STC SA385WE

SA385WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 3 the Civil Air Regulations 3A10 Cessna 310, 310B, 310C, 310D, 310E, 310F, 310G Installation of turbocharged Lycoming IO-540-A1A5 engines in accordance with FAA sealed Rajay Drawing List No. RJ1000-100.

(See continuation sheet 3 of 4) September 26, 1962 January 14, 1969; February 10, 1982; October 30, 1987; September 22, 1995;

December 19, 2003; July 3, 2006; March 16, 2007; March 5, 2018; February 2, 2021; August 31, 2023 April 19, 1963 May 15, 1964 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SA385WE 4

SA385WE Date of Issuance: April 19, 1963 Date Amended: May 15, 1964 Date of Reissuance: August 31, 2023

See attached STC Addendum No. SA385WE which is a part of this certificate.

Supplemental Type Certificate Addendum No. SA385WE

The conditions and limitations of Type Certificate Data Sheet No. 3A10 and STC No.

SA212SO apply except where superseded by the following:

This data sheet, which is a part of Supplemental Type Certificate No. SA385WE, prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Supplemental T.C. Holder TALCO Aviation Corp. dba RAJAY Turbo Products 3015 E. New York St, STE A2-270 Aurora, IL 60504

I - Models 310, 310B, 310C, 310D, 310E, 310F, 310G (Normal Category) as modified by STC Nos. SA385WE and SA212SO

Engine Lycoming IO-540-A1A5 modified to incorporate turbosuperchargers in accordance with Supplemental Type Certificate No. SE6WE.

Fuel 100/130 Mm. Grade Aviation Gasoline 3 4

SA385WE Date of Issuance: April 19, 1963 Date Amended: May 15, 1964 Date of Reissuance: August 31, 2023

Engine Limits Unsupercharged - same as original - 310 Series with SA212SO incorporated Supercharged - Take Off - 27.0 in. Hg at 2575 RPM (3 min.) sea level to 10,000 ft. MSL Max. Continuous - 25.0 in. Hg at 2400 RPM sea level to 25,000 ft. MSL

FAA Approved Riley Turbo Rocket Airplane Flight Manual, dated August 13, 1963, is required with this installation.

Limitation of Applicability: This approval of change in type design applies to Cessna 310 series aircraft that have been previously modified to the Riley Rocket" configuration in accordance with STC SA212SO only. 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.

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