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Aircraft STC directory

Cessna Aircraft 210C STCs

The Jun 30, 2026 FAA DRS snapshot contains 53 selected supplemental type certificates with status Current whose public applicability data names the Cessna Aircraft 210C. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.

53
listed Current at snapshot
36
holder directories
9
modification categories
Aug 31, 2023
latest recorded revision

Modification demand surface

Other aircraft modifications19Fuel systems7Avionics6Engine and powerplant5Flight controls5Aircraft structures5Propellers3Cabin and interiors2Landing gear and brakes1

Recorded holders

Brittain Industries, Inc9Curry Aviation LLC3Hartwig Aircraft Fuel Cell Repair3BF Goodrich Aerospace2TALCO Aviation1Kaman Corporation Aircraft Wheel and Brake LLC1Power Flow Systems Inc.1Petersen Aviation Inc1P2 Incorporated1Flint Aero Inc1Glen A Florence, Aero Technologies, Inc.1Cub Crafters Inc1Teledyne Controls1Selkirk Aviation1Aerospace Welding Minneapolis Inc.1Great Lakes Aero Products Inc1Saf-Air Products Inc.1John Jewell Aircraft Inc1Shadin Avionics1Hartzell Propeller Inc1

Recently revised 210C STCs

Showing the 53 most recently revised records. Each entry links to the FAA source and separates public approval data from private commercial claims.

SA4473NMAircraft structures

Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

FAA holder: G & D Aero Products Inc.

View record
SA01192SEOther aircraft modifications

Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2178, Revision IR, dated January 17 2003, and Installation Manual MA2179, Revision IR, dated February 24, 2003, or later FAA approved revision to either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

FAA holder: Micro AeroDynamics Inc

View record