N73LR
STCs that may be installed · 232
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.
Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2730101'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '29001')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, 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 m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2730101'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '29001')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, s.status = 'Current' DESC, s.status_date DESC, s.stc_numberRun 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.
Airframe · Dassault-Breguet FALCON 10
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