1AD/CESSNA 210/36 - Windshield And Windows - Fatigue Life Limitation

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

Image unavailable in extracted text 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.