STC SA2502CE
FAA DRS lists SA2502CE as Current · Amended, held by Aircraft Development Co, for Cessna Aircraft P206A, Cessna Aircraft TP206D, and Cessna Aircraft U206, and 29 more aircraft configurations. Recorded change: Installation of strut/wing and strut/ fuselage fairings, lightning hole covers, and aerodynamic putty. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA2502CE 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 P206A, Cessna Aircraft TP206D, and Cessna Aircraft U206, and 29 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related aircraft structures STCs
Installation of a wing Strut Tiedown Kit No. SFF-MSTD.
FAA holder: Short Final Fabrication LLC
Installation of additional bunks in the Door 5 Overhead Crew Rest on\nBoeing Model 747-400 series aircraft.
FAA holder: B/E Aerospace, Inc. - FSI
Fabrication of a LiteAir window plug assembly.
FAA holder: LiteAir Aviation Products Inc
FAA record reference
- STC number
- SA2502CE
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- April 21, 1989
- Revision date
- June 23, 2000
- CFR references
- Part 21