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

AW109

AW109直升機(jī) AW109 Helicopter

AW109直升機(jī) AW109 Helicopter

 

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

 

　　AW109SP(Grand New)直升機(jī)是AW109SP家族中最先進(jìn)的一款設(shè)計(jì)，裝備2臺(tái)由全數(shù)字控制系統(tǒng)（FADEC）控制的引擎，由防火墻完全隔離并配有火警檢測(cè)和滅火系統(tǒng)，機(jī)上裝有彩色氣象雷達(dá)、自動(dòng)駕駛儀、儀表著陸系統(tǒng)等，完全具備全天候夜間儀表飛行能力。

　　AW109SP直升機(jī)的客艙可以快速更改結(jié)構(gòu)以適應(yīng)商務(wù)運(yùn)輸、醫(yī)療急救、警務(wù)巡邏等不同的任務(wù)模式。該機(jī)可以在高溫、高原地區(qū)、寒冷地區(qū)、強(qiáng)風(fēng)和近海大濕度、高鹽份環(huán)境下正常飛行，能夠滿(mǎn)足不同地區(qū)和環(huán)境作業(yè)的需求。

　　AW109SP直升機(jī)安裝了復(fù)合材料旋翼、彈性軸承和旋翼夾套以及鈦合金的轉(zhuǎn)子。與其家族中的前輩相比，通過(guò)改良空氣動(dòng)力外形，以及全新的引擎數(shù)字控制系統(tǒng)，使得耗油量大為降低的同時(shí)增加了航程和有效載荷，玻璃化座艙也減少了機(jī)組人員的工作量。

　　特別值得一提的是AW109SP直升機(jī)是同級(jí)別直升機(jī)中唯一安裝輪式起落架的直升機(jī)，這不僅極大地提高飛機(jī)野外著陸的能力也增加絞車(chē)作業(yè)的安全性，同時(shí)輪式起落架滑跑起飛和著陸功能也提高了該機(jī)的作業(yè)性能。該機(jī)可以安裝各種多用途設(shè)備，包括絞車(chē)、應(yīng)急浮筒、紅外夜視儀、外部揚(yáng)聲器、夜間搜索燈、吊掛貨鉤、消防水桶、各種緊急醫(yī)療救護(hù)設(shè)備等。

      AW109直升機(jī)快速檢查單(Quick Reference Handbook(QRH))的主要內(nèi)容包含有：

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)