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 SA01054LAModification for external aft belly radome, radar mounting assembly, and electrical power interface for Litton search radar p/n 10-36400-02.STC ST01617NYInstallation provision Delta Engineering sensor, bracket and wire harnesses for flight data recorder update per Delta Engineering Data List 0149-05128-2048 dtd 12/18/2002.STC ST02616ATInstallation of a Honeywell Iridium Satcom System per Millennium Avionics, LLC Master Drawing List MDL-MA-20455, Rev B, dtd 1/21/03 or later FAA approved revision.STC ST01325NY-DOperational approval of a Dual Honeywell NZ-2000 Flight Management System for GPS non-precision approaches.STC ST01362LA-DInstallation of 13-passenger cabin interior. (Approved for S/N 1489 ONLY.)STC ST10120SCInstallation of a game table.STC ST10121SCInstallation of a new galley.STC ST10122SCInstallation of a cabin bulkhead and door.STC ST10123SCInstallation of a forward left-hand wardrobe and self-contained potty.STC ST10124SCInstallation of a cabin seating configuration.STC SA02609ATInstallation of Enviro Systems Air Conditioner per Air Centers Cool Air Drawings AC-310-062299 dtd 7/24/99 or later FAA approved revision.STC SA2626CEInstallation of a two-place facing divan.STC SA2627CEInstallation of a two-place side facing divan.STC SA2628CEInstallation of a two-place side facing divan.STC ST01324NY-DInstallation of a cabin interior seating update. Limited to installation on serial number 089 ONLY.STC SR01618NYInstallation of a Fuel Drain Collector System.STC ST01423LAUse of High Velocity OXYFUEL (HVOF) Thermal Coating as specified in Southwest Aeroservice Master Data List SWA 32-300M or latest FAA approved revision in lieu of chrome plating for various top assembly landing gear parts.STC ST09966SCInstallation of a Reciruclating Shower in the Forward LavatorySTC SR01653NYInstallation of replacement seats per Amtech Aeronautical Limited Modification Data Summary MDS334201 latest Transport Canada approved revisionSTC ST01422LAInstallation of Am-Safe Inflatable Restraint System on SICMA 2304 series seats.STC SR00242DEInstallation of multipurpose cabin floor for use in an EMS environmentSTC ST02217AT-DInstallation of provisions for a Collins IDC-900.STC ST02611ATInstallation of a VHF transceiver and the replacement of control heads to meet the 8.33 KHz channel space frequencies in accordance with Aero Consulting Services Modification Data Summary C34000, Revision N/C, dated June 29, 1999, or later FAA approved revision. (This approval is limited to only the installation made in Boeing 757-23A Serial Number 25488.)STC SA01163SEInstallation of ARNAV Systems RCOM-100 Globalstar Satellite Telephone per ARNAV Systems, Inc., RCOM-100 Installation Guide, Part Number 570-8050BSTC SA5550NMInstallation of evacuation slide container.STC ST735SOInstallation of protective rigid cover over the tail cone emergency evacuation slide.STC ST00755LA-DInstallation of Gables Engineering ATC control panel part number G6990-51. Approved only for those aircraft equipped with STC ST00137AT.STC ST01003LA-DInstallation of Rockwell Collins 490S-1 HF antenna coupler as a replacement for Rockwell Collins CPL-920D HF antenna coupler.STC ST01259CH-DInstallation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System.STC ST01355CH-DInstallation of a MagnaStar C-2000 digital airborne telephone system. Aproved for serial number 408 ONLY.STC ST08995SCModification of existing dual HF communication system to add simultaneous HF rception mode.STC ST09101SCInstallation of VIP SELCAL system.STC SA980GL-DInstallation of a P/N M45-170093-501 or M45-170093-502 Master Warning Panel.STC ST01669AT-DInstallation of the Class 'E' Provisions, Environmental Control System, and Smoke Detection System on passenger to freighter conversion.STC ST01670AT-DInstallation of Main Deck and Lower Lobe Floor modification and the 9G Restraint System to freighter conversion.STC SA01135WIDesign change to modify Skylight Window Panel to use fitted window stripping for better weatherproofing, corrosion protection, and ease of installation and replacement.STC SR01584NYInstallation of a master mount and gyromaster model M400.STC ST01133WI-DInstallation of Emergency Lighting System for Interior Floor Plan 69-9.STC SB00096NYInstallation of Aerostat Envelopes Model W-175-4 replacement envelope.STC SB00601NYInstallation of Aerostat Envelopes model W-100-4 replacement envelope.STC SB01544NYInstallation of model W-100-6 replacement envelope.STC ST01314CH-DInstallation of provisions for future installation of Universal Avionics Terrain Avoidance Warning System (TAWS).STC ST01582NYInstallation of Thales Electronic Standby Instrument with Goodrich PS-855B Emergency Power Supply.STC SA131CHInstallation of Model M2000 and M3000H fixed skis.STC SA1627SOConversion of a military model C-131A to Civil Model 240-53 freighter with a Class B cargo compartment.STC ST02537AT-DInstallation of a Dual Trimble TA-12 Global Positioning System.STC ST10116SCInstallation of AVTECH Air Transport Selective Calling (ATSCALL) Decoder.STC SA02549ATModification of engine exhaust system for improved engine performance.STC SA09480AC-DInstallation of an L-3 Comm Model FlOOO Flight Data Recorder and a Universal Navigation Corporation Model CVR-30A Cockpit Voice Recorder.STC SA01161SEApproval of this change in type design applies to the airplane models listed above, only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.