STC SA3002WE
FAA DRS lists SA3002WE as Current · Reissued, held by Sierra Industries Ltd., for Piper Aircraft PA-34-200. Recorded change: Installation of wing tip fuel tanks of 17 gal capacity (each). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of wing tip fuel tanks of 17 gal capacity (each).
SA3002WE 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: Piper Aircraft PA-34-200. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-34-200 model, serial range, and configuration?
- 02Which tanks, plumbing, usable-fuel assumptions, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related fuel systems STCs
Installation of auxiliary fuselage fuel tanks in forward and aft cargo compartments. (727-25).
FAA holder: Rogerson ATS
ONE ONLY STC, S/N 25-7556161: Installation of a 38 gallon fuselage tank and selector valve.
FAA holder: Mr. Jerry Hider
Installation of left hand and right hand auxiliary tanks fuel cell assemblies.
FAA holder: FFC Manufacturing
Modification to allow operation at the following weights: takeoff - 142,100 pounds; landing - 114,500 pounds; zero fuel - 109,500 pounds.
FAA holder: Flying Tiger Line Inc