AD/PA-28/84 - Nose Landing Gear - Inspection and Modification Parts I and II

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

Legislation au F2006B05638 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-28 Series Aeroplanes

 

AD/PA-28/84 Nose Landing Gear - Inspection and Modification Parts I and II


5/82

 

Applicability:

PART I -

All models PA-28R-201T Turbo Arrow III S/Nos. 28R-7703001 to 28R- 7803373 and PA-28RT-201T Turbo Arrow IV S/Nos. 28R-7931001 to

28R- 8131193.

 

PART II -

All models PA-28R-200 Arrow II S/Nos. 28R-7635522 to 28R-7635545. All models PA-28R-201 Arrow III S/Nos. 28R-7737001 to 28R-7837317.

All models PA-28RT-201 Arrow IV S/Nos. 28R-7918001 to 28R- 8118082.

 

Document: Piper SB No. 724 Parts I and II.

 

Note: FAA AD 82-06-011 refers.

 

Compliance: Within 100 hours time in service after 31 May 1982.

 

Background: There have been incidents involving inadvertent retraction of the nose landing gear. These incidents were caused by failures of various components of the nose landing gear retraction/extension system including the down lock, link and brace assemblies, actuator housings and attachment brackets.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.