AD/PA-31/58 - Auto Pilot Servo Bridle Clamp Bolt Torque - Modification

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

Legislation au F2006B05762 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-31 Series Aeroplanes

 

AD/PA-31/58 Auto Pilot Servo Bridle Clamp Bolt Torque - Modification


9/77

 

Applicability: Model PA-31 and PA-31-325 S/Nos. 31-712 to 31-7612089. Model PA-31-350 S/Nos. 31-5001 to 31-7652146; Model PA-31P S/Nos. 31P-1 to 31P-7730005; and Model PA-31T S/Nos. 31T-1400002 to 31T-7720025.

 

Document: Piper SB No. 558.

 

Compliance: Within 100 hours time in service after 30 September 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.