TM 55-1520-240-T
11-6.7 PITCH COCKPIT CONTROL DRIVE ACTUATOR
FAILS BRAKE FUNCTION TEST
FAULT ISOLATION PROCEDURE
Personnel Required
INITIAL SETUP
35M20 Avionic Navigation and Flight Control
11-6.7
Applicable Configurations:
Equipment Repairer.
All
Reference:
TM 55-1520-240-23
Tools:
Electronic Repairer’s Tool Kit,
NSN 5180-00-064-5178
Multimeter
Equipment Condition:
Visual Check of CCDA Performed (Task 11-6.2)
Materials:
None
END OF TASK
11-236
