AD/PA-22/13 Amdt 1 - Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection

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Legislation au F2006B05417 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-22 (Tri-Pacer and Colt) Series Aeroplanes

 

AD/PA-22/13

Amdt 1


Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection


5/69

 

Applicability: All models not incorporating SL 362. Document:  1. Piper SB No. 174; or

2. FAA AD 61-6-6.

 

Compliance: At intervals not exceeding 100 hours time in service or 6 months whichever occurs first.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.