AD/CESSNA 210/36 - Windshield And Windows - Fatigue Life Limitation

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

Legislation au F2006B08084 Not 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 210 Series Aeroplanes

 

AD/CESSNA 210/36 Windshield And Windows - Fatigue

Life Limitation


5/79

 

Applicability: All P210 series aircraft.

 

Requirement: 1. Retire the windshield from service.

 

2. Retire the cabin windows from service.

 

Compliance: For Para. 1 - Upon or prior to the accumulation of 19400 pressurised flights. For Para. 2 - Upon or prior to the accumulation of 12000 pressurised flights.

Background: Windshield and window fatigue life limitations are based on fatigue test data provided by the manufacturer.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.