STC SA02168AT
FAA DRS lists SA02168AT as Current · Amended, held by Power Flow Systems Inc., for New Piper Aircraft PA-28-140, New Piper Aircraft PA-28-150, and New Piper Aircraft PA-28-160, and 2 more aircraft configurations. Recorded change: Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System Extractor Exhaust System. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA02168AT 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-28-140, New Piper Aircraft PA-28-150, and New Piper Aircraft PA-28-160, and 2 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
Related engine and powerplant STCs
Installation of air to air intercooler in the engine air induction system. Airplane must have STC SA2689SW incorporated.
FAA holder: Western Skyways Aircraft Modifications Inc.
Installation of an air to air intercooler in the engine induction system downstream of the turbocharger.
FAA holder: Western Skyways Aircraft Modifications Inc.
Installation of an air intercooler in the engine induction system downstream of the turbocharger.
FAA holder: Western Skyways Aircraft Modifications Inc.
Installation of an intercooler in the engine air induction system.
FAA holder: Western Skyways Aircraft Modifications Inc.