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藍(lán)天飛行翻譯公司承接AW169直升機(jī)快速檢查單翻譯任務(wù)

時(shí)間：2019-03-10 18:47來源：藍(lán)天飛行翻譯公司 作者：直升機(jī)翻譯 點(diǎn)擊：次

Miscellaneous System
Pitot Heater Off
Aircraft Never Exceed Speed
Weight On Wheels Switch Failure
Sensor Dormant Failure
Cockpit Door Open
Cabin Door Open
Baggage Bay Door Open
External Power Socket Door Open
Cockpit Vent Fan Failure
Cabin Vent Fan Failure
Cockpit and Cabin Vent Fan Failure
ECS Fail
Audio System Failure
PFD and MFD Messages
Loss of PFD for Pilot in Control
Loss of PFD Pilot not in Control
Loss of Multi Function Display
EDCU Overtemperature
Attitude Display Failure
Heading Display Failure
mag degr caption
ADS Failure
Double RAD ALT Failure
Single Rad Alt Failure
OAT Sensor Failure
Display Unit Messages “REV”
CAS Warning Message List Discrepancy
CAS Caution Message List Discrepancy
Display Unit Monitoring “DU MON” Message on PFD Only
Display Unit Monitoring “DU MON” on PFD and MFD
Display Unit Messages ‘CHECK PFD’
Display Unit Messages “DU OVHT”
Magnetic Variation Invalid
2.5 Minute Message for OEI Conditions
5 Minute Message for AEO Conditions
Engine State Indication on PFD and MFD
NR Miscompare Message
AHRS Miscompare
ADS Miscompare
AHRS Miscompare
RAD ALT Miscompare
Decision Height Caption
Low Height Protection
Height Loss
Power Limit
Power Loss
OAT Sensor Miscompare
LOC/GS Miscompare
LG/vg Miscompare
LOSS OF RADIONAV OR FMS LATERAL AND/OR VERTICAL DEVIATIONS
Loss of VOR Data
Loss of AFCS Communication to PFD
FMS Messages on PFD
FMS DGR + RNP + MSG
RAIM MESSAGE ON PFD
RAIM + GNSS RAIM UNAVAILABLE on EDCU
RAIM + GNSS WILL EXCEED LIMIT on EDCU (DURING APPROACH)
MSG ON PFD + GNSS RAIM ABOVE LIMIT on EDCU
DR ON PFD + UNABLE GNSS RNP ON EDCU
ROTOR AND TRANSMISSION
Rotor Brake Fail
Rotor Brake Inhibit
Rotor Brake Overheat (On Ground)
Main Gearbox Overtorque
Main Gearbox Oil Low
Transmission Chip Detector
Gearbox Chip Sensor Failure
Main Gearbox Input Oil Pressure
Main Gearbox Input Bearing Temperature
Intermediate Gearbox Oil Temperature High
Tail Rotor Gearbox Oil Temperature
AVSR Fail
AVSR Oscillatory Malfunction
Gearbox Chip Detect Unit Malfunction
Single Engine Procedure
Single Engine Descent Checks
Single Engine Approach and Landing
Single Engine Before Landing Checks
Emergency Procedure for Single Engine Failure during Take-Off
Single Engine Failure Recognized in Hover (6 ft (1,8 m) ATS)
OEI Rejected Take-OFF PROCEDURE
OEI Continued Take-Off PROCEDURE
Emergency Procedures For single Engine Failure During Landing approach
OEI Balked Landing PROCEDURE
OEI Landing PROCEDURE

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