AD/M20/11 - Main Landing Gear Retraction Truss - Modification

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

Legislation au F2006B11219 Not 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

 


Mooney M20 Series Aeroplanes

 

AD/M20/11 Main Landing Gear Retraction Truss - Modification 9/67

Applicability: All model M20C with S/Nos. 2807 to 3466 and Model M20E with S/Nos. 470 to 1270.

 

Document: Mooney SB M20-143.

 

Compliance: Within 100 hours time in service after 7 September 1967.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.