AD/SWSA226/38 Amdt 1 - Elevator Return Spring Location - Modification

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

Legislation au F2006B07178 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

 


Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 

AD/SWSA226/38

Amdt 1


Elevator Return Spring Location - Modification


1/82

 

Applicability: 1. All model SA-226-AT with S/Nos. AT-001 to AT-999. All model SA-226-TC with S/Nos. TC-201 to TC-999.

 

2. All model SA-227-AT with S/Nos. AT-423 to AT-469. All model SA-227-AC with S/Nos. AC-420 to AC-473.

 

Document: 1. Fairchild Swearingen SB No. 27-032.

 

2. Fairchild Swearingen SB No. 27-002.

 

Note: FAA AD 81-ASW-39 Amdt. 39-4238 refers.

 

Compliance: Unless already accomplished, modify before 1 March 1982.

 

Background: Relocation of the elevator return spring is necessary to prevent jamming of the elevator control in the event of inflight failure of the spring. This amendment extends applicability by aircraft models and S/Nos.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.