AD/CESSNA 210/58 Amdt 1 - Turbocharger Oil Reservoir Outlet Fitting
1AD/CESSNA 210/58 Amdt 1 - Turbocharger Oil Reservoir Outlet Fitting
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Cessna 210 Series Aeroplanes
AD/CESSNA 210/58
Amdt 1
Turbocharger Oil Reservoir Outlet Fitting 8/85
Applicability: All model P210N, P210R and T210R with S/Nos P21000001 to P21000855, 21064898 to 21064929.
Requirement: Action in accordance with Cessna Service Bulletin SEB 85-11 or FAA AD 85-11-07. Compliance: 1. Before further flight after 13 June 1985.
- Where no cracks are found after initial inspection, repeat inspection every 25 hours time in service until modified in accordance with Requirement Document.
Note: Compliance with the previous issue of this Directive constitutes compliance with this issue.
Background: This Directive has been amended to include Cessna SB SEB 85-11 as a Requirement Document.
Turbocharger oil reservoir outlet fitting may crack, resulting in rapid loss of engine oil.