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时间:2011-04-16 10:11来源:蓝天飞行翻译 作者:航空
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 (b)  
Remove the center manifold.

 (c)  
Install the caps on the manifold tube ends.


 S 024-029-N00
 (12) To remove the right manifold, do the steps that follow:
 (a)  
Turn the manifold counterclockwise (as viewed from rear) until the manifold is clear of the support bracket.

 (b)  
Remove the manifold.

 (c)  
If you will replace the right manifold, remove the plug and the washer from the manifold.


 NOTE: The plug and the washer will be installed on the new
____
 manifold.

 TASK 77-11-02-404-011-N00
 3. Engine Pressure Ratio (PT4.95) Manifold Installation (Fig. 401)
____________________________________________________
 A. Equipment
 (1)  M303, M305, or M307 Bergen Mechanical Crimper
 Bergen Cable Technologies
 170 Greg Street

 P.O. Box 1300
 Lodi New Jersey 07644 USA

 B. Consumable Materials
 (1)  D00390 Oil, Engine
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 77-11-02
 ALL  ú ú N01 Page 406 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(2)  
G02332 Ferrule, Safety Cable (P05-292)

 (3)  
G02334 Lockwire, AS3214-02 (P05-289)

 (4)  
G02335 Cable, Safety (P05-291)

 C.
References

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

 (2)  
AMM 77-11-01/501, Engine Pressure Ratio (EPR) PT4.95 Probe

 (3)  
IPC 77-11-02 Fig. 1

 D.
Access

 (1)  
Location Zone
 412 Engine 1 - Turbine Exhaust Case 4 to 10 o'clock
 422 Engine 2 - Turbine Exhaust Case 4 to 10 o'clock
 432 Engine 3 - Turbine Exhaust Case 4 to 10 o'clock
 442 Engine 4 - Turbine Exhaust Case 4 to 10 o'clock


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


 E.
Procedure


 S 434-012-N00
 (1)  If you will install a new manifold, install the clamps on the
 manifold.

 S 424-013-N00
 CAUTION: DO NOT USE LUBRICANTS ON THE EEC TUBES, ADAPTERS, OR O-RINGS.
_______
 LUBRICANTS CAN CAUSE DAMAGE TO THE EEC.

 (2)  To install the right manifold, do the steps that follow:
 (a)  
If you will install a new manifold, do the steps that follow: 1) Remove the cap from the manifold. 2) Install the plug and the washer to the manifold. 3) Tighten the plug to 40-50 pound-inches

 (4.5-5.6 newton-meters). 4) Install lockwire or the optional safety cable and ferrule to the plug.

 (b)  
Put the right manifold tube end between the support bracket (View G) and the turbine exhaust case.

 (c)  
Turn the manifold clockwise (as viewed from rear) until the manifold tube nut is adjacent to the adapter (installed at the 4 o'clock position - View D) on the EPR probe.

 (d)  
Connect the manifold tube nut to the adapter.

 (e)  
Tighten the manifold tube nut with your hand.


 S 424-014-N00
 (3)  To install the center manifold, do the steps that follow:
 (a)  Put the manifold tube end between the support bracket and the turbine exhaust case (View A-A).
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 77-11-02
 ALL  ú ú N01 Page 407 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(b)  
Turn the manifold counterclockwise until the manifold tube nuts are in the correct position.

 (c)  
Connect the tube nut to the right EPR manifold.

 (d)  
Connect the EEC tube nut to the manifold tee (at the 6 o'clock position).

 (e)  
Tighten the tube nuts with your hand.
 
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