曝光臺 注意防騙
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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 7) Visually inspect the rudder trim tab control linkage (ball control) for play - refer
to 27-20-04 201. 200 X
27-00 8) Check control surfaces for travel, efficiency and direction of flight controls : 000 X
- pitch - refer to 27-30-00 201,
- elevator trim tab - refer to 27-30-03 501, - rudder - refer to 27-20-00 201,
- rudder trim tab - refer to 27-20-04 201, - roll - refer to 27-10-00 201,
- wing flaps - refer to 27-50-00 501.
27-10 Roll
27-10 1) Visually inspect the visible portions of L.H. aileron rods. 500 X
27-10 2) Visually inspect the roll control linkage in 500 X
L.H. wing, inspect bellcranks, attaching
hardware, check play, look for wear,
interference and corrosion - refer
to 27-10-00 201.
27-10 3) Visually inspect the visible portions of R.H. aileron rods. 600 X
27-10 4) Visually inspect the roll control linkage in 600 X
R.H. wing, inspect bellcranks, attaching
hardware, check play, look for wear,
interference and corrosion - refer
to 27-10-00 201.
27-20 Rudder
27-20 1) Visually inspect the rudder and trim tab input rods in the rear fuselage. 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 213
JUN 01
ATA OPERATIONS Area INSPECTIONS
1st
25 hrs 50
hrs 100
hrs Major Ann. Other
27-20 2) Visually inspect the adjustable end of the rudder control (on control surface side). 200 X X
27-20 3) Visually inspect the nose landing
gear/rudder interconnection rods on rudder pedals, check cabin sealing bellows,
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