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时间:2011-04-09 10:08来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (1)  
The following faults are monitored and indicated by illumination of the light:

 (a)  
Disagreement between the directional control and isolation valves located within the reverser hydraulic control valve module, i.e., isolation valve open and directional control valve not in the deploy position.

 (b)  
Disagreement in the positions of the two translating sleeves on one engine for more than two seconds. The two-second time delay allows for any variations in the deploy/stow translation time of the two sleeves on one engine.

 

 (2)  
The 'REVERSER' fault light is included in the master caution and warning system.


 (a)  A time delay inhibits activation of the master caution and warning system for a minimum of 12 seconds following illumination of the 'REVERSER' fault light.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-36-00
 ALL  ú ú C01 Page 1 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

 

PILOTS' CENTER INSTRUMENT PANEL


12
ENGINE
REVERSER REVERSER
PILOTS' AFT OVERHEAD PANEL

Thrust Reverser Indicator Light Location

Figure 1 (Sheet 1)

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 78-36-00
 ALL  ú
 ú  C01  Page 2
 ú  Jul 15/89 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

E3 RACK

FAIL
(FAULT)
LIGHT
(2 LOCATIONS)


Thrust Reverser Indicator Light Location
Figure 1 (Sheet 2)

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 78-36-00
 ALL  ú ú C01 Page 3 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

E3 RACK

FAULT LIGHT (6 LOCATIONS)
RESET SWITCH (2 LOCATIONS)
ENGINE ACCESSORY UNIT

Thrust Reverser Indicator Light Location
Figure 1 (Sheet 3)

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 78-36-00
 ALL  ú ú C01 Page 4 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C98777
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

E3 RACK

FAULT LIGHT (16 LOCATIONS)
ENGINE ACCESSORY UNIT


Thrust Reverser Indicator Light Location
Figure 1 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-36-00
 ALL  ú ú C01 Page 5 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C57140
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)  This delay allows time for completion of the normal stowing cycle, during which there is disagreement between the directional control and isolation valves before the activation of the master caution system.
 3.  Engine Accessory Unit (EAU)
_____________________
 A.  In addition, for maintenance purposes, the 'REVERSER' fault lights are duplicated by lights located on the face of the Engine Accessory Unit (EAU) in the rack in the electronic equipment bay.
 
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