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时间:2011-04-06 23:18来源:蓝天飞行翻译 作者:航空
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A
747-400 MAINTENANCE MANUAL
 G. Return the airplane to its usual condition
 S 865-090
 (1)  
Do the "Put the Air/Ground Relay System Back in the Ground Mode" task (Ref 32-09-02/201).

 S 415-031

 (2)  
If removed, install the ceiling drip shield (25-14-01/401).

 S 415-032

 (3)  
Install ceiling access panels (25-22-01/401).

 S 415-033

 (4)
Install the forward cargo sidewall lining (Ref 25-52-01/401).

 S 865-094

 (5)
Remove electrical power if it is not necessary (Ref 24-22-00/201).


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 21-58-00
 ALL  ú ú 13 Page 537 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 EQUIPMENT COOLING SYSTEM - INSPECTION/CHECK
___________________________________________
 1.  General
_______
 A.  This procedure has one task. The task is a visual inspection of the ducts and clamps of the equipment cooling system for the flight deck, main equipment center, and center equipment center.
 TASK 21-58-00-206-007
 2.  Equipment Cooling System Inspection (Fig. 601)
___________________________________
 A.  References
 (1)  
AMM 25-21-01/401, Main Deck Sidewall Linings and Dado Panels

 (2)  
AMM 25-52-01/401, Containerized Cargo Compartment Ceiling and Sidewall Linings

 (3)  
AMM 25-53-15/401, Ball-Transfer Panel


 B.  Access
 (1)  Location Zone
 116 Area between nose gear well and fuselage, RH 117 Electrical & Electronics Compartment, LH 118 Electrical & Electronics Compartment, RH 121 Forward Cargo Compartment Forward Half, LH 122 Forward Cargo Compartment Forward Half, RH 123 Forward Cargo Compartment Aft Half, LH 124 Forward Cargo Compartment Aft Half, RH 212 Main Deck Portal to Sta 488 - Right Side 221 Control Cabin, LH 222 Control Cabin, RH
 C.  Prepare for the inspection
 S 016-001
 (1)  
Remove the sidewall access panels in the forward cargo compartment on the left side between Sta. 620 and the forward bulkhead (AMM 25-52-01/401).

 S 016-002

 (2)  
Remove the sidewall access panels in the forward cargo compartment on the right side between Sta. 520 and the forward bulkhead (AMM 25-52-01/401).


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 21-58-00
 ALL  ú ú 01 Page 601 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 016-010
 (3)  
Remove the ball-transfer panel in the forward cargo compartment (AMM 25-53-15/401).

 S 016-008

 (4)  
Remove the right side passenger compartment sidewalls at the 6TH and 11TH windows (AMM 25-21-01/401).


 D.  Procedure
 S 216-004
 (1)  Examine the ducts for the following conditions:
 NOTE: When you are instructed to do a duct inspection, you will
____ look for these conditions. If you find any of these conditions, you must repair the defect.
 (a)  
Cracks, dents, or worn areas on the ducts

 (b)  
Duct support clamps that are loose or damaged

 (c)  
Duct couplings that are loose or damaged

 (d)  
Leakage of air from a duct that can be felt by hand

 (e)  
Leakage of air from a duct joint that can be felt by hand


 S 216-012
 (2)  Inspect these ducts in the forward cargo compartment:
 (a)  
Get access to the ducts in the main equipment center through the doors on the left and right sides of the forward bulkhead in the forward cargo compartment. 1) Make an inspection of the ducts to the E1 and E2 racks,

 main power center panels, and the flight deck.

 (b)  
Get access to the area between the nose gear well and the fuselage on the right side. 1) Make an inspection of the ducts that go to the flight

 compartment.
 
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