Document ID: chunk:federal_register_of_legislation:F2006B06287:body:0
Version: federal_register_of_legislation:F2006B06287
Segment Type: other
Provision Reference: 
Character Range: 0–1399

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Propellers - Variable Pitch - McCauley

 AD/PMC/32
 Amdt 1

 Threadless Propeller Hub - Inspection 8/78

            Applicability: D2AF34C305 propellers fitted to the rear engine of Cessna model T337G, T337H and P337H aircraft, which have not been modified in accordance with McCauley SB No. 132.

 Document: McCauley SB No. 128.

            Compliance: For Para. 1.1 - At each daily or overnight inspection, conduct a visual inspection of the hub in accordance with Part 1 of the document.

            For Para. 11.1 - Within 100 hours time in service, after 24 June 1977 and thereafter at periods not exceeding 100 hours time in service, inspect the hub in accordance with Part 11B of the document.

            2. At any time the propeller is removed from the engine, inspect the hub in accordance with Part 11C of the document.

            Note: The inspection detailed in Part 1 of the document shall be entered on the maintenance release as maintenance required. The inspection may be performed by the pilot in command, in which case certification is not required. In all other cases certification may be made on the maintenance release. This inspection may also be performed and certified by any Licensed Aircraft maintenance Engineer.