STC SA3171WE
FAA DRS lists SA3171WE as Current · Reissued, held by Kellstrom Defense Aerospace Inc., for Lockheed Aircraft 382E, Lockheed Aircraft 382G, and Lockheed Aircraft 382F. Recorded change: The auxiliary power unit Model GTC 85-71 located in the forward end of the left hand main landing gear wheel well fairing has been replaced by an AiResearch Gas turbine compressor Model GTCP85-98CK(A). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA3171WE 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: Lockheed Aircraft 382E, Lockheed Aircraft 382G, and Lockheed Aircraft 382F. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related engine and powerplant STCs
Installation of a stainless steel exhaust system.
FAA holder: Summit Aviation Inc
Installation of a Stainless Steel Exhaust System.
FAA holder: Summit Aviation Inc.
Installation of a Teledyne Continental Motors Model IO-550-R engine.
FAA holder: Summit Aviation Inc.
FAA record reference
- STC number
- SA3171WE
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- November 3, 1975
- Revision date
- June 5, 2003
- CFR references
- Part 21