STC SA3700NM
FAA DRS lists SA3700NM as Current · Reissued, held by Airmotive Industries, Inc., for New Piper Aircraft PA-28R-201T, New Piper Aircraft PA-28RT-201T, and New Piper Aircraft PA-28-201T. Recorded change: This modification installs an air to air intercooler in engine air induction system downstream of the turbocharger. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA3700NM 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-28R-201T, New Piper Aircraft PA-28RT-201T, and New Piper Aircraft PA-28-201T. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related engine and powerplant STCs
Removal of the three degree offset from the vertical stabilizer, addition of the airfoil shape to the top of the horizontal stabilizer, and move of the turbine aft by 13 inches in accordance with Drawing Numbers 7061, 7062, 7063, and Drawing List No. 70001 revised 10/10/85.
FAA holder: Turbine Conversions Ltd
Frakes engine cowling, air inlet and filtration system and engine bleed air cockpit heater.
FAA holder: Turbine Conversions Ltd
FAA record reference
- STC number
- SA3700NM
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- Not listed
- Revision date
- August 3, 2001
- CFR references
- Part 21