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.

listed Current at snapshot

aircraft directories

modification categories

Jun 23, 2021

latest recorded revision

Recently revised records

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

19 displayed records.

Search every indexed record for this holder. The table below contains the recently revised records shown on this page.

Mike Jones Aircraft Sales Inc. supplemental type certificates, aircraft applicability, source status and dates
STC and modification	Aircraft / model / TC	Source status and dates	Holder and authority
SA1151SO Installation of Hartzell four-blade Propellers, cowling changes, winglets or wingtip extension, optional governor arm adaptor, and optional engine isolator mounts. Engine and powerplant View record	Piper Aircraft PA-31-350TC A20SO	Current at cited snapshot Revised Jun 23, 2021 Application: Oct 18, 1979	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA01349AT Installation of winglets, P/N's66000-50 and 66000-51. Other aircraft modifications View record	Textron Aviation 58PTC A23CE Textron Aviation 58TC 3A16 Textron Aviation 58ATC 3A16 Textron Aviation G58TC 3A16 Textron Aviation 95-55TC 3A16 Textron Aviation 95-A55TC 3A16 Textron Aviation 95-B55TC 3A16 Textron Aviation 95-B55ATC 3A16 Textron Aviation 95-B55BTC 3A16 Textron Aviation 95-C55TC 3A16 Textron Aviation 95-C55ATC 3A16 Textron Aviation D55TC 3A16 Textron Aviation D55ATC 3A16 Textron Aviation E55TC 3A16 Textron Aviation E55ATC 3A16	Current at cited snapshot Revised Jun 22, 2012 Application: Apr 7, 1997	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA00014AT Installation of Lycoming model L/TIO-540-J2B engines in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Piper Navajo Model PA-31-350 dated October 9, 1992, or later FAA approved, revision. Other aircraft modifications View record	Piper Aircraft PA-31-350TC A20SO	Current at cited snapshot Revised Feb 10, 2011 Application: Oct 5, 1992	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA00336AT Installation of winglets. Other aircraft modifications View record	Piper Aircraft PA-31TC A20SO Piper Aircraft PA-31-325TC A20SO Piper Aircraft PA-31-350TC A20SO Piper Aircraft PA-31PTC A8EA	Current at cited snapshot Revised Feb 10, 2011 Application: Nov 1, 2011	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA00616AT Installation of McCauley Propeller Model 3AF32C504/82NEA, on Beechcraft Models 95-C55, 95-C55A, D55, D55A, E55, & E55A and McCauley Propeller Model, 3AF32C512/82NEA, on Beechcraft Models 58 & 58A, per Colemill Enterprises Installations Instructions dated November 11, 1994, or later FAA Approved Revision. Propellers View record	Hawker Beechcraft 58TC 3A16 Hawker Beechcraft 58ATC 3A16 Hawker Beechcraft 95-C55TC 3A16 Hawker Beechcraft 95-C55ATC 3A16 Hawker Beechcraft D55TC 3A16 Hawker Beechcraft D55ATC 3A16 Hawker Beechcraft E55TC 3A16 Hawker Beechcraft E55ATC 3A16	Current at cited snapshot Revised Feb 10, 2011 Application: Nov 11, 1994	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA1421SO Installation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises, Inc., Installation Instructions dated February 16, 1983, or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1, (a)2, and (a)4 of AD 82-27-13 and restores the 40 (full) flap travel. Flight controls View record	Piper Aircraft PA-31TC A20SO Piper Aircraft PA-31-300TC A20SO Piper Aircraft PA-31-325TC A20SO Piper Aircraft PA-31-350TC A20SO Piper Aircraft PA-31PTC A8EA	Current at cited snapshot Revised Feb 10, 2011 Application: Feb 16, 1983	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA1762SO 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. Other aircraft modifications View record	Raytheon Aircraft E55TC 3A16 Raytheon Aircraft D55TC 3A16 Raytheon Aircraft 95-C55TC 3A16 Raytheon Aircraft 58ATC 3A16 Raytheon Aircraft 58TC 3A16	Current at cited snapshot Revised Feb 10, 2011 Application: Jul 26, 1984	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA1835SO 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. Engine and powerplant View record	Hawker Beechcraft 35-C33ATC 3A15 Hawker Beechcraft A36TC 3A15 Hawker Beechcraft E33ATC 3A15 Hawker Beechcraft E33CTC 3A15 Hawker Beechcraft F33ATC 3A15 Hawker Beechcraft F33CTC 3A15 Hawker Beechcraft S35TC 3A15 Hawker Beechcraft V35TC 3A15 Hawker Beechcraft V35ATC 3A15 Hawker Beechcraft V35BTC 3A15	Current at cited snapshot Revised Feb 10, 2011 Application: Jan 3, 1985	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2103SO 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. Fuel systems View record	Hawker Beechcraft 58TC 3A16 Hawker Beechcraft 58ATC 3A16 Hawker Beechcraft 95-55TC 3A16 Hawker Beechcraft 95-A55TC 3A16 Hawker Beechcraft 95-B55TC 3A16 Hawker Beechcraft 95-B55ATC 3A16 Hawker Beechcraft 95-B55BTC 3A16 Hawker Beechcraft 95-C55TC 3A16 Hawker Beechcraft 95-C55ATC 3A16 Hawker Beechcraft D55TC 3A16 Hawker Beechcraft D55ATC 3A16 Hawker Beechcraft E55TC 3A16 Hawker Beechcraft E55ATC 3A16	Current at cited snapshot Revised Feb 10, 2011 Application: Feb 28, 1986	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2109SO Installation of Teledyne Continental Motors Model IO-470K engine in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna Model 305-A-C-D-F Revised April 24, 1987 and Colemill Enterprises Drawing No. 3000 Revision A dated May 6, 1987. Engine and powerplant View record	Regal