Supplemental type certificates
49,117 STCs, most recently changed first. Search by what an STC changes, its holder or a model.
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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 ST01578CH-DInstallation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System in accordance with Standard Aero Master Data List 71-0735-002, Revision W , dated June 22, 2011 or later FAA approved revision.STC SA02383AKInstallation of offset single handle control yoke (left side, left offset and right side, right offset) with push-to-talk switch, in accordance with Trimmer Aviation, LLC, Drawing No. 2015101, Rev. A, dated May 29, 2011 or later FAA approved revision.STC SR02996NYThe installation of the Quick Release Heli-Utility-Basket is to be done in accordance with Dart Aerospace Ltd. Master Document List, MDL-D407-797, Revision A, dated January 20, 2011, approved by Transport Canada on January 20, 2011, or later Transport Canada approved revision.STC ST02382AKReduction / Limitation of passenger seats to nine (9), in accordance with Bighorn Airways, Inc., Document Number BIG-C-212-AFMS, Revision IR, dated June 15, 2011, or later FAA approved revisions.STC ST02994NYa. Fuselage and wing Fatigue Life Expended (FLE) based on Quest s usage profile and recorded flight data.
b. Fabrication and installation of the fuselage and wing identification placards in accordance with Quest Diagnostics document No.QDTBM-2010-007, Rev.A.
c. The aircraft must be maintained in accordance with Section 6 (Instructions for Continued Airworthiness) of the Maintenance Plan for Continued Airworthiness, QDTBM-2010-006, Rev.A and dated June 13, 2011.STC ST03922ATInstallation of Thales vertical speed / resolution advisory indicator (VSI/RA) in accordance with United Parcel Service Company Master Drawing List (MDL) No. AER10-3440-0013, Rev. A, Dated June 14, 2011, or later FAA approved revision.STC ST01700SE-DInstallation of an upper deck interior reconfiguration on Boeing Model 747-400 series aircraft in accordance with Jamco America, Inc. Master Drawing List (MDL) MDL-0001, Revision B, dated May 13, 2011, or later Federal Aviation Administration (FAA) approved revision.STC ST02995NYInstallation of 60 Hz Inverter and Miscellaneous Cabin Interior Items in accordance with Bombardier Aerospace Master Document List Number BAS31010033, Revision NC, dated September 12, 2007 or later Transport Canada approved revision. Refer to drawings listed in 350VA 60 Hz Inverter, and Misc Cabin Interior Items section of Master Document List Number BAS31010033, Revision NC, dated September 12, 2007 or later Transport Canada approved revision for additional installation requirements.STC ST00186WIInstallation of gallery and interior divider panels per J.T.B., Associates, Inc. Drawing TM 313211 stamped FAA Approved with a date of August 10, 1994.STC ST00991AT-DInstallation and operation of The Shaw Aero Devices, Inc. 331 & 332 Series Waste Drain and 580 Series Lavatory Rinse/Fill Values.STC ST01290AT-DInstallation and operation of a Shaw Aero Devices toilet rinse/fill check valve.STC SA2872WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301.STC SA01154CHInstall McCauley 3A32C406/82NDB-4 propeller on Beech Model S35, V35, V35A or V35B aircraft equipped with Teledyne Continental Motors Model TSIO-520-D, or TSIO-520-DB engines in accordance with D Shannon Products Installation Instructions DSP-101899A, Rev. IR, dated October 18, 1999, or later FAA Approved revisions.STC SA01548CHInstallation of Hartzell Model PHC-(C,L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Continental six-cylinder engines in accordance with D Shannon Products Installation Instructions DSP-043001A, Initial Release, dated April 30, 2001, or later FAA approved revisionSTC SA02192CHIncrease of maximum gross weight from 3600/3650 lb. to 4010 lb. for normal category operation.STC SA02356LAInstallation of Inflight Warning Systems Fan Vibration Monitor Unit, in accordance with FAA approved Inflight Warning Systems Master Data List (MDL) Drawing No. 13601, Rev. A, dated May 31, 2011, or later FAA approved revision.STC SA09145SCInstallation of vortex generators on wing upper surfaces in accordance with J.V.E., Inc. Drawing List JVE-501, Revision IR, dated 01/05/96, and Installation Manual JVE-0596, Revision IR, dated 01/05/96, or