STC SA02433AK
FAA DRS lists SA02433AK as Current · Issued, held by F. Atlee Dodge Aircraft Services, LLC, for FS 2002 Corp PA-14, FS 2003 Corp PA-12, and FS 2003 Corp PA-12S, and 18 more aircraft configurations. Recorded change: Installation of F. Atlee Dodge Oversize rudder and/or elevators. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of F. Atlee Dodge Oversize rudder and/or elevators.
SA02433AK 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: FS 2002 Corp PA-14, FS 2003 Corp PA-12, and FS 2003 Corp PA-12S, and 18 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact FS 2002 Corp PA-14 and FS 2003 Corp PA-12, and 19 more aircraft configurations model, serial range, and configuration?
- 02Which control configuration, rigging, limitations, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related flight controls STCs
Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-568, with optional automatic electric trim system.
FAA holder: S-TEC Corporation
For 182H, 182J, 182K, 182L and 182M include (1) Full span double slotted flaps; (2) Drooped wing leading edge; (3) Aileron actuated drag plates; (4) Nose control surface; (5) Elevator down spring alteration; (6) Relocated pitot head. For 182N, 182P, and 182Q include nose control surface only.
FAA holder: Todd and Jo Peterson
Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, model ST-558, with Optional Automatic Electric Trim System. Eligible when modified per STC SA1525WE (Robertson STOL).
FAA holder: S-TEC Corporation
Installation of vortex generators on the wing and flap surfaces in accordance with Drawing Package MA2153, Revision IR, dated January 26, 2001, and Installation Manual MA2154, Revision IR, dated May 29, 2001, or later FAA approved revision of either of these documents.
FAA holder: Micro AeroDynamics Inc