STC SA02839AT
FAA DRS lists SA02839AT as Current · Issued, held by Aircrafters of Enterprise Inc, for Cessna Aircraft 180, Cessna Aircraft 180A, and Cessna Aircraft 180B, and 9 more aircraft configurations. Recorded change: Modification of the main landing gear bulkhead to improve static strength and fatigue characteristics. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Modification of the main landing gear bulkhead to improve static strength and fatigue characteristics.
SA02839AT 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: Cessna Aircraft 180, Cessna Aircraft 180A, and Cessna Aircraft 180B, and 9 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft 180 and Cessna Aircraft 180A, and 10 more aircraft configurations 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
Installation of conventional landing gear. (PA-22-160 landplane normal category only).
FAA holder: Richard Lach
Installation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft.
FAA holder: Laminar Flow Systems Inc
Use of High Velocity OXYFUEL (HVOF) Thermal Coating as specified in Southwest Aeroservice Master Data List SWA 32-300M or latest FAA approved revision in lieu of chrome plating for various top assembly landing gear parts.
FAA holder: Southwest United Industries Inc.
Type E18S tail wheel fork and truss assembly.
FAA holder: Staggerwing Museum Foundation Inc.