STC SA153SO

SA153SO TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 3 the Civil Air Regulations 3A16 Beech 95, B95, B95A, D95A and E95 Installation of Turbocharged Lycoming O-360-A1A, IO-360-B1A, or IO-360-B1B engines in accordance with Riley Turbo 600 installation drawing, dated August 30, 1965 and FAA Sealed Roto-Master (formerly Riley/Rajay) Drawing List No. R0015 Rev. H, dated January 4, 1985, or later FAA Approved sealed revision.

(See continuation sheet 3 of 4) July 28, 1965 July 15, 1968; January 14, 1969; February 10, 1982; October 30, 1987;

September 22. 1995; January 16, 2004; July 3, 2006; March 16, 2007; March 5, 2018; February 2, 2021;

August 31, 2023 September 9, 1965 November 8, 1965; December 13, 1965; January 12, 1967;

September 17, 1968; February 28, 1969; February 14, 1985 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SA153SO 4

SA153SO Date of Issuance: September 9, 1965 Date Amended: February 14, 1985 Date of Reissuance: August 31, 2023

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. See attached STC SA153SO Addendum which is a portion of this Supplemental Type Certificate.

Supplemental Type Certificate Addendum No. SA153SO

The conditions and limitations of Type Certificate Data Sheet No. 3A16 apply except where superseded by the following:

This data sheet, which is part of Supplemental Type Certificate No. SA153SO, prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Models 95, B95, B95A, D95A, E95 (Normal Category) As Modified By STC No.

SA153SO

Engines: Lycoming O-360-A1A (Models 95 and B95), IO-360-B1A (Models 95 and B95 and B95A) and IO-360-B1B (Models B95A, D95A and E95) modified to incorporate turbochargers. Turbochargers must be incorporated on O-360-A1A and O-360-B1A engines in accordance with Supplemental Type Certificate No. SE154SO and on IO-360-B1A or IO-360-B1B in accordance with STC No.

SE32WE. Refer to applicable FAA Approved Roto-Master (Rajay) airplane flight manual Supplement for engine limits.

SA153SO Date of Issuance: September 9, 1965 Date Amended: February 14, 1985 Date of Reissuance: August 31, 2023

The following FAA Approved Roto-Master (formerly Riley/Rajay) Airplane Flight Manual Supplements are required:

1. Models 95 and B95 with O-360-A1A engines -- supplement dated July 27, 1966 and revised February 14, 1985.

2. Model 95, B95, B95A, D95A, and E95 with IO-360-B1A or -B1B engines -- supplement, dated January 12, 1967, revised September 17, 1968, and revised February 14, 1985.

Limitation of The approval of this change in type design applies to the Applicability Basic Beech 95 series aircraft noted above.

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