STC SA975SO
FAA DRS lists SA975SO as Current · Reissued, held by Culbertson Aviation, for Piper Aircraft PA-32R-300. Recorded change: Installation of two 15-gallon auxiliary fuel tanks, one in each wing. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of two 15-gallon auxiliary fuel tanks, one in each wing.
SA975SO 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-32R-300. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-32R-300 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 a Shadin Co. 910502 or 910504 fuel flow indicating system.
FAA holder: Shadin Avionics
Installation of a Shadin Co. 911218 temperature compensated fuel flow indicating system.
FAA holder: Shadin Avionics
Installation of a Shadin Company fuel flow indicating system.
FAA holder: Shadin Avionics
Installation of a Shadin Company fuel flow indicating system.
FAA holder: Shadin Avionics