TCH.1C-27J-2-27JG
Consumable Material Required:
None
Safety Conditions:
maintenance.
PROCEDURE:
2-54.1
(refer to figure
1.Lock the Control Wheel (2) and the Elevator rear
quadrants (3 and 9) in neutral position by means of
rigging pins (1, 4 and 8) (AGE NO. 00181).
CAUTION
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The PITCH TRIM ACTR (DRIVE) (13) and
the PITCH TRIM ACTR (SLAVE) (12) must
be set to Rig position. If it is not possible
to position the TRIM to rigged position it
can be adjusted manually until this
position is reached.
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2.Remove PITCH TRIM ACTUATOR DRIVE (13) (
) )and PITCH TRIM ACTUATOR
) ) .
3.Remove LH (RH) Q-FEEL ACTUATOR (5) ( (refer to
) ).
4.Hold the pitch Feel Trim Unit (6) and remove bolts (7),
washers (10) and self locking nuts (11) fixing Pitch
Feel Trim Unit (6) to Airframe. Discard removed self
locking nuts.
5.Remove Pitch feel trim unit (6) from the aircraft.
27-30-40
2-458