STC SA02023SE
FAA DRS lists SA02023SE as Current · Issued, held by Sterling Paul, for Piper Aircraft PA-38-112. Recorded change: Fabrication and installation of Frame Station 260.42 Fuselage Bulkhead for the Piper Aircraft PA-38-112. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA02023SE 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: Piper Aircraft PA-38-112. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related aircraft structures STCs
Installation of Wing Spar Reinforcement.
FAA holder: Dynamic Aviation Group Inc.
Installation of front spar reinforcement kit.
FAA holder: Dynamic Aviation Group Inc.
Installation of upper wing reinforcing kit.
FAA holder: Dynamic Aviation Group Inc.
Installation of upper wing reinforcement kit.
FAA holder: Dynamic Aviation Group Inc.
FAA record reference
- STC number
- SA02023SE
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- August 4, 2007
- Revision date
- August 3, 2009
- CFR references
- Part 21, Part 23