AD/CESSNA 210/46 - Turbocharger - Inspection
1AD/CESSNA 210/46 - Turbocharger - Inspection
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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 210/46 Turbocharger - Inspection 6/80
Applicability: Model T210 S/Nos. T210-0001 thru T210-0454. Model 210 S/Nos. 21058140, 21059200 thru 21063954.
Document: 1. Cessna SIL No. SE 80-24; or
- FAA AD 80-07-01, Amdt. 39-3719.
Compliance: Within 100 hours time in service after 30 June 1980.
Background: This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of the pressure and scavenge pumps.