AD/SWSA226/44 - Main Landing Gear Door System - Inspection

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

Legislation au F2006B07184 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/SWSA226/44 Main Landing Gear Door System - Inspection 1/83

Applicability: Models SA226-T(B), S/N T(B)276, T(B)292 thru T(B) 397. SA226-T, S/N T201 thru T275 and T277 thru T291. SA226-AT, S/N AT001 thru AT074. SA226-TC, S/N TC201 thru TC396.

 

Document: Fairchild Swearingen SB No. 32-026.

 

Note: FAA AD 82-23-06 Amendment 39-4493 refers.

 

Compliance: Unless already accomplished, within 100 hours time in service after 31 January, 1983.

 

Background: Shifting of the main landing gear doors has occurred which resulted in the landing gear locking in the up position.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.