STC SA01252SE
FAA DRS lists SA01252SE as Current · Reissued, held by Fessler Aviation Inc., for Piper Aircraft PA-30 and Piper Aircraft PA-39. Recorded change: Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA01252SE 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-30 and Piper Aircraft PA-39. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related engine and powerplant STCs
Installation of P&WACL PT6A-34, -34AG, -15AG, -20A, -41, -41G, -36, -135, -135A, or -28 engine.
FAA holder: Turbine Conversions Ltd
Installation of Engine Monitoring System and Fuel Indication with multifunction displays (MFD-5200).
FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane
FAA record reference
- STC number
- SA01252SE
- Product
- Aircraft
- Country
- United States
- Application date
- July 29, 2003
- Revision date
- January 20, 2004
- CFR references
- Part 3, Part 21