AD/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
View image in the official source 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.
- 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.