STC SA02204AK
FAA DRS lists SA02204AK as Current · Issued, held by Wagner Dane, for New Piper Aircraft PA-18, New Piper Aircraft PA-18-105 (Special), and New Piper Aircraft PA-18-125 (Army L-21A), and 15 more aircraft configurations. Recorded change: Fabrication of replacement engine exhaust system assembly. Limited to airplanes equipped with FAA approved installations of Textron Lycoming O-320 model series engines having a compression ratio of 8.5:1 and a rated power of 160 hp for all operations. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA02204AK 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: New Piper Aircraft PA-18, New Piper Aircraft PA-18-105 (Special), and New 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 replacement Interstage Turbine Temperature gages in the cockpit.
FAA holder: Mitsubishi Heavy Industries America Inc
Installation of Continental IO-470-N engine.
FAA holder: D'Shannon Products Ltd.
FAA record reference
- STC number
- SA02204AK
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- November 3, 1999
- Revision date
- April 29, 2003
- CFR references
- Part 21