STC SA891SO
FAA DRS lists SA891SO as Current · Reissued, held by D'Shannon Products Ltd., for Piper Aircraft PA-24, Piper Aircraft PA-24-250, and Piper Aircraft PA-24-260, and 2 more aircraft configurations. Recorded change: Remove existing windshield and install single piece windshield. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA891SO 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-24, Piper Aircraft PA-24-250, and Piper Aircraft PA-24-260, and 2 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related other aircraft modifications STCs
Installation of balance weights(Brittain Aircraft P/N 3010) on leading edge of Navion ailerons.
FAA holder: General Aviation Modifications Inc.
Installation of air conditioning system.
FAA holder: Fargo Manufacturing Co.
Installation of Two-In-One-Solution (TIOS) Ka-Band Radome.
FAA holder: Lufthansa Technik AG
Transmitting Portable Electronic Devices (T-PED) Aircraft Tolerance Testing.
FAA holder: EPPS Air Service dba EPPS Aviation
FAA record reference
- STC number
- SA891SO
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- March 5, 1976
- Revision date
- August 16, 2011
- CFR references
- Part 3, Part 21