AD/CESSNA 400/66 - Aileron and Elevator Control Surfaces - Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08351 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.