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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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CONTROL CABLE TCC AIR VALVE  (2 PLACES) MOUNT SHAFT ACTUATOR RAIL BRACKET (4 PLACES) HINGED CLAMP (4 PLACES) BOLT ENGAGEMENT CABLE INNER TCC AIR VALVE ACTUATOR  (SHT 2) CSEE  SEE  A 
NUT COUPLING  SEE  B 
FWD  TCC AIR VALVE ACTUATOR 
GROUND STRAP  BOLT  ELECTRICAL CONNECTOR EEC 

TCC AIR VALVE CONTROL CABLE 

FWD 
DRAIN 
SERVO FUEL  TUBE 
SUPPLY TUBE 
SERVO FUEL 
RETURN TUBE 

Turbine Case Cooling Air Valve Actuator Installation 
Figure 401 (Sheet 1) 

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 ALL  ú ú N01 Page 402 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(b)  Make sure the applicable FUEL SPAR VLV 1, 2, 3, or 4 status message does not show.
___
 S 864-005-N00
 (4)  For the applicable engine, open these circuit breakers on the main power distribution panel, P6, and install the DO-NOT-CLOSE tags:
 (a)  
6G1 FUEL SHUTOFF VALVE ENG 1

 (b)  
6G15 SCU ALT PWR ENG 1

 (c)  
6G23 ENG SCU 1

 

FWD
Turbine Case Cooling Air Valve Actuator Installation
Figure 401 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(d)  
6G2 FUEL SHUTOFF VALVE ENG 2

 (e)  
6G16 SCU ALT PWR ENG 2

 (f)  
6G24 ENG SCU 2

 (g)  
6G3 FUEL SHUTOFF VALVE ENG 3

 (h)  
6G17 SCU ALT PWR ENG 3

 (i)  
6G25 ENG SCU 3

 (j)  
6G4 FUEL SHUTOFF VALVE ENG 4

 (k)  
6G18 SCU ALT PWR ENG 4

 (l)  
6G26 ENG SCU 4


 S 014-050-N00
 (5)  Open the right fan cowl panel (AMM 71-11-04/201).
 S 044-049-N00
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
 (6)  
Do this procedure: Thrust Reverser Deactivation for Ground
 Maintenance (AMM 78-31-00/201).


 S 014-048-N00

 (7)  
Open the right core cowl panel (AMM 71-11-06/201).


 S 014-047-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (8)  
Open the right thrust reverser (AMM 78-31-00/201).

 E.  
Procedure


 S 024-056-N00
 (1)  
Remove the actuator:

 (a)  
Disconnect the EEC electrical connector from the actuator.


 1)  Install protection caps to the EEC electrical connector and the receptacle on the actuator.
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 ALL  ú ú N03 Page 404 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(b)  
Remove the bolt and nut which attach the rod end bearing of the control cable to the idler arm on the HPT cooling-air shutoff valve.

 (c)  
Disconnect the coupling nut of the control cable from the actuator shaft.

 (d)  
Put the container below the fuel lines to catch the remaining fuel.

 (e)  
Disconnect the servo fuel supply, servo fuel return and drain tubes from the actuator.

 (f)  
Remove the bolt which attaches the ground strap to the actuator.
 
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本文链接地址:747-400 AMM 飞机维护手册 大气 AIR 1(70)