STC SE124SO

SE124SO TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part * the Federal Aviation Regulations E-275 Lycoming GO-480-C1B6, -G1B6, -G1D6 Installation of two (2) Roto-Master Turbochargers Models 3DT5FF10J2, P/N 600572-00 (formerly Rajay Model 315F10, P/N RJ0080-102), in accordance with FAA sealed Roto-Master (formerly Rajay) - Drawing List R00408, Revision A, dated May 24, 1983, or later FAA - approved Revision.

(See continuation sheet 3 of 3) January 7, 1965 1/14/69, 2/10/82, 10/30/87, 9/22/95, 1/16/04, 6/26/06, 3/16/07, 3/12/18, 2/2/2021; 8/31/2023 March 19, 1965 July 13, 1966, July 15, 1983 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SE124SO 3

SE124SO Date of Issuance: March 19, 1965 Date Amended: July 15, 1983 Date of Reissuance: August 31, 2023

*CAR 13 effective June 15, 1956 as amended by 13-1.

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

This approval covers engine-turbocharger compatibility only. For power limitations with this installation refer to Roto-Master Drawing R00408. The approval of this change in type design applied basically to GO-480-C1B6, G1B6, G1D6, engines only. This determination should include consideration of significant weight distribution such as an increase in the fixed disposable weight in the fuselage.

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