AD/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
View image in the official source 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.
- 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.