THRUST LEVER ANGLE RESOLVER AND AUTOTHROTTLE BRAKE ASSEMBLY - ADJUSTMENT/TEST
1. General
A. This procedure has two tasks:
(1) Thrust Lever Angle Resolver Adjustment
(2) Autothrottle Brake Assembly Test.
TASK 76-11-05-820-801-F00
2. Thrust Lever Angle Resolver Adjustment
(Figure 501 and Figure 502)
A. General
(1) This task provides the instructions on how to adjust the Thrust Lever Angle (TLA) resolver.
(2) TLA resolver is referred to as the resolver.
(3) The adjustment procedure is the same for each resolver.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
31-51-00-730-802 Landing Warning System Test (P/B 501)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
112A Forward Access Door
E. Prepare for the Adjustment
SUBTASK 76-11-05-910-001-F00
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 76-11-05-860-011-F00
(2) Make sure that these circuit breakers are closed:
CAPT Electrical System Panel, P18-2
Row Col Number Name
A 4 C01390 ENGINE 1 ALTN PWR CHAN B
A 5 C01314 ENGINE 1 ALTN PWR CHAN A
A 6 C01017 FMCS CMPTR 1
ILF 401, 405, 409, 410, 412, 416, 424, 425, 427-429, 496, 500, 504, 507, 515, 518-520, 530-532, 556,
557, 560, 703; ILF 402, 452, 508, 510, 523, 525-528 PRE SB 737-23-1353; ILF 491, 492, 559 PRE SB
737-34-3136
A 7 C01018 FMCS CDU 1
ILF ALL
D 2 C01372 DISPLAY CTR UPR
D 5 C01359 DISPLAY DEU 1 PRI
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-05
Page 501
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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