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Fuel systems

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.

FAA-listed holder
Del-Air
Aircraft configurations
3
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

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.

New Piper Aircraft PA-28-1802A13New Piper Aircraft PA-28-1402A13New Piper Aircraft PA-28-1502A13

Buyer checks

Confirm before sourcing

Related fuel systems STCs

SA281SWFuel systems

Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Ector Aircraft Company Drawing No. 271000 dated 9/16/1963; 72000 Rev. 2/18/1964, Ector Aircraft Drawings dated 10/16/1963 and 7/1/1963, or later FAA approved revisions and seven photographs. Or Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Air Repair, Inc. Engineering Report AR063 dated May 12, 2009, or later FAA approved revision.

FAA holder: Steve Noyes

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