STC SA3259NM
FAA DRS lists SA3259NM as Current · Reissued, held by Lawrence G. Kirkwood, for Piper Aircraft PA-22-108. Recorded change: Increase maximum weight to 1736 pounds. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Increase maximum weight to 1736 pounds.
SA3259NM 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: Piper Aircraft PA-22-108. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-22-108 model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Increase in takeoff weight from 3200 lbs to 3350 lbs for Bell 206B, serial numbers 5101 and subsequent.
FAA holder: Bell Helicopter Textron
Installation of Helicopter Performance Monitoring System is to be done in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332101, Revision 1, dated July 25, 2003, or later Transport Canada approved revision. Audio option is to be installed in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332102, dated April 2, 2003, or later Transport Canada approved revisions.
FAA holder: Aero-Dyne Repair Services Ltd.
Installation of Aero-Dyne model 2000 helicopter performance monitoring system.
FAA holder: Aero-Dyne Repair Services Ltd.
Installation of Helicopter Performance Monitoring System.
FAA holder: Aero-Dyne Repair Services Ltd.