Document ID: chunk:federal_register_of_legislation:F2006B06293:body:0
Version: federal_register_of_legislation:F2006B06293
Segment Type: other
Provision Reference: 
Character Range: 0–1469

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

 Propellers - Variable Pitch - McCauley

 AD/PMC/38
 Amdt 1

 Blade and Ferrule - Inspection 3/86

            Applicability: Hub and blade models 2A34C66/90AT-2 with hub serial numbers in the range of 777425 through 7910103; E2A34C73/90 AT-8 with serial numbers 735111 and 774297 through 796442 and 2A36C23/84B-0 with serial numbers 778768 and 7710176 through 7910666 that have accumulated 400 hours time in service or more and have not been reconditioned since new.

            Note: For qualification of the actual affected serial numbers refer to Table 1 of SB. 151A.

 Document: McCauley Service Bulletin 151A.

            Compliance: Unless already accomplished prior to issue of the next maintenance release after 31 March 1986.

            Background:  The manufacturer advises the need to carry out a one time inspection of the blade retention threads for scratches caused by a sharp edge on the hub thread. Affected propellers may be installed on but not limited to Cessna 180, 180A through 180J, 188, 188A, 188B, P206, P206A thru P206E, 210E thru 210L. This AD is revised to include certain 2A36C23 propellers installed on but not limited to the following Beech Aircraft; 35-33, -A33, -B33, -C33, -C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36.