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"
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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 ST02992NYInstallation of a dual CMA-1100, Class II Electronic Flight Bag (EFB) in accordance with Avionics Design Services Ltd Master Drawing List document Number MDL09134, Revision C, approved April 14, 2010 or later Transport Canada accepted revision.STC ST03004NYInstallation of new MIL-C-5015 connectors at the wing to fuselage interface must be in accordance with Kelowna Flightcraft Ltd.Master Drawing List K116-00002 Revision NC, dated March 20, 2009 or later Transport Canada approved revision.STC SB03003CHReplace the Lindstrand Balloons Ltd Basket/Burner system with the Aerostar International Basket, Part Number 51620, S/N CWS-3070, and the Aerostar International Burner, Part Number 52350, S/N HP3D-3290. Replace the Lindstrand Balloons Ltd fuel tanks with the Aerostar International Model V-15 Fuel Tanks, Part Number 51977, S/Ns 5091, 5103, and 5118. The Aerostar International Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments.STC ST00462LAModification of the engine exhaust system.STC SA1-368Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company s Manual SFE-35(III) dated July 15, 1959, Tip Tank Installation, Type III Kit, utilizing parts listed on Bamber Wing Tanks Type III Kit Contents dated July 15, 1959.
This wing tip tank installation may be used in combination with either the wing auxiliary tanks or a baggage auxiliary tank, but not when both are installed. Complete installed weight empty is 23.7 lb. at 89.1 inches. The CG of the tip fuel is 87.0 inches.STC SA1-460: Installation of auxiliary wing tip fuel tanks in accordance with Drawing Number RB1-001B and Installation Instructions number RB-1, Revision of April 1, 1960.
This wing tip tank installation is acceptable with either the baggage auxiliary tanks, or the wing auxiliary tanks. However, it is not acceptable with both auxiliary installations incorporated simultaneously.STC SA144EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20, 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15, 1964 is required.STC SA181EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing tip fuel tanks (ref STC SA3OEA, Configuration 2 or 3) and Type II or III Kit transfer fuel system. This system eligible with Beech 20 gal wing aux. tanks or baggage compartment tanks, but not both. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. C dated February 15, 1964 is required.STC SA2335WEInstallation of one-piece windshield and relocation of compass.STC SA23EAInstallation of Third Cabin Window on both sides of Fuselage in accordance with Glenn Floyd Stauffer Drawing Nos. 42601, Revision A dated 31 May 1962 and 42602, Revision A dated 13 June 1962.STC SA2653SWInstallation of Instrument Panel in accordance with 1998-54 Installation Manual and Drawings 1998A200, 1998A300, 1998A400, and 1999 all dated July 1, 1977; Battery Box Kit per 1998-84 Installation Manual and Drawing 2000 dated July 1, 1977; Radio Cooling Kit per 1998-86 Installation Manual and Drawing 2002 each dated July 1, 1977.STC SA2771WEInstallation of Long Fiberglass tailcone to replace the short factory installed tailcone in accordance with FAA Sealed N.E. Coote Tool and Machine Drawing List Report No. 1 dated September 2, 1970.STC SA28EAInstallation of 12-gallon fiberglass wing tip fuel tanks.STC SA2CEInstallation of Doyn Model 1600 Dorsal Fin per Doyn Drawing No. 1600, Revision A, dated January 5, 1962.STC SA3-333Installation of Doyn fiberglass wheel fairings.STC SA3-363Installation of Doyn Fiberglass Wheel Fairings in accordance with Doyn Drawingg No. 1300 and Doyn Process Specification for Fiberglass Parts No. PS-100.STC SA3-690Installation of Doyn Kit No. 1400 Swept-Tail Assembly per Doyn Drawing No. 1400, Revision B, dated August 18, 1961.STC SA3-691Installation of Doyn swept-tail