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 269/64
Amdt 1
Tail Rotor Assembly - Component Replacement, Inspection and Revised Assembly Procedures
10/83
Applicability: All models referred to in Hughes SIN No. N-155.2. Document: Hughes SIN N-155.2.
Compliance: Unless already accomplished within 100 hours TIS after 31st October, 1983.
Background: This directive is raised in issue to reflect increased model and component applicability as referred to in revised requirement document.