時(shí)間：2014-12-02 10:10來源：藍(lán)天飛行翻譯公司 作者：公務(wù)機(jī)翻譯 點(diǎn)擊：次
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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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