# STC SA432SO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Mike Jones Aircraft Sales Inc., United States - Description: Installation of two Teledyne Continental Motors (TCM) model IO-520-E engines (derated to 260hp) and Hartzell model EHC-A3VF-2B/V7636D propellers and related changes in accordance with Colemill Enterprises Drawing AC5600 dated February 23, 1970, revised April 22, 1970. - Applied: February 25, 1970 - Status date: February 10, 2011 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16) - Certificate PDF: https://openairdocs.org/files/sha256/f8/8a/f88a2f377cc28b05676da9301b395322d620a150e3f7d73438b6c37b24590e4e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4885E5AC0FD1C6198625784E007CAA4F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA432SO ## ADs that name it (0) None. ## Approved models (5) - Hawker Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SAA3250 This certificate issued to: Mike Jones Aircraft Sales, Inc. 1932 Memorial Blvd Murfreesboro, TN 37129 Part 3 of the Civil Air Begulations. Original Product Type Y'erlificate Nunter: ЗА16 Make: Raytheon Model: 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B Description of Type Design Change: Installation of two Teledyne Continental Motors (TCM) model I0-520-E engines (derated to 260hp) and Hartzell model EHC- A3VF-2B/V7636D propellers and related changes in accordance with Colemill Enterprises Drawing AC5600 dated February 23, 1970, revised April 22, 1970. Drawing AC5600 revised December 15, 1981, for the installation of Hartzell EHC-G3YF-2(U) (F)/FC7663(D) (B) propellers. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. suspended revsked or a lemmination date is cherwise estattlished by the Administrater of the Federal. Aviation Administration Fate c/ apylicalion: February 25, 1970 Date Reissued: February 24, 2000; February 10, 2011 Jule of issuance: April April 1970 Date Amended: 6/21/1971; 2/23/1982; 4/9/1995; 9/14/1995, 11/10/2005 FEDERAL AVIATION By direcion of the. codministrator (Sign TOMNISTRATO Melvin D. Taylor Manager Atlanta Aircraft Certification Office (Title) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA43250 Date of Issuance: April 23, 1970 Date Amended: November 10, 2005 Description of Type Design Change: , Continued: Installation Instructions for this modification are dated April 22, 1970. The models 95-55 and 95-A55 are eligible for 5200 pound takeoff weight and 4800 pound maximum landing weight when the described modification is accomplished. When the EHC-A3VF-2B/V7636D propellers are installed on the models 95-55 and 95-A55, Colemill Enterprises Airplane Flight Manual Supplement (AFMS) dated June 21, 1971, or February 23, 1982, is a required part of this modification. When these propellers are installed on the model 95-B55, AFMS dated June 21, 1971, or February 23, 1982, is a required part of this modification. When the EHC-G3YF-2(U) (F)/FC7663(D) (B)-4T propellers are installed on the models 95-55 and 95-A55, Colemill Enterprises AFMS dated February 23, 1982 is required for this modification. When these propellers are installed on the model 95-B55, AFMS also dated February 23, 1982 is required for this modification. Drawing AC56000 was revised January 24, 1990, for the installation of TCM model 10-550-E engines (derated to 260 hp) and Hartzell model EHC-G3YF-2(U) (F)/FC7663(D) (B)-4T propellers with 3567-1P spinners on the models 95-55, 95-A55, and 95- B55. Installation instructions were also revised January 24, 1990. Colemill Enterprises AFMS dated April 9, 1990 (for the model 95-55 and 95-A55) or AFMS also dated April 9, 1990, (for the model 95-B55), is required with the 10-550-E modification. Drawing AC5600 and the Installations Instructions were both revised on August 28, 1995, for the installation of TCM model IO- 550-E engines and either Hartzell model EHC-A3VF-2B/V7636D propellers with 826-25P or 836-36P spinners or model EHC- G3YF-2(U) (F)/FC7663(D) (B)-4T propellers with 3567-1P spinners on the models 95-B55A and 95-B5SB. AFMS dated September 14, 1995, is required with this modification. Later FAA approved revisions of any of these documents are applicable. -END- ## Every issue (2) - February 10, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f8/8a/f88a2f377cc28b05676da9301b395322d620a150e3f7d73438b6c37b24590e4e) - November 10, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ae/32/ae32d4228d907da80dd674e33201f0a6bd2f6c188b6f50048b997f56af0b748a) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.