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 ST01846NYInstallation of Avionics Upgrade.STC ST02132CHInstallation of a Honeywell Mark VII Enhanced Ground Proximity Warning System with Terrain Display and Runway Awareness Advisory System (RAAS).STC ST10253SC-DInstallation of Oxygen SystemSTC SB02131CHDescriptive 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 Ltd (Colt) Model 120A, Serial No. 3135USA. This STC does not permit manufacturing of parts for multiple installations.STC SE02881ATSTC for the conversion of Teledyne Continental Motors (TCM) Models IO-520-B, -BA or -BB to AvPower Model IO-550-B-AP which has the same ratings and limitations as TCM Model IO-550-B, or the conversion of TCM Model IO-520-C or -CB to AvPower Model IO-550-C-AP which has the same ratings and limitations as TCM Model IO-550-C. Conversion of the Models IO-520-B, -BA, or -BB to the Model IO-550-B-AP shall be performed in accordance with AvPower Report AP1004-3 Master Parts List, Revision B dated March 26, 2004 and AvPower Report AP1004-6 Assembly Instructions, Revision B dated March 26, 2004, or later FAA approved revisions. Conversion of the Models IO-520-C or -CB to the Model IO-550-C-AP shall be performed in accordance with AvPower Report AP1004-4 Master Parts List, Revision B dated March 26, 2004 and AvPower Report AP1004-7 Assembly Instructions, Revision B dated March 26, 2004, or later FAA approved revisions.STC ST00983CHInstallation of AlliedSignal Enhanced Ground Proximity Warning System.STC ST02102CHInstallation of an L3 Communications (Goodrich) GH-3100 Electronic Standby Instrument System (ESIS).STC ST03070ATInstallation of a Honeywell LSZ-860 Lightning Sensor SystemSTC ST03082ATInstallation of Honeywell Mk VII Enhanced Ground Proximity Warning System (EGPWS) with internal Global Positioning System (GPS).STC ST10209SCInstallation of Dual Innovative Solutions & Support (IS&S) air data display system units.STC SA01929NYInstallation of Thunder Bay Aviation utility passenger seats.STC SA09622ACInstallation of S-TEC Magic 2100 Digital Flight Control System (DFCS) Part No. 01298-01-01-03 or 01304-01-01-003 in accordance with S-TEC Master Drawing List No. 921220, Revision 8, dated March 02, 2005 or later FAA approved revision. S-TEC Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement (AFMS) No. 892126, Revision 1, dated October 2, 2003 or No. 892143, no revision, dated April 4, 2005 or later FAA approved revision is required for this modification.STC ST01185WI-DModification of an existing FAA approved Collins HF Communication System with HFS-900D Receiver/Transmitter.STC SA01314WIReplace the original equipment oil temperature, oil pressure, and fuel pressure 3-in-1 gauges and dual cylinder head temperature gauge with oil temperature, oil pressure, and cylinder head temperature 3-in-1 gauges and dual fuel pressure gauge.STC ST00683CH-DInstallation of a Universal Avionics UNS-1C, Dual (FMS) Flight Management System with GPS as a primary means of navigation.STC ST01455SEUpper deck stowage bin and closet modification of 747-400 Series airplanes in accordance with JAMCO America, Inc., Master Drawing List IA-104MDL, Revision B, dated September 9, 2004, or later Federal Aviation Administration (FAA) approved revision.STC ST02980AT-DInstallation of a External Camera System (Securaplane) in accordance with Gulfstream Aerospace Corporation Index List GC415058000, Revision E, dated March 31, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement, GC41505M003, Revision NC, dated April 01, 2005, or later FAA approved revision is required.STC ST09664ACInstallation of a 6/106 (1st class/coach) passenger cabin configurationSTC ST10387SCConversion of a 4 place seating group (divan) to a 3 place seating group (divan)STC ST334CH-DInstallation of an AlliedSignal avionics MK-V, Enhanced Ground Proximity Warning System.STC SA02237AKLimit the maximum seating capacity to 9 passengers or less in accordance with TransNorthern Drawing TNA-99-01, Revision OR, dated