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Note: The fuel quantity indication will be re-established within one min. 28 Loss of fuel quantity indication or Simultaneous triggering of FUEL L XFR VALVE CLOSED and FUEL R XFR VALVE CLOSED, although FUEL SD indicates no anomaly. FQIC CAUTION The FUEL AUTO FEED FAULT ECAM caution will be lost for the remainder of the flight. In flight: If center tank ‐ is not empty, while one inner tank contains less than 5 000 kg (11 000 lb) of fuel: • FUEL MODE SEL (MAN) ‐ When center tank is empty: • CTR TK PUMP 1 and 2 (OFF) • 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. 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 38 Failure messages on the CIDS FAP in the cabin Vacuum System Controller On ground, or in flight: ‐ Pull C/B 35 MG on 2001VU, aft cabin, ‐ Wait 30 s , then push the C/B 35 MG. 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. ENG IGN A+B FAULT FADEC and EIU Refer to FCOM/PRO-ABN-70-K ENG 1(2) IGN 70 ENG 1(2) FADEC FAULT (IGN A + B Fault) if applicable. 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......................................................................................................................... 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 BOOK6
