AD/PA-44/4 - Throttle Cable Installation - Modification

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

Legislation au F2006B06010 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-44 (Seminole) Series Aeroplanes

 

AD/PA-44/4 Throttle Cable Installation - Modification 5/79

Applicability: Model PA44-180 with S/Nos. 44-7995001 to 44-7995144, 44-7995146 to 44-

7995180, 44-7995182 to 44-7995186, 44-7995190, 44-7995192, 44-7995193, 44-

7995195 and 44-7995197.

 

Document: 1. Piper SB No. 639; or

 

2. FAA AD 79-05-11, Amendment 39-3433.

 

Compliance: Within 25 hours time in service after 5 April 1979.

 

Background:  There are reports of engine throttle cable breakage due to excessive spring-back induced by the present cable layout. The throttle cable support bracket is to be relocated to correct this condition.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.