Skip to content

Aircraft STC directory

Cessna Aircraft 210F STCs

The Jun 30, 2026 FAA DRS snapshot contains 50 selected supplemental type certificates with status Current whose public applicability data names the Cessna Aircraft 210F. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.

50
listed Current at snapshot
32
holder directories
8
modification categories
Dec 16, 2022
latest recorded revision

Modification demand surface

Other aircraft modifications17
Fuel systems9
Flight controls5
Avionics5
Aircraft structures4
Engine and powerplant4
Propellers4
Cabin and interiors2

Recorded holders

Brittain Industries, Inc8Hartwig Aircraft Fuel Cell Repair3S-TEC Corporation3Curry Aviation LLC2Hartzell Propeller Inc2Precise Flight Inc2Power Flow Systems Inc.1Air Plains Services Corporation1P2 Incorporated1Horsham Aviation Services1Glen A Florence, Aero Technologies, Inc.1Cub Crafters Inc1Teledyne Controls1BF Goodrich Aerospace1C J Aviation1Aerospace Welding Minneapolis Inc.1Saf-Air Products Inc.1John Jewell Aircraft Inc1Shadin Avionics1Aero Fabricators Co1

Recently revised 210F STCs

Showing the 50 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