• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-06 23:18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

 1.  General_______
 A.  This procedure has these ground tests, operational tests, and system tests for the Equipment Cooling System:
 (1)  
Ground Test - Equipment Cooling

 (2)  
Ground Test - E/E Detector

 (3)  
Operational Test - Override Mode Test

 (4)  
Operational Test - Bypass Valve and Supply/Exhaust Fan Test

 (5)  
Operational Test - Low Flow Detector Test

 (6)  
Operational Test - E6/E9 Valve

 (7)  
System Test - Differental Pressure Switch Test

 (8)  
System Test - E30 Rack Pressure

 (9)  
System Test - E1/E2 Rack Pressure

 (10)
 System Test - CARGO FIRE Switch Test

 (11)
 System Test - Electrical Test


 B.  The electrical system test does a check of the equipment cooling system in each mode of operation. The test also includes a check of the overheat switch.
 C.  The Equipment Cooling ground test includes a check of the clean cycle logic.
 D.  The Detector Ground Test does a check of the equipment cooling low flow (cooling effect) detectors and the smoke detector (Ref 26-16-51).
 E.  All circuit breakers for the equipment cooling system must be closed before a test is done.
 F.  The tests that follow include valve position checks. To find the position of the equipment cooling inboard supply valve, inboard exhaust valve, bypass valve, E6/E9 valve, smoke/override valve, and 3-way valve, look at the position indicator on the valve actuator. The position of the ground exhaust valve must be found by a visual check of the flapper position.
 TASK 21-58-00-705-001
 2.  Ground Test - Equipment Cooling_______________________________
 A.  General
 (1)  The ground test for the equipment cooling system commands the equipment cooling card to do a self-test and the equipment cooling system to go to the override mode. When the system is in the override mode, these conditions will occur:
 (a)  The supply and exhaust fans to stop.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-58-00
 ALL  ú ú 12 Page 501 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M03103
Pressure Correction
___________________  BAROMETRIC PRESSURE (IN. HG)
A747-400MAINTENANCE MANUAL
Gage Pressure Correction Chart
Figure 501

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.ú
 21-58-00
ALL  úú 02 Page 502 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.  
Obtain local ambient barometric pressure (Pbar).

2.  
Measure E/E bay air temperature (Tbay).

3.  
Locate E/E bay temperature on left axis of table and follow row to the column corresponding to the Barometric pressure. Read the correction factor (Cf).

4.  
Calculate the corrected pressure (Pcor)as follows:


E/EPcor = P*Cf (Where: P is measured Baypressure)Temp (`F)Example
P = 2.6 IN. H O
2
Pbar = 30.1 IN. HG
Tbay = 46`F
From table: (45`F/30.2 IN. HG) Cf = 0.95
Pcor = 2.6 IN. H2O*0.95 = 2.47 IN. H2O
____ For ambient conditions outside the range
NOTE: of the table, the correction factor mustbe calculated as follows:
10  28.7  29.0  29.3  29.6  29.9  30.2  30.5  30.8 
0.93  0.92  0.91  0.90  0.89  0.88  0.87  0.86 
15  0.94  0.93  0.92  0.91  0.90  0.89  0.88  0.87 
20  0.95  0.94  0.93  0.92  0.91  0.90  0.89  0.88 
25  0.96  0.95  0.94  0.93  0.92  0.91  0.90  0.89 
30  0.97  0.96  0.95  0.94  0.93  0.92  0.91  0.90 
35  0.98  0.97  0.96  0.95  0.94  0.93  0.92  0.91 
40  0.99  0.98  0.97  0.96  0.95  0.94  0.93  0.92 
45  1.00  0.98  0.97  0.96  0.96  0.95  0.94  0.93 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 空调 AIR CONDITIONING 2(62)