30-41-00
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757
FAULT ISOLATION/MAINT MANUAL

SEE

SEE
D MAIN EQUIPMENT CENTER
NOTE:  IF INSTALLED, TB106 AND TB107 ARE AT THE REAR OF THE E1 SHELF.

NOTE:  THIS UNIT IS NOT ELECTROSTATIC SENSITIVE.

LEFT OR RIGHT WINDOW HEAT CONTROL UNIT, M191 OR M192

Flight Compartment Window Anti-Icing System - Component Location
Figure 102 (Sheet 2)

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 30-41-00
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757 MAINTENANCE MANUAL
 FLIGHT COMPARTMENT WINDOW ANTI-ICING - ADJUSTMENT/TEST
______________________________________________________
 1.  General_______
 A.  This procedure contains two tasks. The first task is an operational test of the window anti-icing system for the flight compartment. The second task is a test of the resistances of the window heater element loop.
 B.  The tests are done on the flight deck and in the main E/E equipment bay, with only the test equipment on the airplane.
 C.  This procedure includes the resistance values for the window heater element. You can use these resistance values to find if the window heating element loop has the correct specification. These values are only for checks made across the window heater terminals.
 TASK 30-41-00-715-001
 2.  Operational Test - Flight Compartment Window Anti-Icing System______________________________________________________________
 A.  References
 (1)  
06-41-00/201, Fuselage (Major Zones 100 and 200) Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 (3)  
31-41-00/501, Engine Indication and Crew Alerting System (EICAS)

 B.  Access
 (1)  
Location Zones
 119/120 Main Equipment Center
 211/212 Control Cabin - Section 41

 (2)  
Access Panel
 119BL E/E Bay Access Door

 C.  Prepare for the Test
 S 865-002
 (1)  
Supply electrical power (Ref 24-22-00).

 S 715-003

 (2)  
Make sure the Engine Indication and Crew Alerting System (EICAS) is serviceable (Ref 31-41-00).

 S 215-004

 (3)  
Make sure the four WINDOW HEAT switches on the window heat control panel M10395 (panel P5) are in the OFF position.

 (4)  
　
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本文鏈接地址：757 AMM 飛機維護手冊 防冰和排雨 CHAPTER 30 - ICE AND RAIN PROTECTION(117)