Document ID: chunk:federal_register_of_legislation:F2006B05944:body:0:p2
Version: federal_register_of_legislation:F2006B05944
Segment Type: other
Provision Reference: 
Character Range: 5173–5931

that of other directives. There are some differences between some of the lives shown above and the corresponding lives shown in SB 744 and the FAA AD, however all Australian lives derive directly from the fatigue test program.

            This amendment is issued to clarify that for spar assemblies P/N 97701, only the upper and lower spar caps need be retired.
            Amendment 2 of this Airworthiness Directive became effective on 1 September 1982. The original issue of this Airworthiness Directive became effective on
            29 November 1974.

 Bernard Malcolm Hole
 Delegate of the Civil Aviation Safety Authority 31 May 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 14 June 2000.

 AL 7/2000