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时间:2011-04-17 09:13来源:蓝天飞行翻译 作者:航空
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 S 024-051-N00
 (3)  For the left control valve (4), if it is necessary to replace the control valve (4), do the steps that follow:
 (a)  
ENGINES POST-PW-SB 75-62R2 OR PRE-PW-SB 75-91;
 Remove the cap assembly (12) from the adapter (11).


 (b)  
Remove the adapter (11) and gasket (10) from the control valve (4). 1) Discard the gasket (10).

 (c)  
Remove the plug (13) and gasket (10) from the adjacent port. 1) Discard the gasket (10).

 (d)  
Remove the bolts (1) that attach the cover (9).
 1) Remove the cover (9) from the control valve (4).


 (e)  
Remove the bolts (1) that attach the bracket (14) and the cover (2). 1) Remove the cover (2) and the bracket (14) from the control


 valve (4).
 S 024-055-N00
 (4)  For the right control valve (4), if it is necessary to replace the control valve (4), do the steps that follow:
 (a)  
ENGINES POST-PW-SB 75-62R2 OR PRE-PW-SB 75-91;
 Remove the cap assembly (12) from the adapter (11).


 (b)  
Remove the adapter (11) and gasket (10) from the control valve (4). 1) Discard the gasket (10).


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 75-33-01
 ALL  ú ú N03 Page 407 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(c)  
Remove the plug (13) and gasket (10) from the adjacent port. 1) Discard the gasket (10).

 (d)  
Remove the bolts (1) that attach the cover (9). 1) Remove the cover (9) from the control valve (4).

 (e)  
Remove the bolts (1) that attach the cover (2). 1) Remove the cover (2) from the control valve (4).


 S 024-054-N00
 (5) Install protection caps to all openings in the control valve (4).
 TASK 75-33-01-404-012-N00
 3. Install the HPC Secondary Flow Control Valve (Fig. 401)
____________________________________________
 A. Equipment
 (1)  M303, M305, or M307 Bergen Mechanical Crimper
 Bergen Cable Technologies Inc
 170 Gregg St

 P.O.
 Box 1300
 Lodi, NJ 07644-9982


 B.
Consumable Materials


 (1)  
D00390 Oil - Engine

 (2)  
G00767 Wax - Paraffin, PMC 9552

 (3)  
G00964 Compound - Antigalling, Fel-Pro C-200

 (4)  
G02334 Lockwire - AS3214-02

 (5)  
G02332 Ferrule - P05-292 (Optional)

 (6)  
G02335 Cable - Safety - P05-291 (Optional)


 C. Parts ~............................................................................... | AMM | | AIPC | ....................... ........................... | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................. | 401 | 3 | Gasket | 75-33-01 | 01 | 50 | | | 4 | HPC Secondary Flow Control | | | 45 | | | | Valve | | | | | | 10 | Gasket | 75-33-51 | 01 | 15 | 2..........…..........…...............................…..........….....…........1
 D. References
 (1)  
AMM 36-11-01/401, Pneumatic Manifold

 (2)  
AMM 70-24-05/201, Electrical Harnesses

 (3)  
AMM 71-00-00/501, Power Plant

 (4)  
AMM 71-11-04/201, Fan Cowl Panels

 (5)  
AMM 71-11-06/201, Core Cowl Panels

 (6)  
AMM 78-31-00/201, Thrust Reverser System

 E.
Access

 (1)  
Location Zone
 412 Engine 1 - HPC Fwd Case 3:30 or 9:30 o'clock
 422 Engine 2 - HPC Fwd Case 3:30 or 9:30 o'clock
 432 Engine 3 - HPC Fwd Case 3:30 or 9:30 o'clock
 442 Engine 4 - HPC Fwd Case 3:30 or 9:30 o'clock

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-33-01
 ALL  ú ú N03 Page 408 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(2)  
 
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