STC SA1072CE
FAA DRS lists SA1072CE as Current · Reissued, held by Curry Aviation LLC, for Piper Aircraft PA-28-140, Piper Aircraft PA-28R-180, and Piper Aircraft PA-28-150, and 3 more aircraft configurations. Recorded change: Installation of wing leading edge cuffs and droop tips, dorsal fin and vertical stabilizer vortex generator. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of wing leading edge cuffs and droop tips, dorsal fin and vertical stabilizer vortex generator.
SA1072CE 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-28-140, Piper Aircraft PA-28R-180, and Piper Aircraft PA-28-150, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-28-140 and Piper Aircraft PA-28R-180, and 4 more aircraft configurations model, serial range, and configuration?
- 02Which load analysis, wiring changes, protection, and limitations apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related electrical systems STCs
Fabrication of a vortex generator system.
FAA holder: Aeronautical Testing Service Inc.
Installation of a Dual 16VDC cockpit power supply system.
FAA holder: Learjet Inc