REVERSE THRUST INTERLOCK SOLENOID - REMOVAL/INSTALLATION
1. General
A. This procedure has two tasks:
(1) Reverse Thrust Interlock Solenoid Removal
(2) Reverse Thrust Interlock Solenoid Installation.
TASK 76-11-06-000-801-F00
2. Reverse Thrust Interlock Solenoid Removal
(Figure 401 and Figure 402)
A. General
(1) This task provides the instructions on how to remove the reverse thrust interlock solenoid from
the autothrottle assembly.
(2) There are two interlock solenoids installed in the autothrottle and they are not interchangeable.
B. References
Reference Title
20-10-91-000-801 Control Cables Removal (P/B 401)
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
78-31-00-040-802-F00 Thrust Reverser Deactivation For Ground Maintenance
(P/B 201)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
113 Area Above and Outboard of Nose Landing Gear Wheel Well - Left
114 Area Above and Outboard of Nose Landing Gear Wheel Well - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
112A Forward Access Door
114AW Forward Nose Wheel Well Panel
E. Prepare for the Removal
SUBTASK 76-11-06-860-001-F00
WARNING
MOVE ALL PERSONS AND EQUIPMENT AWAY FROM THE TRAILING EDGE
FLAPS, AND THE LEADING EDGE FLAPS AND SLATS. THESE SURFACES
WILL MOVE AND CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
EQUIPMENT.
(1) Operate the stabilizer trim system to provide cable clearance for access of the autothrottle
assembly.
(a) Set the stabilizer trim lever at 4.2 degrees or the NOSE UP stop.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-06
Page 401
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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