn in headingAC ON (AC OFF correction not calculated!)VLS 5 (Correction for increased approach speed not calculated

ENGINE OUT MISSED APPROACH(EOMA) A320-232REV. 00PAGE 1 OF 2Published Missed Approach Vs Takeoff EOSIDThe flow chart details the process of determining whether an aircraft hasthe performance to meet the published missed approach procedure in theengine out scenario. If it does not, then the takeoff EOSID shall be flownas the EOMA.QTR/FO/106

ENGINE OUT MISSED APPROACH(EOMA) A320-232REV. 00PAGE 2 OF 2Maximum Structural Landing Mass (66,000kg)Approach Climb CONF 3PressureISA 25 andISA 30ISA 35ISA 40Altitudebelow0 ft1000 ft2000 ft3000 ft4000 ft5000 ft6000 ft7000 ft5700 ft6300 ft7100 ft7800 ft8400 ft9100 ft9700 ft10300 ft5700 ft6300 ft6900 ft7600 ft8200 ft8800 ft9500 ft5100 ft5700 ft6300 ft7000 ft7600 ft8300 ft4500 ft5100 ft5700 ft6400 ftTable 1: Maximum Level-off Altitude TableMaximum Structural Landing Mass (66,000kg)Approach Climb CONF 2PressureISA 25 andISA 30ISA 35ISA 40Altitudebelow0 ft1000 ft2000 ft3000 ft4000 ft5000 ft6000 ft7000 ft6000 ft6700 ft7400 ft8100 ft8700 ft9400 ft10000 ft10600 ft6000 ft6600 ft7200 ft7900 ft8500 ft9100 ft9700 ft10400 ft5400 ft6000 ft6600 ft7300 ft7900 ft8600 ft9200 ftTable 2: Maximum Level-off Altitude TableBased on:Climbing on Runway heading followed by a 180 turn in headingAC ON (AC OFF correction not calculated!)VLS 5 (Correction for increased approach speed not calculated)4700 ft5400 ft6000 ft6600 ft7300 ft

ENGINE OUT MISSED APPROACH(EOMA) A321-232REV. 00PAGE 1 OF 2Published Missed Approach Vs Takeoff EOSIDThe flow chart details the process of determining whether an aircraft hasthe performance to meet the published missed approach procedure in theengine out scenario. If it does not, then the takeoff EOSID shall be flownas the EOMA.QTR/FO/107

REV. 00ENGINE OUT MISSED APPROACH(EOMA) A321-232PAGE 2 OF 2Maximum Structural Landing Mass (77,800kg and below)Approach Climb CONF 3PressureAltitude0 ft1000 ft2000 ft2500 ftISAISA 20ISA 25ISA 304500 ft5100 ft5700 ft5900 ft4300 ft5000 ft5600 ft5900 ft3800 ft4500 ft5100 ft3200 ftISA 35ISA40Table 1: Maximum Level-off Altitude TableLanding Mass 74,000kg and belowApproach Climb CONF 3PressureAltitude0 ft1000 ft2000 ft3000 ft4000 ftISAISA 20ISA 25ISA 30ISA 355300 ft5800 ft6300 ft6900 ft7400 ft5100 ft5800 ft6300 ft6900 ft7400 ft4600 ft5300 ft5900 ft6500 ft4000 ft4700 ft5300 ft3300 ftISA 40Table 2: Maximum Level-off Altitude TableMaximum Structural Landing Mass (77,800kg and below)Approach Climb CONF 2PressureAltitude0 ft1000 ft2000 ft3000 ft4000 ftISAISA 20ISA 25ISA 30ISA 355500 ft6100 ft6600 ft7100 ft7600 ft5400 ft6000 ft6600 ft7100 ft7600 ft4900 ft5500 ft6100 ft6700 ft4200 ft4900 ft5500 ft3500 ftISA 40Table 3: Maximum Level-off Altitude TableLanding Mass 74,000kg and belowApproach Climb CONF 2PressureAltitude0 ft1000 ft2000 ft3000 ft4000 ft5000 ftISAISA 20ISA 25ISA 30ISA 355700 ft6400 ft6900 ft7400 ft7900 ft8400 ft5700 ft6300 ft6800 ft7400 ft7900 ft8400 ft5200 ft5800 ft6400 ft7100 ft7700 ft8300 ft4600 ft5200 ft5900 ft6600 ft3900 ft4600 ftTable 4: Maximum Level-off AltitudeBased on:Climbing on Runway heading followed by a 180 turn in headingAC ON (AC OFF correction not calculated!)VLS 5 (Correction for increased approach speed not calculated).ISA 40

318/319/320/321 QRH VOL.3 REV040BCROSS REFERENCE TABLETHIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCEBETWEEN :- THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES- THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS 7-ADI2288A7-ADJ2341A7-CJB3071QTR0.0403 OCT 2006PAGE : CRT001

318/319/320/321 QUICK REFERENCE HANDBOOKREV040BLIST OF EFFECTIVE PAGES (LEP)M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----M ---PAGE--- SEQ- --REV-- ----VALIDATION --------------------------------NN0 .000010 .00A0010 .010 .02001001LIST OF CODESLIST OF CODES0 .02A001LIST OF CODES0 .02B001LIST OF CODES0 .02C001LIST OF CODES0 .02D001LIST OF CODES0 .02E001LIST OF CODES0 .02F001LIST OF CODES0 .02G001LIST OF CODES0 .02H001LIST OF CODES0 .02I001LIST OF CODES0 .02J001LIST OF CODES0 .02K001LIST OF CODES0 .02L001LIST OF CODES0 .02M001LIST OF CODES0 .02N001LIST OF CODES0 .02O001LIST OF CODES0 .03-001LIST OF TEMPORARY REVISIONS0 .04-001CROSS REFERENCE TABLE0 .06-001LIST OF EFFECTIVE PAGES0 .07-001LIST OF MOD/MP/SB1 .000011 .011 .022051001 .011 .024101001 .031 .042003501 .0

A319 QUICK REFERENCE CHECK LIST REV. 06 ENGINE TAILPIPE FIRE Internal engine fire may be encountered during engine start or engine shutdown. It may be seen by t