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蓝天飞行翻译公司承接湾流G280公务机飞机飞行手册翻译任务(2)

时间:2014-12-02 10:10来源:蓝天飞行翻译公司 作者:公务机翻译 点击:


OXYGEN SYSTEM
ENGINE INSTRUMENTS AND CREW ALERTING SYSTEM (EICAS)
OMS
GENERAL EICAS RANGE MARKINGS COLORS
POWERPLANT EICAS INDICATIONS
FUEL EICAS INDICATIONS
FUEL TANK TEMPERATURE INDICATIONS
APU EICAS INDICATIONS
APU RPM
CAS MESSAGES
AUXILIARY POWER UNIT (APU)
APU OPERATION
APU GENERATOR LOAD LIMITS
MAXIMUM PERMISSIBLE EGT
MAXIMUM ROTOR SPEED
POWERPLANT
ENGINE GROUND START
ENGINE GROUND OPERATIONS
ENGINE IN FLIGHT OPERATIONS
ENGINE FUEL AND CONTROL SYSTEMS
ENGINE FUEL TEMPERATURE
PRIMARY ACCEPTABLE FUEL TYPES
OTHER ACCEPTABLE TYPE FUELS
ANTI-STATIC ADDITIVES
EGME-BASED FUEL ICING INHIBITORS
DiEGME-BASED FUEL ICING INHIBITORS
RUSSIAN (CIS) FUEL SYSTEM ICING INHIBITORS
FUNGICIDE/BIOCIDE INHIBITORS
ANTI-CORROSION ADDITIVES
ENGINE EXHAUST
THRUST REVERSERS
ENGINE OIL
OIL INLET TEMPERATURE
APPROVED OILS
OIL PRESSURE
Engine Oil Pressure
ENGINE STARTING
STARTER DUTY
Section II - Emergency Procedures
LIST OF FIGURES
EICAS WARNING MESSAGES
COLLECTOR CAS MESSAGE
SA (SITUATIONAL AWARENESS) CAS MESSAGE
GENERAL GUIDANCE
WARNING MESSAGES (RED)
ATA 21 - AIR CONDITION AND PRESSURIZATION
RAPID DECOMPRESSION
CABIN UNDERPRESSURIZATION
Oxygen Duration; 123.4 CU FT
Oxygen Pressure Versus Temperature
EMERGENCY DESCENT
BLEED AIR LEAK
DUAL FAILURE
SINGLE FAILURE
CABIN OVER PRESSURIZATION
ATA 22 - AUTO FLIGHT
AUTOMATIC DESCENT MODE (ADM)
ATA 26 - FIRE PROTECTION
ENGINE FIRE ON GROUND
ENGINE FIRE IN FLIGHT
APU FIRE
AIRCRAFT INTERIOR FIRE / SMOKE / FUMES
SECTION A: FIRE / SMOKE / FUMES IN COCKPIT, CABIN, OR BAGGAGE COMPARTMENT
SECTION B: SMOKE FROM AIR CONDITIONING OUTLETS (POSSIBLE BLEED AIR SOURCE)
SECTION C: ELECTRICAL FIRE / SMOKE SOURCE UNKNOWN
RIGHT AFT RADIO RACK HOT
ATA 27 - FLIGHT CONTROLS
Stall Recovery
ATA 28 - FUEL
FUEL LEAK
A. FUEL LEAKAGE IS VISIBLE OR SUSPECTED FROM WING / FUSELAGE
B. FUEL LEAKAGE IS NOT VISIBLE AND ONE OF THE FOLLOWING IS SUSPECTED
FUEL PRESSURE LOW
ATA 32 - LANDING
BLOWN TIRE DURING TAKEOFF
ATA 72-80 - ENGINE
TAKEOFF ABORT
ENGINE FAILURE DURING TAKEOFF ABOVE V1
SINGLE ENGINE FAILURE IN FLIGHT
ENGINE EXCEEDANCE
ENGINE SHUTDOWN IN FLIGHT
ENGINE RESTART IN FLIGHT
Engine Start Envelope
A. STARTER-ASSIST AIR-START (CROSS-BLEED)
B. WINDMILLING AIR-START
C. APU-ASSIST AIR-START (BELOW 15,000 FT)
D. AFTER START
SINGLE-ENGINE APPROACH AND LANDING
SINGLE ENGINE GO-AROUND
DUAL ENGINE FAILURE
DUAL ENGINE FAILURE EMERGENCY LANDING
ENGINE OIL PRESSURE LOW
THRUST REVERSER UNLOCKED OR DEPLOYED DURING TAKEOFF
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