AD/PA-23/51 Amdt 1 - Landing Gear Selector Lever - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B05478 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.