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
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.
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FAA holder: Laminar Flow Systems Inc
Type E18S tail wheel fork and truss assembly.
FAA holder: Staggerwing Museum Foundation Inc.
FAA record reference
- STC number
- SA02839AT
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- September 15, 2000
- Revision date
- April 13, 2004
- CFR references
- Part 3, Part 21