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Avionics

STC SA02255NY

FAA DRS lists SA02255NY as Current · Amended, held by Innovative Solutions & Support Inc, for Pilatus Aircraft PC-12, Pilatus Aircraft PC-12/45, and Pilatus Aircraft PC-12/47. Recorded change: Configuration A Dual 15 Flat Panel Display System (Pilot and Copilot Positions) Installation of Innovative Solutions & Support - (IS&S) Dual 15 Flat Panel Display System Configuration B 10 Flat Panel Display System (Pilot and Copilot/Pilot Side Only Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System Configuration C 10 Flat Panel Display System (Pilot Side) and 15 Flat Panel Display System (Copilot Side) Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System. Snapshot dated June 30, 2026.

FAA-listed holder
Innovative Solutions & Support Inc
Aircraft configurations
3
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

Configuration A Dual 15 Flat Panel Display System (Pilot and Copilot Positions) Installation of Innovative Solutions & Support - (IS&S) Dual 15 Flat Panel Display System Configuration B 10 Flat Panel Display System (Pilot and Copilot/Pilot Side Only Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System Configuration C 10 Flat Panel Display System (Pilot Side) and 15 Flat Panel Display System (Copilot Side) Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System.

SA02255NY 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: Pilatus Aircraft PC-12, Pilatus Aircraft PC-12/45, and Pilatus Aircraft PC-12/47. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Pilatus Aircraft PC-12A78EUPilatus Aircraft PC-12/45A78EUPilatus Aircraft PC-12/47A78EU

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Pilatus Aircraft PC-12 and Pilatus Aircraft PC-12/45, and 1 more aircraft configuration model, serial range, and configuration?
  2. 02Which part numbers, software versions, interfaces, and manual changes apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

Related avionics STCs

SA3036WE-DAvionics

Modifies aircraft to install dual Delco C-IV Inertial Navigation Systems (INS) for attitude and direction reference, navigation, and auto-pilot steering. Also adds a Sperry DG-207 Directional Gyro in the Aux position and Azimuth switching capability. The VG-DG racks are replaced by the INS Navigation units in the above configuration, but the modification permits replacing the INS Navigation units with VG-DG racks to provide triple VG-DG for attitude and direction reference only. The installation is in accordance with DAS-1-WE Approved United Air Lines Drawing List No. COA 3-2023, dated March 22, 1977, or later FAA approved revisions. United Air Lines FAA Approved Flight Manual Supplement to McDonnell Douglas Flight Manual Document Number MDC-J1010 dated February 17, 1977, or later FAA approved revision is required as part of this installation.

FAA holder: United Airlines Inc

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SA3038WE-DAvionics

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FAA holder: United Airlines Inc

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