TM 55-1520-240-23-9
11-162
INSTALL PITCH CCD ACTUATOR
11-162
INITIAL SETUP
Applicable Configurations:
All
Tools:
Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692
Torque Wrench, 30 to 150 Inch-Pounds
Materials:
Lockwire (E227)
Parts:
Cotter Pins
Personnel Required:
Medium Helicopter Repairer
Inspector
References:
TM 55-1520-240-23P
Task 1-13
Task 11-38
Task 11-54
Task 11-279
Make sure bushings are in arm before
installing bolts or component damage
will result.
NOTE
Impedance bolts are installed in flight
control connections. These bolts are
self-retaining and require a special
nut and torque (Task 1-13).
1.
If pitch CCD actuator (1) is a replacement, check
if actuator arm is at neutral (Task 11-38).
2.
Position two supports (2 and 3) on actuator (1),
lugs (4) away from actuator. Install four bolts
(5) and four washers (6). Torque bolts to 40
inch-pounds.
3.
Lockwire four bolts (5). Use lockwire (E227).
INSPECT
11-660