Skip to content
Avionics

STC SH1025NE

FAA DRS lists SH1025NE as Current · Reissued, held by Helicopter Aviation Services Corporation, for Bell Helicopter Textron 412. Recorded change: Installation of Bendix/King 660 flight management system, RDS84VP weather rader, and GC 360A radar graphics, and a radio package modification. Snapshot dated June 30, 2026.

FAA-listed holder
Helicopter Aviation Services Corporation
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SH1025NE 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: Bell Helicopter Textron 412. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Bell Helicopter Textron 412H4SW

Buyer checks

Confirm before sourcing

Related avionics STCs

ST10981SC-DAvionics

Avionics and Interior Installation in accordance with Data List Report No. F2EX-01040 Revision A dated 27-Oct-2011, or later FAA approved revision. FAA Approved AFM Supplement, Report 37159-F2EX-D704 dated October 27, 2011 or later FAA approved revision is required. Supplemental Maintenance Manual, Report SMM F2000EX-SN 227, revision A, dated August 30, 2011 or later FAA approved revision is required. Supplemental Illustrated Part Catalog, Report SIPC F2000EX-SN 227, revision B, dated October 20, 2011 or later FAA approved revision is required. Supplemental Wiring Diagram Manual, Report F2MB-001-D704, revision G, dated October 3, 2011 or later FAA.

FAA holder: Dassault Falcon Jet Corp.

View record
SA00736DEAvionics

This Supplemental Type Certificate authorizes autopilot-coupled RNAV (GPS) approaches to LPV and LNAV/VNAV minima when there is a functioning Pilatus option radar altimeter installed and the aircraft verified to meet the requirements of Pilatus Business Aircraft Installation Instructions Document No. P25-486-007 Revision IR, dated August 15, 2011, FAA approved October 25, 2011, or later FAA approved revision.

FAA holder: Pilatus Business Aircraft

View record
SR09547RCAvionics

Installation of Dual TDR-94D/RTU-4200 Transponders with extended squitter (ADS-B) in accordance with PHI Master Document List No. PHI-S92-DL-0003, Rev. 4, dated September 10, 2011, or later FAA approved revision. The dual installation is further defined in PHI Top Drawing No. PHI-S92-60667-01, Rev. IR, dated April 8, 2009, or later FAA approved revision. Rotorcraft Flight Manual Supplement Number PHI-959-S92-RTU-001, dated May 29, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness PHI Document No. PHI-S92-ICA-0004, Rev. B, dated September 9, 2011, or later FAA accepted revision is required.

FAA holder: PHI Inc

View record
SR09548RCAvionics

Installation of dual WAAS (Pilot/Copilot) Flight Management System (FMS) and single FMS configurations in accordance with PHI Master Document List No. PHI-S92-DL-0002, Rev. 8, dated October 10, 2011, or later FAA approved revision. The dual and single FMS configurations are further defined in PHI Top Drawing No. PHI-S92-60662, Rev. A, dated August 29, 2011, or later FAA approved revision. Rotorcraft Flight Manual Supplement Number PHI-959-S92-FMS-001B, Rev. 1, dated September 1, 2011, or later FAA approved revision is required for the dual FMS installation. Rotorcraft Flight Manual Supplement Number PHI-959-S92-FMS-001A, dated August 18, 2009, or later FAA approved revision is required for the single FMS installation. Instructions for Continued Airworthiness PHI Document No. PHI-S92-ICA-0003, Rev. C, dated September 12, 2011, or later FAA accepted revision is required.

FAA holder: PHI Inc

View record