AD/CESSNA 210/43 Amdt 1 - Alternator Ground Strap - Installation
1AD/CESSNA 210/43 Amdt 1 - Alternator Ground Strap - Installation
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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 210/43
Amdt 1
Alternator Ground Strap - Installation 9/82
Applicability: All model 210/P210/T210 with S/Nos. 21058783 to 21062666 except 21062650 and 21062662, P21000001 to P21000026, T210-0001 to T210-0454.
Document: 1. Cessna SIL SE79-59; or
- FAA AD 79-25-07.
Compliance: 1. Within 100 hours time in service after 31 March 1982.
- Each time an engine is installed in an aircraft following initial compliance.
Background: Compliance has been amended by item 2 due to reports from industry that ground straps are being omitted from refitment on engine reinstallations.