AD/SWSA226/37 - Fuselage, Lower L.H. Cargo Area Belt Frames - Inspection and Modification

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

Legislation au F2006B07177 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

 


Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 

AD/SWSA226/37 Fuselage, Lower L.H. Cargo Area Belt

Frames - Inspection and Modification


10/81

 

Applicability: All model SA226-AT with S/Nos. AT-001 to AT-074. All model SA226-TC with S/Nos. TC-201 to TC-419.

 

Document: Fairchild Swearingen SB No. 53-007. Compliance: As per Requirement Document.

Background: Cracks may develop in the lower left belt frames at the cargo door latch receptacles.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.