STC SA2570NM
FAA DRS lists SA2570NM as Current · Reissued, held by Javelin Conversions Inc., for Cessna Aircraft P210N. Recorded change: Installation of stiffening ribs in the aileron and rudder surfaces and redistribution of the mass balance in the aileron, rudder and elevator. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA2570NM 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: Cessna Aircraft P210N. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related flight controls STCs
Installation of MPC Products Corp. Rotary Variable Transformer (RVT) P/N GA2200A (3-position sensors right side; Rudder pedal-yaw, and control column-pitch and roll,) and p/n GA2202A (2-position sensors left side, column-itch and roll) to replace existing Flight Data Recorder System (FDRS) Potentiometers position sensors.
FAA holder: Chippewa Aerospace, Inc.
Installation of new rudder bar bushings and bearings.
FAA holder: Hal's Aircraft
Installation of Burbank frangible stop flap guard at 30 degrees maximum approach flap position.
FAA holder: Topeka Management, Inc.
FAA record reference
- STC number
- SA2570NM
- Product
- Aircraft · Small Airplane
- Country
- United States
- Application date
- September 20, 1984
- Revision date
- July 31, 2012
- CFR references
- Part 3, Part 21