AIM
Validity : S / N 1 - 9999 05-20-05 (JA) Page 207
JUN 01
ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
27-00 55) Visually inspect the control wheels for security on torque tubes. 200
27-00 56) Visually inspect roll stops and ball joints for condition and play. 200
27-00 57) Visually inspect the roll control, behind the instrument panel, for R.H. and L.H. gimbal joint play, the pylon and check that the control wheel can move forth and back without resistance. 200
27-00 S / N 275 - 9999 200
58) Visually inspect the elevator trim tab control linkage
(cables, pulleys) for play - refer to 27-30-03 601,
20-00-07 201.
27-00 S / N 1 - 9999 200
59) Visually inspect the flight controls control linkage (along the 3 axes) for play, check cabin sealing bellows for condition :
- roll - refer to 27-10-00 201,
- rudder and elevator - refer to 27-20-00 201,
27-30-00 201.
NOTE : Make sure that flight control stops are reached before rudder and elevator control stops.
27-00 60) Visually inspect the rudder trim tab control linkage (ball control) for play - refer to 27-20-04 201. 200
27-20 61) Visually inspect the rudder and trim tab input rods in the rear fuselage. 200
27-20 62) Visually inspect the adjustable end of the rudder control 200
(on control surface side).
27-20 63) Visually inspect the nose landing gear/rudder
interconnection rods on rudder pedals, check cabin sealing bellows, bellcranks and attaching hardware for condition - refer to 27-20-01 201. 200
27-30 64) Visually inspect the elevator and trim tab control input rods in the rear fuselage. 200
27-30 65) Visually inspect the support of the electrical pitch trim control servo-actuator and its attach fittings (if installed). 200
27-50 66) Visually inspect the flap controls and the indicator - refer to 27-50-01 201. 200
28-20 S / N 731 - 9999 200
67) Visually inspect the electric pump, the support, the unions, the vent hose and the connections.
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