STC SA1679CE
FAA DRS lists SA1679CE as Current · Reissued, held by Sabreliner Aviation LLC, for Sabreliner NA-265-40. Recorded change: Installation of modernized avionics. Snapshot dated June 30, 2026.
FAA-listed holder
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued
Recorded modification
What the FAA record covers
Installation of modernized avionics.
SA1679CE 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: Sabreliner NA-265-40. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Sabreliner NA-265-40 model, serial range, and configuration?
- 02Which part numbers, software versions, interfaces, and manual changes apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related avionics STCs
ST00483WIAvionics
Replacement of the existing engine instruments with the Spirent Systems Wichita, Inc. Flat Panel Engine Instrument Display System (EIDS) Model 94002, in accordance with (1) Installation Data referenced on Continuation Sheet 2; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Continuation Sheet 2.
FAA holder: Teledyne Controls
ST00759WIAvionics
Replace existing engine instruments with the Penny & Giles Aerospace, Inc. Engine Instruments Display System (EIDS). Model 94002, in accordance with (1) Installation Data referenced on Continuation Sheet 2; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Continuation Sheet 2; or later FAA Approved Revisions to (1) or (2). \n(see continuation sheet 2 of 2).
FAA holder: Teledyne Controls
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