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时间:2011-04-17 09:11来源:蓝天飞行翻译 作者:航空
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 (e)  Remove the cover assemblies on the two sides of the engine on the rear collector.
 S 034-006-N00
 (6)  Remove the bolts and nuts which attach the collector and lower support link to the support bracket and the shutoff valve flange for the LPT case cooling air (section A-A).
 S 034-007-N00
 (7)  Remove the bolts and clamps which attach the inboard bracket on the collector to the bracket on the flange N.
 S 024-008-N00
 (8)  Remove the bolts, nuts, and clamps which attach the collector to the brackets on the flange P.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-24-08
 ALL  ú ú N02 Page 405 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 024-023-N00
 (9)  
Remove the collector from the engine.

 S 034-009-N00

 (10)
 Install the protection caps to the collector and the openings on the cooling air tubes and shutoff valve.


 TASK 75-24-08-404-010-N00
 3. Install the Low Pressure Turbine Case Cooling Collector (Fig. 401)
_______________________________________________________
 A. Consumable Materials
 (1)  
D00390 Oil - Engine

 B.
References

 (1)  
AMM 71-11-06/201, Core Cowl Panels

 (2)  
AMM 75-24-09/401, Low Pressure Turbine Case Cooling Manifolds

 (3)  
AMM 78-31-00/201, Thrust Reverser Systems

 (4)  
IPC 36-11-01 Fig. 5

 (5)  
IPC 75-24-00 Fig. 10

 (6)  
IPC 75-24-09 Fig. 1

 (7)  
IPC 75-24-09 Fig. 5

 C.
Access

 (1)  
Location Zone
 412 Engine 1 - LPT Case 3 o'clock
 422 Engine 2 - LPT Case 3 o'clock
 432 Engine 3 - LPT Case 3 o'clock
 442 Engine 4 - LPT Case 3 o'clock


 (2)  
Access Panel
 417 and 418 Core Cowl Panels - Engine 1
 427 and 428 Core Cowl Panels - Engine 2
 437 and 438 Core Cowl Panels - Engine 3
 447 and 448 Core Cowl Panels - Engine 4


 D.
Procedure

 (1)  
Remove the protection caps.

 S 424-012-N00

 (2)  
Put the collector below the LPT case cooling air shutoff valve on the LPT case.

 S 644-024-N00

 (3)  
Lubricate the threads of the bolts, which attach the collector, with engine oil.

 S 434-013-N00

 (4)  
Attach the collector to the support bracket and shutoff valve with bolts (use the longer bolt at the support link location) and nuts (section A-A).

 (a)  
Tighten the bolts with your hand.


 S 434-011-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-24-08
 ALL  ú ú N01 Page 406 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(5)  S 434-014-N00Install the clamps on the forward inboard bracket of the collector.
 (6)  S 644-025-N00Lubricate the threads of the bolts, which attach the clamps, with engine oil.
 (7)  S 434-026-N00Attach the clamps to the bracket on the flange N with the bolts. (a) Tighten the bolts with your hand.
 (8)  S 434-015-N00Install the clamps on the aft collector mount.
 (9)  S 644-027-N00Lubricate the threads of the bolts, which attach the clamps on the aft collector mount, with engine oil.
 S 434-028-N00

 (10) Attach the clamps to the brackets on the flange P with the bolts and nuts.
 (a) Tighten the bolts with your hand.
 S 434-016-N00
 (11)
 Tighten the bolts which attach the collector to the support bracket and the shutoff valve flange to 85-95 pound-inches (9.6-10.7 newton-meters).

 S 434-017-N00

 (12)
 Tighten the bolts which attach the forward collector mount to the flange N bracket to 36-40 pound-inches (4.1-4.5 newton-meters).

 S 434-018-N00

 (13)
 Tighten the bolts which attach the clamps on the aft collector mount to the flange P brackets to 36-40 pound-inches (4.1-4.5 newton-meters).
 
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