AD/CESSNA 210/43 Amdt 1 - Alternator Ground Strap - Installation

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Legislation au F2006B08092 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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

 

2. FAA AD 79-25-07.

 

Compliance: 1. Within 100 hours time in service after 31 March 1982.

 

2. 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.