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 SA00067MCEstablishment of a ground minimum control speed operating limitation in accordance with Airplane Flight Manual Supplement Document Number 0223-00-9007, Revision A, dated October 31, 2011, or later FAA approved revision.STC ST02204SEInstallation of a Thrane & Thrane Aero-HSD+ satellite communications (SATCOM) system per Master Data List document AM0254-DL02-00, Revision , dated October 13, 2011 or later FAA approved revision.STC ST02776NYModification of PATS Aircraft, LLC Auxiliary Fuel Tank SystemSTC ST02935NYa. Modification of PATS Aircraft, LLC Auxiliary Fuel Tank System to be in compliance to SFAR 88 requirements for Boeing 757-200 Series airplane in accordance with Master Drawing List QWT757901, Rev C, dated February 11, 2011.
b. The aircraft must be maintained in accordance with Instruction for Continued Airworthiness QWT757921 Rev B, dated January 3, 2011.
c. Quiet Wing Technologies, Inc. Airplane Flight Manual Supplement QWT757901-2J4, Revision Original, FAA approved
March 9, 2011, is also required for this modification.STC ST02945NYa. Modification of PATS Aircraft, LLC Auxiliary Fuel Tank System to be in compliance to SFAR 88 requirements for Bombardier, Inc CL-600-2B19 airplane in accordance with Master Drawing List QWTCL600101, Revision A, dated March 21, 2011.
b. The aircraft must be maintained in accordance with Instructions for Continued Airworthiness QWTCL600121 Revision B, dated March 24, 2011.
c. Quiet Wing Technologies, Inc. Airplane Flight Manual Supplement QWTCL6001001, Revision Original, FAA approved
March 28, 2011, is also required for this modification.STC ST03032NYInstallation of the Flap Actuator Heater SystemSTC SA00310BOModel DFC90, p/n 700-00170-002, loaded with Release 2 software (or later FAA approved release)
OR
Model DFC100, p/n 700-00170-003, loaded with Release 2 software (or later FAA approved release)
Avidyne Corporation Autopilot as a replacement for the S-TEC System 55X Autopilot, p/n 1192-( )-( ), in accordance with the Avidyne Corporation Master Document List, Document AVDFC-077, Rev 02, dated November 16, 2011, or later FAA-approved revisions.STC SR03027CHInstallation of Air Ambulance Unit in accordance with Ocean Air Master Data List, Report AC-BO105, Revision Original, Dated February 1st 2011 or later FAA Approved Revision.STC ST02107SE-DInstallation of an interior reconfiguration on Boeing Model 777-300 series aircraft in accordance with Jamco America, Inc. Master Drawing List (MDL) MDL1724-1, Revision B, dated November 3, 2011, or later Federal Aviation Administration (FAA) approved revision.STC SA00959WIInstallation of SPIRENT Systems Wichita Cabin Information Display System in Cessna Model 525 aircraft. Data required: (1) Spirent Systems Installation Manual, Publication Number 90006-003-011, Revision B, dated April 2, 2001; (2) Spirent Systems Wichita Drawing Number 90006-003-015, Revision IR, FAA Approved Airplane Flight Manual Supplement (AFMS), dated April 12, 2001; or later FAA Approved Revisions to (1) or (2).
