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时间:2011-04-11 09:19来源:蓝天飞行翻译 作者:航空
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 29-17-01
 ALL  ú ú 01 Page 204 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 B. Parts
 ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 201 | 1 | Reservoir Pressurization Module | 29-17-01 | 02 | 1 | | | 2 | Bolt | 29-17-51 | 01 | 35 | | | 3 | Washer | | | 40 | | | 4 | Jumper Assembly | | | 30 | | | 6 | Adapter | | | 110 | | | 7 | Nut | | | 105 | | | 8 | Packing | | | 95 | | | 9 | Packing | | | 90 | | | 10 | Ring | | | 85 | | | 11 | Plug | | | 60 | | | 12 | Packing | | | 70 | | | 15 | Adapter | | | ---| 2......…........…...................................…..........….....….........1
 C. References
 (1)  
AMM 20-22-01/601, Electrical Bonding

 (2)  
AMM 36-00-00/201, Pneumatic System

 (3)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 (4)  
AMM 54-62-02/501, Nacelle Strut Access Doors

 D.
Access

 (1)  
Location Zone
 454 System 1 - Strut Aft Fairing
 464 System 2 - Strut Aft Fairing
 474 System 3 - Strut Aft Fairing
 484 System 4 - Strut Aft Fairing


 (2)  
Access Panel 454AL Trailing Edge Fairing Doors - System 1 464AL Trailing Edge Fairing Doors - System 2 474AL Trailing Edge Fairing Doors - System 3 484AL Trailing Edge Fairing Doors - System 4

 E.
Procedure


 S 432-010
 (1)  
Remove the covers from the open tubes and the ports of the module (1) for reservoir pressurization.

 S 432-011

 (2)  
If you must install a new module (1), install the fittings in the new module:

 (a)  
Apply lubricant to the packings and the threads on the fittings.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 01 Page 205 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  
Install the nut (7) and the packings (8, 9, and 10) on the adapter (6).

 (c)  
Install the adapter (6) in the RES port.

 (d)  
Install the packing (12) on the plug (11) (2 locations).

 (e)  
Install the plugs (11) in the ports GA and T.

 (f)  
Install the packings (8, 9, and 10) on the adapter (15).

 (g)  
Install the adapter (15) in the IN port.


 S 422-012
 (3)  
Put the module (1) in its position.

 S 432-065

 (4)  
Install the bonding jumper (4), and the four bolts (2) and washers (3).

 S 762-013

 (5)  
Make sure the resistance of the electrical bond is less than 0.0025 ohms (AMM 20-22-01/601).

 S 642-066

 (6)  
Apply Lubricant to the threads on the adapters (6 and 15).

 S 432-067

 (7)  
Connect the tubes to the adapters (6 and 15).

 S 792-015

 (8)  
Apply some leak detector on all the tube and fitting connections.

 S 862-068

 (9)  
Pressurize the pneumatic system (AMM 36-00-00/201).

 S 212-069

 (10)
 Examine all the tube and fitting connections for leakage:

 (a)  
If bubbles come slowly into view, the quantity of leakage is satisfactory.

 (b)  
If you find a high concentration of leakage, you must repair the cause of the leakage.


 S 862-017
 (11) Release the pressure in the pneumatic system if it is not necessary (AMM 36-00-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-17-01
 ALL  ú ú 01 Page 206 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 212-070
 
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