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See below INOP SYS To be continued on next page A318/A319/A320/A321 FLIGHT CREW OPERATING MANUAL PROCEDURES ABNORMAL AND EMERGENCY PROCEDURES POWER PLANT A318/A319/A320/A321 FLEET PRO-ABN-70 P 136/194 FCOM 19 AUG 10 ENG DUAL FAILURE (Cont'd) G+Y HYD F/CTL PROT STABILIZER R AIL REVERSER 1+2 ADR 2+3 IR 2+3 RA 1+2 SPLR 1+2+4+5 ELAC 2 SEC 2+3 FLAPS YAW DAMPER A/CALL OUT AP 1+2 A/THR FUEL PUMPS ANTI SKID N/W. STEER AUTO BRK L/G RETRACT CAB PR 1+2 PACK 1+2 (1) AL2t landing gear extension, control reverts to direct law in pitch as well as in roll (Refer to 00011770 **Not found**). A slight transient pitch up may occur, depending on the frozen THS position. (2) 7 full brake applications are available. A318/A319/A320/A321 FLIGHT CREW OPERATING MANUAL PROCEDURES ABNORMAL AND EMERGENCY PROCEDURES POWER PLANT A318/A319/A320/A321 FLEET PRO-ABN-70 P 137/194 FCOM 19 AUG 10 ENG DUAL FAILURE Applicable to: L2 The ENG DUAL FAILURE warning inhibits the ELEC EMER CONFIG warning. The FCOM Volume 3 includes all steps of the ECAM ENG DUAL FAILURE procedure. However, to facilitate handling of all the ECAM procedures associated with a dual engine failure, it is recommended using the QRH ENG DUAL FAILURE paper procedure that also includes the DITCHING and FORCED LANDING procedures. When applying the QRH ENG DUAL FAILURE paper procedure: If one or more engines are recovered, apply the corresponding ‐ ECAM procedure instead ‐ If no engines are recovered, continue to apply the QRH ENG DUAL FAILURE paper procedure. If time permits, clear ECAM alerts, and check the STATUS SD page. L1 LAND ASAP ENG MODE SEL............................................................................................................................IGN L2 An immediate relight attempt is made. L1 THR LEVERS............................................................................................................................. IDLE OPTIMUM RELIGHT SPD........................................................................................................280 KT L2 The optimum airspeed to allow an effective windmilling start attempt is 280 kt. Note: In the case of an “ENG DUAL FAILURE” during high power operations (i.e. climb, cruise), it is mandatory to fly at or above the optimum relight speed in order to prevent engine core lock. In case of a speed indication failure (volcanic ash), the pitch attitude for optimum relight speed is 2.5 ° down. For weight above 50 000 kg/110 000 lb, raise the nose by 1 ° for every additional 10 000 kg/22 000 lb (e.g. if weight is 60 000 kg/132 000 lb pitch is 1.5 ° down). At 280 kt, the aircraft can fly up to about: 2.2 nm per 1 ‐ 000 ft at 50 000 kg/110 000 lb ‐ 2.5 nm per 1 000 ft at 60 000 kg/132 000 lb ‐ 2.7 nm per 1 000 ft at 70 000 kg/154 000 lb L1 EMER ELEC PWR (IF EMER GEN NOT IN LINE)...............................................................MAN ON L2 Pressing EMER ELEC PWR MAN ON pb allows extension of RAT and emer gen coupling. L1 VHF 1/HF 1 /ATC 1.............................................................................................................. USE L2‐ In Elec emer configuration only VHF 1, HF 1 and ATC 1 are supplied. L12‐ Notify traffic control of the nature of the emergency and state intention. To be continued on next page A318/A319/A320/A321 FLIGHT CREW OPERATING MANUAL PROCEDURES ABNORMAL AND EMERGENCY PROCEDURES POWER PLANT A318/A319/A320/A321 FLEET PRO-ABN-70 P 138/194 FCOM 19 AUG 10 ENG DUAL FAILURE (Cont'd) If there is no contact with air traffic control, switch to code A7700 or transmit a distress message on one of the following frequencies, VHF frequency 121.5 MHz, HF 2 182 kHz or 8 364 kHz. L1 FAC 1.......................................................................................................................... OFF THEN ON L2 Aircraft is out of trim due to right aileron up float. Resetting FAC 1 permits to recover rudder trim even if no indication is available. L1 IF NO RELIGHT AFTER 30 S: ENG MASTERS...................................................................................................... OFF 30 S/ON L2 Engine masters sw must be left OFF for 30 s to allow ventilation of combustion chamber. L1 If UNSUCCESSFUL: APU (IF AVAIL)........................................................................................................... START L2 If the APU is available, APU may be started when below FL 250, and APU BLEED may be used for engine start below FL 200 if the speed is ≥ 150 kt, or below FL 150 if the speed is www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320机组操作手册FLIGHT CREW OPERATING MANUAL 11
