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时间:2011-04-19 08:02来源:蓝天飞行翻译 作者:航空
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 (1)  AMM 20-41-01/201, Electro-Static Sensitive Devices
 B. Access
 (1)  Location Zone
 100 Lower Half of Fuselage

 C. Procedure
 S 214-012
 (1)  
Make sure that the rubber plugs are installed in the metering tray at the correct locations. Compare the tray orifice configuration with that shown on the decal.

 S 034-013

 (2)  
Remove the dust caps.

 S 214-014

 (3)  
Make sure that the tray gasket and restrictor plugs (adjustment number) did not move. Install if necessary.

 S 214-015

 (4)  
Make sure that the guide pins on the tray will engage with the E/E box.


 S 214-016
 CAUTION: ELECTRICAL PINS ON THE E/E BOX CONNECTOR AND THE TRAY CONNECTOR
_______ MUST NOT BE BENT OR DAMAGED. INSTALLATION OF THE E/E BOX WITH DAMAGED PINS COULD RESULT IN DAMAGE TO THE E/E BOX, THE TRAY ELECTRICAL CONNECTOR, OR THE SYSTEM COMPONENTS.
 (5)  Make sure that the electrical pins of the E/E box and the tray connector are not bent or damaged. Replace damaged components.
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 20-10-01
 ALL  ú ú 02 Page 404 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 S 434-017
 CAUTION:_______SOME E/E BOXES ARE STATIC SENSITIVE. TAKE THE NECESSARY PRECAUTIONS WHEN YOU ARE TO HOLD THE E/E BOXES. READ THE PROCEDURE ON HOW TO HOLD ELECTROSTATIC-DISCHARGE SENSITIVE DEVICES (AMM 20-41-01/201). THE E/E BOXES CONTAIN DEVICES THAT CAN BE DAMAGED BY STATIC DISCHARGE.
 (6)  Carefully move the E/E box in the tray and engage the electrical connector.
 NOTE: The E/E box front-face can be lifted about 1/8 inch above the
____ tray surface. This will permit better installation.
 The E/E box front-face can be moved right to left (about 1/8 inch). This will help engage the electrical connector. During installation apply a light pressure to the front-face of the E/E box. Do not use force during installation.
 S 434-018
 (7)  
Turn the keeper to align the deep slot with the T-hook.

 S 434-019

 (8)
Set the extractor on the T-hook and turn the keeper 180 degrees.

 S 434-020

 (9)  
Tighten the front hold-down extractor. Turn the front hold-down extractor clockwise until the extractor clutch is fully engaged.

 S 714-021

 (10)
 Move the E/E box left to right.  Make sure that the E/E box is tight.

 S 434-022

 (11)
 Tighten the extractor.

 (12)
 Make sure that the electrical connector is engaged.

 (13)
 Install the connections to the E/E box front if applicable.

 (14)
 Close all applicable circuit breakers.


 S 214-023
 S 434-024
 S 864-025
 TASK 20-10-01-024-026
 4.  Remove the Circuit Card Assembly________________________________
 A. Reference
 (1)  AMM 20-41-01/201, Electro-Static Sensitive Devices
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 20-10-01
 ALL  ú ú 01 Page 405 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 B. Access
 (1)  Location Zone
 100 Lower Half of Fuselage

 C. Procedure (Fig. 402)
 S 864-027
 (1)
Open the applicable circuit breakers to remove electrical power.

 S 014-028

 (2)  
Open the card file door.


 S 034-029
 CAUTION:_______CARD ASSEMBLIES ARE STATIC SENSITIVE. TAKE THE NECESSARY PRECAUTIONS WHEN YOU ARE TO HOLD THE CARD ASSEMBLIES. READ THE PROCEDURE ON HOW TO HOLD ELECTROSTATIC-DISCHARGE SENSITIVE DEVICES (AMM 20-41-01/201). THE CARD ASSEMBLIES CONTAIN DEVICES THAT CAN BE DAMAGED BY STATIC DISCHARGE.
 (3)  
Turn the ejectors on the card assembly until the card is loose in the guides.

 S 024-030

 (4)  
Carefully slide the card out along the guides.


 
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