STC SA02339AK
FAA DRS lists SA02339AK as Current · Issued, held by Aero Twin Inc, for Quest Aircraft Design Kodiak 100. Recorded change: Installation of main gear gravel deflectors, PN GDQ-100, on the main landing gear of the Quest Kodiak 100. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of main gear gravel deflectors, PN GDQ-100, on the main landing gear of the Quest Kodiak 100.
SA02339AK identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Quest Aircraft Design Kodiak 100. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Quest Aircraft Design Kodiak 100 model, serial range, and configuration?
- 02Which gear, wheel, brake, tire, and hydraulic configurations apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related landing gear and brakes STCs
Manufacture of High Skid Landing Gear in accordance with Aeronautical Accessories, Inc. Report No. AA-97077, Revision A, dated August 14, 1997 or later FAA approved revisions and installation per Report No. AA-95050, Revision G, dated February 6, 1997, or later FAA approved revisions.
FAA holder: Bell Helicopter Textron Inc.
Manufacture of Low Skid or High Skid Landing Gear.
FAA holder: Bell Helicopter Textron Inc.
Installation of lockable, full swivel tail wheel per Drawing FA7027H, dated 5/11/78, or later FAA approved revision.
FAA holder: Turbine Conversions Ltd
Modification of the nose wheel shimmy damper in accordance with Down Time Aviation, LLC, drawing number DTA-TBM700-3252 (sheets 1-7); sheets 1-3 and 5-6 Revision A; sheet 4 Revision B; and sheet 7 Revision IR, all dated 12/7/2010 or later FAA approved revision. The aircraft is to be maintained per the Modification Instructions and Instructions for Continued Airworthiness, Document Number 32-52-01, Revision IR, dated January, 2011, or later FAA accepted revision.
FAA holder: Down Time Aviation LLC