• 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

A 737-300/400/500MAINTENANCE MANUAL

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-55-02
 ú ú 01 Page 103 ú Nov 15/91

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 DME SYSTEM - ADJUSTMENT/TEST
____________________________
 TASK 34-55-02-735-023
 1.  DME System Test_______________
 A. General
 (1)  
This procedure has two tasks. One is an operational test; the other is a system test. The operational test is a fast check of the DME system by the system BITE. The system test first does the operational test. Then, it does a test of the DME's identification reception with external test eqiupment.

 (2)  
These tests of the DME system No. 1 or 2 use the applicable VHF NAV control panel and DME indications on the captain and first officer RDDMI and EHSI.


 TASK 34-55-02-715-001
 2.  Operational Test - DME System No. 1 and 2_________________________________________
 A. References
 (1)  
AMM 21-58-03/501, Equipment Cooling System

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

 (3)  
AMM 34-22-00/201, Electronic Flight Instrument System (EFIS)

 (4)  
AMM 34-28-01/201, Inertial Reference System (IRS)


 B. Procedure
 S 865-002
 (1)  Supply electrical power (AMM 24-22-00/201).
 S 865-201
 CAUTION: MAKE SURE THE COOLING EQUIPMENT IS WORKING CORRECTLY BEFORE YOU
_______ TURN ON THE ELECTRONIC SYSTEMS OR DAMAGE TO EQUIPMENT MAY RESULT. EQUIPMENT COOLING SYSTEM MUST BE SET FOR NORMAL COOLING AS DESCRIBED IN AMM 21-58-03/501.
 (2)  Provide equipment cooling (AMM 21-58-03/501).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-55-02
 ú ú 02 Page 501 ú Jul 12/99

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-025
 (3)  Make sure these circuit breakers on the P6 and P18 panel are closed:
 (a)  
Close these circuit breakers on P6-1:
 ~..................................................
 | DME-2 | DAA NO. 2 FMC AC |
 ....................................................
 | F/O RDDMI | DAA NO. 2 IRS AC |
 ....................................................
 | INST XFMR-2 | DAA NO. 2 DC |
 ....................................................
 | VHF NAV-2 VOR/ILS | IRS NO. 2 AC |
 ....................................................
 | EFIS SYM GEN R | IRS NO. 2 DC |
 ....................................................
 | EFIS CONT PANEL R | DAA FMC NO. 2 |
 ....................................................
 | EHSI | |
 2........................….........................1


 (b)  
Close the following circuit breakers on P6-2:
 ~..................................................
 | INTERPHONE | AUTO FLT CONT SYS B |
 ....................................................
 | CAPT BAT | FCC DC |
 ....................................................
 | CAPT NO. 2 BUS | |
 ....................................................
 | CAPT AUDIO | |
 ....................................................
 | OBS' AUDIO | |
 ....................................................
 | F/O's AUDIO | |
 ....................................................
 | F/O's BAT | |
 ....................................................
 | F/O NO. 2 BUS | |
 2........................….........................1


 (c)  
Close the following circuit breakers on P18-1:
 ~..................................................
 | | AUTO FLT CONT SYS A |
 ....................................................
 | VHF NAV-1 VOR/ILS | FCC DC |
 ....................................................
 | DME-1 | |
 
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(33)