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时间:2011-04-02 23:24来源:蓝天飞行翻译 作者:航空
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 TASK 34-22-11-004-001
 2.  EFIS Control Panel Removal__________________________
 A.  Access
 (1)  Location Zones
 101/102 Flight Compartment

 B.  Procedure
 S 864-002
 (1)  Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  
P6 Circuit Breaker Panel
 1) EFIS CONT PANEL R
 2) EFIS SYM GEN R


 (b)  
P18 Circuit Breaker Panel
 1) EFIS CONT PANEL L
 2) EFIS SYM GEN L

 

 S 034-003
 CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE EFIS
_______ CONTROL PANEL. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE EFIS CONTROL PANEL.
 (2)  Loosen the four quarter-turn fasteners on the front of the EFIS control panel.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-22-11
 ú ú 01 Page 401 ú Jul 15/91

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 024-035
 (3)  
Pull the EFIS control panel out to get access to the electrical connectors .

 S 034-031

 (4)  
Disconnect the electrical connector on the rear of the EFIS control panel.

 S 034-040

 (5)  
Install dust caps on the electrical connectors.


 TASK 34-22-11-404-006
 3. EFIS Control Panel Installation
_______________________________
 A. References
 (1)  
AMM 21-58-02/501, EFIS Cooling System

 (2)  
AMM 24-22-00/201, Manual Control


 B. Access
 (1)  Location Zones
 101/102 Flight Compartment

 C. Procedure
 S 864-007
 (1)  Make sure these circuit breakers are open:
 (a)  
P6 Circuit Breaker Panel
 1) EFIS CONT PANEL R
 2) EFIS SYM GEN R


 (b)  
P18 Circuit Breaker Panel
 1) EFIS CONT PANEL L
 2) EFIS SYM GEN L

 

 S 024-046
 CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE EFIS
_______ CONTROL PANEL. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE EFIS CONTROL PANEL.
 (2)  Remove the dust caps from the electrical connectors.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-22-11

 ú ú 01 Page 402 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 434-039
 (3)  
Connect the electrical connector at the rear of the EFIS control panel.

 S 424-009

 (4)  
Put the EFIS control panel into position on the pilot's aft
 electronics panel, P8.

 

 NOTE: If there was a blank placard on the range switch of the old
____ EFIS control panel, make sure you put it on the new EFIS control panel
 S 434-010
 (5)  Tighten the four quarter-turn fasteners on the front of the EFIS control panel.
 D. Prepare for the EFIS Control Panel Test
 S 864-011
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 864-012

 (2)  
Make sure the BAT switch on the pilots' forward overhead panel is in the ON position.

 S 864-013

 (3)  
Make sure the STANDBY POWER switch on the pilots' forward overhead panel is in the AUTO position.


 S 884-014
 CAUTION: MAKE SURE THAT YOU OPERATE THE EQUIPMENT COOLING SYSTEM BEFORE
_______ YOU ENERGIZE AN ELECTRONIC SYSTEM. TOO MUCH HEAT CAN CAUSE DAMAGE TO ELECTRONIC EQUIPMENT.
 (4)  
Supply the cool air from the equipment cooling system
 (AMM 21-58-02/501).


 S 864-029

 (5)
Close these circuit breakers and remove the DO-NOT-CLOSE tags:


 (a)  P6 Circuit Breaker Panel
 1) EFIS CONT PANEL R
 2) EFIS SYM GEN R

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
 
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