Document ID: chunk:federal_register_of_legislation:F2006B07422:body:0
Version: federal_register_of_legislation:F2006B07422
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 AlliedSignal (Garrett/AiResearch) Turbine Engines - TPE 331 Series

 AD/TPE 331/14
 Amdt 1

 Fuel Control Drive - Inspection and Replacement 5/96

 Applicability: TPE-331-25AA, -25DA, 25FA. TPE-331-43A, -47A, -55A, -61A, -25AB, -25DB, -
            43BL, -55B unless incorporating SB TPE-331-73-0056 and SB TPE-331-72-0123. TPE-331-1-100F, -101B, E, F, J, L, Z. TPE-331-1-151A, G, and K. TPE-331-2- 201A and C. TPE-331-2UA-203D,TPE-331-5-251M, TPE-331-6-252M, -252B, TPE-331-5-251C, K. TPE-331-6-251M, TPE-331-3U-303G, N, V & TPE-331-3U- 304G. TPE-331-5-252M, TPE-331-5-252K, unless incorporating SB TPE-331-73-
            0051 or TPE-331-73-0054 and SB TPE/TSE 331-72-0104.

            Requirement: Inspect and lubricate the fuel pump drive shaft splines in accordance with Garrett (AiResearch) SB No. TPE/TSE 331-72-0027, Rev. 9.

            Note 1. FAA AD 73-26-07 R3 also refers. Note 2. This AD supersedes AD/AIR-T/17E.
            Note 3. Compliance with AD/AIR-T/17E meets the intent of this AD.

 Compliance: As detailed in the requirement document.

            This amendment becomes effective on 25 April 1996.

            Background: Wear has been observed in the fuel pump drive shaft splines. This Directive mandates a periodic inspection of the splines area.

            This amendment includes an additional engine model, the TPE331-3U-304G to the applicability listing.