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 ST03071ATInstallation of Avionics System for Reduced Vertical Separation Minimum (RVSM) Provisions into a Boeing 727-200 aircraft in accordance with Avionics Support Group, Inc Master Drawing List (MDL) No. 23509-MDL Rev A, dated 05/27/04, or later FAA approved revision.STC SR01430LAInstallation of Stainless Steel Skid shoes.STC ST01676LA-DInstallation of a 17-passenger cabin interior and associated aircraft completion alterations on model GV-SP, serial number 5054 ONLY.STC ST02947AT-DDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Gulfstream GV-SP, Serial Number 5056. This STC does not permit manufacturing of parts for multiple installations.STC ST03061AT-DInstallation of Honeywell Airborne Flight Information System (AFIS) Upgrade in accordance with Gulfstream Aerospace Corporation Index List CE51 3068000 Rev. A, dated March 14, 2005 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement
CE51 306M000, Rev. NC, dated March 21, 2005 or later FAA approved revision is required.STC SA01951NY-DInstallation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system.STC ST01778NY-DInstallation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) with Runway Awareness and Alerting System (RAAS).STC ST02066NYInstallation of a second (No. 2) Collins ADF-60A or Honeywell (Bendix/King) KDF-806 ADF System in accordance with Transport Canada Civil Aviation (TCCA) approved Western Avionics Engineering Order 99459-401, original issue dated August 31, 2004 or later TCCA approved revision.STC SB02125CHDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Cameron Balloons US Model Z-90, Serial No. 6388. This STC does not permit manufacturing of parts for multiple installations.STC ST00578DEReduce number of passenger seats installed from 8 to 4 passengers.STC ST02116CHInstallation of Composites Unlimited Cart Stowage Units in accordance with Armstrong Aerospace Master Data List, Doc. No. DC104-3087-00, Revision B, dated February 11, 2005, or later FAA approved revision.STC SA02865ATInstallation of ACS Products Company cockpit control wheels. Limited to installation on PA-22-150, serial number 22-2895 ONLY.STC ST01675LA-DFor installation on GV-SP, serial number 5053 ONLY, for a 13-passenger cabin interior.STC ST02063NYInstallation of Zonal Drying System in accordance with Lufthansa Technik Supplemental Type Definition Document
STDD 21-04/01M, Issue 01, dated January 4, 2005.STC ST02064NYInstallation of the Delastek Bleed Leak Monitoring System, P/N DK-329-001, to be done in accordance with Delastek Inc. Master Document List, MDL-DK-329-001, Revision 1, dated October 25, 2004, or later Transport Canada approved revision.STC ST01922NYInstallation of an AHS 1000 altitude heading reference system.STC SA1-619Installation of Continental A-65-8F engine and McCauley 1A90CF-7147 propeller.STC ST00210BOInstallation of Universal Avionics Terrain Awareness Warning System (TAWS).STC ST01674LA-DInstallation of 14-passenger cabin interior on model GV-SP, serial number 5050 ONLY.STC ST02062NYDescriptive data pertaining to this design change is considered inadequate for duplication in other products. This approval is limited to only the installation made in Bombardier, CL-600-2B16 (604 variant), Serial Number 5455. This STC does not permit manufacturing of parts for multiple installations.STC ST03064ATInstallation of a Honeywell MK VI Enhanced Ground Proximity Warning System (EGPWS).STC ST10155SC-DIncrease T/C Seat Capacity.STC SA00233SEInstallation of the Precise Flight Series 100 Speedbrake SystemSTC SA1781NMInstallation of Precise speedbrake system.STC SA2171NMInstallation of Precise Flight speedbrake system.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)STC SA3522NMInstallation of Precise flight series 400 speedbrake system.STC SE1780NMInstallation of Precise Flight standby vacuum system (SVS III).STC ST02061NYInstallation of Side-Facing DivanSTC ST10154SC-DInstall two ozone convertors.STC SA00212BOInstallation of Lycoming O-320-A2B engine and Sensenich 74DM6S8-1-52 propeller limited to 7ECA, serial number 328 ONLY.STC ST00821WIInstallation of the AlliedSignal MK-VII Enhanced Ground Proximity Warning System (EGPWS).STC ST10250SC-DAircraft ComplianceSTC ST10251SC-DInstallation of Aircraft ComplianceSTC ST01747LACabin interior re-configurationSTC SA02115CHInstallation of a dual Shadin ADC-6000 Air Data Computer System.STC ST02059NYInstallation of the Connexion By Boeing Next Generation Antenna System, in accordance with Lufthansa Technik Supplemental Type Definition Document STDD00-04/10M, Issue 00, dated May 25, 2003, to be used for Airborne Local Area Network System by passengers.STC ST02060NYInstallation of network services via Wireless Airborne Local Area Network (Wireless ALAN) in accordance with Lufthansa Technik Supplemental Type Definition Document STDD 00-04/09M, Issue 00, dated May 25, 2003. The airborne LAN system provides internet services to the passengers and interfaces with the Connexion by Boeing Next Generation Antenna System.STC ST02949AT-DDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Gulfstream GV-SP, Serial Number 5051. This STC does not permit manufacturing of parts for multiple installations.STC ST01311WI-DInstallation of 15.1-inch monitor.STC ST01254LA-DInstallation of an Artex ELT with Nav Interface per Master Drawing List HC25615000 latest FAA revision.STC ST01595LA-DInstallation of Control Wheel Lighted Chart Holders.STC ST03028AT-DInstallation of Motorola Satellite Telephone (Iridium) System in accordance with Gulfstream Aerospace Corporation Index List GC512038000, Revision C, dated March 01, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement, GC51203M000, Revision NC, dated March 02, 2005, or later FAA approved revision is required.STC ST09663ACInstallation of passenger cabin configuration to a 6/106 mixed class layoutSTC SR01104SEFabrication of AMC AM369D21800-501 Tail Rotor Pitch Control AssemblySTC SR01119SEFabrication of AMC 600X5630-501 Cooling Blower AssemblySTC SR01136SEFabrication of AMC AM369A6200-45, -46, -57, -58 Landing Gear Fillet Fairings and AM369H6200-73, and -74 Landing Gear Fairing Guides per AMC Master Drawing List No. MDL-AMC-003, Rev A, dated August 29, 2002 or later FAA approved revision; and installation of this assembly in accordance with the Maintenance Manual for the rotorcraft, document number CSP-HMI-2, Rev 21, or later FAA approved revision.STC SR01171SEFabrication of AMC AM369H8092 engine cooling duct orificeSTC SR01172SEFabrication of AMC AM369H8064 cabin vent valve housing assembly in accordance with AMC Master Drawing List No. MDL-AMC-011, Revision A, dated November 11, 2002, or later Federal Aviation Administration (FAA) approved revision. The housing assembly must be installed in accordance with AMC Installation Instructions MI-02004, Revision IR, dated November 15, 2002, or later FAA approved revision.STC SR01204SEFabrication of AMC AMC369H92827 pin, clevis-rotor brake