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bellcranks and attaching hardware for
condition - refer to 27-20-01 201. 200    X X 
27-20 4) Visually inspect the adjustable end of the rudder trim tab control (on control surface side). 300    X X 
27-30 Elevator       
27-30 1) Remove the servo-actuator of the electrical pitch trim control (if installed). Check setting and inspect for corrosion - refer
to 27-30-06 201, 22-11-00 201 and 200    X X 
 22-12-00 201. Install the servo-actuator.       
27-30 2) Visually inspect the elevator and trim tab control input rods in the rear fuselage. 200    X X 
27-30 3) Visually inspect the support of the electrical pitch trim control servo-actuator and its attach fittings (if installed). 200    X X 
27-30 4) Visually inspect the stall warning device, check attach fittings and connectors - refer to 27-30-04 201. 500    X  
27-30 5) Visually inspect the adjustable end of the elevator and the trim tab (on control surface side). 300    X X 
27-50 Wing flaps       
27-50 1) Visually inspect the flap relays, check attach fittings and lugs. 200    X  
27-50 2) Visually inspect the flap actuator and the supports for cracks. Using a mirror, inspect for cracks on frame C4 - refer to 200    X  500 hrs
 27-50-01 201.       
27-50 3) Visually inspect the flap controls and the indicator - refer to 27-50-01 201. 200    X X 

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform the operations identified with a "0" unless the annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
AHAA
Validity : S / N 1 - 9999 05-20-01 Page 214
(IA) JUN 01
 

ATA OPERATIONS  INSPECTIONS
  Area 1st
25 hrs 50
hrs 100
hrs Major Ann. Other
27-50 4) Visually inspect (do not remove) the L.H. flap control rods. 500    X X 
27-50 5) Remove and clean the L.H. flap control bellcrancks. Perform a detail examination. 500    X  1000 hrs
 Lubricate. Install.       
27-50 6) Visually inspect (do not remove) the flap control linkage for security of attach fittings, play, evidence of wear, interference and corrosion - refer to 27-50-01 201. 000    X  1000 hrs
　
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