Document ID: chunk:federal_register_of_legislation:F2006B08351:body:0
Version: federal_register_of_legislation:F2006B08351
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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.