assembly kit 1400.STC SA30EAInstallation of 13.5 gallon fiber-glass wing tip tank assembly.STC SA808SOInstallation of Beryl D Shannon Aviation Specialists, Inc., Fiberglass tip tanks (15 gallons each) and fuel transfer system in accordance with Beryl D Shannon Aviation Specialists, Inc., Installation Kit Drawing KB1401, Rev E, dated May 19, 1977, or later FAA approved revisions. Drawing KB1401 Revision F, dated April 12, 1979, includes optional wing-tip anti-collision light installation. This STC requires operation in the Normal Category.STC SA891SORemove existing windshield and install single piece windshield.STC SA930SOInstallation of Beech Aircraft wing tip assemblies in accordance with Beryl D Shannon Aviation Specialties, Inc., Drawing B1990, dated December 15, 1976, or later FAA approved revision.STC SH261WEInstallation of an external load attachment mechanism in accordance with FAA Approved USDA Forest Service Master Drawing List and Rotorcraft Flight Manual Supplements, per Approved Model List SH261WE, and all subsequent FAA approved revisions to these documents.STC SH4547NMInstallation of a fixture for attachment of rappelling ropes under rear seat in accordance with FAA approved STC Data Package Master Drawing List , MTDC-951, Revision B, dated 10/7/97, and Rotorcraft Flight Manual Supplement for Bell Model 206B/L-1/L-3/L-4 and Model 407 with Bell 206/407 Series Helicopter Rappelling Kit , dated 11/26/97, or later FAA approved revisions.STC SR00123LA-D: Installation of External Load Attaching Means in accordance with Heli-Support, Inc. Master Index List No. 121-401, Revision A, dated September 20, 2001, or later approved revision. Rotorcraft Flight Manual Supplement No. 121-121 requested for this installation is listed on the approved Master Document List.STC SR00125LA-DInstallation of Internal Load Attaching Means (ILAM) in accordance with Heli-Support, Inc. Master Document List (MDL) No. 123-000, Revision C, dated April 12, 2002, or later FAA approved revision. Rotorcraft Flight Manual Supplement No. 123-121, Revision A, dated April 12, 2002, or later FAA approved revisions required as part of these modifications.STC SR03008NYInstallation of a Check Engine Instruments Audio Alert System in accordance with Skye Avionics Ltd., Master Drawing List AER-MDL-034, Revision NC, dated May 02, 2011, Transport Canada approved May 02, 2011, or later Transport Canada approved revision.STC SB03001CHReplace the Thunder and Colt Basket with the Ultramagic Basket Model C-6, S/N C6/85, using the existing standard Cameron Balloons US carabiner attachments.STC ST01777CHInstallation of an Innovative Solutions & Support Duplex Altimetry System.STC ST02822CH-DInstallation of an Auxiliary Fuel Tank System in accordance with Standard Aero Master Data List 09-025-MDL001, Revision (M), dated May 27, 2011 or later FAA approved revision.STC ST02993CHInstallation of Universal Avionics Systems, EFI-890R, UNS1Lw, ASU, SSDTU, and RCU, Cobham Audio Control Panels, L3 Communications ESIS, WSI AV-350 and Astro-Med. Printer in accordance with AMES, Inc. Master Data List, Report No. 46220MDL01, Revision E, dated August 09, 2011, or later FAA approved revision.STC ST10480SC-DInterior reconfiguration, new lavatories and In Flight Entertainment Equipment upgrade in accordance with Master Data List, F1378-MDL, Revision D, 19 January 2010, or later ODA-700094-SW approved revision and Airplane Flight Manual Supplement, Document Number F1378-AFMS, Revision B, dated 19 January 2010, or later ODA-700094-SW approved revision.STC SR02298LAInstallation of Amfuel S92 Internal Auxiliary Fuel System Completion Kit P/N 508617-2.STC ST01640WI-DInstallation of a 16 Passenger Cabin Configuration. Data Required: (1) Duncan Aviation Inc., Document List No. 110310010, Revision A, dated August 10, 2011, or later FAA Approved Revisions.STC ST02138SEInstallation of an electronic Remote Access System (RAS) on cockpit