Document ID: chunk:federal_register_of_legislation:F2006B05875:body:0
Version: federal_register_of_legislation:F2006B05875
Segment Type: other
Provision Reference: 
Character Range: 0–1140

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

 Piper PA-32 (Cherokee Six) Series Aeroplanes

 AD/PA-32/8
 Amdt 1

 Engine Air Inlet Duct - Inspection 12/67

            Applicability: Model PA32-300 with S/Nos. 32-15, 32-40000 to 32-40399 which have not been modified in accordance with Piper SB No. 260.

             Requirement:  1. Inspect the flexible duct Piper P/N 457599 between the engine air box and engine throttle body assembly for loose and/or collapsed wire reinforcing coils inside the duct. Each end of the reinforcing wire must be secured under th duct end clamps.

             2. If loose and/or collapsed wire reinforcing coils are found, remove the duct from service and install a modified duct in accordance with Piper SB No. 260.

            Note: Inspection may be accomplished by removal of the entire engine cowling and the intake air hose cover P/No. 68047.

            Compliance: Within 10 hours time in service after 8 November 1967 and there- after at intervals not exceeding 50 hours time in service.