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(5) Lost, when speed is below 50 kt. LGCIU SYS 1 Norm Norm Norm ABCU Norm Norm Norm L/G BRK PRESS IND Norm Norm Norm PARK BRK Norm Norm Norm LIGHTS EEMMEERR CCAKBPT NNoorrmm NNoorrmm NNoorrmm IR N° 1 only (2) N° 1 only (2) N° 1 only (2) ADR N° 1 only N° 1 only N° 1 only ADF N° 1 only Inop Inop VOR-MMR N° 1 only N° 1 only N° 1 only (1) DME N° 1 only Inop Inop VOR/DDRMI Norm Norm Norm (1) ATC N° 1 only Inop Inop NAV ISIS Norm Norm Norm (1) IR2 and IR3 are lost 5 min after failure of the main generators. But, if IR3 replaces IR1 (ATT-HDG selector at CAPT3), IR3 remains supplied (6) Lost, when speed is below 50 kt. ENG 1 BLEED Norm BMC 1 inop BMC 1 inop ENG 2 BLEED BMC 2 inop BMC 2 inop BMC 2 inop APU BLEED Inop Inop Inop (1) PNEU X BLEED (MAN CTL) Norm Inop Inop (7) Restored, when speed is below 100 kt. ECB - STARTER Norm (2) Inop Inop (1) APU FUEL LP VALVE Norm Norm Norm FUEL PUMP Norm Norm Norm (1) Restored, when speed is below 100 kt. (2) For APU start only. FADEC A + B (1) A + B (1) A + B (1) PWR PLT IGNITION A only A only A only HP FUEL VALVE closure Norm Norm Norm (1) Channels A and B are self-powered above 10 % N2. If N2 is below 10 % , only Channel A is powered. MISC MECH HORN Norm Norm Norm FLT ON BAT ONLY Flight time on batteries only may be increased to at least 30 min as follows: ENG MODE SEL................................................................................................................................. NORM ANTI ICE PITOT 1 C/B (D02).................................................................................................................PULL 26 V ADIRU 1 C/B (F07)........................................................................................................................PUL L CM 1 altitude, speed, and vertical speed indication on PFD are lost. Use standby instruments ? 7 min before landing: ANTI ICE PITOT 1 C/B (D02)....................................................................................................... RESET ? After 1 min: CAUTION This time delay is necessary to ensure reliable speed information even in icing conditions when the ADIRU is reset to ON. 26 V ADIRU 1 C/B (F07)........................................................................................................ RESET ABN-24 3/4 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 A318/A319/A320/A321 FLEET MSN ELEC EMER CONFIG SUMMARY CRUISE MAX SPD.................................................................................................................................. ......... 320 KT ALTN LAW : PROT LOST ONLY CAPT PITOT AND AOA HEATED FUEL: CTR TK UNUSABLE. COM: VHF1, ATC1, RMP1, only NAV: ILS1, VOR1, GPS1 (if MMR is installed) only LANDING CONF APPROACH SPEED Use FLAP 3 VAPP = VREF + 10 kt + APPR COR/140 kt APPROACH MINIMUM RAT SPEED 140 KT CAT 2 INOP SLATS FLAPS SLOW ? When L/G down: USE MAN PITCH TRIM. LANDING FLARE: Only 2 spoilers per wing. Direct law SPOILERS: Only 2 per wing NO?REVERSER BRAKING: ALTERNATE without antiskid MAX BRK PR 1000 PSI NO?NOSEWHEEL?STEERING GO-AROUND NIL ACTUAL LANDING DISTANCES (m) WITH FAILURE WITHOUT REV WEIGHT (1000 KG) 46 50 54 58 62 66 70 74 78 DRY runway 2 180 2 300 2 400 2 490 2 620 2 810 3 090 3 380 3 630 WET runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULL and apply LDG DIST Factor = 2.40 CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULL and apply LDG DIST Factor = 2.15 CORRECTIONS +1 000 ft above SL +10 kt tailwind DRY Runway +3 % +18 % Refer to ABN-80 VAPP CALCULATION for the approach speed computation method. ABN-24 4/4 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 Intentionally left blank A318/A319/A320/A321 FLEET MSN ABN-24 1/4 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 A318/A319/A320/A321 FLEET MSN ELEC EMER CONFIG SYS REMAINING ELEC EMER CONFIG SYS REMAINING EMER GEN RUNNING IN FLIGHT BAT ONLOYN THE GROUND PRESS AUTO SYS 1 Norm Norm Norm MAN PRESS CTL Inop Inop Inop (1) RAM AIR Norm Norm Norm PACK VALVE 1 Norm Closure Inop Closure Inop PACK VALVE 2 Closure Inop Closure Inop Closure Inop (1) AVIONIC VENT Norm Norm Partial www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A318/A319/A320/A321QRH快速检查单QUICK REFERENCE HAND BOOK3