security doors, in accordance with Cascade Aviation Services Inc. Master Drawing List 07CAS442-MDL, Revision D, dated October 3, 2011, or later Federal Aviation Administration (FAA) approved revision.STC ST02049CH-DInstallation of the Securaplane Security System in accordance with Gulfstream Aerospace Corporation Master Drawing List GC514566000, Rev. G dated January 28, 2010, or later FAA Approved revision.STC ST02581CH-DInstallation of a Forward Vestibule with Flight Crew Sleeping FacilitySTC ST04203AT-DInstallation of Provisions for Dual Electronic Flight BagsSTC SA00945SEInstallation of a Ladder Bracket in accordance with Western Aircraft Drawing 00-G2295-1, Revision B, dated June 26, 2001 or later FAA approved revision.STC SA02183LAInstallation of Door Gas Springs in accordance with FAA approved Master Drawing List FIV-1000 Revision B dated March 13, 2010 or later FAA approved revision.STC ST01994SEInstallation of a lower lobe crew rest on Boeing Model 767-400ER series airplanesSTC SA01361SEInstallation of a Honeywell TPE331-10, -10U, -10UF, -10UG, -10UGR, -10UR engine in combination with Hartzell Propeller Model HC-B4TN-5NL/LT10890N, or HC-B4TN-5PL/LT10890N, or Honeywell TPE331-11U or -11UA engine in combination with a Hartzell HC-B5MP-5BL/LM11692N propeller.STC SH1919NMFabrication and installation of P/N L8500A-1 or L8500R-1 left ski and P/N L8500A-2 or L8500R-2 right ski.STC ST04235AT-DInstallation of an Executive Completion in accordance with Gulfstream Aerospace Index List GC422048005, Rev. -, dated April 18, 2011, or later FAA approved revision.
FAA Approved Airplane Flight Manual Supplement GC42204M046, Rev. -, dated April 18, 2011 or later FAA approved revision is required.STC ST01822AT-DInstallation of an APU Fire Bottle in accordance with Gulfstream Aerospace Corporation Index List GC514428001 Rev L, dated July 31, 2011 or later FAA approved revision.
FAA accepted Airplane Flight Manual Supplement, GC51442M001, dated April 8, 1999 or later FAA approved revision is required for fully operational configurations (non-spare). For the model GV, Instructions for Continued Airworthiness, GC51442A001, Revision C, dated September 28, 2010 or later FAA accepted revision is required, and must be made available to the operator at the time of installation. For the model GV-SP, Instructions for Continued Airworthiness, CE52442A000, Revision A, dated October 04, 2010 or later FAA accepted revision is required, and must be made available to the operator at the time of installation.STC SR02335AKInstallation of two or three tank fuel quantity indicating systems when installedSTC SR02336AKInstallation of an Integrated Cockpit Display System (ICDS) with an Attitude and Heading Reference System (AHRS) for Dual Pilot Instrument Flight Rules Category A and B operation in accordance with Vector Aerospace Helicopter Services Inc. Master Drawing List , HP 61-34-33-105, Revision A, dated February 28, 2011, or later FAA approved revision.STC ST02999CHModification of an Executive Interior Arrangement including Cabin Double Seats, Divans, Oxygen System, Emergency Lighting, and Emergency Equipment in accordance with Jet Aviation Master Data List 05-299G001 Revision D, dated July 22, 2011 and FAA Approved Jet Aviation Airplane Flight Manual Supplement 05-169M001, Revision NC, dated July 29, 2011, or later FAA approved revisions.STC SB03002CHReplace the Lindstrand Balloons Ltd Basket/Burner system with the Aerostar International Basket, Part Number 51620, S/N CWS-3051, and the Aerostar International Burner, Part Number 52350, S/N HP3D-3013. Replace the Lindstrand Balloons Ltd fuel tanks with the Aerostar International Model H-20 Fuel Tanks, Part Number 07752, S/N 135, and Model V-15 Fuel Tanks, Part Number 51977, S/N 3155. The Aerostar International Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments.STC ST00146BOInstallation of a Goodrich analog Transient Suppression Device (ATSD)