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 06 (EA) Page 225
JUN 01
ATA ANNUAL INSPECTION (AI)
STABILIZER INSPECTION (AREA 300) AREA OTHER INSPECTION
PERFORMED
BY
55-00 STABILIZER INSPECTION (AREA 300) 300
55-00 1) Perform an overall visual inspection of area 300. 300
11-00 2) Check installation and legibility of exterior placards and markings - refer to 11-20-00 1. 300 NOTE 1
55-20 3) Visually inspect the elevator hinge bearings. 300 1000 hrs or
S / N 1 - 1864, 1867 - 1869 2 years
Refer to the latest issue of SB 10-101-55.
55-20 4) Check the balancing weight and the boom for security and evidence of corrosion. 300 NOTE 1
55-40 5) Visually inspect the rudder hinges and check for loose rivets, cracks and evidence of corrosion. 300
55-40 6) Check the balancing weight for attachment, and check for evidence of corrosion ; in case of doubt, remove the vertical stabilizer tip - refer to 55-40-00 201. 300 NOTE 1
55-00 7) Visually inspect the stabilizer and trim tab hinges. 300
Perform an operational test.
55-00 8) Visually inspect (do not remove) the visible portions of both elevator and vertical stabilizer, check for loose rivets, cracks and evidence of corrosion. 300
30-10 9) Visually inspect the porous leading edges (if installed) on the stabilizers. 300 NOTE 1
27-20 10) Visually inspect the adjustable end of the rudder trim tab control (on control surface side). 300
27-30 11) Visually inspect the adjustable end of the elevator and the trim tab (on control surface side). 300
24-00 12) Visually inspect all cable connections in the vertical stabilizer. 300
Replace cables if damaged. Inspect cables for routing, clamp security, lugs and cleanliness.
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