蓝天飞行翻译公司承接AW109直升机快速检查单翻译任务
时间：2020-08-28 18:13来源：蓝天飞行翻译公司 作者：直升机翻译 点击：次
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single gps system failure DOUBLE GPS SYSTEM FAILURE gps loss of integrity GPS DATA discrepancy Excessive Glide slope discrepancy HEADING DATA discrepancy airspeed DATA discrepancy LOSS OF IDU POWER REDUNDANCY idu discrepancy ON PILOT SIDE idu discrepancy ON COPILOT SIDE Excessive localiser discrepancy LOSS of OAT data radio altimeter DATA loss SCC FAILURE ADS-B TRANSPONDER FAILURE (IF INSTALLED) door Open baggage compartment door Open parking brake on (Not applicable to EDU P/N 109-0900-76-2A05 and subs) Pitot Heat failed cockpit fan failed EFIS FANs Failed landing gear Retracted LANDING GEAR FAILS TO RAISE air data unit failure attitude and heading reference system failure vne exceeded Deviation from selected altitude/HEIGHT DEVIATION FROM ABOVE TO BELOW MIN ALTITUDE USE OF WARNINGS, CAUTIONS AND NOTES USE OF PROCEDURAL WORDS GENERAL Types of OPERATION MINIMUM FLIGHT CREW Number of Occupants WEIGHT AND CENTER OF GRAVITY Limitations AIRSPEED Limitations GROUND SPEED Limitations WIND SPEED limitations for rotor starting and stopping ALTITUDE Limitations AMBIENT AIR TEMPERATURE Limitations slope limitations Engine Limitations Engine Starter Duty Cycle GAS GENERATOR SPEED (N1) All Engines Operating (AEO) One Engine Inoperative (OEI) POWER TURBINE SPEED (N2) All Engines Operating (AEO) One Engine Inoperative (OEI) TURBINE OUTLET TEMPERATURE (TOT) Engine Starting All Engines Operating (AEO) One Engine Inoperative (OEI) ENGINE OIL PRESSURE ENGINE OIL TEMPERATURE ROTOR Limitations POWER-ON (AEO) POWER-ON (OEI) POWER-OFF TRANSMISSION Limitations TORQUE (TRQ%) (AEO) TORQUE (TRQ%) (OEI) TRANSMISSION oil pressure TRANSMISSION oil temperature FUEL Limitations FUEL PRESSURE FUEL quantity total unusable fuel APPROVED FUELS Emergency fuels luBRICANTS Limitations AUTHORIZED ENGINE OILS AUTHORIZED TRANSMISSION OILS HYDRAULICS Limitations MAIN SYSTEM FLUID PRESSURE NORMAL UTILITY SYSTEM - FLUID PRESSURE EMERGENCY UTILITY SYSTEM - FLUID PRESSURE Approved Fluids GENERATOR LOAD Limitations (FOR EACH GENERATOR) AVIONIC Limitations Magnetic compass FLIGHT MANAGEMENT SYSTEM EFIS HTaws automatic flight control system Flight director Upper and FLIGHT DIRECTOR MODES ENGAGeMENT LIMITS and Minimum USE Height (MUH) MISCELLANEOUS Limitations rotor brake BAGGAGE COMPARTMENT fuel management system PASSENGERS CABIN LIMITATIONS doors opened or removed sun glasses GENERAL FLIGHT PLANNING PREFLIGHT CHECKS ENGINE PRE-START CHECKS Initial checks Electrical power-up ENGINE START NORMAL ENGINE START ENGINE 1 start: ENGINE 2 start: QUICK engine START ABORTED ENGINE START DRY MOTORING RUN SYSTEMS CHECKS HYDRAULIC SYSTEMs FUEL SYSTEM ELECTRICAL A.C. SYSTEM RCP AFCS MISCELLANEOUS BEFORE TAKE-OFF CHECKS Ground TAXIING TAKE-OFF HOVER TAKE-OFF ROLLING TAKE-OFF IN FLIGHT SEARCHLIGHT OPERATING PROCEDURE automatic flight control system ils approaches EFIS SYSTEM flight management system TAWS APPROACH and landing vertical landing running landing SHUTDOWN POST FLIGHT CHECKS FLIGHT HANDLING characteristics engine limit governing climb speed autorotative descent steep approaches and vertical descent manoeuvres DENSITY ALTITUDE POWER ASSURANCE CHECKS POWER CHECK INTERVALS HOVER ceiling RATE OF CLIMB FUEL CONSUMPTION AT 3175 KG HEIGHT-VELOCITY DIAGRAMS OPERATION VS ALLOWABLE WIND QRH GENERAL INFORMATION CONTENT FLIGHT MANUAL QRH LIMITATIONS QRH NORMAL PROCEDURES |
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