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 SR00548DEInstallation of Emergency Medical System (EMS) and a Liquid Oxygen (LOX) system.STC ST00485WI-DModification of a single Collins AMS-850 Avionics Management System to a dual Collins AMS-5000 AMS system, modification of an APS-850 autopilot system to an APS-4000 APS, installation of a single or dual Collins GPS-4000 GPS, and modified PFD-MDF-PFD (3 tube) or PFD-MFD-MFD-PFD (4 tube) EFIS display. For model 400, serial number RJ-061 ONLY.STC ST01972CHInstallation of wiring provisions for Traffic/Terrain Collision Avoidance (TCAS) and Enhanced Mode S systems.STC ST02844ATManufacture of electrically powered window shades for the passenger cabin in accordance with Aerospace Technologies Group (ATG) Master Drawing List No. ATG- WS- 1204DL, Revision D, dated March 3, 2004, or later FAA approved revision. Installation of window shades in accordance with ATG Drawing No. ATG-IP-1204, dated March 3, 2004, or later FAA approved revision.STC SA01629LAInstallation of AM-Safe Inflatable Restraint System on pilot and co-pilot seats of the Zenair CH-2000STC SH390NWInstallation of an electronic weighing system, for monitoring cargo hook weight, in accordance with Measurement Systems International, Inc., Installation drawing No. D00327, Sheets 1 and 2, or Drawing D00473, Rev. E.STC SH46NWInstallation of an electronic weighing system, for monitoring cargo hook weight, in accordance with Measurement Systems International, Inc., Installation drawing No. D00409, Rev. A, or Drawing D00471, Rev. IR.STC SA00743SEInstallation of vortex generators on the wing leading edge, underside of the horizontal stabilizer, and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117, Revision IR, dated July 14, 1999, and Installation Instructions MA2118, Revision IR, dated September 21, 1999, or later FAA approved revisions to either of these documents.
NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthySTC SA00887SEInstallation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated
March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.STC SA01373NYInstallation of landing lights IAW Arrow Light Company Adaptation and Installation Instructions and drawing number 2002-A-1, Rev IR, dtd 7/10/01.STC ST01260LA-DInstallation of an Executive Interior.STC SA01415CHInstallation of camera provisions in fuselage floor cut-out. Responsible FAA office is Chicago ACO.STC SA1637WEInstallation of cargo door approximately 80 inches high by 144 inches long in left side of fuselage forebody.STC SA1754WEInstallation of cargo doors, cargo floor and other changes. (188A, 188C Aircraft SN 1070 and higher are eligible.)STC SA3408NMInstallation of an 'executive' interior in the cabin compartment, modification of the flight station, and installation of instrumentation and communications equipment. (L1011-385-3 S/N 193H, 1247 AND UP)STC SA4-1403Installation of a Lockheed Aircraft Service model 109C flight data recorder.STC SA5301NM-DInstallation of a satellite communication (SATCOM) system.STC SA5302NM-DReinforcement of Inertial Navigation System (INS) battery rack and installation of heavier batteries.STC SA5312NM-DInstallation of C & D Interiors video control center, P/N 8181001-101.STC SA5314NM-DModification and installation of Hughes-Avicom Video Display Unit Consoles, P/N 612630 and 612640.STC SA5315NM-DModification and installation of Hughes-Avicom video display unit consoles, P/N 612630 and 612640.STC SA707EARelocation of cabin window right-side from fuselage station 217-236 to fuselage station 333-352.STC SA708EAInstallation of opening in fuselage right hand for emergency exit between fuselage station 226 and fuselage station 253.4. Is approved only for its structural, electrical and mechanical provisions and can be incorporated with STC SA707EA and STC SA709EA.STC SA709EAInstallation of floor structure and miscellaneous modifications. Is approved only for its structural and electrical provisions and can be incorporated with STC SA707EA and SA708EA.STC ST02813ATRemoval of Cessna Cabin/Lavatory Fluorescent Lighting System and/or Cessna Reading Lights and the Installation of B/E Aerospace LED Indirect Lights and/or Reading Lights Assemblies in accordance with B/E Aerospace Master Drawing List BE-MDL-001 Rev. A, dated
