AD/CESSNA 400/66 - Aileron and Elevator Control Surfaces - Modification (Cth)
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 400 Series Aeroplanes
AD/CESSNA 400/66 Aileron and Elevator Control
Surfaces - Modification
Applicability: All model 441 with S/Nos. 441-0001 to 441-0090. Document: Cessna Customer Care Owner Advisory No. PJ 79-3A.
(FAA AD 79- 09-02 Amdt. 39-3453 refers).
Compliance: Within 100 hours time in service after 30 June 1979.
6/79
Background: An inflight aileron vibration/flutter incident was caused by an accumulation of water in one of the aileron control surfaces.