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SPEED............................................................................................................................. ........320/0.82 See the following table for the IAS/M relationship for 0.82 FL 390 370 350 330 310 290 280 and below MAX SPD 252 265 278 290 305 315 320 WHEN L/G DN: DIRECT LAW At landing gear extension, control reverts to direct law in pitch, as well as in roll . Note: Use manual control of cabin pressurizationRefer to FCOM/99 Duref Cible QRH MODE SEL..............................................................................................................................M AN MAN V/S CTL...................................................................................................................AS RQRD STATUS MAX SPEED.................................................................. 320/0.82 RUD WITH CARE ABV 160 kt See (1) APPR PROC: FOR LDG...........................................................................USE FLAP 3 GPWS LDG FLAP 3......................................................................... ON APPR SPD..................................................................... VREF + 10 KT LDG DIST PROC........................................................................APPLY Refer to FCOM/99 Duref Cible QRH ? FOR L/G GRVTY EXTN (not on the ECAM): GRVTY GEAR EXTN handcrank..................................................... ............................................................................ PULL AND TURN L/G LEVER........................................................................... DOWN WHEN L/G DN : DIRECT LAW ? DURING FINAL APPR V/S CTL............................................................................ FULL UP Note: In case of a go-around, respect maximum speed 215 kt in CONF 1+F, due to the loss of flap auto retraction to CONF 1. CAUTION Check that the outflow valve is fully open, and that cabin altitude is at airfield elevation before opening the doors. INOP SYS ATT LIMIT OVSP LIMIT ALPHA LIMIT ADR 1+2+3 WINDSHEAR DET RUD TRV LIM 1+2 A/THR AP 1+2 GPWS Other INOP SYS CAB PR1+2 RAT auto extension ATC ALTI MODE TCAS ? L/G RETRACT (1) At slats’ extension, full rudder travel authority is recovered. ABN-34 2/10 AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1 ABNORMAL AND EMERGENCY PROCEDURES 30 AUG 10 A318/A319/A320/A321 FLEET ALL ADR OFF SPD................................................................................................................................... FLY THE GREEN Fly within the green area of the speed scale to ensure safe flight. For slats/flaps retraction, it is better to fly at the top of the green area of the speed scale. CAUTION The altitude displayed on the PFD is a GPS altitude. BACK UP NAV................................................................................................................................ ........USE When ADRs are OFF, both FMs are lost. Revert to Back Up Nav via the NAV B/UP prompt on the MCDU MENU page. NAVAID TUNING.......................................................................................................................... .USE RMP Set both RMPs to NAV. MANUAL CABIN PRESSURE CONTROL MODE SEL.................................................................................................................................. .......MAN MAN V/S CTL............................................................................................................................AS RQRD MAN CAB PR CTL TGT V/S : CLIMB 500 ft/min DESC 300 ft/min A/C GPS ALT CAB ALT TGT 410 350 300 250 <200 8000 6500 5000 2500 0 FOR APPROACH SPD............................................................................................................................... FLY THE GREEN Before extending the slats/flaps, it is better to fly at the bottom of the speed scale green area, and to be in straight flight. FOR LDG.............................................................................................................................. USE FLAP 3 LDG DIST PROC............................................................................................................................A PPLY Refer to FCOM/99 Duref Cible QRH APPR SPD........................................................................................................................... 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 BOOK4
