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Aircraft STC directory

Cessna Aircraft 210-5 (205) STCs

The Jun 30, 2026 FAA DRS snapshot contains 52 selected supplemental type certificates with status Current whose public applicability data names the Cessna Aircraft 210-5 (205). Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.

52
listed Current at snapshot
32
holder directories
8
modification categories
Nov 17, 2023
latest recorded revision

Modification demand surface

Other aircraft modifications20
Fuel systems7
Flight controls6
Engine and powerplant5
Avionics5
Aircraft structures4
Propellers3
Cabin and interiors2

Recorded holders

Brittain Industries, Inc10Hartwig Aircraft Fuel Cell Repair3S-TEC Corporation3Aerospace Welding Minneapolis Inc.2Curry Aviation LLC2BF Goodrich Aerospace2Texas Skyways Inc2TALCO Aviation1Power Flow Systems Inc.1Airwolf Filter Corporation1Storehouse LLC1Flint Aero Inc1Glen A Florence, Aero Technologies, Inc.1Cub Crafters Inc1Teledyne Controls1Great Lakes Aero Products Inc1Saf-Air Products Inc.1Hartzell Propeller Inc1McCauley Propeller Systems1Aero Fabricators Co1

Recently revised 210-5 (205) STCs

Showing the 52 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