STC SA02115AK
FAA DRS lists SA02115AK as Current · Amended, held by F Atlee Dodge Aircraft Service, for New Piper Aircraft PA-18-150, New Piper Aircraft PA-18A-150, and New Piper Aircraft PA-18AS-150, and 6 more aircraft configurations. Recorded change: Fabrication and installation of 30.5 gallon wing fuel tank sight gages. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Fabrication and installation of 30.5 gallon wing fuel tank sight gages.
SA02115AK 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: New Piper Aircraft PA-18-150, New Piper Aircraft PA-18A-150, and New Piper Aircraft PA-18AS-150, and 6 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact New Piper Aircraft PA-18-150 and New Piper Aircraft PA-18A-150, and 7 more aircraft configurations 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 auxiliary fuel system in the forward baggage compartment. (727-2M7).
FAA holder: Southeast Aero-Tek Inc
Increase in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).
FAA holder: Aircraft Modification Design Services