TM 55-1520-240-T
11-6.8 PITCH COCKPIT CONTROL DRIVE ACTUATOR
FAILS TRIM MOTOR TEST
FAULT ISOLATION PROCEDURE
Personnel Required:
INITIAL SETUP
35M20 Avionic Navigation and Flight Control
Equipment Repairer.
Applicable Configurations:
All
Reference:
TM 55-1520-240-23
Tools:
Electronic Repairer’s Tool Kit,
NSN 5180-00-064-5178
Equipment Condition:
Visual Check of CCDA Performed (Task 11-6.2)
Multimeter
Materials:
None
11-6.8
END OF TASK
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