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.
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
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 ST01347WI-DInstallation of an Airshow 4000 system.STC ST02158NYInstallation of Artex ELT C406.STC ST00786WI-DInstallation of Allied Signal MVII Enhanced GPWS/Windshear SystemSTC ST01904CHInstallation of IS&S Air Data Display Units 9D-80130-15, Analog Interface Unit 9B-81040-30, and Rosemount model 0856NA pitot-static probes. Limited to Learjet 24 models with MKII wings, 300 kts Vmo airspeed limitation, and JET FC-110 autopilot. Excludes serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.STC ST02016CHCertification for Reduced Vertical Separation Minimum (RVSM) operational capability. Excluding serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.STC ST03144ATInstallation of a Honeywell CAS-67A Traffic Alert and Collision Avoidance System-II (TCAS-II).STC ST01599LA-DInstallation of an ICG Iradium Satcom System.STC SA2479CEInstallation of dual openable hatches on the belly of the fuselage.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 ST01463SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-LJ-0121 Rev. New," dated September 17, 2004, or latest FAA-approved revision.STC ST01922NY-DInstallation of an AHS-1000S Attitude Heading Reference System.STC ST00504DE-DInstallation of Dual IS&S Air Data Display Unit (ADDU) systems.STC ST09484AC-DInstallation of MFDAU/DFDR.STC ST09485AC-DInstallation of MFDAU/DFDR.STC ST09490AC-DInstallation of DGPS equipment.STC ST01264WI-DInstallation of Rosen 5.6 inch monitors.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 ST00578DEReduce number of passenger seats installed from 8 to 4 passengers.STC ST01311WI-DInstallation of 15.1-inch monitor.STC ST01382SEGroup 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 31, Serial Numbers 033, 033A, 033C, and 033D only.STC ST01498SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 55, Serial Number 085 only.STC ST01302WIRevise the environmental control system ducting to add two outlets on the cockpit center pedestal for improved crew comfort in accordance with STC Drawing list No. 67-269L001, Rev. C, dated November 18, 2004, stamped FAA Approved January 20, 2005, or later approved revision.STC ST00321WI-DInstall Rosemount Pitot/Static probes per Learjet Master Document List, M1001651CT latest FAA revision.STC ST01613LA-DInstallation of a Honeywell KGP-860 Terrain Awareness Warning System (TAWS).STC ST01612LA-DInstallation of a Honeywell KGP-860 Terrain Awareness Warning System (TAWS).STC ST10342SCInstallation of an AC Generator system.STC ST10343SCInstallationSTC ST01272WIProvisions for installation of Special Mission Equipment and modification of extended range tip tanks to incorporate a dry bay in Learjet 35A, S/N 35A-611.STC 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 ST10278SCInstallation of a single Honeywell KGP-860 Class B Enhanced Ground Proximity Warning System (EGPWS) in accordance with the Master Document List BAS55010057, Rev. A, dated August 30, 2004, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement BAS55040030, Rev. NC, dated September 1, 2004, or later FAA approved revision is required.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 ST01940NYInstallation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced with a Bendix/King (Honeywell) KMD-850 multi-function display.STC ST01941NYInstallation of a Bendix/King (Honeywell) ART 2000 Radar Transceiver/Antenna interfaced with a Bendix/King (Honeywell) KMD-850 Multi-Function Display.STC ST00988WI-DIncorporation of a Universal Avionics Terrain Awareness Warning System (TAWS) on Learjet Model 60 in accordance with Learjet Master Document List M100325ICT, revision (C), dated August 1, 2001, FAA approved August 28, 2001, or later approved revision.STC ST01236WI-DAMS-850 FMS Software Upgrade on aircraft Learjet 60 in accordance with Learjet Master Document List BAS60015037, revision (G), released July 12, 2004, FAA approved July 12, 2004, or later approved revisionSTC ST00550DEModification and installation of an optical glass in forward right hand passenger window.STC ST01249LA-DInstallation of a Honeywell MK VIII Enhanced Ground Proximity Warning System.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 ST01245WIReduced Vertical Separation Minimum (RVSM) non-group (individual) airworthiness approval of specific Learjet Model 55 aircraft in accordance with Kohlman Systems Research (KSR) Master Drawing List Lear 55 RVSM, Drawing No. MDL 1002, Rev. A , dated March 16, 2004, or later FAA approved revision.STC SA1170CEStretcher installation in cabin area.STC SA8098NM-DInstallation of an R134a Air Conditioning System.STC ST02841ATInstallation of a lower pressure bulkhead penetration at FS 346.6 (Frame 15) and structural reinforcement in accordance with Kruse Aerospace Corporation (KAC) Drawing No. 200402, dated April 7, 2004, and DCN A1, dated April 17, 2004, or later FAA approved revision.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 ST00112WI-DInstallation of a Rosemount Ice Detector System on Learjet Model 60 aircraft in accordance with Learjet Master Document List (MDL) M100028ICT Revision H dated March 10, 2004, FAA approved March 19, 2004 or later FAA approved revision.STC ST01865NYInstallation of CAS 67A TCAS II and Dual MST 67A transponders.STC ST01705NYInstallation must be in accordance with Section 1 of DECA Modification Summary MS02051, Rev 2, dated March 7, 2003.STC ST01231WIUpgrade of dual Collins ADS-80 Air Data System for RVSM Capability. Data required: (1) Duncan Aviation Document List 031103026, Revision A, dated March 3, 2004; and (2) FAA Approved Flight Manual Supplement 031103030, dated March 3, 2004, or later FAA Approved revisions to (1) or (2).
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