STC SH3889SW
FAA DRS lists SH3889SW as Current · Reissued, held by Apical Industries, Inc. dba Dart Aerospace, for Bell Helicopter Textron 212. Recorded change: Installation of 155 gallon capacity external auxiliary fuel system on high skid landing gear configured helicopter or 145 Gallon capacity external auxiliary fuel system on low skid landing gear configured helicopter. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SH3889SW 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: Bell Helicopter Textron 212. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related landing gear and brakes STCs
Fabrication and installation of p/n 3284 three-inch extended PA-18 type main landing gear, together with p/n 3164-4 extended shock strut assemblies. Applies to those models previously modified by SA148AL, SA543AL, or SA669AL, or for Piper PA-12S models, planes must have been converted to landplane configuration.
FAA holder: F Atlee Dodge Aircraft Service
Installation of brake components listed on Nasco Aircraft Brake drawing 737001, Rev G dtd 9/21/01, for use in Honeywell or Bendix brake assemblies 2606672-2, -3, -4 per Nasco Configuration Control Drawing NCC006, Rev A, dtd 11/19/01 or later FAA approved revision.
FAA holder: NASCO Aircraft Brake Inc
FAA record reference
- STC number
- SH3889SW
- Product
- Aircraft · Rotorcraft
- Country
- United States
- Application date
- May 5, 1987
- Revision date
- August 19, 2014
- CFR references
- Part 21, Part 29