FAA-PMA

CD21412 is an FAA-PMA part by Hartzell Engine Technologies LLC

PMA PQ1383CE. Approved as a replacement for 6310040081, K271-38SSL on Beechcraft Corporation D18S, S/N A-38 thru A-1019, 56TC, A56TC S/N TG-1 thru TG-94, 58, S/N TH-1 thru TH-436, 58A, 58P, 60, A60, B60, 76, 95, B95, B95A, D95A, E95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A) Bell Helicopter Textron Canada Limited (206A, 206A-1, 206B, 206B-1, 206L) B-N Group Ltd. (BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T) RUAG Aerospace Services GmbH (Dornier) (Do 28 A-1, Do 28 B-1, Do 28 D, Do 28 D-1) Fuji Heavy Industries, Ltd. (700, 710) M7 Aerospace LLC (Fairchild) (SA-26-AT) Piaggio & C. (P.136-L, P.136-L1, P.136-L2) Piper Aircraft, Inc. (PA-23, PA-23-160, PA-23-235, PA-23-250, PA-30, PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31P-350, PA-31T1, PA-31T2, PA-31T3, PA-34-200, PA-34-200T, PA-34-220T, PA-39, PA-40, PA-44-180, PA-44-180T) Textron Aviation Inc. (Cessna) (T303, 310, S/N 310-35547 and up, 310B, 310C, 310D, 310E, 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 335, 336, 337, 337A, 337B, M337B, T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, T P337H, 337H, T337H-SP, 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411, S/N 411-0001 thru 411-0250, 411A, 414, 414A, 421, 421A, 421B, 421C) Vulcanair S.p.A. (Partenavia) (P.68, P.68B, P.68C, P.68C-TC, P.68 OBSERVER, P.68TC OBSERVER, P.68 OBSERVER 2 (Bearing) · Current, Jun 2016.

A PMA part is approved for the specific eligibility listed on its FAA record; whether it may be installed on a particular aircraft, engine or component is the installer's determination. This page states the FAA record and the listings on PartsAndPlanes.