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Fuel systems

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.

FAA-listed holder
Aircraft configurations
2
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

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.

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.

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Cessna Aircraft 414A and Cessna Aircraft 402C model, serial range, and configuration?
  2. 02Which tanks, plumbing, usable-fuel assumptions, and inspections apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?