AD/HU 269/100 Amdt 1 - Clutch Control Spring

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Legislation au F2006B10576 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

 


Schweizer (Hughes) 269 Series Helicopters

 

AD/HU 269/100

Amdt 1


Clutch Control Spring 5/95

 

Applicability: All model 269A, 269A-1, 269B, 269C and all TH55A helicopters. Requirement:  Action in accordance with Schweizer Mandatory Service Bulletin B-256-2.

Note: FAA AD 95-03-12 amdt 39-9148 refers and supersedes FAA Priority Letter AD 93-03-01.

 

Compliance: Unless previously inspected for wear and security in accordance with Schweizer SB B-256-1, carry out Part 1 of the Requirement Document by 28 April 1995.

Thereafter, reinspect at intervals not exceeding 100 hours time in service.

 

Background: The manufacturer has advised that due to the failure of a clutch control spring assembly on a 269C helicopter, an accident has occurred. This amendment has been raised to incorporate the requirements of the manufacturer’s SB and the later FAA AD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.