9 February 2004 or later FAA approved revision.STC SR09290RC-DInstallation of horizontal tip position/anti-collision strobe lights.STC SA02827ATInstallation of a cargo restraint net and protective flooring in accordance with Zerotime Aviation, LLC Report No. 33126, dated April 18, 2004, or later FAA approved revision.STC ST02846ATOne time installation of the Honeywell EDZ-805 Electronic Flight Instrument (EFI) System on Boeing 727-212, serial number 21945, in accordance with Jossair Engineering Report 1452MD01, Revision D, dated April 21, 2004, Master Document List and Compliance Check List- Installation of a Honeywell EDZ-805 Electronic Flight Instrument (EFI) System.STC ST02847ATOne time installation of the Honeywell P880 Primus Radar System and LSZ-850 Lightning Strike Sensor System on Boeing 727-212, serial number 21945STC ST02848ATOne time installation of the Honeywell FMZ-2000 Flight Management System (FMS) on Boeing 727-212, serial number 21945.STC ST01507LA-DInstallation of 16-passenger cabin interior. Limited to installation on GV-SP serial number 5020 ONLY.STC ST01890NYInstallation of an AlliedSignal CAS-67A TCAS II System.STC ST02675ATInstallation of acoustical insulation blankets for interior noise reduction in accordance with engineering top-level drawing 53g2521522 Rev I/R dated 3/15/2003 and installation instructions document no. AIMS-INST-1 Rev I/R dated 4/16/2003 or later approved revision(s).STC SA8098NM-DInstallation of an R134a Air Conditioning System.STC SR09281RC-DInstallation of a Garmin Global Positioning System (GPS) 500.STC ST01399SEInstall two side facing divans and associated interior changesSTC ST01772NY-DInstallation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System. Limited to installation on 1124A, serial number 337 ONLY.STC ST01773NY-DInstallation of an L3 Communications F1000 Digital Flight Data Recorder. Limited to installation on 1124A, serial number 337 ONLY.STC SA01961CHInstall OFEK Holding Corporation camera provisions installed pursuant to STC SA01415CH or STC SA01962CH.STC SA01962CHInstallation of camera provisions in fuselage floor cut-out. Approved for installation serial number 31T-7820042 ONLY.STC SA298NEInstallation of Simmonds Precision Computerized Fuel Quantity Indicator System in accordance with Simmonds Precision Installation Drawing List, Report Numbers E-2447, Revision E; and E-2523(optional), no revision, or later FAA-approved revisions.STC SA365NEInstallation of Simmonds Precision computerized volumetric top-off units.STC ST02841ATInstallation of a lower pressure bulkhead penetration at FS 346.6 (Frame 15) and structural reinforcement in accordance with Kruse Aerospace Corporation (KAC) Drawing No. 200402, dated April 7, 2004, and DCN A1, dated April 17, 2004, or later FAA approved revision.STC ST09487AC-DInstallation of Emergency Locator Transmitter (ELT).STC SA2384NMInstallation of Pacific Propeller, Inc. 22D40/AG200-2 and 22D40/6533A-12 propellers, governors, and associated systems on Pratt & Whitney R-1340 series engines in accordance with FAA sealed Pacific Propeller, Inc. Installation Instructions No. 8002 and 8003, respectively.STC SR09404RCInstallation of single pilot IFR avionics in accordance with Metro Aviation, Inc. Master Drawing List, MDL 145M-150, Revision B, dated March 22, 2004, or later FAA approved revision.STC ST00898CHInstallation of a Honeywell enhanced gournd proximity warning system.STC ST01237WI-DInstallation of a Honeywell KGP 860 EGPWS (without Terrain Display) on Learjet Model 31/35/35A/36/36A aircraft in accordance with Learjet Master Document List BAS35015049, revision (A), dated April 14, 2004, FAA approved April 16, 2004, or later approved revision.STC ST01238WIReduced Vertical Separation Minimum (RVSM) group airworthiness approval.STC ST09486AC-DInstallation of a Microwave Scanning Beam Landing System (MSBLS).