AD/PA-23/51 Amdt 1 - Landing Gear Selector Lever - Inspection
1AD/PA-23/51 Amdt 1 - Landing Gear Selector Lever - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-23 (Apache and Aztec) Series Aeroplanes
AD/PA-23/51
Amdt 1
Landing Gear Selector Lever - Inspection 3/79
Applicability: All models PA-23, PA-23-235 and PA-23-250 unless fitted with landing gear selector lever P/N 761-213.
Requirement: Inspect landing gear lever P/N 752-303 for cracks in the vicinity of the two right- angle bends. Where adhesive tape has been used to secure the warning light wires to the lever, the tape shall not be replaced over the area between the bends.
Note: Piper SB No. 635 refers to this subject.
Compliance: At intervals not exceeding 100 hours time in service.