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时间:2011-04-02 23:33来源:蓝天飞行翻译 作者:航空
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_______ ACCESSORY UNIT. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE FROM YOUR BODY CAN CAUSE DAMAGE TO THE ACCESSORY UNIT.
 (2)  
Do this task to remove the flight instrument accessory unit from the E1 equipment rack: Remove the Rack-Mounted E/E Box (AMM 20-10-07/201).

 (3)  
Install dust caps on the electrical connectors.


 S 034-028
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-31-62
 ú ú 01 Page 401 ú Jul 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 34-31-62-404-047
 3.  Flight Instrument Accessory Unit Installation_____________________________________________
 A. General
 (1)  The flight instrument accessory unit (M160) is on shelf No. 2 of the electronic equipment rack (E1).
 B. References
 (1)  
AMM 20-10-07/201, E/E Rack-Mounted Components

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

 (3)  
AMM 34-31-02/501, VOR/ILS Navigation System


 C. Access
 (1)  
Location Zone
 205 Electronics Compartment


 (2)  
Access Panel
 1201L Electronic Equipment Access Door

 

 D. Procedure
 S 864-030
 (1)  Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  
P18 Load Control Center - Left
 1) INSTR XFR
 2) IRS NO. 1 DC
 3) VHF NAV-1 VOR/ILS


 (b)  
P6 Load Control Center - Right
 1) IRS NO. 2 AC
 2) IRS NO. 2 DC
 3) VHF NAV-2 VOR/ILS

 

 S 434-033
 CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE
_______ ACCESSORY UNIT. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE FROM YOUR BODY CAN CAUSE DAMAGE TO THE ACCESSORY UNIT.
 (2)  
Remove the dust caps from the electrical connectors.

 S 424-034

 (3)  
Do this task to install the flight instrument accessory unit in the E1 equipment rack: Install the Rack-Mounted E/E Box (AMM 20-10-07/201).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-31-62

 ú ú 05 Page 402 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (4)  S 864-035Remove the DO-NOT-CLOSE tags and close these circuit breakers. (a) P18 Load Control Center - Left 1) INSTR XFR 2) IRS NO. 1 DC 3) VHF NAV-1 VOR/ILS (b) P6 Load Control Center - Right 1) IRS NO. 2 AC 2) IRS NO. 2 DC 3) VHF NAV-2 VOR/ILS
 (5)  S 714-048Do the VHF NAV Transfer Switch Test part of the VOR/ILS Operational Test (AMM 34-31-02/501).
 (6)  S 864-043If electrical power is not necessary, do this task to remove the electrical power: Manual Control (AMM 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-31-62
 ú ú 05 Page 403 ú Jul 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TRANSFER RELAYS - REMOVAL/INSTALLATION
______________________________________
 1.  General_______
 A.  This subject has two tasks. The first task is the removal of the transfer relay. The second task is the installation of the transfer relay and a test of the transfer relay.
 B.  These are the relays included in this subject:
 (1)  
Two antenna transfer relays:

 (a)  
ILS transfer relay No. 1 (R315)

 (b)  
ILS transfer relay No. 2 (R316)

 

 (2)  
Two VHF NAV transfer relays:

 (a)  
VHF NAV transfer relay No. 1 (R44)

 (b)  
VHF NAV transfer relay No. 2 (R45)

 
 
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