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
Fabrication and installation of Frame Station 260.42 Fuselage Bulkhead for the Piper Aircraft PA-38-112.
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.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-38-112 model, serial range, and configuration?
- 02Which configuration, loads, materials, inspections, and damage limits apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
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.