AD/CESSNA 150/39 - Rudder Pedal Torque Tube

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

Legislation au F2006B04937 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 150, F150, 152 & F152 Series Aeroplanes

 

AD/CESSNA 150/39 Rudder Pedal Torque Tube 4/84

Applicability: All models listed in Cessna Service Information Letter SE83-31 which have not been modified in accordance with that document.

 

Requirement: Visually inspect the rudder pedal torque tubes for cracking in the vicinity of the welded joints between the torque tube and the pedal arm spigots.

 

Compliance: Prior to issue of the next Maintenance Release after 30 April 1984, and thereafter at each issue of a new Maintenance Release.

 

Background: Several failures of rudder pedal torque tubes have occurred in Cessna 150 series aircraft causing loss of rudder and braking control.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.