AD/CESSNA 337/16 - Alternator Cable Protection - Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08235 Not 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 337 Series Aeroplanes

 

AD/CESSNA 337/16 Alternator Cable Protection - Modification 8/74

Applicability: All models with S/Nos. 337-0756 to 337-01550.

 

Requirement: Install a circuit protective device (i.e. fuse or circuit breaker in the rear alternator output supply cable as close as practical to the battery relay connection.

 

Note: Air Navigation Order 108.32, Appendix 3, Table 6, provides a suitable cable and circuit protector co-ordination chart.

 

Compliance: Within 200 hours time in service after 31 January 1975.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.