STC SA01143WI
FAA DRS lists SA01143WI as Current · Reissued, held by Laminar Flow Systems Inc, for New Piper Aircraft PA-28-140, New Piper Aircraft PA-28-150, and New Piper Aircraft PA-28-151, and 10 more aircraft configurations. Recorded change: Installation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft.
SA01143WI 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-28-151, and 10 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-28-140 and New Piper Aircraft PA-28-150, and 11 more aircraft configurations model, serial range, and configuration?
- 02Which gear, wheel, brake, tire, and hydraulic configurations apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related landing gear and brakes STCs
Manufacture of High Skid Landing Gear in accordance with Aeronautical Accessories, Inc. Report No. AA-97077, Revision A, dated August 14, 1997 or later FAA approved revisions and installation per Report No. AA-95050, Revision G, dated February 6, 1997, or later FAA approved revisions.
FAA holder: Bell Helicopter Textron Inc.
Manufacture of Low Skid or High Skid Landing Gear.
FAA holder: Bell Helicopter Textron Inc.
Installation of lockable, full swivel tail wheel per Drawing FA7027H, dated 5/11/78, or later FAA approved revision.
FAA holder: Turbine Conversions Ltd
Modification of the nose wheel shimmy damper in accordance with Down Time Aviation, LLC, drawing number DTA-TBM700-3252 (sheets 1-7); sheets 1-3 and 5-6 Revision A; sheet 4 Revision B; and sheet 7 Revision IR, all dated 12/7/2010 or later FAA approved revision. The aircraft is to be maintained per the Modification Instructions and Instructions for Continued Airworthiness, Document Number 32-52-01, Revision IR, dated January, 2011, or later FAA accepted revision.
FAA holder: Down Time Aviation LLC