Document ID: chunk:federal_register_of_legislation:F2006B06131:body:0
Version: federal_register_of_legislation:F2006B06131
Segment Type: other
Provision Reference: 
Character Range: 0–562

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

 Pilatus Porter PC-6 Series Aeroplanes

 AD/PC-6/28
 Amdt 1

 Wing Strut Attachment - Inspection 12/80

 Applicability: All models with S/Nos. 338 to 701. Document:  Pilatus SB No. 93.
 Compliance: At intervals not exceeding 100 hours time in service.

            Background:  Service experience indicates that the inspection for corrosion in the wing strut attachment can be extended to 100 hourly intervals.