AD/CESSNA 337/16 - Alternator Cable Protection - Modification
1AD/CESSNA 337/16 - Alternator Cable Protection - Modification
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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 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.