TASK 76-11-01-420-801-F00
3. Thrust levers Installation
(Figure 401, Figure 402, Figure 403, Figure 404, Figure 405, Figure 406, Figure 407, Figure 408)
A. General
(1) This task gives you instructions on how to install the thrust levers into the aisle control stand.
B. References
Reference Title
22-11-39-400-801 TOGA Switch Installation (P/B 401)
22-31-51-400-801 Autothrottle Disengage Switch Installation (P/B 401)
25-11-01-400-801 Captain's and First Officer's Seat Installation (P/B 401)
27-41-00-820-801 Stabilizer Control Cable and Chain - Adjustment (P/B 501)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-06-730-802 Flap Control Lever Position Sensor System Test (P/B 201)
27-62-00-820-801 Speed Brake Control Lever Adjustment (P/B 501)
76-11-03-400-802-F00 Control Stand Seal, Spacer and Retainer Installation (P/B 401)
76-11-03-400-804-F00 Control Stand Cover and Stop Installation (P/B 401)
76-11-03-420-801-F00 Control Stand Lightplate Installation (P/B 401)
76-11-05-820-801-F00 Thrust Lever Angle Resolver Adjustment (P/B 501)
78-31-00-700-801-F00 Thrust Reverser Normal Operation Test (P/B 501)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1585 Kit - Rigging Pin
737-600, -700, -800
Part #: F70207-109 Supplier: 81205
SPL-2409 Dowel Set - Thrust Lever, Control Stand
737-600, -700, -800
Part #: F80195-1 Supplier: 81205
SPL-2411 Tool Set - Control Stand Disassembly
737-600, -700, -800
Part #: C76002-26 Supplier: 81205
D. Consumable Materials
Reference Description Specification
D00013 Grease - Aircraft And Instrument Grease MIL-PRF-23827 (NATO
G-354) (Supersedes
MIL-G-23827)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-01
Page 423
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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