STC SA1696SO
FAA DRS lists SA1696SO as Current 路 Reissued, held by LP Aero Plastics, for Piper Aircraft PA-28-140, Piper Aircraft PA-28-150, and Piper Aircraft PA-28-151, and 15 more aircraft configurations. Recorded change: Installation of one-piece windshield. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA1696SO 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 15 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related other aircraft modifications STCs
Installation of a shoulder restraint system for the entrance compartment jumpseat.
FAA holder: Bombardier Completion Center Inc
Installation of dual Honeywell LASEREF IV Inertial Reference Systems.
FAA holder: Gulfstream Aerospace Corporation
FAA record reference
- STC number
- SA1696SO
- Product
- Aircraft 路 Small Airplane
- Country
- United States
- Application date
- April 20, 1984
- Revision date
- February 26, 2014
- CFR references
- Part 3, Part 21