AD/CESSNA 210/44 - Flying Control System Turnbuckles - Inspection
1AD/CESSNA 210/44 - Flying Control System Turnbuckles - 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 210/44 Flying Control System Turnbuckles - Inspection
Applicability: All models 210 and P210 with S/nos. 21061697 to 21063605, P2100001 to P2100362.
Document: Cessna SIL No. SE 80-16.
Compliance: Within 100 hours time in service after 30 April 1980.
4/80
Background: Some of the AN 155 brass turnbuckles in the control system may have longitudinal cracks radiating from the ends of the turnbuckle.