北京藍天飛行翻譯公(gōng)司承接大型直升機公(gōng)司的AW109直升機快速檢查單翻譯任務(wù) AW109 Quick Reference Handbook(QRH) Translation

AW109

AW109直升機 AW109 Helicopter

AW109直升機 AW109 Helicopter

 

AW109直升機快速檢查單 AW109 Quick Reference Handbook(QRH)

 

　　AW109SP(Grand New)直升機是AW109SP家族中(zhōng)最先進的一款設計，裝(zhuāng)備2台由全數字控制系統（FADEC）控制的引擎，由防火牆完全隔離并配有(yǒu)火警檢測和滅火系統，機上裝(zhuāng)有(yǒu)彩色氣象雷達、自動駕駛儀、儀表着陸系統等，完全具(jù)備全天候夜間儀表飛行能(néng)力。

　　AW109SP直升機的客艙可(kě)以快速更改結構以适應商(shāng)務(wù)運輸、醫(yī)療急救、警務(wù)巡邏等不同的任務(wù)模式。該機可(kě)以在高溫、高原地區(qū)、寒冷地區(qū)、強風和近海大濕度、高鹽份環境下正常飛行，能(néng)夠滿足不同地區(qū)和環境作(zuò)業的需求。

　　AW109SP直升機安(ān)裝(zhuāng)了複合材料旋翼、彈性軸承和旋翼夾套以及钛合金的轉子。與其家族中(zhōng)的前輩相比，通過改良空氣動力外形，以及全新(xīn)的引擎數字控制系統，使得耗油量大為(wèi)降低的同時增加了航程和有(yǒu)效載荷，玻璃化座艙也減少了機組人員的工(gōng)作(zuò)量。

　　特别值得一提的是AW109SP直升機是同級别直升機中(zhōng)唯一安(ān)裝(zhuāng)輪式起落架的直升機，這不僅極大地提高飛機野外着陸的能(néng)力也增加絞車(chē)作(zuò)業的安(ān)全性，同時輪式起落架滑跑起飛和着陸功能(néng)也提高了該機的作(zuò)業性能(néng)。該機可(kě)以安(ān)裝(zhuāng)各種多(duō)用(yòng)途設備，包括絞車(chē)、應急浮筒、紅外夜視儀、外部揚聲器、夜間搜索燈、吊挂貨鈎、消防水桶、各種緊急醫(yī)療救護設備等。

      AW109直升機快速檢查單(Quick Reference Handbook(QRH))的主要内容包含有(yǒu)：

INTRODUCTION
DEFINITIONS
SAFE OEI FLIGHT
EMERGENCY LANDING GUIDANCE
Pilot alertness level
EMERGENCY & MALFUNCTION PROCEDURES
CAS warning messages
AWG TEST Procedure
EMERGENCY AUTOROTATION PROCEDURE
ENGINE FIRE ON GROUND
ENGINE FIRE IN FLIGHT
Smoke in cabin, toxic fumes, etc.
MAIN GEARBOX OIL PRESSURE LOW
MAIN GEARBOX OIL TEMPERATURE HIGH
ROTOR UNDER SPEED
ROTOR OVERSPEED
ROTOR brAkE FAILURE
MAIN ROTOR CONTROLS SEIZURE
TAIL ROTOR DRIVE FAILURE
TAIL ROTOR DRIVE FAILURE IN HOVER
Tail rotor drive failure in forward flight, power-on
Tail rotor drive failure in forward flight, low power or power-ofF
Tail rotor drive failure in forward flight, low power or power-ofF (CONT’D)
Tail rotor control failure in hover
Tail rotor control failure in forward flight
Tail Rotor Control Seizure in hover
Tail Rotor Control Seizure in forward flight
ENGINE FAILURE
Double Engine Failure
ENGINE SHUTDOWN IN AN EMERGENCY
EMERGENCY/POST CRASH SHUTDOWN and egress
ENGINE OIL PRESSURE
ENGINE ECU FAIL
DOUBLE DC GENERATOR FAILURE
DOUBLE DC GENERATOR FAILURE (CONT’D)
Double DC Generator Failure (Extended Flight Endurance)
Double DC Generator Failure (Extended Flight Endurance) (CONT’D)
Double DC Generator Failure (Extended Flight Endurance) (CONT’D)
SERVICES retained DURING DOUBLE DC GENERATOR failure
Services lost during DOUBLE DC GENERATOR failure
battery Discharging
battery Discharging (CONT’D)
battery hot
Electrical Fire / Smoke (in Flight)
Electrical Fire / Smoke (in Flight) (CONT’D)
LANDING GEAR FAILS TO LOCK DOWN (Total or partial failure)
EMERGENCY DOWN LANDING GEAR PROCEDURE
STATIC PORT OBSTRUCTION
flight in thunderstorm - Lightning strike
CAUTION messages
VOICE ONLY CAUTIONS
COMPRESSOR STALL
Unusual Engine noise
Attempted take-off with one engine in idle
ENGINE OIL Temperature
ENGINE OIL CHIP (Helicopters not equipped with pulsed chip detector system P/N 109-0811-48)