STC SA02828CH
FAA DRS lists SA02828CH as Current · Amended, held by H. O. Aircraft Inc., for Piper Aircraft PA-18, Piper Aircraft PA-18-105 (Special), and Piper Aircraft PA-18-125 (Army L-21A), and 15 more aircraft configurations. Recorded change: Installation of the Lycoming IO-390-A1A6 engine, MT model MTV-15-B/210-58 constant speed propeller and associated accessories. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA02828CH 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-18, Piper Aircraft PA-18-105 (Special), and Piper Aircraft PA-18-125 (Army L-21A), and 15 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related engine and powerplant STCs
Installation of an engine Inlet Barrier Filter System.
FAA holder: Aerometals Inc.
Installation of Chuck Ney Enterprises, Inc. CNE IO-470-C/N-MOD Model Engine (STC SE02261CH).
FAA holder: Cygnet Aerospace Corp.
Installation of a Lycoming O-360 150HP or 160HP engine and engine mount.
FAA holder: Airmotive Components LLC
Installation of Engine Vibration Indicator.
FAA holder: Icarus Aero Inc.
FAA record reference
- STC number
- SA02828CH
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- March 24, 2009
- Revision date
- January 15, 2014
- CFR references
- Part 3, Part 21