AD/HU 269/104 - Rudder Pedal Bulkhead Gusset

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Legislation au F2006B10580 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 269/104 Rudder Pedal Bulkhead Gusset 12/94

Applicability: Models 269A, A-1, B, and C.

 

Requirement: Action in accordance with Schweizer SB B-247.

 

Note: FAA AD 94-16-04 refers.

 

Compliance: Within 100 hours time in service after 10 November 1994.

 

Background: Tail rotor pedal gussets were not installed on 269A aircraft, and other aircraft have been found with the gussets cracked or with loose or missing rivets.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.