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Avionics

STC SA09896SC

FAA DRS lists SA09896SC as Current · Reissued, held by Hawker Beechcraft Services Inc., for Hawker Beechcraft 65-90, Hawker Beechcraft 65-A90, and Hawker Beechcraft B90, and 3 more aircraft configurations. Recorded change: Installation of a Honeywell KMH-880 Multi-Hazard Awareness System with a Multi-Function Display (MFD), an operational portion of the Honeywell IHAS 8000 (Integrated Hazard Awareness System), resulting in a Traffic Advisory System (TAS) and an Enhanced Ground Proximity Warning System (EGPWS) to reduce the likelihood of controlled flight into terrain and/or collision with another aircraft. Snapshot dated June 30, 2026.

FAA-listed holder
Hawker Beechcraft Services Inc.
Aircraft configurations
6
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SA09896SC 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: Hawker Beechcraft 65-90, Hawker Beechcraft 65-A90, and Hawker Beechcraft B90, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Hawker Beechcraft 65-903A20Hawker Beechcraft 65-A903A20Hawker Beechcraft B903A20Hawker Beechcraft C903A20Hawker Beechcraft C90A3A20Hawker Beechcraft E903A20

Buyer checks

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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

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