TCDS A10CE

STCs approved under this data sheet · 1,102

Current certificates first, most recently changed first.

Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date
  FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s
  WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A10CE')
  ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

STC ST01370WI-DInstallation of the Honeywell HF 1050, HF Communication SystemLearjet IncSTC ST01421WI-DInstallation of the Airshow 410 System on Learjet 60XR aircraft.Learjet IncSTC ST01424WI-DInstallation of an Emergency Power Supply #1 Replacement on a Learjet Model 60 aircraft.Learjet IncSTC ST10617SCInstallation of a window shade system assembly.Lou Martin & AssociatesSTC ST01955LAInstallation of provisions for terrain mapping radar equipmentIntermap TechnologiesSTC ST02374NYInstallation of Collins TCAS 4000 including dual TDR-94D Mode S transpondersAero-Dienst GmbH & Co KGSTC SA30GLInstallation of electronic engine synchronizer system.Ontic Engineering and Manufacturing Inc.STC SA412CEInstallation of Woodward Electronic Engine synchronizer system.Ontic Engineering and Manufacturing Inc.STC ST00703CH-DInstallation of an AlliedSignal Digital Electronic Engine Control (DEEC).Honeywell International IncSTC ST01756SEONE-ONLY: Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM), S/N 36-036.AeroMech IncorporatedSTC ST01753SEONE-ONLY: Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM), S/N 36-008.AeroMech IncorporatedSTC ST02352NYThe installation of a Honeywell KGP 860 Class B GA-EGPWSAvionics Design Services Ltd.STC ST01724SEInstallation of a drag reduction system (contoured flap)Raisbeck EngineeringSTC ST01142WI-DModification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head.Rockwell Collins IncSTC ST01412WIInstallation of the Revue Thommen 2 Standby AltimeterRevue Thommen AGSTC ST01845CHInstallation of a Honeywell CAS-67A Traffic Alert and Collision Avoidance System (TCAS II)West Star AviationSTC ST01846CHInstallation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System with Terrain Display.West Star AviationSTC ST01892CHInstallation of dual Universal Avionics UNS-1B+ Flight Management Systems.West Star AviationSTC ST01082WI-DInstallation of a Universal Avionics UNS-1C+ or UNS-1E FMS with 801.X software level.Learjet IncSTC ST00844WI-DModification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter.Rockwell Collins IncSTC ST01394WI-DModification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation.Rockwell Collins IncSTC ST01225WI-DInstallation of a M60 TDR-94D Transponder Elementary Surveillance Upgrade.Learjet IncSTC ST01727LA-DInstallation of a Honeywell KHF-1050 HF Communication System.Learjet Inc.STC SA1727CEInstallation of dual Litton LTN-211 VLF/OMEGA navigation system.Eaglejet Aviation Inc.STC SA644CEInstall drift sight provisions. Limited to installation on Learjet model 24, serial number 124.Eaglejet Aviation Inc.STC ST01325WIInstallation of B/E Aerospace LED Washlighting Assemblies and Dimming Interface Modules.Eaglejet Aviation Inc.STC ST02215CHInstallation of a one-piece cabin headlinerWest Star AviationSTC ST01531SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) are contained in AeroMech Document No. AMI-QD-LJ-0416 Rev. New, dated April 8, 2005 or latest FAA approved revision.AeroMech IncorporatedSTC ST01157WI-DInstallation of an L-3 Communications F1000 Solid State Flight Data Recorder (SSFDR) System.Duncan Aviation IncSTC ST03275ATInstallation of a Honeywell Mark VII Enhanced Ground Proximity Warning System (EGPWS)Averitt Aviation Inc.STC ST01159WI-DInstallation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).Duncan Aviation IncSTC SA8930SWInstallation of Bizjet International Inlet Anti-ice Heat Blanket.Bizjet International Sales & Support IncSTC ST01381WI-DInstallation of a LED Position lights system.Learjet IncSTC ST01051CH-DInstallation of an AlliedSignal Inc TFE731-3C/3CR Turbofan engine(s).Landmark AviationSTC ST0836CH-DInstallation of Honeywell N1 Digital Electronic Engine Control (DEEC)Landmark AviationSTC ST00913WI-DInstallation of Innovative Solutions & Support (IS&S) Dual Altimeter / ADC System equipped with a FC-530 or FC-535 Autopilot.Learjet Inc.STC ST02265CHInstallation of Thrust Reverser Hydraulic System Modifications that were previously installed by STC SA1731SW, SA1669SW or SA1670SWLeading Edge Designs LLCSTC ST01656SENon-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM). Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 35A, Serial Number 183 only.AeroMech IncorporatedSTC ST02240NYReplacement of engine N2 and ITT indicators with Diamond J equivalent gauges.Insight Instrument CorporationSTC ST02234NYDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in airplane Serial Number 133 only. Installation of Flap Preset Control System.Insight Instrument CorporationSTC ST00423DE-DInstallation of Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS).Learjet IncSTC ST00300DE-DInstallation of a single Universal Avionics Systems Corporation UNS-1K Flight Management System.Learjet IncSTC ST01181WI-DInstallation of a Honeywell IHAS-8000 Multi-Hazard Awareness System Installation.Learjet IncSTC ST01524LAInstallation of Rosemount Pitot Static Probes, part numbers 856NA1 and 856NA2.West Star AviationSTC ST01525LAInstallation of the Honeywell AZ-252 air data computer.West Star AviationSTC ST01526LAAircraft modifications for establishing approval basis for Reduced Vertical Separation Minimum as contained in STCs ST01524LA and ST01525LA.West Star AviationSTC ST02242CHInstallation of a Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS) with Windshear and Terrain DisplayAlternative Aviation CoSTC ST01352WI-DModification of a Collins ADC-850 ( ) Air Data computer installation.Rockwell Collins IncSTC ST00346WI-DInstallation of Allied Signal (Bendix King) CAS 67 TCAS II Traffic Alert and Collision Avoidance System.Learjet IncSTC ST00506DE-DInstallation of a Collins TCAS-4000 TCAS II system displayed on VSI/TRA indicators with dual Collins TDR-94D Mode S transponders.Learjet Inc
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