Document ID: chunk:federal_register_of_legislation:F2008L04421:body:0:p2
Version: federal_register_of_legislation:F2008L04421
Segment Type: other
Provision Reference: 
Character Range: 2962–3610

with the CASA-approved reinforcement, repeat replacement of the fin forward spar attachment plate was extended to 5000 hours reflecting similarity with SB 710.

             Amendment 6 cancels requirement 2(b) based on a once-only inspection in Piper SB No. 628A and USA AD 78-26-06 which were only applicable to aircraft with serial numbers through to 38-78A0749.  At requirement 2 (c), amendment 6 gives credit for fuselage bulkhead assembly P/N 77553-06 to match USA AD 82-27-08 (a)(2).  Amendment 6 also changes the reference from USA AD 81-04-07 to 82-27-08.

David Villiers
Delegate of the Civil Aviation Safety Authority

6 November 2008