AD/AA-1/16 - Structural and Control Surface Bondlines - Inspection
1AD/AA-1/16 - Structural and Control Surface Bondlines - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Gulfstream (Grumman American/ American Aviation) AA-1 Series Aeroplanes
AD/AA-1/16 Structural and Control Surface Bondlines - Inspection
9/76
Applicability: All models AA1 and AA1A with S/Nos. 0001 and subsequent and all model AA1B with S/Nos. 0001 to 0641.
Document: 1. Grumman American SB No. 155; or 2. FAA AD 76-17-03.
Compliance: Within 25 hours’ time in service after 21 September 1976 and there- after at intervals not exceeding 100 hours’ time in service until modified in accordance with SB No.