CTHIn ForceLegislation
AD/CESSNA 400/66 - Aileron and Elevator Control Surfaces - Modification
//
© 2026 Zoe. All rights reserved.
Zoe is a legal information platform. Always consult the Federal Register of Legislation for authoritative text.
AD/CESSNA 400/66 - Aileron and Elevator Control Surfaces - Modification
Start here
Turn the raw legal text into a practical explanation grounded in AD/CESSNA 400/66 - Aileron and Elevator Control Surfaces - Modification.
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Cessna 400 Series Aeroplanes
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.
Background: An inflight aileron vibration/flutter incident was caused by an accumulation of water in one of the aileron control surfaces.