STC SA5679SW
FAA DRS lists SA5679SW as Current · Reissued, held by Aero Safe Corporation, for Piper Aircraft PA-28-140, Piper Aircraft PA-28-150, and Piper Aircraft PA-28-151, and 6 more aircraft configurations. Recorded change: Installation of an electrical driven vacuum pump as a standby auxiliary pump. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA5679SW 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-28-150, and Piper Aircraft PA-28-151, and 6 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related electrical systems STCs
Installation of a vortex generator kit.
FAA holder: Micro AeroDynamics Inc
Installation of Aircraft Parts generator control units.
FAA holder: Aircraft Parts Corporation
Installation of generator control unit GCSG 501.
FAA holder: Aircraft Parts Corporation
FAA record reference
- STC number
- SA5679SW
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- October 18, 1983
- Revision date
- April 6, 2007
- CFR references
- Part 3, Part 21