later FAA approved revisions.STC SA09222SCInstallation of B-1112 air/oil separator in accordance with J.V.E., Inc. Drawing List DL-8800, Revision 3, dated 03/14/96, Installation Manual BOS-AO1, Revision A, dated 01/22/96, or later FAA approved revisions.STC SA09255SCIncrease in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.STC SA09256SCIncrease in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.STC SA1-569Installation of Continental IO-470-J engine (fuel injection) and Hartzell BHC-92ZF-lDl / 8447 propeller in accordance with Stauffer drawing No. 7 dated May 2, 1961, and Stauffer Flight Manual Supplement No. 7, FAA approved May 5, 1961.STC SA1166GLInstallation of McCauley Model 3A32C406/82NDB-2 propeller in accordance with the appropriate installation instruction drawing as determined by Master Eligibility List No. PR0P406, Rev. A, dated February 5, 1987, or later FAA approved revision.STC SA168CHInstallation of Hartzell PHC-L3YF-1RF/F8468A-6R propeller in accordance with D Shannon Products installation instruction document DSP3533L3YF, no revision, dated 09/30/92, or later FAA Approved revisions.STC SA1691GLInstallation of McCauley Propeller Model 3A34C423/90DFA-10 in accordance with D Shannon Drawing No. 533420, Revision C, dated October 26, 1991, or later FAA Approved revision.STC SA197NWInstallation of Clark three- light gear position indicator system.STC SA203CHInstallation of Hartzell PHC-C3YF-1RF/F8468A(B,K)-6R propeller in accordance with D Shannon Products installation instruction drawing number C3YF93, no revision, dated 12/13/93, or later FAA Approved revisions.STC SA238GLInstallation of Continental I0-470-N engine and McCauley 2A36C23/84B-0 propeller in accordance with Stewart Gross Installation Instructions dated April 26, 1978.STC SA2858WEInstallation of right and/or left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB -1301.STC SA2870WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301 or later FAA approved revision.STC SA2871WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301.STC SA414CHReplace Beech lower cowling access panels with D'Shannon Products part numbers J1101-1 (left hand side)and J1101-2 (right hand side).STC SA4196SWInstallation of one piece windshield according to Blue Star Conversion One Piece Windshield Installation, Rev. 2, dated 3/28/80, or later FAA approved revision.STC SA450CHInstallation of Hartzell PHC-C3YF-1RF/F7691 propeller in accordance with D Shannon Installation Instruction Drawing No. DSP-769194, dated 2/21/94, or later FAA Approved revisions.STC SA525CH100-1b. increase in maximum gross weight with installation of Continental I0-550-B engine in accordance with D Shannon Products Installation Instruction 71-20-00, dated 10/20/88, or later FAA-approved revision; and installation of Cooling Air Baffles in accordance with D Shannon Products Installation Instruction DSP1M95-2, dated 6/1/95, FAA-approved 6/21/95 or later FAA-approved revision.STC SA619CHInstall McCaulley 3A32C406/82NDB-4 propeller on Beech A36TC aircraft in accordance with D Shannon Products installation instructions DSP-121895A, rev. 1, dated February 8, 1996, or later FAA Approved revision.STC SA632CEInstall wing leading edge fuel t anks.
Data required: FLOAIR Drawings 56001 Documents 1440
56002 Sheets 1 & 2 1450
56003 1460
56004
56005
56006 56008
56007 56009STC SA681CEInstallation: Wing leading edge fuel tanks
Data required: Floair Document 141-3.21.1 dated June 23, 1972, and approved Airplane Flight Manual Supplement, Floair Document 141-3.91 dated July 24, 1972.STC SA686CEInstallation of Continental IO-520-B engine derated to power shown in the appropriate Airplane Flight Manual Supplement and Hartzell HC-C3YF-1/8468A-8R (Low 10.0 .2, High 36.0 1.0 Blade Angle Stop at 30 inch Sta.) propeller or McCauley 2A36C23/84B-2 (Low 13.3 , High 29.7 Blade Angle Stop from Ref. Sta. 30) propeller in accordance with AeroStol drawing 3100B, Sheet 1, Rev. B, dated 11/15/75 and 3100, Sheet 2, dated 9/18/75, or later FAA approved revisions, for all of the above Beech model aircraft, except Model G33. For Model 33 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 2A36C23/84B-O (Low 13.3 , High 29.7 Blade Angle Stop, Ref. Sta. 30) propeller in accordance with D Shannon Products Drawing G3M2686BB, Rev. 1, dated 2/27/86 (5 sheets), or later FAA approved revisions.
