AD/PA-28/38 - Stabilator Hinge Attaching Bolts - Inspection (Cth)
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-28 Series Aeroplanes
AD/PA-28/38 Stabilator Hinge Attaching Bolts - Inspection 6/78
Applicability: All models referenced in requirement documents. Document: 1. Piper SL No. 614; or
2. FAA AD 72-14-7.
Compliance: Within 100 hours time in service after 31 August 1972.