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•FUEL MODE SEL (MAN) 31 FWS FWC 1(2) FAULT FWC On ground: Pull, then push, the C/B of the affectedFWC: ‐ FWC 1 (E2 on 49VU) ‐ FWC 2.(Q7 on 121VU) Wait 50 s after pushing the C/Bs. In flight: Pull, then push, the C/B of the affected FWC: ‐ FWC 1 (E2 on 49VU) ‐ FWC 2 (Q7 on 121VU) Braking malfunction BSCU Refer to FCOM/PRO-SUP-32 BSCU Reset 32 L/G LGCIU 1(2) FAULT LGCIU 1(2) On ground only: The flight crew must reset the LGCIU after depressurizing the green hydraulic system. ‐ ENG MASTER switch 1 OFF ‐ PTU OFF When there is no green hydraulic pressure: ‐ To reset LGCIU 1: ▪Pull C/B Q34 on 121VU, then C09 on 49VU ▪Wait for 15 s , then push the C/Bs ‐ To reset LGCIU 2: ▪Pull C/B Q35 on 121VU ▪Wait for 15 s , then push the C/B NAV TCAS FAULT TCAS On ground only: ‐ Pull C/B K10 on 121VU. ‐ Wait 5 s, then push the C/B. 34 ISIS malfunction ISIS On ground only: With aircraft not moving: ‐ Pull C/B F12 on 49VU, ‐ Wait 5 s ,then push the C/B, ‐ Normal operation is expected after approximately 2 min. Note: In the case of small aircraft motion during the C/B reset (refueling, cargo loading conditions, etc.), the ATT red flag may appear on the ISIS. In this case, press the RST P/B for 2 s wait 2 min additional to recover normal operation. 46 ATSU Malfunction ATSU An ATSU reset should be attempted, if: key selection has no effect on any of the MCDU ATSU DATALINK submenus. On ground, or in flight: ‐ Pull the C/Bs in the following order: L16, L15 on 121VU ‐ Wait 5 s , then:. ‐ Push the C/Bs in the following order: L15, L16. 70 ENG IGN A+B FAULT FADEC and EIU Refer to FCOM/PRO-ABN-70-K ENG 1(2) IGN FAULT (IGN A + B Fault) if applicable. To be continued on next page ABN-80 32/32 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 A318/A319/A320/A321 FLEET , Continued from previous page ENG 1(2) FADEC A(B) FAULT FADEC Refer to FCOM/PRO-ABN-70 ENG 1(2) FADEC A(B) FAULT if applicable. EMERGENCY EVACUATION AIRCRAFT/PARKING BRK..............................................................................................................STOP/ON ATC (VHF 1)..................................................................................................................................... NOTIFY CABIN CREW (PA)............................................................................................................................ ALERT ΔP (only if MAN CAB PR has been used)...............................................................................CHECK ZERO If not zero, MODE selector on MAN, V/S CTL FULL UP. ENG MASTERS (ALL)............................................................................................................................O FF FIRE Pushbuttons (ALL : ENG and APU)............................................................................................. PUSH AGENTS (ENG and APU)...............................................................................................................AS RQRD If Evacuation required: EVACUATION................................................................................................................ ............ INITIATE If Evacuation not required: CABIN CREW and PASSENGERS (PA)..................................................................................... NOTIFY ABN-80 1/32 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 A318/A319/A320/A321 FLEET , , CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE LANDING WEIGHT......................................................................................................................... ...CHECK if the aircraft weight is above the maximum weight for circling in CONF 3 (given in the table below): The aircraft cannot maintain flight level with CONF 3 and the landing gear down. FOR LDG............................................................................................................................US E FLAP 3 CONF 3 is preferred, to minimize a configuration change in short final. GPWS LDG FLAP 3............................................................................................................................ ON Delay gear extension. Note: If the approach is flown at less than ‐ 750 ft RA, the “L/G NOT DOWN” warning will be www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：空客320快速检查单QRH QUICK REFERENCE HAND BOOK8
