Aircraft STC directory

Cessna Aircraft M337B STCs

The Jun 30, 2026 FAA DRS snapshot contains 14 selected supplemental type certificates with status Current whose public applicability data names the Cessna Aircraft M337B. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.

listed Current at snapshot

holder directories

modification categories

Jul 21, 2011

latest recorded revision

Modification demand surface

Fuel systems4 Other aircraft modifications3 Aircraft structures3 Engine and powerplant2 Avionics1 Propellers1

Recorded holders

Aviation Enterprises6 Icarus Avionics, LLC1 AirScan Inc1 P2 Incorporated1 MT-Propeller USA Inc.1 Garmin AT Inc.1 Micro AeroDynamics Inc1 Flint Aero Inc1

Recently revised M337B STCs

Showing the 14 most recently revised records. Each entry links to the FAA source and separates public approval data from private commercial claims.

SA00243BO (3 OF 5)AvionicsRevised Jul 21, 2011

Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).

FAA holder: Icarus Avionics, LLC

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SA02094SEOther aircraft modificationsRevised Jan 31, 2011

Installation of a CO Guardian 452R Carbon Monoxide Detector per AeroMech, Inc., Master Data List document AM0243-DL02-00, Revision A, dated December 8, 2010, or latest FAA-approved revision.

FAA holder: AirScan Inc

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SA02110CH (PAGE 2)Other aircraft modificationsRevised Jan 11, 2010

Installation of a Time Trac Data Recorder.

FAA holder: P2 Incorporated

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SA02460ATPropellersRevised May 16, 2006

Replace propellers with MT-Propeller Company model MTV-12 propellers per Coastal Planes installation manual. No intermixing of propellers is allowed.

FAA holder: MT-Propeller USA Inc.

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SA03100ATFuel systemsRevised Jun 15, 2005

Installation of Wing Auxiliary Fuel Tanks.

FAA holder: Aviation Enterprises

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SA02307ATAircraft structuresRevised Dec 28, 2004

Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, or later FAA approved revisions.

FAA holder: Aviation Enterprises

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SA02308ATFuel systemsRevised Dec 28, 2004

Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions.

FAA holder: Aviation Enterprises

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SA02217AK (3 OF 5Other aircraft modificationsRevised Nov 30, 2004

Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.

FAA holder: Garmin AT Inc.

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ST01548LAEngine and powerplantRevised Aug 16, 2004

Installation of external landing gear position verification mirrors and aft engine cowl observation mirrors.

FAA holder: Wheeler Don E. dba Legal Mirrors

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SA02686ATEngine and powerplantRevised Jul 21, 2003

Installation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions, dated June 15, 2003, or later FAA approved revision.

FAA holder: Aviation Enterprises

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SA02055ATFuel systemsRevised Jul 3, 2003

Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.

FAA holder: Aviation Enterprises

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SA01215SEAircraft structuresRevised May 13, 2003

Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.

FAA holder: Micro AeroDynamics Inc

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SA5090NMFuel systemsRevised Feb 25, 2000

Installation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip.

FAA holder: Flint Aero Inc

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SA02056ATAircraft structuresRevised Jan 14, 2000

Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.

FAA holder: Aviation Enterprises

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