Learjet 35A
STCs that may be installed · 228
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 ('5170802', '5170711')
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 ('5170802', '5170711')
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 ST02419LAModifies aircraft originally outfitted with a 24-inch wide executive door to accommodate the standard 36-inch wide cargo doorSTC ST01988NY-DInstallation of a Collins TCAS-4000.STC ST01289WIInstallation of a Davtron Fuel Temperature System. Data Required:
1) LJSC, Ltd. Master Document List MDL4035-28280, Revision B, dated November 19, 2004; and
2) LJSC, Ltd. Airplane Flight Manual Supplement FMS4035-28280, Revision NC, dated November 19, 2004; or later FAA approved revisions to (1) or (2).STC ST01295WIInstallation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System (EGPWS).STC ST00673WI-DModification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation.STC ST00682WI-DModification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.STC SA1489CERemoval of 24-inch wide executive door and installation of 36-inch wide cargo door per AVCON Drawing List 36000 stamped FAA Approved with a date of May 8, 1979, July 3, 1980, November 15, 2010, or later approved revision for Learjet Models 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A, 36, and 36A.STC ST00858WI-DInstallation of Collins TCAS-94 TCAS II systemSTC ST00952SE-DGroup aircraft approved for Reduced Vertical Separation Minimum (RVSM).STC ST00013WI-DInstallation of a modified engine bleed air mixing valve regulated air source.STC ST00032MCInstallation of the Rockwell Collins AHC-3000S Attitude Heading Reference System.STC ST00510WIInstallation of tip tank baggage compartments.STC ST00031MCInstallation of the Universal Avionics Sytems Corporation Vision-1 System.STC ST00034MCInstallation of (a) the Universal Avionics Systems Corporation UNS-1LW & UNS-1FW Flight Management System with a Wide Area Augmentation System and (b) the Trimble Model TA-12 Global Positioning System.STC ST00077WI-DInstallation of a Sundstrand Mark VII Ground Proximity/Windshear Warning System.STC ST02755CHInstallation of a Universal Avionics Systems Corporation UNS-1Lw Flight Management System and an LP/LPV MonitorSTC ST01195WIInstallation of Rosemount Pitot/Static Probes, altimeters, and associated equipment in Learjet 20 series aircraft to obtain Reduced Vertical Separation Minimum approval.STC ST00432WIInstallation of Avcon fins(Aft Body Strakes).STC ST02401CHInstallation of a Universal Avionics Class A or Class B Terrain Awareness Warning Systems (TAWS) and optional Universal Avionics Vision 1 Synthetic Vision System.STC ST02399CHInstallation of a Universal Avionics EFI-890R Electronic Flight Instrument System.STC ST02402CHInstallation of an L3 Avionics GH-3100 Electronic Standby Instrument System (ESIS).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 ST10617SCInstallation of a window shade system assembly.STC ST01955LAInstallation of provisions for terrain mapping radar equipmentSTC 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 ST01325WIInstallation of B/E Aerospace LED Washlighting Assemblies and Dimming Interface Modules.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 ST01157WI-DInstallation of an L-3 Communications F1000 Solid State Flight Data Recorder (SSFDR) System.STC ST01159WI-DInstallation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).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 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.STC ST02240NYReplacement of engine N2 and ITT indicators with Diamond J equivalent gauges.STC 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.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.
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