TM 55-1520-240-23-6
7-99
ADJUST PITCH, ROLL, OR YAW INTEGRATED LOWER CONTROL ACTUATOR (ILCA)
CROSS FEEDBACK TRANSDUCER ON AIRCRAFT
7-99
INITIAL SETUP
Applicable Configurations:
All
Tools:
AFCS Line Test Set 145G0009-1
Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692
Dial Indicating Scale, 0 to 10 Pounds
Materials:
Lockwire (E230)
Personnel Required:
Avionics Mechanic
Inspector
References:
TM 55-1520-240-23P
TM 55-4920-429-13
Task 7-87
Task 7-88
Equipment Condition:
AFCS Line Test Set 145G0009-1 Prepared For Use
With No. 1 AFCS Computer (TM 55-4920-429-13)
Pitch, Roll Or Yaw Cross Transducers Tested For Null
(Task 11-280, Test 1, 3, or 5)
Flight Controls Closet Acoustic Blanket Removed
(Task 2-107)
Flight Control Closet Panel Removed (Task 2-2)
Integrated Lower Control Pitch, Roll or Yaw Actuator
(ILCA) Removed (Task 7-84)
7-473