STC SA01063CH
FAA DRS lists SA01063CH as Current · Reissued, held by Univair Aircraft Corporation, for New Piper Aircraft PA-16, New Piper Aircraft PA-18, and New Piper Aircraft PA-20, and 7 more aircraft configurations. Recorded change: Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA01063CH 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-16, New Piper Aircraft PA-18, and New Piper Aircraft PA-20, and 7 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related landing gear and brakes STCs
Installation of Take-off Configuration Test Switch and Nose Landing Gear Pin Position Switch.
FAA holder: Aero Consulting Services Ltd
Eliminate 27,000 landing cycle life limit of the landing gear by placing aircraft on an inspection program described by the Murray Aviation document titled CASA C212-200 Series Aircraft Landing Gear Continued Airworthiness Limitations , no revision, dated January 23, 1996, or later FAA Approved Revision.
FAA holder: Presidential Airways Inc
FAA record reference
- STC number
- SA01063CH
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- February 19, 1996
- Revision date
- February 16, 2006
- CFR references
- Part 21