曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

OUT and IN values for channels A and B are the torque motor
demand and return path current values.
LPTACC DATA
The LPTACC DATA pages give you the low pressure turbine
active clearance control demand and position values for
channel A and B.The V1 and V2 values are voltages from the
linear variable differential transformer (LVDT) feedbacks. The
OUT and IN values for channels A and B are the torque motor
demand and return path current values.
Training Information Point
If a parameter is not available, (?) symbols are put in place of
the parameter. If the parameter is out of range, (-) symbols are
put in place of the parameter.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 5
EFFECTIVITY
GUN ALL 73-21-00
Page 98.40
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-243
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 5
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 5
EFFECTIVITY
GUN ALL 73-21-00
Page 98.41
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-243
General
GUN ALL PRE SB CFM56-7B 73-44
More transient bleed valve (TBV) and burner staging valve
(BSV) parameters show on these CDU pages. You see these
pages when you select TBV or BSV from the INPUT
MONITORING CONTROL LOOPS page.
GUN ALL POST SB CFM56-7B 73-44
More transient bleed valve (TBV) parameters show on these
CDU pages. You see these pages when you select TBV from the
INPUT MONITORING CONTROL LOOPS page.
GUN ALL
The ACT CH A shows the active channel or the channel that
controls the engine. The GMM CH A shows the ground
maintenance mode (GMM) channel or the channel that
controls CDU BITE.
TBV DATA
The TBV DATA pages give you the transient bleed valve
demand and position values for channel A and B. The V1 and V2
values are voltages from the linear variable differential
transformer (LVDT) feedbacks. The OUT and IN values for
channels A and B are the torque motor demand and return path
current values.
GUN ALL PRE SB CFM56-7B 73-44
BSV POSITION DATA
The BSV POSITION DATA pages give you the burner staging
valve demand and position values for channel A and B. The
SW1 and SW2 values are the position switch feedback signals.
The OUT and IN values for channels A and B are the solenoid
demand and return path current values.
GUN ALL
Training Information Point
If a parameter is not available, (?) symbols are put in place of
the parameter. If the parameter is out of range, (-) symbols are
put in place of the parameter.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 6
EFFECTIVITY
GUN ALL 73-21-00
Page 98.42
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-245
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 6
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 6
EFFECTIVITY
GUN ALL PRE SB CFM56-7B 73-44 73-21-00
Page 98.43
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-245
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 6
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PAGE 6
EFFECTIVITY
GUN ALL POST SB CFM56-7B 73-44 73-21-00
Page 98.44
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-245
General
More thrust resolver angle (TRA) and thrust reverser position
(REV) parameters show on these CDU pages. You see these
pages when you select TRA or REV from the INPUT
MONITORING CONTROL LOOPS page.
The ACT CH A shows the active channel or the channel that
controls the engine. The GMM CH A shows the ground
maintenance mode (GMM) channel or the channel that
controls CDU BITE.
TRA SELECTION
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NGAMM9(39)