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