Document ID: chunk:federal_register_of_legislation:F2006B03056:body:0
Version: federal_register_of_legislation:F2006B03056
Segment Type: other
Provision Reference: 
Character Range: 0–1233

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 747 Series Aeroplanes

 AD/B747/154
 Amdt 1

      Nacelle Strut and Wing Structure - Rolls Royce RB211 Series Engine

 2/96

            Applicability: Model 747 series aircraft with line positions 292 through 1033, equipped with Rolls Royce RB211 series engine.

            Requirement: Action in accordance with the technical requirements of FAA AD 95-13-05 Amdt 39- 9285.

            Note: Boeing Alert Service Bulletin 747-54A2157 Revision 1 refers.

 Compliance: As specified in the Requirement Document.

            The Compliance of the initial issue of this Directive remains unchanged. This Amendment is effective from 1 February 1996.

            Background: The FAA requires the incorporation of a modification of the strut and wing structure that has been developed by the manufacturer to improve the damage tolerance capability and durability of the strut-to-wing attachments, and reduce reliance on inspections of those attachments. Amendment 1 is issued to introduce a revision of the manufacturer's service bulletin which is related to this Directive.