STC SA1575CE-D
FAA DRS lists SA1575CE-D as Current · Reissued, held by Honeywell International Inc, for Piper Aircraft PA-34-200T and Piper Aircraft PA-34-220T. Recorded change: Install KAP-100 single axis, KAP-150 two or three axis or KFC-150 two or three axis flight control system, optional KAS-297B vertical speed and altitude selector and KFC-150 system with optional flight director displays. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA1575CE-D 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-34-200T and Piper Aircraft PA-34-220T. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related avionics STCs
Installation of Airworthy Products Volt/Amp Meter Display.
FAA holder: Airworthy Products
Installation of a Universal Avionics, Terrain Awareness Warning System (TAWS).
FAA holder: Gulfstream Aerospace Corporation
Installation of Avionics System for Reduced Vertical Separation Minimum (RVSM) Provisions into a Boeing 727-200 aircraft in accordance with Avionics Support Group, Inc Master Drawing List (MDL) No. 23509-MDL Rev A, dated 05/27/04, or later FAA approved revision.
FAA holder: Avionics Support Group Inc
FAA record reference
- STC number
- SA1575CE-D
- Product
- Aircraft · Small Airplane
- Country
- United States
- Application date
- December 9, 1982
- Revision date
- March 25, 2020
- CFR references
- Part 21, Part 23