STC SA09860AC
FAA DRS lists SA09860AC as Current · Reissued, held by Textron Aviation Inc, for Textron Aviation T206H. Recorded change: Increase the maximum ramp weight to 3,806 pounds and maximum takeoff weight to 3,789 pounds. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Increase the maximum ramp weight to 3,806 pounds and maximum takeoff weight to 3,789 pounds.
SA09860AC 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: Textron Aviation T206H. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Textron Aviation T206H model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.
FAA holder: D'Shannon Products Ltd.
Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.
FAA holder: D'Shannon Products Ltd.
Installation of Gross Weight Increase Kit No. 10B1-6521, in accordance with Wipaire Inc. Installation Drawing No. 10B1-6521, no revision, dated December 17, 1998, or later FAA approved revisions.
FAA holder: Wipaire Inc
Gross weight increased to 6530 pounds.
FAA holder: Mike Jones Aircraft Sales Inc.