STC SA1572CE-D
FAA DRS lists SA1572CE-D as Current · Reissued, held by Honeywell International Inc, for New Piper Aircraft PA-32R-301(SP), New Piper Aircraft PA-32R-301(HP), and New Piper Aircraft PA-32R-301T. Recorded change: Installation of KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system, and optional KAS 297B vertical speed and altitude selector. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA1572CE-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: New Piper Aircraft PA-32R-301(SP), New Piper Aircraft PA-32R-301(HP), and New Piper Aircraft PA-32R-301T. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related flight controls STCs
Installation of rudder centering device in lieu of ventral fin.
FAA holder: M R Borer Aircraft Svc
Installation of a Sperry Digital Automatic Flight Control System, Single and Two Pilot IFR.
FAA holder: American Eurocopter Corporation
FAA record reference
- STC number
- SA1572CE-D
- Product
- Aircraft · Small Airplane
- Country
- United States
- Application date
- September 17, 1982
- Revision date
- March 25, 2020
- CFR references
- Part 3, Part 21