Air 305ATC 5A5 Regal Air 305CTC 5A5 Regal Air 305DTC 5A5 Regal Air 305FTC 5A5	Current at cited snapshot Revised Feb 10, 2011 Application: Jul 10, 1985	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2207SO 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. Other aircraft modifications View record	Cessna Aircraft 310RTC 3A10 Cessna Aircraft T310PTC 3A10 Cessna Aircraft T310QTC 3A10 Cessna Aircraft T310RTC 3A10	Current at cited snapshot Revised Feb 10, 2011 Application: Jun 29, 1987	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2996SO Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-15 Rev. A dated July 5, 1991. Propellers View record	Cessna Aircraft 310GTC 3A10 Cessna Aircraft 310HTC 3A10 Cessna Aircraft 310ITC 3A10 Cessna Aircraft 310JTC 3A10 Cessna Aircraft 310J-1TC 3A10 Cessna Aircraft 310KTC 3A10 Cessna Aircraft 310LTC 3A10 Cessna Aircraft 310NTC 3A10 Cessna Aircraft 310PTC 3A10 Cessna Aircraft 310QTC 3A10 Cessna Aircraft 310RTC 3A10	Current at cited snapshot Revised Feb 10, 2011 Application: Feb 21, 1991	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2997SO Installation of McCauley propeller governor. Propellers View record	Hawker Beechcraft 58TC 3A16 Hawker Beechcraft 95-55TC 3A16 Hawker Beechcraft 95-A55TC 3A16 Hawker Beechcraft 95-B55TC 3A16 Hawker Beechcraft 95-C55TC 3A16 Hawker Beechcraft D55TC 3A16 Hawker Beechcraft E55TC 3A16	Current at cited snapshot Revised Feb 10, 2011 Application: Nov 1, 2011	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA2998SO Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-10 February 15, 1991. Propellers View record	Piper Aircraft PA-31TC A20SO Piper Aircraft PA-31-325TC A20SO Piper Aircraft PA-31-350TC A20SO	Current at cited snapshot Revised Feb 10, 2011 Application: Feb 21, 1991	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA366SO Gross weight increased to 6530 pounds. Aircraft performance View record	Twin Commander Aircraft 500-ATC 6A1	Current at cited snapshot Revised Feb 10, 2011 Application: Apr 27, 1966	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA412SO Installation of Continental IO-520-E or IO-550-E engines per Colemill Enterprises, Inc. Installation Instructions for modification of Cessna 310 and Drawing AC5400, as revised March 19, 1969, or later FAA approved revision of these documents. Other aircraft modifications View record	Cessna Aircraft 310GTC 3A10 Cessna Aircraft 310HTC 3A10 Cessna Aircraft 310ITC 3A10 Cessna Aircraft 310JTC 3A10 Cessna Aircraft 310KTC 3A10 Cessna Aircraft 310LTC 3A10 Cessna Aircraft 310NTC 3A10 Cessna Aircraft 310PTC 3A10 Cessna Aircraft 310QTC 3A10	Current at cited snapshot Revised Feb 10, 2011 Application: Nov 5, 1968	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA432SO 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. Other aircraft modifications View record	Hawker Beechcraft 95-55TC 3A16 Hawker Beechcraft 95-A55TC 3A16 Hawker Beechcraft 95-B55TC 3A16 Hawker Beechcraft 95-B55ATC 3A16 Hawker Beechcraft 95-B55BTC 3A16	Current at cited snapshot Revised Feb 10, 2011 Application: Feb 25, 1970	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA518SO Installation of Continental IO-520-E derated engines and McCauley D3AF32C87/82NC-6 or -8 propellers. Modification to be accomplished in accordance with Colemill Enterprises, Inc. Drawing AC5800 Rev. A and AC5801 Rev A and Installation Instructions dated 7 July 1972 and revised 21 August 1972. Owner s Manual Supplement dated 21 August 1972 included in data. Other aircraft modifications View record	Cessna Aircraft 320TC 3A25 Cessna Aircraft 320-1TC 3A25 Cessna Aircraft 320ATC 3A25 Cessna Aircraft 320BTC 3A25 Cessna Aircraft 320CTC 3A25	Current at cited snapshot Revised Feb 10, 2011 Application: Jul 7, 1972	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record
SA970SO 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. Fuel systems View record	Piper Aircraft PA-31TC A20SO Piper Aircraft PA-31-325TC A20SO	Current at cited snapshot Revised Feb 10, 2011 Application: Aug 19, 1977	FAA holder: Mike Jones Aircraft Sales Inc. FAA authority record

Mike Jones Aircraft Sales Inc. STCs

Modification mix

Aircraft represented

Recently revised records

Installation of Hartzell four-blade Propellers, cowling changes, winglets or wingtip extension, optional governor arm adaptor, and optional engine isolator mounts.

Installation of winglets, P/N's66000-50 and 66000-51.

Installation of Lycoming model L/TIO-540-J2B engines in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Piper Navajo Model PA-31-350 dated October 9, 1992, or later FAA approved, revision.

Installation of winglets.

Installation of Teledyne Continental Motors Model IO-470K engine in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna Model 305-A-C-D-F Revised April 24, 1987 and Colemill Enterprises Drawing No. 3000 Revision A dated May 6, 1987.

Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-15 Rev. A dated July 5, 1991.

Installation of McCauley propeller governor.

Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-10 February 15, 1991.

Gross weight increased to 6530 pounds.

Installation of Continental IO-520-E or IO-550-E engines per Colemill Enterprises, Inc. Installation Instructions for modification of Cessna 310 and Drawing AC5400, as revised March 19, 1969, or later FAA approved revision of these documents.

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.