• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 23:40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


 S 624-025
 S 424-026
 S 864-027
 (a)  P18 Circuit Breaker Panel
 1)  AIRPLANES WITHOUT EFIS;
 ADF-1 AC or INST XFMR-1

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-57-21

 ALL  ú ú 03 Page 404 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 2) AIRPLANES WITH EFIS;
 ADF-1 AC or EXCIT XFMR-1
 3) ADF-1 DC

 (b)  P6 Circuit Breaker Panel
 1) AIRPLANES WITHOUT EFIS;
 ADF-2 AC or INST XFMR-2
 2) AIRPLANES WITH EFIS;

 ADF-2 AC or EXCIT XFMR-2
 3) ADF-2 DC

 S 714-023
 (11)
 Do the System Test of the ADF system (AMM 34-57-00/501 or 34-57-01/501).

 (12)
 Remove electrical power if it is not necessary (AMM 24-22-00/201).


 S 864-041
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-57-21

 ALL  ú ú 04 Page 405 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ADF SENSE ANTENNA - REMOVAL/INSTALLATION
________________________________________
 TASK 34-57-31-004-001
 1.  ADF Sense Antenna Removal_________________________
 A. General
 (1)  
The ADF sense antenna is flamesprayed on the reinforced wing body fairing. The metal layer of the fairing is used as the antenna element and is not removable from the fairing.

 (2)  
To remove or replace the wing body fairing, refer to AMM 53-51-21, Aft Wing-to-Body Fairing - Removal/Installation.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-57-31

 ALL  ú ú 02 Page 401 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AUTOMATIC DIRECTION FINDER CONTROL PANEL - REMOVAL/INSTALLATION
_______________________________________________________________
 1.  General_______
 A.  This procedure has two tasks. One is for the removal of the ADF control panel; the other is the installation of the ADF control panel.
 B.  The ADF control panel(s) are installed on the center aisle stand, P8.
 TASK 34-57-41-004-001
 2.  ADF Control Panel Removal_________________________
 A.  Access
 (1)  Location Zones
 101 Flight Compartment, Left
 102 Flight Compartment, Right

 B.  Procedure
 S 864-092
 (1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  
P18 Circuit Breaker Panel
 1) AIRPLANES WITHOUT EFIS;
 ADF-1 AC or INST XFMR-1
 2) AIRPLANES WITH EFIS;


 ADF-1 AC or EXCIT XFMR-1 3) ADF-1 DC

 (b)  
P6 Circuit Breaker Panel
 1) AIRPLANES WITHOUT EFIS;
 ADF-2 AC or INST XFMR-2
 2) AIRPLANES WITH EFIS;

 

 ADF-2 AC or EXCIT XFMR-2 3) ADF-2 DC
 S 024-050
 (2)  
Loosen the captive dzus fasteners on the control panel.

 S 014-051

 (3)  
Move the control panel out to get access to the electrical connectors.

 (4)  
Disconnect the electrical connectors.

 (5)  
Remove the ADF control panel.


 S 024-052
 S 024-058
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-57-41

 ALL  ú ú 06 Page 401 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 导航 NAVIGATION 4(58)