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庞巴迪环球5000公务机机组操作手册 Bombardier Global-动力装置(32)

时间:2011-11-11 09:42来源:蓝天飞行翻译 作者:公务机 点击:
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GF1810_101a
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2

POWER PLANT
 

A/T ADC MISCMP
Indicates that the A/T is not available due to an ADC data miscompare.


A/T 1 (2) FAIL
Indicates that the A/T is invalid, or reporting a hardware or servo failure.


L (R) IGNITION ON
Indicates that the IGNITION switch has been selected and the EEC is activating all
igniters.

 

A/T IRS MISCMP
Indicates that the A/T is not available
due to an IRS data miscompare.

ENG SYNC FAIL
Indicates that the affected

SYNC system has failed.

ENG SYNC LIMITED
Indicates that the selected SYNC system is unable to function due authority limit or engine split greater than SYNC authority.


L (R) ENG BLEED ON
Indicates that the selected bleed
has been selected ON.

L (R) ENG BLEED OFF
Indicates that the selected bleed
has been selected OFF.

L (R) FADEC N1 CTL
Indicates that the affected engine is in N1 control, by switch selection on the engine control panel.

 


L (R) ENG SHUTDOWN

Indicates that the crew has initiated shutdown on the affected engine.
GF1810_102a
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

POWER PLANT EMS CIRCUIT PROTECTION
CB - ENGINE SYSTEM

L ENG FUEL HPSOV L ENG IGN 1 L ENG IGN 2 L ENG START A L ENG START B BATT BATT BATT BATT BATT CB . ENGINE SYSTEM L FADEC CH A BATT  IN IN IN IN IN 1/3 IN 
CB . ENGINE SYSTEM  2/3 
L FADEC CH B R ENG FUEL HPSOV R ENG IGN 1 R ENG IGN 2 R ENG START A BATT BATT BATT BATT BATT R ENG START B BATT  IN IN IN IN IN IN 
CB . ENGINE SYSTEM  3/3 
R FADEC CH A R FADEC CH B BATT BATT VIBE MONITOR DC 1  IN IN IN 


GF1820_001
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2

POWER PLANT
 

EMS CIRCUIT PROTECTION
 

 

NOTE
The OIL TANK PROBE power source is tied to the MAP LTS circuit breaker, therefore, the OIL TANK PROBE circuit breaker is OUT for airplanes incorporating SB 700.1A11.79.001.
FGF1820_001
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

POWER PLANT EMS CIRCUIT PROTECTION
CB - THRUST REV SYSTEM

L T/R LOWER LOCK L T/R TQA LOCK L T/R UPPER LOCK L T/R CTL VALVE BATT BATT BATT BATT CB . THRUST REV SYSTEM R T/R CTL VALVE R T/R LOWER LOCK BATT BATT  IN IN IN IN 1/2 IN IN 
CB . THRUST REV SYSTEM  2/2 
R T/R UPPER LOCK R T/R TQA LOCK BATT BATT  IN IN 

GF1820_004
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2

THIS PAGE INTENTIONALLY LEFT BLANK

Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

 


 
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