Supplemental type certificates
49,117 STCs, most recently changed first. Search by what an STC changes, its holder or a model.
Query with SQL
duckdb -csv -c "SELECT stc_number, description, holder, status, status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' ORDER BY status_date DESC NULLS LAST, 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 stc_number, description, holder, status, status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' ORDER BY status_date DESC NULLS LAST, 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 SR09160RCInstallation of an antenna pod provisions. Approval is limited to installation made in Bell 430 serial number 49009 with high skid gear and without floats ONLY.STC SA01046WIInstallation of a two-place side facing divan.STC SA5171SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-173-40/50.STC ST00267LAInstallation of Patient Loading and Utility System.STC ST00781LAInstallation of continuous side rails, floor vent panels, up-lock fittings, stabilization straps, and floor beam fasteners. Either STC SA1509SO and SA1543SO, or SA1797SO and SA1798SO must have already been installed on this aircraft.STC ST01608CHInstallation of brake assemblies, p/n 9560164-2 or 9560166, with non-asbestos linings, p/ns 5013028 and 5013029.STC ST02453ATInstallation of AlliedSignal Enhanced Ground Proximity Warning System.STC ST00266ATInstallation of Pratt & Whitney JT3D-3B Engine with long duct nacelles and cutback pylonsSTC ST01036SENon-group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-CL600-0020, Rev. NEW, dated January 10, 2002, or later FAA-approved Revisions. Approved for serial number 1055 ONLY.STC ST01037SENon-group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-CL600-0104, Rev. NEW, dated January 10, 2002, or later FAA-approved Revisions. Approved for serial number 1036 ONLY.STC ST02452ATInstallation of an AlliedSignal CAS 67 (TCAS-II), on a Raytheon/Beechcraft Super King Air 200.STC SA00621LAInstallation of an electronic digital engine tachometer, horizon model P-1000.STC SA00622LAInstallation of an electronic digital engine tachometer horizon model P-1000.STC SA5821NMInstallation of an electronic digital engine tachmoter, Model P-1000.STC SA5823NMInstallation of an engine electronic digital tachometer, Model P-1000.STC SA5824NMInstallation of an engine electronic digital tachometer, Model P-1000.STC SA5838NMInstallation of an engine electronic digital tachometer.STC SA5841NMInstallation of an engine electronic digital tachometer.STC SA5843NMInstallation of an engine electronic digital tachometer.STC SA5844NMInstallation of an electronic digital engine tachometer, Model P-1000, P/N P100030- .STC SA6016NMInstallation of an electronic digital engine tachometer, Horizon Model P-1000, P/N P100050-( ).STC SA6018NMInstallation of an electronic digital engine tachometer, Model P-1000, P/N P100074-.STC SA6019NMInstallation of an electronic digital engine tachometer.STC SA6022NMInstallation of an electronic digital engine tachometer, Model P-1000. Issued 5/18/93.STC SA6023NMInstallation of an electronic digital engine tachometer, Model P-1000.STC SA7092NMInstallation of an engine Electronic Digital Tachometer Horizon Model P-1000, P/N P100200- .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 215STC ST01605CHInstallation of an Allied Signal CAS-67A TCAS II Traffic Alert and Collision Avoidance System in accordance with Pro-Tech Avionics Corporation Master Drawing List Document No. 81-328L001, Revision E, dated December 6, 2001, or later FAA approved revision.STC SA02188AKFabrication and installation of p/n 3284 three-inch extended PA-18 type main landing gear, together with p/n 3164-4 extended shock strut assemblies. Applies to those models previously modified by SA148AL, SA543AL, or SA669AL, or for Piper PA-12S models, planes must have been converted to landplane configuration.STC SA02189AKFabrication and installation of p/n 3344 main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to planes modified by installation of 3-inch extended main landing gear per STCs SA02152AK or SA02175AK.STC SA02190AKFabrication and installation of p/n 3344A main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to those aircraft previously modified by STCs such as SA02188AK.STC SA5240SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-189-40/50.STC ST01013SEInstallation of the General Dynamics EmPower and EmPort SystemsSTC ST00993LA-DInstallation of Rockwell Collins SAT-2000 AERO I SATCOM, System, Airshow 420 System and Magnastar C-750 cabin telephone system.STC ST01429NY116 passengers modification. Approved for model 737-700, serial numer 30279 and 30280 ONLY.STC SA09518AC-DInstallation of S-TEC System 20/30 single and two-axis automatic flight guidance systems, Model ST-892-20/30STC ST01443NYInstallation of Matsushita Avionics Systems 3000 passenger enertainment system.STC SA01033SEInstallation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2162, Revision IR, dated November 1, 2001, and Installation Manual MA2163, Revision IR, dated December 3, 2001, or later FAA approved revisions. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.STC SA02448ATReplace exhaust system with a tuned exhaust system.STC ST01441NYInstallation of Honeywell TCAS2000, Traffic Alert and Collision Avoidance System. Approved for installation on serial number 5146 ONLY.STC ST01602CHNon-group aircraft approval for Reduced Vertical Separation Minimum (RVSM). Approved for serial number 5211 ONLY.STC ST01279LAInstallation of Airshow AS420 In-Flight Entertainment (IFE) System.STC SA01380NYInstallation of Sealand jump seats.STC SA09517AC-DInstallation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-887-20/30.STC SE01604CHConvert Honeywell TPE331-10AV-511B to a TPE331-10AV-511KA.STC SA09011AC-DInstallation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-592STC SR01439NYThe Heli-Grad installation using DECA Modification Summary MS00011965, Rev 3, dtd 6/21/01 or later revision. Rotorcraft is converted to a Restricted Category rotorcraft.STC ST01442NYInstallation of Artex ELT110 Series Emergency Locator Transmitter. AFM 727003FMS00 Transport Canada approved 7/20/01 required.STC SA2878SWInstall two two-place side facing couches.