76-11-01
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 434-045-N00
 (6)  Connect the electrical connectors as follows: (a) P12 (b) P13 (c) P14 (d) P15 (e) P19 (f) P20 (g) P21 (h) P22
 S 434-018-N00
 (7)  Attach the wire bundle to the wire guide with a lockstitch.
 S 414-019-N00
 (8)  Install the ceiling panels in the passenger cabin (AMM 25-22-01/401).
 S 434-020-N00
 (9)  Connect the control rods to the thrust levers with bolts, washers and nuts.
 S 824-021-N00

 (10)
 Do this task: Adjust the Thrust Lever Assembly (AMM 76-11-01/501).

 S 414-034-N00

 (11)
 Do this task: Install the Engine Start Module (AMM 76-11-03/201).

 S 414-035-N00

 (12)
 Do this task:  Install the Thrust Lever Rails on the Control Stand (AMM 76-11-03/201).

 S 414-036-N00

 (13)
 Do this task:  Install the Thrust Lever Cover on the Control Stand (AMM 76-11-03/201).

 S 414-037-N00

 (14)
 Do this task:  Install the Side Panels on the Control Stand (AMM 76-11-03/201).

 S 864-038-N00

 (15)
 Do this task:  Activation Procedure for the Autothrottle Servomotor (AMM 76-11-03/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-01
 ALL  ú ú N01 Page 406 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 864-039-N00
 (16)
 Do this task:  Energize the Thrust Lever Switches (AMM 76-11-03/201).

 S 864-040-N00

 (17)
 Do this task:  Energize the Fuel Control Toggle Switches (AMM 76-11-03/201).

 S 864-041-N00

 (18)
 Do this task:  Energize the STAB TRIM Switches and Indicators (AMM 76-11-03/201).

 S 864-024-N00

 (19)
 Do this task:  Activation Procedure for the Captain and the First Officer Seats (AMM 76-11-03/201).

 S 714-025-N00

 (20)
 Do this task: Thrust Reverser Operational Test (AMM 78-31-00/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-01
 ALL  ú ú N02 Page 407 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
THRUST LEVER ASSEMBLY - ADJUSTMENT/TEST
_______________________________________
 1.  General
_______
 A.  This procedure makes sure that the thrust lever assemblies are correctly adjusted and operate correctly.
 B.  You must do the adjustment at an ambient temperature of 60°-90°F.
 C.  All test equipment must operate for a minimum of 10 minutes before you use it, to let the temperature become stable.
 D.  You can read the thrust lever angle from the EICAS EPCS maintenance page when you do not have a digital thrust lever protractor. But, you are recommended to find the thrust lever angle with the thrust lever protractor G76002-14.
 TASK 76-11-01-825-001-N00
 2.  Adjust the Thrust Control Lever Assembly
________________________________________
 A.  Equipment
 (1)  
G12001-1 Rig Pin Set

 (a)  TL1, MS20392-4C or equivalent 0.309-0.311 inch (7.85-7.90 mm) diameter rod or bolt by 12.0 inches (305 mm) in length

 (2)  
G76002-14 Protractor - Thrust Levers, Forward and Reverse

 (3)  
Gage - Dial push/pull, DPP-25 (DPP-125N),
 25-pound (125N) capacity

 B.  References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 27-62-09/401, Auto Speed Brake Arming Switch

 (3)  
AMM 31-61-00/501, Integrated Display System

 (4)  
AMM 32-09-02/201, Air/Ground Relays

 (5)  
AMM 76-11-03/201, Control Stand

 (6)  
AMM 76-11-02/501, Thrust Lever Position Resolver
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 發(fā)動機控制 ENGINE CONTROLS(8)