1AD/PA-28/9 - Battery Lead Attachment - Inspection and 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 Piper PA-28 Series Aeroplanes

 

AD/PA-28/9 Battery Lead Attachment - Inspection

and Modification

12/66

 

Applicability: All models with the battery mounted aft of the luggage locker and the main electrical power supply cable routed above the stabilator control cables.

 

Requirement: 1. Inspect the installation of the main electrical power supply cable and verify that it is not in danger of being chafed by the stabilator cables.

 

2. Install an additional “P” clip P/N AS755-8-2-6 midway between the existing two PVC “P” clips approximately 1 1/2 inches on the port side of the stabilator cable.

 

Compliance: 30 December 1966.