• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 23:33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 725-027
 (6)  
Do the altitude reporting test with sufficient number of test altitude.

 S 725-028

 (7)  
If the ATC control panel has an altitude source switch, do the altitude reporting test again with the altitude source switch set to the other position.

 S 865-029

 (8)  
Set the ATC system on STBY.

 S 865-030

 (9)  
Open these circuit breakers.

 (a)  
P6 Load Control Center - Right
 1) ATC 2
 2) DADC RIGHT
 3) ALTM FIRST OFFICER


 (b)  
P18 Load Control Center - Left
 1) ATC 1
 2) DADC LEFT
 3) ALTM CAPTAIN

 

 

 S 865-143
 (10) Remove electrical power if it is not necessary (Ref 24-22-00/201).
 TASK 34-53-00-735-116
 4. ATC System Test - Using TEL-Instruments T-33B Test Set
______________________________________________________
 A. General
 (1)  This system test is a more complete check of the ATC system. The system test first does the ATC Operational Test. Then it uses a ramp test set to examine the left and the right ATC system.
 B. Standard Tools and Equipment
 (1)  ATC Transponder Ramp Test - T.I.C. T-33B
 C. References
 (1)  AIRPLANES WITH EFIS;
 AMM 34-11-01/501, Pitot Static System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT MODE S ú

 34-53-00
 ú ú 02 Page 507 ú Mar 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (2)  
AIRPLANES WITH EFIS;
 AMM 34-11-00/501, Pitot Static System


 (3)  
AIRPLANES WITHOUT EFIS;
 AMM 34-12-00/501, Air Data Computer System


 (4)  
AIRPLANES WITH EFIS;
 AMM 34-12-01/501, Air Data Computer System


 (5)  
34-22-00/201, Manual Control

 (6)  
34-53-11/401 Antenna Removal/Installation


 D. Access
 (1)  
Location Zones
 101/102 Flight Compartment
 205 Electronic Compartment


 (2)  
Access Panels
 1201 Electronic Equipment Access Door

 

 E. Prepare for the System Test
 S 715-031
 (1)  
Do the ATC System - Operational Test.

 S 025-032

 (2)  
Remove appropriate ATC antenna (Ref 34-53-11/401).

 S 865-033

 (3)  
Connect the antenna end of transmission line to the T-33B test set as follows:


 CAUTION: DO NOT CONNECT THE TEST SET'S TNC CONNECTOR DIRECTLY TO
_______ THE ATC TRANSPONDER. THIS WILL CAUSE DAMAGE TO THE TEST SET.
 (a)  
The antenna must be disconnected from the TNC connector and protector cap must be installed on this TNC connector to prevent signals leak.

 (b)  
Connect a six foot test cable to the TNC connector on the test set.

 (c)  
With the right adapter, connect the other end of test cable to the ATC antenna transmission line.


 S 865-034
 (4)  Set the test set controls on the test set as follows:
 RCVR SENS - 65
 1090 - Zero
 REPLY/SLS - 100%
 MODE - 3/A
 READOUT - PILOT


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT MODE S ú

 34-53-00

 ú ú 03 Page 508 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-035
 (5)  Turn on the test set. Make sure the BATTERY CHECK meter is in the white part of the scale. If it is not, recharge the battery from a 115V AC 50-400 Hz source.
 NOTE: You can operate the test set while the battery is being
____
 charged.

 F. ATC System Test
 S 865-036
 (1)  Close these circuit breakers
 (a)  
P6 Load Control Center - Right
 1) ATC-2
 2) DADC RIGHT
 3) ALTM FIRST OFFICER
 
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 3(159)