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承接2017年12月12日版本空客A319-115 飞机飞行手册翻译任务

时间:2018-01-06 08:58来源:蓝天飞行翻译公司 作者:民航翻译 点击:


CAT II / CAT III Operations
23 COMMUNICATIONS
SATCOM Voice System
24 ELECTRICAL POWER
Electrical
28 FUEL
Fuel and Additive Specifications
Usable Fuel
Fuel Imbalance
Fuel Temperature Limits
29 HYDRAULIC
Hydraulics Fluid
32 LANDING GEAR
Tire Speed
34 NAVIGATION
Weather Radar
Inertial Reference System (IRS)
Reduced Vertical Separation Minimum (RVSM)
Mode S - EHS Enhanced Surveillance
Mode S - EHS Enhanced Surveillance
Mode S - ADS-B Out Enhanced Surveillance
46 INFORMATION SYSTEMS
Airline Operation Control Applications
49 AUXILIARY POWER UNIT
Auxiliary Power Unit (APU)
70 POWER PLANT
Main Engines
Engine Parameters
Reverse Thrust
Oil
Reduced Thrust Takeoff
Operations in Icing Conditions
EMERGENCY PROCEDURES
Preliminary Pages
GENERAL
INTRODUCTION
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE
21 AIR COND/PRESS/VENT
CAB PR - EXCESS CAB ALT
CAB PR - EXCESS RESIDUAL PR
24 ELECTRICAL POWER
ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED)
26 FIRE/SMOKE
GENERAL
ENG 1 (2) FIRE (In Flight)
ENG 1 (2) FIRE (On Ground)
APU FIRE
SMOKE - FWD or AFT CARGO SMOKE
SMOKE/FUMES/AVNCS SMOKE
REMOVAL OF SMOKE/FUMES
27 FLIGHT CONTROLS
F/CTL - L + R ELEV FAULT
F/CTL - FLAP LVR NOT ZERO
29 HYDRAULIC
HYD - G + B SYS LO PR
HYD - B + Y SYS LO PR
HYD - G + Y SYS LO PR
32 LANDING GEAR
L/G - GEAR NOT DOWNLOCKED
LOSS OF BRAKING
34 NAVIGATION
Abnormal V Alpha Prot
NAV - ADR 1+2+3 FAULT
70 POWER PLANT
ALL ENGINES FAILURE
DUAL ENG FAILURE (BOTH ENGINES FLAME OUT)
ENG - 1(2) OIL LO PR
90 MISCELLANEOUS
STALL RECOVERY
EMER DESCENT
EMER DESCENT
EMERGENCY EVACUATION
DITCHING
FORCED LANDING
Emergency Landing (All Engines Failure)
ABNORMAL PROCEDURES
Preliminary Pages
GENERAL
INTRODUCTION
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE
ONE ENGINE INOPERATIVE
TO TAKEOFF
ENGINE FAILURE BEFORE V1 (REJECTED TAKEOFF)
ENGINE FAILURE BETWEEN V1 AND V2
ENGINE FAILURE DURING INITIAL CLIMB OUT
LDG APPROACH AND LANDING
APPROACH AND LANDING
MISSED APPROACH (FROM INTERMEDIATE APPROACH CONFIGURATION)
BALKED LANDING
21 AIR COND/PRESS/VENT
AIR - PACK 1 + 2 FAULT
CAB PR - SYS 1 + 2 FAULT
CAB PR - SAFETY VALVE OPEN
COND - HOT AIR FAULT
VENT - SKIN VALVE FAULT
22 AUTO FLIGHT SYSTEM
AUTO FLIGHT SYSTEM
AUTO FLT - FCU 1(2) FAULT
AUTO FLT - RUD TRV LIM SYS
AUTO FLT - FAC 1+2 FAULT
AUTO FLT - YAW DAMPER SYS
22-CATII FAILURES OR WARNINGS DURING A CAT II APPROACH WITH OR WITHOUT AUTOMATIC LANDING
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