Document ID: chunk:federal_register_of_legislation:F2006B10580:body:0
Version: federal_register_of_legislation:F2006B10580
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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.