AD/SWSA226/34 - Fuselage Skin and Aft Belly Fairing - Inspection

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

Legislation au F2006B07174 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

 


Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 

AD/SWSA226/34 Fuselage Skin and Aft Belly Fairing - Inspection

Applicability: All model SA226T with S/Nos. T201 to T275 and T277 to T291; All model


9/81

SA226AT with S/Nos. AT001 to AT074; All model SA226TC with S/Nos. TC201 to TC407.

 

Document: 1. Swearingen SB No. 53-006, and

 

2. FAA AD 81-15-01 refers.

 

Compliance: Unless already accomplished, within 250 hours time in service after 30 September 1981.

 

Background: Chafing may occur on the lower fuselage skin due to contact between the aft belly fairing stringers and the fuselage.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.