Document ID: chunk:federal_register_of_legislation:F2006B10576:body:0
Version: federal_register_of_legislation:F2006B10576
Segment Type: other
Provision Reference: 
Character Range: 0–1053

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.