11-6.4 THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS
BRAKE FUNCTION TEST
FAULT ISOLATION PROCEDURE
Personnel Required:
INITIAL STEP
35M20 Avionic Navigation and Flight Control
Equipment Repairer.
Applicable Configurations:
All
Reference:
TM 55-1520-240-23
Tools:
Electronic Repairer’s Tool Kit,
Equipment Condition:
NSN 5180-00-064-5178
Visual Check of CCDA performed (Task 11-6.2)
Multimeter
Materials:
None
TM 55-1520-240-T
11-6.4
END OF TASK
11-233
