Supplemental type certificates
49,120 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 ST00933SEThis approval is limited to the Sabreliner 265-65, Serial Number 465-74. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-SL65-0101, Revision "New," dated June 14, 2001.STC ST09939SCPermanent change in seating capacity from a maximum of 10 passenger to a maximum of 9 passengers. Approval limited to Serial number 13 ONLY.STC SA7311SW-DInstallation of the Honeywell traffic alert and collision avoidance system(TCAS).STC SR09320RCInstallation of passenger sliding door kit.STC SA09511AC-DInstallation of S-TEC System 20/30 single and two-axis automatic flight guidance systems, model ST-888-20/30.STC ST09887SCInstallation of a dual IS&S air data system consisting of electric altimeters and air data computers.STC SA09470SCInstallation of Starter Indicator light system.STC ST01104LA-DInstallation of 15-passenger cabin interior. Approved for G-IV serial number 1024 ONLY.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC ST00395ATInstallation of a first class and 175-tourist class seating configuration using Aero Design Services master drawing list AB93-1089, Rev A, dtd 12/15/93, or later FAA approved revision. FAA approved AFM Supplement dtd 12/15/93 is a required part of this STC only when the airplane is equipped with alternate (dual) maximum operating airspeed capability (350/390 KIAS).STC ST00974NYInstallation of Claircom Air Terminal systems.STC ST00989CHInstallation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCASII).STC ST01061LAInstallation of Custom Interface Units between existing Litton LTN-92 Inertial Navigation System (INS), and Performance Management System (PMS).STC ST01182CH-DInstallation of a potable water and drain system.STC ST01400LAInstallation of Universal Avionics Terrain Awareness and Warning System (TAWS) in accordance with FAA Approved JWT Aircraft Holdings Master Drawing List Document JWT-5213-001, Revision No. A , dated September 15, 2002, or later FAA approved revision. FAA Approved Flight Manual Supplement, Document NO. JWT-5213-100, revision IR , dated October 21, 2002, or later FAA approved revision.STC SA3394WEReplacement of cargo barrier net installed per STC SA1467SW with a rigid cargo barrier partition.STC SA3953NMInstallation of thru access buckles in barrier net assembly, Air Cargo Equipment Corporation p/n 43275-102.STC SA4818NMInstallation of through access buckles in Barrier Net Assembly, Air Cargo Equipment Corporation p/n 43275-103.STC SR01360NYInstallation of particle separator (with or without Bell Snow Deflector Kit). Installation of STC SH5695SW including FMS is a prerequisite to this particular separator installation.STC ST01103LA-DInstallation of 17-passenger cabin interior. Approved for GV serial number 614 ONLY.STC ST02224ATManufacture of a Sterling Beverage System (SBS) portable beverage dispensing system, P/N 12-0001, in accordancd with SBS, Inc., Master Drawing List Report No. 20001, dtd 6/30/00, or later FAA approved revision. Aircraft installation in accordance with SBS Drawing No. 12012, "Galley Interface Criteria," dtd 11/14/00, or later FAA approved revision. Model applicability listed on AML No. ST02224AT is a required part of this STC.STC SA00243SEGross weight increase as modified per STC SA5691NM.STC SA00692SEReplacement of certain BF Goodrich pneumatic deicer bootsSTC SA00694SEReplacement of certain BF Goodrich pneumatic deicer boots.STC SA00930SEInstallation of vortex generators on the wing and flap surfaces in accordance with Drawing Package MA2153, Revision IR, dated January 26, 2001, and Installation Manual MA2154, Revision IR, dated May 29, 2001, or later FAA approved revision of either of these documents.STC ST01359NYInstalation of Air Canada 'Tenzing' E-Mail file server. For model aircraft Boeing 767-233.STC ST02177AKReduction/limitation of passenger seats to nine (9) or fewer and installation of a cargo net restraint system using Flight Alaska Drawing No. FA-C212-CC-01, original issue dtd 6/5/01, or later FAA approved revision.STC SA00425DEInstallation of model FB-02 'Fixed Arm' Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System.STC SA00426DEInstallation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.STC SA09453AC-DInstallation of S-TEC System 20/30 single and two-axis automatic flight guidance systems, model ST-876-20/30.STC SA6061NMInstallation of electrothermal upper wing anti-ice system.STC SH2603SOModify cabin floor to add six inspection holes.STC SR00877AT-DInstallation and operation of a Honeywell AA-300 radio altimeter system.STC SR00880AT-DInstallation and operation of an AlliedSignal KTU-709 TACAN System.STC ST00946WI-DInstallation of Bose Noise Cancelling Headsets into the cockpitSTC SA00453DEInstallation of Oilamatic preoiler system using FAA approved drawing list no. STEA400, Initial release, dtd 6/11/01 or later FAA approved revision.STC SA09009AC-DInstallation of S-TEC System 55/55X two axis autmatic flight guidance system, Model ST-588STC ST01096CH-DProvisions only for an AlliedSignal Mark VII Enhanced Ground Proximity Warning System using -208-208 software. Approved only for serial number 058.STC ST01358NYInstallation of Matsushita Avionics System Corporation replacement PVSCU for MPES MK II Video Entertainment System.STC ST00452DEReconfigure aircraft to a maximum seating of 19 passengers.STC ST02330ATInstallation of flame resistant barrier over metalized mylar thermo-acoustic insulation blankets IAW the Controlled Documents defined in Delta Engineering Report 9-76452-20, Rev B, dtd 6/6/01, or later FAA approved revision.STC SA00451DEInstallation of auto ignition system.STC SR00512NYInstallation of Heli-Rappel.STC SR00513NYInstallation of HeliRappel.STC ST01459CH-DInstallation of Honeywell YG1779 Inertial Reference Systems.STC ST01474CHInstallation of Rosemount Aerospace model 1833D pressure transducers.STC SR00511NYInstallation of Heli-Rappel.STC ST00116SEIncrease in the maximum taxi and flight weights up to 197,700 and196,000 lbs.STC ST00117SEFor operation up to 197,700 lb maximum taxi weight, Increase in the maximum zero fuel weight to 155,000 lbs and increase in the maximum landing weight up to 164,000 lbsSTC ST00922SEThis approval is limited to the Hawker 125-700, Serial Number NA0334. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-H700-0016, Rev. "NEW," dated April 25, 2001.