SA01365ATEngine and powerplant
Installation of a Lycoming O-360 150HP or 160HP engine and engine mount.
FAA holder: Airmotive Components LLC
Aircraft STC directory
Univair Aircraft 108-5 STCs
The Jun 30, 2026 FAA DRS snapshot contains 8 selected supplemental type certificates with status Current whose public applicability data names the Univair Aircraft 108-5. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.
8
listed Current at snapshot
6
holder directories
3
modification categories
Jan 27, 2026
latest recorded revision
Modification demand surface
Other aircraft modifications5
Landing gear and brakes2
Engine and powerplant1
Recently revised 108-5 STCs
Showing the 8 most recently revised records. Each entry links to the FAA source and separates public approval data from private commercial claims.
View record
SA343WEOther aircraft modifications
Installation of 8:50 x 6 aircraft tires and 8:50 x 6 tubes.
FAA holder: River View Heights LLC
SA3-423Other aircraft modifications
Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels.
FAA holder: F.Atlee Dodge Aircraft Services
SA03030CHLanding gear and brakes
Installation of the Custom Fiberglass Molding, Inc. (CFMI) model 3000 Aircraft Main Landing Gear Skis, with optional CFMI Model 1500 Tail Wheel Ski.
FAA holder: Silveraire LLC
SA01765SE (PAGE 2)Other aircraft modifications
Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels, Part Number (P/N) ABI-1010.
FAA holder: Alaskan Bushwheel Inc.
SA899GLOther aircraft modifications
Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.
FAA holder: EAA Aviation Foundation
SA799WELanding gear and brakes
Installation of George M. Adams DGA-2000 or Bodell BMI-2000 wheel assemblies in lieu of Firestone wheel assembly No. DFA 180. (DGA-2000 wheel approved under TSO-C26a.).
FAA holder: Skybound Manufacturing Inc.
SA01137SEOther aircraft modifications
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2159, Revision IR, dated February 15, 2002, and Installation Manual MA2160, Revision IR, dated October 9, 2002, or later FAA approved revision to either of these documents.
FAA holder: Micro AeroDynamics Inc