TCDS A33EU
STCs approved under this data sheet · 231
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 = 'A33EU') 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.
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 = 'A33EU') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC ST02657CHInstallation of dual Universal Avionics Systems Corporation UNS-1Lw Flight Management Systems.STC ST02194CHInstallation of a Universal Avionics Systems Corp. (UASC) EFI-890R Electronic Flight Instrument System (EFIS) and Dual IS&S Air Data Computers (ADCs).STC ST01699LAInstallation of Rosemount Pitot-Static Probes Part Numbers, 856NA1 and 856NA2, and Honeywell Air Data System comprised of AZ-252 Air Data Computers, BA-250 Altimeter Display and AM-250. AltimeterSTC ST01187SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM)STC ST01641CH-DInstallation of Innovative Solutions & Support (IS&S) dual Air Data Display Units (ADDU) and IS&S Analog Interface Unit (AIU).STC ST01367CH-DInstallation of Collins TCAS-4000 Traffic Alert and Collision Avoidance System.STC ST01374CH-DInstallation of Innovative Solutions & Support Air Data Display Unit (ADDU).STC ST01366CH-DInstallation of Honeywell MK-VII Enhanced Ground Proximity Warning System (EGPWS) with -213 -213 software, optinal windhsear detection, and terrain display.STC ST02624CHInstallation of Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) and TDR-94D Mode S TranspondersSTC ST02547CHInstallation of a Universal Avionics Systems Corporation UL-701 UniLink SystemSTC ST02548CHInstallation of an International Communications Group ICS-120 Iridium Satellite Telephone SystemSTC ST01005CH-DInstallation of Honeywell (formerly AlliedSignal Aerospace) N1 Digital Electronic Engine Control (DEEC)STC ST02438NYInstallation of Honeywell Multi-function Radar Display and Enhanced Ground Proximity Warning System (EGPWS) MK VIII.STC ST02443NYInstallation of Rockwell Collins TCAS-4000 including dual Mode S Transponder TDR-94D.STC ST02437NYInstallation of Kannad 406 Emergency Locator Transmitter.STC ST02431CHInstallation of a Universal Avionics Application Server Unit (ASU).STC ST01119WI-DModification of Collins TDR-94 or TDR-94D Mode S Transponder System installation with stand-alone Collins RTU-4210 or RTU-4220 Radio Tuning Unit(s) to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with standalone Collins RTU-4210 or RTU-4220 per Collins Installation Instruction listed on AML No. ST01119WI-D, latest revision.STC 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.STC ST00875WIInstallation of a Universal Avionics System Corporation Terrain Awareness Warning System (TAWS)STC ST01666CHInstallation of Collins Traffic Alert and Collision Avoidance TCAS 4000 system.STC ST01072CHNon-group aircraft approval for Reduced Vertical Separation Minimum (RVSM).STC 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.STC ST01282SENon-Group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM)STC ST01006CH-DInstallation of an AlliedSignal Engines TFE731-2C Turbofan Engine.STC ST01817LAInstallation of Dual Collins ADC-87A Air Data Computers, Collins ALI-80A altimeter, Collins MSI-80C Mach Airspeed Indicator, Thommen Standby Altimeter, and Horizon Aerospace Standby Airspeed Indicator.STC ST01333WI-DModification of a Collins Airshow 400 System.STC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationSTC ST10115SCInstallation of a Universal Avionics Systems Terrain Awareness Warning System (TAWS).STC ST01229WIReduced Vertical Separation Minimum (RVSM) non-group (individual) airworthiness approval of specific AMD/BA Falcon 10 aircraft.STC ST01922CHInstallation of the Innovative Solutions & Support (IS&S) Air Data Display Unit (ADDU) with the IS&S Analog Interface Unit (AIU).STC ST10184SCInstallation of Innovative Solutions & Support (IS&S) air data system.STC ST02662ATInstallation of a Collins ADC-87A Air Data Computer (ADC) and an Innovative Solutions & Support (IS&S) Air Data Display Unit (ADDU) and an optional Stand-by Altimeter.STC ST01806CHCertification of Reduced Vertical Separation Minimum (RVSM) operational capability.STC ST01131WIInstallation of Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).STC ST01448CH-DInstallation of Universal Avionics EFI-550 Flat Panel Electronic Flight Instruments.STC ST01138SENon-group aircraft approval for Reduced Vertical Separation Minimum Qualification Document. Approved for installation on model Falcon 10, serial number 102 ONLY.STC ST01147SENon-group aircraft approval for Reduced Vertical Separation Minimum Qualification Document, Dassault Model Falcon 10, SN 107, per AeroMech Document No. AMI-QD-F10-0203, dated October 30, 2002, or latest FAA approved revision.STC ST01723CHCertification of Reduced Vertical Separation Minimum (RVSM) operational capability.STC ST01361CH-DInstallation of a Rockwell Collins ADC-80K air data computer, Rockwell Collins AL1-80A Altimeter (Copilot), Aerosonic 2" standby altimeter system, and Rosemount Aerospace Model 102AU1AG IAW Garrett drawing list 68-9708-04, dtd 1/17/01, or later FAA approved revision.STC SA5017SW-DInstallation of automated flight information system AFISSTC SA5031SW-DInstallation of a B & D cabin display system including true airspeed, altitude, outside air temperature and timeSTC SA5038SW-DInstallation of additional indicator for airspeed calibration standard.STC ST00135DE-DInstallation of Collins TCAS-94 TCAS II system.STC SA2702NMInstallation of dual Universal UNS-1 navigation system with dual UNS Omega sensors, a Litton Model 91 inertial reference system, and a Collins Model 42 DME.STC SA2727NMReplacement of existing fan speed indicators (N1), turbine speed indicators(N2), and interstage turbine.STC ST153RMInstallation of Canadian Marconi CMA-734 Omega Navigation System.STC ST01625CHCertification of Reduced Vertical Separation Minimum (RVSM) operational capability initiated per FAA approved Instructions for Initial and Continued Airworthiness, Garrett Aviation Services Doc. No. 68-8008-004, dtd 2/21/02 or later FAA approved revision. Approved for instalation on serial number 201 ONLY.STC ST364CHInstallation of a TCAS I (Model TCAS791).STC ST01035SENon-group aircraft approval for Reduced Vertical Separation Minimum Qualification Document, Dassault Model Falcon 10, SN 157, in accordance with AeroMech Document No. AMI-QD-F10-0021, Revision New, dated January 14, 2002. Approved for serial number 157 only.STC ST01038SEONE ONLY STC Serial Number 215 - Non-group aircraft approval for Reduced Vertical Separation Minimum Qualification Document, Dassault Model Falcon 10, SN 215
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