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corrosion - refer to 27-30-06 201, 22-11-00 201 and 200  
 22-12-00 201. Install the servo-actuator.   
22-10 30) Remove the servo-actuators of the autopilot (if installed), check setting and inspect for corrosion - refer to 200 1000 hrs 
 22-11-00 201 or 22-12-00 201 or 22-12-03 401 or   
 22-12-04 401 or 22-12-06 401. Install the
servo-actuators.   
22-10 31) Visually inspect the supports, levers, attachments of the autopilot (if installed) servo-actuators. Inspect
servo-actuator links to flight control linkages. 200 1000 hrs 
27-00 32) 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  
27-20 33) Visually inspect the rudder and trim tab input rods in the rear fuselage. 200  
27-20 34) Visually inspect the adjustable end of the rudder control 200  
 (on control surface side).   

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05 20-06Page 206
(EA) JUN 01
 

ATA ANNUAL INSPECTION (Al)
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
27-20 35) 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 36) Visually inspect the elevator and trim tab control input rods in the rear fuselage. 200  
27-30 37) Visually inspect the support of the electrical pitch trim control servo-actuator and its attach fittings (if installed). 200  
27-50 38) Visually inspect the flap controls and the indicator - refer to 27-50-01 201. 200  
28-20 S / N 731 - 9999 200  
 39) Visually inspect the electric pump, the support, the unions, the vent hose and the connections.   
73-30 40) Visually inspect the fuel flow totalizer sensor under the cabin floor (if installed), check the unions and connections for condition. 200  
28-20 S / N 1 - 9999 200  
 41) Visually inspect the fuel lines for routing and leaks.   
28-20 S / N 731 - 9999 200  
　
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