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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(5)

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:


Avionics and Instruments
ENGINE START
First engine start
Second engine start
AFTER START
STAB TRIM SETTINGS FOR TAKEOFF, FLAPS - 20°, 10° AND 0°
TAXIING
BEFORE TAKEOFF
LINE UP
AFTER TAKEOFF
IN FLIGHT
CLIMB TRANSITION
CRUISE
CABIN ALTITUDE / PRESSURE SCHEDULE
Cabin Altitude Schedule
Cabin Differential Pressure Schedule
BEFORE DESCENT
DESCENT TRANSITION
BEFORE LANDING
GO AROUND (TWO-ENGINE)
AFTER LANDING
ENGINE SHUT-DOWN
ALTERNATE NORMAL PROCEDURES
BLEED AIR OFF TAKEOFF
ENGINE CROSS START ON GROUND
ENGINE START USING GROUND AIR SOURCE
APU START USING EXTERNAL POWER
ENGINE DRY CRANKING
ENGINE MOTORING IN HOT WEATHER CONDITIONS
OPERATING AT AN AIRPORT NOT IN FMS DATABASE
HIGH ELEVATION AIRPORT OPERATION (ABOVE 8000 FT MSL)
COLD WEATHER OPERATIONS
A. PRE-FLIGHT
B. DE-ICING PROCEDURE
C. SYSTEMS START
D. ENGINES START
E. AFTER ENGINES START
F. TAXI
G. BEFORE TAKEOFF
H. DESCENT (Below 30,000 ft)
I. AFTER LANDING
GROUND OPERATIONS IN FREEZING FOG CONDITIONS
ICE SHEDDING IN FLIGHT
ICING CONDITIONS ABOVE 35,000 FT
ICING GENERAL
TURBULENCE PENETRATION / SEVERE GUST ENCOUNTER
VOLCANIC ASH ENCOUNTER
WAAS LPV
SBAS / LPV APPROACH GENERAL DESCRIPTION
PRINCIPLES OF LPV APPROACH
PRINCIPLES OF SBAS L/V APPROACH
USE OF VNAV
SBAS INTEGRITY
CONTINGENCIES
RNAV (GPS) APPROACH PROCEDURE
POLAR NAVIGATION
POLAR REGION DEFINITIONS
FMS NAVIGATION
STBY INSTRUMENT
Section V - Performance Wet and Dry
GENERAL INFORMATION
COMPLIANCE
STANDARD PERFORMANCE CONDITIONS
VARIABLE FACTORS AFFECTING PERFORMANCE
DEFINITIONS
ATMOSPHERIC
AIRSPEEDS
DISTANCES
GRADIENT OF CLIMB
HEIGHT
ICING
PERFORMANCE CONFIGURATIONS
DEMONSTRATED CROSSWIND
NOISE LEVELS
PITOT-STATIC POSITION ERROR CALIBRATION
PITOT-STATIC POSITION ERROR CALIBRATION WITH FAILED AOA READING
ENGINE PERFORMANCE
APPROVED FLIGHT ENVELOPE
REFERENCE STALL SPEEDS - IDLE THRUST
TAKEOFF PERFORMANCE
MAXIMUM ALLOWABLE TAKEOFF WEIGHT
Determination Of Maximum Allowable Takeoff Weight
MAXIMUM TAKEOFF WEIGHT AS PERMITTED BY CLIMB GRADIENT REQUIREMENTS
MAXIMUM TAKEOFF WEIGHT AS PERMITTED BY BRAKE ENERGY LIMITATIONS
MAXIMUM TAKEOFF WEIGHT AS PERMITTED BY TIRE SPEED LIMITATIONS
TAKEOFF FIELD LENGTH
TAKEOFF SPEEDS (V1, VR, V2)
MINIMUM CONTROL SPEED - AIR (VMCA)
TAKEOFF CHARTS AND TABLES
Tables to determine V1, VR, V2, second segment climb gradient (GR2) and takeoff field length (TOFL) for zero wind, zero runway gradient conditions
For wet runways (with both thrust reversers operative at dispatch)
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