or,
Installation of SPIRENT Systems Wichita Cabin AvVisor Plus Information Display System in Cessna Model 525 aircraft. Data required: (3) Spirent Systems Installation Manual, Publication Number 90007-003-011, Revision C, dated January 9, 2003; (4) Spirent Systems Wichita Drawing Number 90007-003-016, Revision IR, FAA Approved Airplane Flight Manual Supplement (AFMS), dated January 10, 2003; or later FAA Approved Revisions to (3) or (4).STC SA2274CEInstallation of B&D Instruments, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments, Inc. Drawing List No. 0530-010-001, Rev. H, dated August 20, 1987, or B&D Instruments, Inc. Installation Manual Part No. 0530-010-011, Rev. A, or later FAA Approved revision; and (2) copy of this certificate.STC SA2373CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-008, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.STC SA2375CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-011, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.STC SA2470CEInstallation of B&D Instruments & Avionics, Inc. Electronic Propeller Gear Box Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7330-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7330-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2471CEInstallation of B&D Instruments & Avionics, Inc. Electronic Engine Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7380-003-024, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7380-003-024, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2472CEInstallation of B&D Instruments & Avionics, Inc. Electronic Gas Generator Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7320-003-011, dated January 23, 1989, or later FAA Approved revision; for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7320-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (2) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7321-004-011 dated September 12, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2473CEInstallation of B&D Instruments & Avionics, Inc. Electronic Torque Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7300-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7300-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7301-003-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.STC SA2493CEInstallation of B&D Instruments & Avionics, Inc. Electronic Interturbine Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision A, dated March 13, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision D, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2494CEInstallation of B&D Instruments & Avionics, Inc. Electronic Propeller Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7310-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7310-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7311-004-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.STC SA2825CEInstallation of B&D Instruments & Avionics, Inc. Electronic N2 Gas Compressor Indicator. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 55006-003-011, Revision A, dated April 6, 1992, or later "FAA Approved" revision; and (2) copy of this certificate.STC SA2826CEInstallation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators.STC ST00084WIReplacement of the Exhaust Gas Temperature indicators with B&D Instruments Models 65006-003, 65006-004, 65006-005, 65006-006, 65006-007. Recording Exhaust Gas Temperature indictors in accordance with B&D Installation Manual 65006-003-011, Revision D dated November 19, 1996 or later FAA approved revision; and Flight Manual Supplement 65006-003-013 dated July 26, 1993, Flight Manual Supplement 65006-003-014 dated October 3, 1994, or Flight Manual Supplement 65006-003-015, 65006-003-16 or 65006-003-017 dated November 16, 1996.STC ST00483WIReplacement of the existing engine instruments with the Spirent Systems Wichita, Inc. Flat Panel Engine Instrument Display System (EIDS) Model 94002, in accordance with (1) Installation Data referenced on Continuation Sheet 2; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Continuation Sheet 2.STC ST00700WIInstallation of Penny & Giles Recording Exhaust-Gas Temperature Indicator 65009-004 EGT in accordance with: (1) Penny & Giles Aerospace, Inc. Recording EGT Model 65009 Installation Manual Document #65009-004-011, Revision -, dated May 1, 1998; and (2) Penny & Giles Aerospace, Inc. Airplane Flight Manual Supplement (AFMS) Drawing #65009-004-013, Revision "original", dated August 19, 1998; or later FAA Approved Revisions to (1) or (2).STC ST00759WIReplace existing engine instruments with the Penny & Giles Aerospace, Inc. Engine Instruments Display System (EIDS). Model 94002, in accordance with (1) Installation Data referenced on Continuation Sheet 2; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Continuation Sheet 2; or later FAA Approved Revisions to (1) or (2).
(see continuation sheet 2 of 2)STC SA03029CHInstallation of Honeywell Engine Model TPE-331-1-151A with a Hartzell HC-B3TN-5M/T10282N+4 model propeller in accordance Project Report Number JTC2010ST001, Revision NC, date March 3, 2011, and submitted previously FAA Approved data accomplished under Federal Aviation Administration (FAA) Field Approval process.STC SA08998SCInstallation of Pratt & Whitney Canada PT6A-42 engines.STC SB03028CHReplace the Lindstand Balloons Ltd Basket/Burner system and fuel tanks with the Cameron Balloons Basket Model CBUS754, S/N 9629, the Cameron Balloons Burner Model CB2075-2, S/N B6870-B6882, and the Cameron Balloons fuel tanks , P/N CBUS 1060, S/Ns 50066, 50099, and 50102, and Cameron Balloons fuel tank, P/N CB250, S/N 43549J. The Cameron Balloons Basket/Burner is installed is installed via the standard Lindstrand Balloons Ltd carabiner (snaplink) attachments.STC SA00428WIInstallation of McMauley D3A34C402/90DFA -2, -4, -6, -8, & -10, propellers and associated changesSTC SA02203SEInstallation of a Hartzell Propellers, Inc. model HC-C2YK-1BLF/FL7666A-4Q constant speed propeller in accordance with Installation Instructions Document No. 012-010 dated September 20, 2011.STC SR03028NYThe installation of a SkyTrac ISAT-200 Airborne Position/Data CommunicatorSTC ST02375LAInstallation of a main deck cargo container fire suppression system in accordance with Ventura Aerospace Inc. Master Data List VA-FSS-1002, Revision "E", dated September 13, 2011 or later FAA approved revision.STC SR03027NYInstallation of an External ITT and Torque Indicating SystemSTC ST03026NYInstallation of the Cockpit Door Hold Open LatchSTC ST10890SC-DAft RH Divan Installations in accordance with Data List Report No. F2EX-01038 Revision AG dated 14-Apr-2011, or later FAA approved revision.
FAA Approved AFM Supplement, Report 40709-1 dated April 14, 2011 or later FAA approved revision is required.