March 15, 2002, or later FAA approved revision.STC SA10392SCInstallation of a dual Innovative Solutions & Support (IS&S) Altimeter System.STC ST03080ATInstallation of a Honeywell MK VI Enhanced Ground Proximity Warning Systems (EGPWS).STC SA01328LAModification of right hand side door to provide an openable window.STC SA01660LAInstallation of Air-Tec Alternator kit. Descriptive data pertaining to this design change are considered inadequate for duplication in other aircraft. This approval is limited to the installation on Mooney M20B, S/N 1900 only.STC SA02039NYInstallation of Skywatch Traffic Advisory, King Ground Proximity Warning System TAWS, and Multi-Hazard Awareness System.STC SA02072NYInstallation of updated fuel system components must be done in accordance with Viking Air Ltd., Master Document Index (MDI), VT2MK1372, Issue 1, dated June 8, 2004, Transport Canada approved September 14, 2004, or later Transport Canada approved revision.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA02236AKFabrication and installation of F. Atlee Dodge Heavy Duty Standard Length Main Landing Gear, P/N 3225A, in accordance with F. Atlee Dodge Master Data List No. 3225-1.5, Revision: None dated March 14, 2005, or later FAA approved revisions.STC SR01750LAInstallation of Airworthy Products Volt/Amp Meter DisplaySTC SR09397RCIncrease in takeoff weight from 3200 lbs to 3350 lbs for Bell 206B, serial numbers 5101 and subsequent.STC ST01515SEInstallation of heat shields for exhaust manifold heat deflection; manufactured and installed in accordance with Drawing List DL180, Rev. B, dated February 9, 2005, or later FAA approved revisions.STC SR01278NYInstallation of L-3 Communications FA2300 Series Combined Flight Data Acquistion Unit/Flight Data Recorder/Cockpit Voice Recorder.STC ST03002ATInstallation of a Honeywell Enhanced Ground Proximity Warning System in accordance with General Aerospace Master Drawing List No. GA672-EGPWS-MDL, Revision A, dated November 9, 2004 or later FAA approved revisions.STC ST03076ATDescriptive data pertaining to this installation are considered inadequate for duplication in other products. This approval is limited to only the installation made in Boeing 737-700, Serial No. 30754. Installation of executive interiorSTC ST02071NYInstallation of the Circulating Potable Water System.STC ST10302SC-DInstallation of a Universal Avionics, Terrain Awareness Warning System (TAWS).STC SA02070NYDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Bombardier, CL-600-2A12 (601 Variant) s/n 3057. Installation of Honeywell Mk VIII EGPWS.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 ST03072ATInstallation of a Sandel ST3400 Terrain Awareness Warning SystemSTC ST10252SC-DAircraft ComplianceSTC ST10301SC-DInstallation of an executive cabin interior.STC SA02087CHInstallation of MT-Propeller model MTV-15-C/200-50 or MTV-15-B/210-58 constant speed propellerSTC SA02097CHInstallation of a McCauley Propeller Systems B3D32C414/82NDA-2 propeller with optional LORD engine mount isolators.STC SA620NEInstallation of a Pratt & Whitney Canada PT6A-27, PT6A-15AG or PT6A-34 engine.STC SR01745LAOne-time STC to install a hand control device for the anti-torque pedal control on Bell 47J-2A, serial number 3305.STC ST02068NYInstallation of a Universal Terrain Awareness Warning System (TAWS) to be done in accordance with Avionics Design Services Ltd. Master Drawing List MDL04110, Revision N/C, dated January 20, 2005, or later Transport Canada approved revision.STC ST02916AT-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 GIV-X, Serial Number 4005. This STC does not permit manufacturing of parts for multiple installations.STC ST03047AT-DInstallation of Airshow (Moving Map and In-Flight Information System), in accordance with Gulfstream Aerospace Corporation Index List GC41 5048001, Revision D, dated March 14, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement, GC41 504M001, Revision NC, dated March 22, 2005, or later FAA approved revision is required