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FAA-listed STC holder

Mike Jones Aircraft Sales Inc. STCs

The Jun 30, 2026 FAA DRS snapshot lists 19 selected supplemental type certificates with status Current under Mike Jones Aircraft Sales Inc.. The records span 72 public aircraft directories and 6 modification categories. This is a research directory, not a claim that any specific kit or service is currently offered.

19
listed Current at snapshot
72
aircraft directories
6
modification categories
Jun 23, 2021
latest recorded revision

Modification mix

Other aircraft modifications8
Propellers4
Engine and powerplant3
Fuel systems2
Flight controls1
Aircraft performance1

Aircraft represented

Cessna Aircraft T310Q73 STCsCessna Aircraft 310I72 STCsCessna Aircraft 310Q72 STCsCessna Aircraft T310P71 STCsCessna Aircraft 310J71 STCsHawker Beechcraft A3669 STCsCessna Aircraft 310G68 STCsCessna Aircraft 310R67 STCsCessna Aircraft T310R67 STCsCessna Aircraft 310H67 STCsCessna Aircraft 310K67 STCsCessna Aircraft 310P67 STCsCessna Aircraft 310L65 STCsCessna Aircraft 310N64 STCsHawker Beechcraft F33A60 STCsPiper Aircraft PA-31-35057 STCsHawker Beechcraft V3557 STCsHawker Beechcraft V35B57 STCsHawker Beechcraft 35-C33A56 STCsHawker Beechcraft S3556 STCs

Recently revised records

Showing the 19 most recently revised records. Category directories provide the complete paginated discovery path.

SA1762SOOther aircraft modifications

Install two Teledyne Continental Motors model IO-550-C engines, Hartzell or McCauley propellers, nose cowling (P/N 74000-1) per Colemill Enterprises, Inc. Dwg. No. 74000, Initial Release dated October 29, 1984, and winglets (P/N 66000-50 and -51) per Colemill Enterprises Dwg. No. 66000, Initial Release dated October 29, 1984, in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Beechcraft Models: C55, D55, E55, and 58 , dated September 14, 1984, or later FAA approved revision of this document or either drawing.

FAA holder: Mike Jones Aircraft Sales Inc.

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SA1835SOEngine and powerplant

Install Teledyne Continental Motors Model IO-550-B engine, Hartzell HC-C4YF-1E/FC7063Q propeller and Hartzell D4511P, spinner on all models per Colemill Drawing P/N 82000C. Install Teledyne Continental Motors Model IO550-B engine, McCauley 3A32C76/82NB-2 propeller and McCauley D3584 spinner on models S-35, V35A, V35B, E33A, E33C, 35-C33A, F33A, and F33C per Colemill Drawing No. 82000, Rev. D. dated 10-30-87 or later FAA approved revision. Engines installed on models S35, V35, V35A, V35B, E33A, E33C, 35-C33A, F33A, and F33C are derated to 285 horsepower per AFMS. For 36/A36 models only, stall strip P/N 82000-4, per Colemill Drawing P/N 82000C, is required.

FAA holder: Mike Jones Aircraft Sales Inc.

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SA2103SOFuel systems

Installation of auxiliary fuel wing tips and winglets in accordance with Colemill Enterprises Installations Instruction for Modification of Beechcraft Baron Model 55 and 58 Aux Fuel Tank Installation revised July 28, 1986 and Colemill Enterprises Drawing No. 7800 Rev. A dated July 28, 1986. Colemill Enterprises Airplane Flight Manual Supplement dated April 28, 1987, is required with this installation.

FAA holder: Mike Jones Aircraft Sales Inc.

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SA2207SOOther aircraft modifications

Installation of two Teledyne Continental Motors Model IO-550-A engines in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna model 310R in Accordance with Colemill Enterprises, Inc. Drawing AC6200 dated June 15, 1987, or later FAA approved revision. Colemill Enterprises Pilot s Operating Handbook and FAA Approved Flight Manual Supplement dated November 20, 1987, or Pilot s Operating Handbook and Airplane Flight Manual Supplement dated February 18, 2000 or later FAA approved revision is required for S/N 310R1501 and subsequent. Colemill Enterprises Supplemental Airplane Flight Manual Revised May, 11, 2001 or latter FAA approved revision is required for T310P S/Ns 310P0001 through 310P0240, T31Q S/Ns 310Q0001 through 310Q1160 and 310R/T 310R S/Ns 310R0001 through 310R2140.

FAA holder: Mike Jones Aircraft Sales Inc.

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SA970SOFuel systems

Installation of Lycoming TIO-540-J2BD or TIO-540-J2B engines and Hartzell propellers HC-C4YR-2/FC7663D-4R or HC-C4YR-2/FC7663D-6Q, additional fuel pump and related cowling changes.Modification Drawing Piper Navajo PA-31 Navajo-Panther-Drawing 68000, Revision D, Dated 5/17/82. Installation Instructions for Modification of Piper Navajo Model PA-31 and PA-31-325, Drawing 68000, change D dated 5/17/82 and Supplemental Type Certificate (STC) SA970SO. Installation Procedures Boost Pump PA-31 Drawing 62000 A Change dated November 30, 1977. (PA-31 Only) Piper Kit 760-905 Colemill Enterprises, Inc., Process Specification for Drawings 64000 and 66000, dated August 31, 1977. Colemill Enterprises, Inc., Process Specification #500 for Piper Wing Caps and Winglets, dated September 1, 1981. Later FAA approved revisions of the above data are acceptable.

FAA holder: Mike Jones Aircraft Sales Inc.

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