TM 55-1520-240-T
11-6.5 THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS NULL VOLTAGE AND PHASING TEST
11-6.5
FAULT ISOLUTION PROCEDURE
INITIAL SETUP
Personnel Required:
Applicable Configurations:
Avionic Navigation and Flight Control
All
Equipment Repairer.
Tools:
Reference:
Electronic Repairer’s Tool Kit,
TM 55-1520-240-23
NSN 5180-00-064-5178
Equipment Condition:
Multimeter
Visual Check of CCDA Performed (Task 11-6.2)
Materials:
None
D145-12474-SPA
END OF TASK
11-234
Change 14
