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
Installation of tail rotor assemblies, P/N 350TR1000-101/301.
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.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Airbus Helicopters AS350B and Airbus Helicopters AS350B1, and 5 more aircraft configurations model, serial range, and configuration?
- 02Which configuration, parts, installation data, limitations, and ICAs apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related other aircraft modifications STCs
Non-group aircraft approval for Reduced Vertical Separation Minimum Qualification Document, Dassault Model Falcon 10, SN 107, per AeroMech Document No. AMI-QD-F10-0203, dated October 30, 2002, or latest FAA approved revision.
FAA holder: AeroMech Incorporated
Replace existing lead-acid batteries with Gill BB638/T1-E lead acid batteries, part numbers BSI 200 left and BSI 200 right.
FAA holder: Aviall Services, Inc.
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