STC SA3831NM
FAA DRS lists SA3831NM as Current · Amended, held by Raisbeck Engineering, for Raytheon Aircraft 200, Raytheon Aircraft 200C, and Raytheon Aircraft 200CT, and 8 more aircraft configurations. Recorded change: Installation of improved leading edge consisting of inboard leading edges,deice boots, leading edge ducts, leading edge to nacelle fairing and associated hardware. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA3831NM 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: Raytheon Aircraft 200, Raytheon Aircraft 200C, and Raytheon Aircraft 200CT, and 8 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 an engine inlet screen assembly, Tri-State Aviation P/N TSA001M.
FAA holder: Helicopter Support Inc Services Div
Installation of exhaust ejector Sikorsky P/N 76305-07501 and exhaust duct assembly Sikorsky P/N 76305-07500-042 repaired and modified.
FAA holder: Helicopter Support Inc Services Div
Installation of engine exhaust ejector assembly 212-061-200-011/012.
FAA holder: Helicopter Support Inc Services Div
Installation of engine exhaust assembly Messerschmitt P/N 117-65135-01/02.
FAA holder: Helicopter Support Inc Services Div