Gates Lear Jet 36
STCs that may be installed · 186
In force first, then newest. The registry doesn’t record which STCs an aircraft has.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('5170601')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
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, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('5170601')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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.
STC ST02403CHInstallation of a single Universal Avionics UNS-1L Flight Management System or single or dual Universal Avionics UNS-1Lw or UNS-1Fw Flight Management Systems.STC ST02597CHInstallation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II).STC ST01842SEInstallation of a Sandel Avionics Horizontal Situation Indicator (HSI) and Attitude Direction Indicator (ADI)STC ST02400CHInstallation of dual Rockwell Collins AHS-1000A Attitude Heading Reference Systems.STC ST00563DE-DInstallation of a Pilots and Co-Pilots Upgraded Altimeter System.STC ST00836CH-DInstallation of AlliedSignal Aerospace N1 Digital Electronic Engine Control (DEEC).STC ST00657DEInstallation of an Intermap Technologies Radar Pod.STC ST00932WI-DInstallation of an Universal Avionics Terrain Awareness and Warning System (TAWS).STC ST00653DELatitude Technologies Corp. SkyNode S200 SATCOM system in Lear Jet Model 31, 31A, 35, 35A, 36, 36A airplanes.STC ST01955LAInstallation of provisions for terrain mapping radar equipmentSTC ST01756SEONE-ONLY: Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM), S/N 36-036.STC ST01753SEONE-ONLY: Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM), S/N 36-008.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 ST01412WIInstallation of the Revue Thommen 2 Standby AltimeterSTC 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 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.STC ST0836CH-DInstallation of Honeywell N1 Digital Electronic Engine Control (DEEC)STC ST00913WI-DInstallation of Innovative Solutions & Support (IS&S) Dual Altimeter / ADC System equipped with a FC-530 or FC-535 Autopilot.STC ST00423DE-DInstallation of Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS).STC ST00300DE-DInstallation of a single Universal Avionics Systems Corporation UNS-1K Flight Management System.STC ST01181WI-DInstallation of a Honeywell IHAS-8000 Multi-Hazard Awareness System Installation.STC ST01524LAInstallation of Rosemount Pitot Static Probes, part numbers 856NA1 and 856NA2.STC ST01525LAInstallation of the Honeywell AZ-252 air data computer.STC ST01526LAAircraft modifications for establishing approval basis for Reduced Vertical Separation Minimum as contained in STCs ST01524LA and ST01525LA.STC ST02158NYInstallation of Artex ELT C406.STC ST03144ATInstallation of a Honeywell CAS-67A Traffic Alert and Collision Avoidance System-II (TCAS-II).STC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationSTC ST01199NY-DInstallation of 2 Innovative Solutions & Support Air Data Dislay Unit Instruments, P/N 9D-80130-1.STC ST01922NY-DInstallation of an AHS-1000S Attitude Heading Reference System.STC ST01468SEInstallation of a drag reduction system (including outboard trailing edge extension, leading edge vortilons, and contoured flap) in accordance with Raisbeck Engineering Drawing Number 202L-5700, Revision A, dated August 29, 2004, or later FAA approved revisions.STC ST00321WI-DInstall Rosemount Pitot/Static probes per Learjet Master Document List, M1001651CT latest FAA revision.STC ST10342SCInstallation of an AC Generator system.STC ST10343SCInstallationSTC ST01611LA-DOptional location for fire extinguisher.STC ST01186WI-DInstallation of an Universal UNS-1L Flight Management System on Learjet Model 31/35/35A/36/36A aircraft in accordance with Learjet Master Document List BAS35010062, revision (E), released February 17, 2004 FAA approved February 19, 2004, or later approved revision.STC ST01946NYCockpit voice recorder replacement with Universal CVR 30B or CVR120.STC ST01259WI-DIncorporation of a UNS-1D (SCN 702) Upgrade to UNS-1D+ MMMS (SCN 902)STC ST01242WI-DInstallation of Iridium Satcom Antenna on Learjet Model 35/35A/36/36A aircraft in accordance with Learjet Master Document List BAS35010064, revision (G), dated May 12, 2004, FAA approved May 12, 2004, or later approved revision.STC SA1170CEStretcher installation in cabin area.STC ST01237WI-DInstallation of a Honeywell KGP 860 EGPWS (without Terrain Display) on Learjet Model 31/35/35A/36/36A aircraft in accordance with Learjet Master Document List BAS35015049, revision (A), dated April 14, 2004, FAA approved April 16, 2004, or later approved revision.STC ST01705NYInstallation must be in accordance with Section 1 of DECA Modification Summary MS02051, Rev 2, dated March 7, 2003.STC ST00361DEInstallation of Puritan Bennett or B/E Aerospace Sweep on 2000 or Zodiac Intertechnique EROS crew oxygen mask.STC SA3343NMCockpit Sun Visor installationSTC ST01635NYInstallation of insulation blankets.STC ST01748CHInstallation of a Universal Terrain Avoidance and Warning System (TAWS).STC ST01749CHInstallation of a 4-tube Universal Avionics Electronics Flight Instrumentation System (EFI-550).STC ST00371DE-DInstallation of dual LITEF - Altitude Heading Reference Source (AHRS) system.STC ST01051WI-DIncorporation of a Universal Avionics Terrain Awareness and Warning Systems (TAWS).STC ST00465DEInstallation of Bendix/King Multi-Hazard Awareness System and Traffic Advisory System (MHAS/TAS).STC ST00955WIInstallation of Phoenix Aerospace, Inc Solid State Voltage Regulator Model No. BG- 1010-24-SA, in place of existing voltage regulator
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