AD/PA-38/3 Amdt 1 - Vertical Fin/Rudder Leading Edge - Inspection and Modification

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

Legislation au F2006B05968 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-38 (Tomahawk) Series Aeroplanes

 

AD/PA-38/3

Amdt 1


Vertical Fin/Rudder Leading Edge - Inspection and Modification


1/79

 

Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0215 and 38-78A0217 to 38-78A0226.

 

Document: 1. Piper SB No. 607A, Parts I and II; or

 

2. FAA AD 78-22-01, Amdt. 39-3323.

 

Compliance: 1. Inspect at intervals not exceeding 25 hours time in service; and

 

2. Modify within 50 hours time in service after 20 November 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.