AD/SD3-60/8 Amdt 2 - Elevator Torque Shaft Assembly

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

Legislation au F2006B06913 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

 


Short SD3-60 Series Aeroplanes

 

AD/SD3-60/8

Amdt 2


Elevator Torque Shaft Assembly 6/85 DM

 

Applicability:  All Models SD-360 aircraft. Requirement: 1. Shorts SB SD360-27-A06 Rev 1.

2. Shorts SB SD360-27-06.

 

Compliance: 1. Prior to 14 March 1985 and thereafter at intervals not exceeding 60 hours time in service or pre-first flight following parking in severe wind gust conditions.

 

2. Prior to 15 August 1985.

 

Background: This Directive was issued after loss of elevator control on a SD3-30 aircraft. Rev 1 extended the inspection area and introduced a repetitive inspection. Rev 2 introduces mandatory modification to reinforce the attachment of the elevator torque shaft housings.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.