時(shí)間：2018-01-06 08:58來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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NAV - ADR 1+2 FAULT NAV - ADR 1+3 FAULT NAV - ADR 2+3 FAULT ADR 1+2+3 FAULT NAV ADR DISAGREE UNRELIABLE AIRSPEED INDICATION UNRELIABLE AIRSPEED INDICATION 36 PNEUMATIC AIR - ENG 1(2) BLEED HI TEMP AIR - ENG 1(2) BLEED FAULT AIR - ENG 1+2 BLEED FAULT AIR - ENG 1(2) BLEED ABNORM PR AIR - X BLEED FAULT AIR - L (R) WING LEAK AIR - ENG 1(2) BLEED LEAK AIR - ENG 1(2) BLEED LO TEMP AIR - ENG 1 + 2 BLEED LO TEMP 52 DOORS DOOR - DOOR NOT CLOSED 70 POWER PLANT ENG - STALL ENG COMPRESSOR VANE/ENG STALL on ground ENG - FAIL ENG - SHUTDOWN ENG - REV PRESSURIZED ENG - REVERSE UNLOCKED ENG - REVERSER FAULT ENG - THR LEVER FAULT ENG - THR LEVER DISAGREE ENG - OIL HI TEMP ENG - FADEC FAULT ENG - FADEC HI TEMP (FADEC OVHT) ENG - N1 (N2) (EGT) OVERLIMIT ENG RELIGHT IN FLIGHT 90 MISCELLANEOUS BOMB ON BOARD OVERWEIGHT LANDING REJECTED TAKEOFF WITH ALL ENGINES OPERATIVE NORMAL PROCEDURES Preliminary Pages GENERAL Introduction PREFLIGHT CHECKS Electrical Cockpit Door Braking EfficiencyTest TAKEOFF Takeoff Procedure FLIGHT Buffet Onset Flight in Severe Turbulence APPROACH AND LANDING Normal Landing Balked Landing (AllEngines Operating) Reverse Thrust Autobrake 22 AUTO FLIGHT SYSTEM 22-CONF Demonstrated System Configuration AP/FD, Speed modes,Autothrust Takeoff Climb, Cruise, Descent Non Precision Approach CAT I ILS Approach CAT II ILS Approach CAT II/III ILS Approachand Automatic Approach Precision ApproachRadar (PAR) Go-around Altitude Loss afterAutomatic Go-around Initiation 22-NPA Non Precision Approach General Instrument Approach Using NAV Mode 22-PA Precision Approach CAT II and CAT IIIApproach and/or Automatic Landing Required Equipment for CAT II and CAT III Approach and Landing 28 FUEL Fuel System 30 ICE AND RAIN PROTECTION Operations in IcingConditions Rain Repellent (IfActivated) 34 NAVIGATION Ground ProximityWarning System (GPWS) Inertial ReferenceSystem (IRS) Reduced VerticalSeparation Minimum (RVSM) Windshear Warningand Guidance System Integrated Standby Instrument System (ISIS) 49 AUXILIARY POWER UNIT Auxiliary PowerUnit (APU) PERFORMANCE Preliminary Pages Summary of Highlights GENERAL Introduction Aircraft Configuration Maximum Demonstrated Crosswind at Takeoff and Landing AIRSPEED AND ALTITUDE CALIBRATION TAKEOFF Speed Corrections in Ground Effect Speed Corrections out of Ground Effect Altitude Corrections CRUISE (Clean Configuration) |