Instructions for Continue Airworthiness, Report ICA-F2EX-01038-501, revision Original, dated 21-Jan-2011 or later FAA approved revision is required.STC ST10981SC-DAvionics and Interior Installation in accordance with Data List Report No. F2EX-01040 Revision A dated 27-Oct-2011, or later FAA approved revision.
FAA Approved AFM Supplement, Report 37159-F2EX-D704 dated October 27, 2011 or later FAA approved revision is required.
Supplemental Maintenance Manual, Report SMM F2000EX-SN 227, revision A, dated August 30, 2011 or later FAA approved revision is required.
Supplemental Illustrated Part Catalog, Report SIPC F2000EX-SN 227, revision B, dated October 20, 2011 or later FAA approved revision is required.
Supplemental Wiring Diagram Manual, Report F2MB-001-D704, revision G, dated October 3, 2011 or later FAASTC SA02049AKFabrication and installation of Airglas Engineering Co., Inc. Model LTC18 cargo pod/bellSTC SA02388AKInstallation of Alaska Aircraft Products, LLC PA-12 Hot Rod MufflerSTC SB03031CHReplace Balony Kubicek Basket/Burner system and fuel tanks with the Aerostar International Basket Model RWSW AFX, S/N 128; the Aerostar International Burner Model HP III Dual, S/N 3867; Aerostar International Model V-18 Fuel Tank, S/N 99175 and 99177. The Aerostar International Basket/Burner is installed via the standard Balony Kubicek carabiner (snaplink) attachments.STC ST02608CHInstallation of a corporate interior including seats, bulkheads, tables, entertainment system, lighting system and lavatorySTC ST02650CHInstallation of a galley per Indianapolis Jet Center Drawing List DL5008-01, Rev. IR, dated October 17, 2008 or later FAA approved revision.STC SA5262NMInstallation of the Skyote Gap Flap System.STC SA5263NMInstallation of the Skyote Gap Flap System. (180 SERIES)STC ST471CHInstallation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II).STC SA00736DEThis Supplemental Type Certificate authorizes autopilot-coupled RNAV (GPS) approaches to LPV and LNAV/VNAV minima when there is a functioning Pilatus option radar altimeter installed and the aircraft verified to meet the requirements of Pilatus Business Aircraft Installation Instructions Document No. P25-486-007 Revision IR, dated August 15, 2011, FAA approved October 25, 2011, or later FAA approved revision.STC SA02331AKInstallation of a Secondary Forward Baggage Door Latch in accordance with Plane Miracles LLC Master Data List, MDL1125AK, Revision IR, dated January 6, 2009, or later FAA approved revision.STC SR01343LAInstallation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01343LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861345, Revision N/C, dated May 31, 2002, or later FAA approved revisions.STC SR09547RCInstallation of Dual TDR-94D/RTU-4200 Transponders with extended squitter (ADS-B) in accordance with PHI Master Document List No. PHI-S92-DL-0003, Rev. 4, dated September 10, 2011, or later FAA approved revision. The dual installation is further defined in PHI Top Drawing No. PHI-S92-60667-01, Rev. IR, dated April 8, 2009, or later FAA approved revision. Rotorcraft Flight Manual Supplement Number PHI-959-S92-RTU-001, dated May 29, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness PHI Document No. PHI-S92-ICA-0004, Rev. B, dated September 9, 2011, or later FAA accepted revision is requiredSTC SR09548RCInstallation of dual WAAS (Pilot/Copilot) Flight Management System (FMS) and single FMS configurations in accordance with PHI Master Document List No. PHI-S92-DL-0002, Rev. 8, dated October 10, 2011, or later FAA approved revision. The dual and single FMS configurations are further defined in PHI Top Drawing No. PHI-S92-60662, Rev. A, dated August 29, 2011, or later FAA approved revision. Rotorcraft Flight Manual Supplement Number PHI-959-S92-FMS-001B, Rev. 1, dated September 1, 2011, or later FAA approved revision is required for the dual
FMS installation. Rotorcraft Flight Manual Supplement Number PHI-959-S92-FMS-001A, dated August 18, 2009, or later FAA approved revision is required for the single FMS installation. Instructions for Continued Airworthiness PHI Document No. PHI-S92-ICA-0003, Rev. C, dated September 12, 2011, or later FAA accepted revision is required.STC SA5749NMInstallation of a galley in accordance with Showa Aircraft Industry Co., LTD. Master Drawing List 60210-000000, Revision G, dated March 10, 1993, or later FAA-approved revisions.