(5)  
Weight - 10 Pounds (44.5 N)

 (6)  
Shock Cord

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

 (2)  
AMM 25-22-01/401, Main Passenger Cabin Ceiling Panels

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-02
 ALL  ú ú N01 Page 501 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(3)  
AMM 31-61-00/501, Integrated Display System

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

 (5)  
AMM 76-11-01/501, Thrust Lever Assembly

 (6)  
AMM 76-11-03/201, Control Stand

 D.
Access

 (1)  
Location Zone
 211 Passenger Cabin - Nose to First Door, LH
 212 Passenger Cabin - Nose to First Door, RH
 221 Control Cabin LH
 222 Control Cabin RH

 E.
Preconditions

 S 865-109-N00
 (1)  
These conditions are necessary for this task:

 (a)  
Electrical power on (AMM 24-22-00/201).

 (b)  
Integrated Display System serviceable (AMM 31-61-00/501).

 (c)  
Airplane must be in the Ground Mode (AMM 32-09-02/201).

 F.
Adjustment Procedure

 S 865-002-N00
 (1)  
Do the deactivation procedure for the captain and first officer
 seats (AMM 76-11-03/201).

 S 015-003-N00

 (2)  
Remove the side panels on the control stand (AMM 76-11-03/201).

 S 865-004-N00

 (3)  
Remove the electrical power from the position resolvers, thrust lever switches, and interlock actuators for the reverse thrust lever (AMM 76-11-03/201).

 S 015-005-N00

 (4)  
Remove the ceiling panels to get access to the position resolver
 (AMM 25-22-01/401).

 (5)  
Hang a 10-pound (44.5 N) weight from the resolver crank.

 S 495-006-N00
 NOTE: You must have a load of sufficient weight to prevent the
____ effects of the backlash. But, the weight must not be more than 10 pounds (44.5 N).
 S 495-007-N00
 (6)  
Move all four thrust levers forward until you can install the rig
 pin TL1 through all four brake assemblies and each inboard side
 frame of the control stand (Fig. 501).

 (7)  
Install the rig pin TL1.

 S 495-092-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-02
 ALL  ú ú N03 Page 502 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(8)  S 495-008-N00Adjust the thrust levers (AMM 76-11-01/501).
 (9)  S 495-009-N00Adjust the connecting rods to the position resolvers for the No. 1 and No. 4 thrust levers until you can install the rig pin TR1 through the two resolver arms and the resolver mounting brackets (Fig. 501).
 S 495-093-N00

 (10)
 Install the rig pin TR1.

 S 495-010-N00

 (11)
 Adjust the connecting rods to the position resolvers for the No. 2 and No. 3 thrust levers until you can install the rig pin TR2 through the two resolver arms and the resolver mounting brackets (Fig. 501).

 S 495-094-N00

 (12)
 Install the rig pin TR2.

 S 435-011-N00

 (13)
 Tighten the jamnuts for the connecting rod.

 S 425-012-N00

 (14)
 Install the inspection seal on the connecting rods.

 NOTE: You cannot do the adjustment of the connecting rod again
____ after you do this step.
 S 035-013-N00
 (15) Disconnect the electrical connectors for the Channel A as follows:
 (a) P1 of T1742 for the position resolver of the No. 1 thrust lever
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 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 發動機控制 ENGINE CONTROLS(15)