STC SR11808LA
FAA DRS lists SR11808LA as Current · Amended, held by Van Horn Aviation LLC, for Airbus Helicopters AS350B, Airbus Helicopters AS350B1, and Airbus Helicopters AS350B2, and 4 more aircraft configurations. Recorded change: Installation of tail rotor assemblies, P/N 350TR1000-101/301. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SR11808LA 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: Airbus Helicopters AS350B, Airbus Helicopters AS350B1, and Airbus Helicopters AS350B2, and 4 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related other aircraft modifications STCs
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability.
FAA holder: Garrett Aviation Services
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2159, Revision IR, dated February 15, 2002, and Installation Manual MA2160, Revision IR, dated October 9, 2002, or later FAA approved revision to either of these documents.
FAA holder: Micro AeroDynamics Inc
FAA record reference
- STC number
- SR11808LA
- Product
- Aircraft · Rotorcraft
- Country
- United States
- Application date
- August 9, 2021
- Revision date
- December 4, 2025
- CFR references
- Part 27