STC SE135SO

SE135SO TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part * the Federal Aviation Regulations E-275 Lycoming GO-480-D1A Installation of two (2) Rajay turbochargers Model 315A10.

(See continuation sheet 3 of 3) October 13, 1964 7/15/66, 1/14/69, 10/23/87, 12/24/03, 6/16/05, 6/26/06, 3/16/07, 3/12/18, 2/2/2021; 8/31/2023 June 9, 1965 11/1/65, 2/17/67, 7/30/68, 2/20/69, 2/10/82, 2/14/85 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SE135SO 3

SE135SO Date of Issuance: June 9, 1965 Date Amended: February 14, 1985 Date of Reissuance: August 31, 2023

*CAR 13 effective 3.5.52 and amendments 13-1 and 13-2.

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 FAA approved Riley Drawing R00523. The approval of the change in type design applied basically to GO-480-D1A 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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