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.

FAA-listed holder

F. Atlee Dodge Aircraft Services, LLC

Aircraft configurations

FAA revision date

May 2, 2014

FAA status

Current · Issued

Recorded modification

What the FAA record covers

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

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SA8906SW-DFlight controlsRevised Jul 21, 2001

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

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SA485SWFlight controlsRevised Jul 3, 2001

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

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SA8889SW-DFlight controlsRevised Jul 2, 2001

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

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SA00930SEFlight controlsRevised Jun 13, 2001

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

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What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

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.

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.

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).

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.