藍天飛行翻譯公司承接AW109直升機快速檢查單翻譯任務(wù)
時間：2020-08-28 18:13來源：藍天飛行翻譯公司 作者：直升機翻譯 點擊：次
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ENGINE OIL CHIP (Helicopters equipped with pulsed chip detector system P/N 109-0811-48) Engine power lever remote control fail Engine power Lever position Engine Mode select switch Failure Engine Drive shaft failure Engine power turbine overspeed Engine power turbine overspeed detect failure N2 overspeed control circuit test failure OEI 2.5 min Rating outside limits Data Collection unit malfunction engine control unit - maintenance required ENGINE CONTROL UNIT - LOSS OF DATA Engine Hot start Tot limiter malfunction Torque limiter malfunction mGT Mismatch Rotor Speed Selector malfunction engine fire detector system failure Fire extinguisher bottle discharged ENGINE RESTART IN FLIGHT Procedure In flight restart procedure in auto mode In flight restart procedure in manual mode ABORTED ENGINE START PROCEDURE Auto to Manual Mode transfer ENgine sTART in manual mode (ON GROUND) Engine shutdown in manual mode ENGIne OPERATION in manual mode One engine in MANUAL mode and one in AUTO mode Both engines in MANUAL mode ENGINE Power lever (PLA) jammed procedure DC generator control battery off EXTERNAL POWER ON Failure of a generator BUS tie open Generator overload inverter failure SERVO HYDRAULIC SYSTEM N?1 MALFUNCTION sERVO HYDRAULIC SYSTEM N?2 MALFUNCTIOn Jamming of a main rotor servo valve Tail rotor servo valve jamming NORmal utility hydraulic PRESSURE LOW Emergency utility hydraulic PRESSURE LOW Normal utility hydraulic system charging EMERGENCY utility hydraulic system charginG Main Transmission OVERTORQUe MAIN transmission chip (Helicopters not equipped with pulsed chip detector system P/N 109-0811-48) MAIN transmission chip (Helicopters equipped with pulsed chip detector system P/N 109-0811-48) tail GEARBOX chip (Helicopters not equipped with pulsed chip detector system P/N 109-0811-48) tail GEARBOX chip (Helicopters equipped with pulsed chip detector system P/N 109-0811-48) ROTOR brAkE system degraded fuel low FUEL PRESSURE LOW fuel pump failed and airframe fuel filter clogged Airframe fuel filter clogged ENGINE fuel filter clogged Fuel low sensor failure fuel drain valve open Aural warning system failure Pilot’s OR COPILOT’S ICS failure master AVIONICS switch failure radio tuning unit failure Attitude MODE off autopilot cas fail AUTOPILOT AHRS FAiL AP degraded (Not applicable to EDU P/N 109-0900-76-2A05 and subs) AP STDBY FAIL (Applicable to EDU P/N 109-0900-76-2A05 and subs) AUTOPILOT TEST FAIL AFCS pft partially completed (Not applicable to EDU P/N 109-0900-76-2A05 and subs) AFCS pft partially completed (Applicable to EDU P/N 109-0900-76-2A05 and subs) AP CHANNEL FAILURE APMS PANEL FaIL MISTRIM pitch trim fail roll trim fail yaw trim fail collective trim fail autopilot off autopilot FAIL autopilot Hot pitch autopilot fail roll autopilot fail yaw autopilot fail AFCS oscillatory malFUNCTIoN Electronic display unit 1 complete Failure Electronic display unit 1 degradation Electronic display unit 2 complete Failure ELECTRONIC display unit 2 degradation miscompare of DAU primary parameters INCORRECT DAU HARDWARE CONFIGURATION (Applicable to EDU P/N 109-0900-76-2A05 and subs) EFIS Caution Annunciation Captions Failure of pilot’s PFD Failure of copilot’s PFD REBOOT OF PILOT’S (OR COPILOT’S) MFD MFD BACKGROUND NOISE LOSS of data from air data COMPUTER loss of data from attitude heading reference system LOSS OF HEADING (For EFIS software versions up to 8.0E included) LOSS OF HEADING (For EFIS software versions 8.0H or later) aLtitude DATA discrepancy pitch and roll attitude DATA discrepancy IDU OVERTEMPERATURE |
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