STC SA5131NM
FAA DRS lists SA5131NM as Current · Amended, held by Micro AeroDynamics Inc, for Cessna Aircraft 414A and Cessna Aircraft 402C. Recorded change: Install vortex genertors on the wing and vertical tail surfaces and an increase in maximum takeoff weight, maximum zero fuel weight, and maximum ramp weight. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA5131NM 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 414A and Cessna Aircraft 402C. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related fuel systems STCs
Installation of Learjet Model 36A fuselage fuel cells.
FAA holder: Avcon Industries, Inc
Installation of Wipaire Fuel Handles, Steps and Mirrors.
FAA holder: Wipaire Inc
Installation of an auxiliary fuel tank system.
FAA holder: Quiet Wing Aerospace LLC
FAA record reference
- STC number
- SA5131NM
- Product
- Aircraft · Small Multi-Engine
- Country
- United States
- Application date
- October 8, 1990
- Revision date
- January 7, 2008
- CFR references
- Part 3, Part 21