STC SA4276WE
FAA DRS lists SA4276WE as Current · Reissued, held by Del-Air, for New Piper Aircraft PA-28-180, New Piper Aircraft PA-28-140, and New Piper Aircraft PA-28-150. Recorded change: Installation of SDI CFS-1000, -1001, or FT-100 fuel flow indicating system system and facet P/N 480543 auxiliary fuel pump. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of SDI CFS-1000, -1001, or FT-100 fuel flow indicating system system and facet P/N 480543 auxiliary fuel pump.
SA4276WE 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-28-180, New Piper Aircraft PA-28-140, and New Piper Aircraft PA-28-150. 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-28-180 and New Piper Aircraft PA-28-140, and 1 more aircraft configuration 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 Locking Fuel Cap Kit, P/N 407-701-002.
FAA holder: Bell Helicopter Textron Inc.
Increase in maximum zero fuel weight.
FAA holder: L-3 Communications Integrated Systems LP
ONE ONLY, SN 49670: Installation of Olympic Aero Services Transient Suppression Devices on aircraft equipped with auxiliary fuel system.
FAA holder: OLYMPIC AERO SERVICES INC.