For Model H35 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 3A32C406/82NDB-2 propeller in accordance with D Shannon Products Drawing H353A32C406BB Rev. 1, dated 11/25/86 (5 sheets), or later FAA approved revisions.STC SB02984CHReplace the Lindstrand Balloons Ltd Basket/Burner system and fuel tanks with the FireFly Balloons Basket Model 6072, S/N C007; the FireFly Balloons Burner Model T3-017, S/N 2666L and the FireFly Balloons Burner Model F1 Mirage, S/N 548; and FireFly Balloons fuel tanks, Part Number C6G001F, S/Ns 67844J, 69465J, 69586J, and 70385J, and Part Number C6G003I, S/Ns 67926J and 67936J. Replace the existing instruments with the Flytec Model Number 3040, S/N 11835/6837. The FireFly Balloons Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments as specified in the FAA Approved Balloon Flight Manual Supplement dated June 15, 2011.STC SB02985CHReplace Balony Kubicek Basket/Burner system and fuel tanks with the Aerostar International Basket Model CWS S/N 104; the Aerostar International Burner Model HP III Dual, S/N 3556; Aerostar International Model H-20 Fuel Tank, S/Ns 20197-013 and 20197-017. The Aerostar International Basket/Burner is installed via the standard Balony Kubicek carabiner (snaplink) attachments.STC SR01649LAInstallation of a camera view port in the floor of the passenger cabin, in accordance with FAA Approved Aspen Helicopters, Inc. Master Data List MDL040631, Revision A dated May 8, 2004, or later FAA Approved Revisions.STC ST02697CH-DInstallation of a Forward Vestibule with Crew Communications Area in accordance with Gulfstream Aerospace Index List GC521048003, Rev. A, dated October 25, 2010, or later FAA approved revision.STC ST04227AT-DInstallation of an Aircell ATG-5000 w/ WLAN in accordance with Gulfstream Aerospace Master Data List CE413028002, Rev. A, dated February 1, 2011, or later FAA approved revision.
FAA Approved Airplane Flight Manual Supplement CE41302M002, Rev. -, dated February 3, 2011, or later FAA approved revision is required.STC SA02134SEControl gap seals manufactured in accordance with the latest Federal Aviation Administration (FAA) approved revision of Cub Crafters Drawing RM0601, installed in accordance with the installation instructions listed in AML SA02134SE, and maintained in accordance with the maintenance manual supplement listed in AML SA02134SE.STC ST01399LAInstallation of Honeywell TCAS 2000/Dual Mode S ATC Transponder Systems. Limited to installation on Lockheed 1329-25, serial number 5213.STC ST02142LAInterior Modifications in accordance with BaySys Technologies, LLC Master Data List 8119-MDL, Revision D, dated June 19, 2008, or later FAA approved revision.STC ST02646NY-DInstallation of a Panasonic Avionics Corporation System 3000iSTC SA02789CEInstallation of a Bendix/King CAS-81 TCAS System. Data Required: (1) Jet Aviation Certification Drawing List No. AD910011, Revision F, dated March 11, 2011, (2) Jet Aviation Report No. 13-328M001, Revision F, FAA Approved Flight Manual Supplement for the Avions Marcel Dassault-Breguet Aviation Model Mystere-Falcon 50 Airplane, dated May 13, 2011, or later FAA approved revision of (1) or (2).STC ST00403WIInstallation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II) and Collins TDR-94D Mode S Transponder (Dual).
Data Required: (1) Jet Aviation Certification Drawing List No. AD 950011, Revision C, dated April 13, 2011, (2) Midcoast Aviation, Inc. Report No. 32-328M002, FAA Approved Flight Manual Supplement, dated February 7, 1996; or later FAA approved revisions to (1) or (2).STC ST10161SC-DReconfigure the interior cabin and install updated IFE products