Document ID: chunk:federal_register_of_legislation:F2006B10998:body:0
Version: federal_register_of_legislation:F2006B10998
Segment Type: other
Provision Reference: 
Character Range: 0–542

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Pratt and Whitney Turbine Engines - JT8D Series

AD/JT8D/8 Second Stage Fan Blade Pin Rivets 7/76

            Applicability: All JT8D-9, -11, -15 and -17 engines containing second stage fan blade pin P/N 520456, rivet P/N 520457 and bushing P/N 520458.

 Document: 1. FAA AD 76-12-06 : Amendment 39-2639; or

            2. AD/PW-T/36.

 Compliance: As detailed in the Requirement Document.