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 ST10383SCInstallation of four different interior configuration options in accordance with DRB Aviation Consultants, Inc., Master Data List DL1150M01, Revision C, dated February 16, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. 1150R25C02, Revision IR, dated February 16, 2005, or later FAA approved revision is required.STC SA4381NMInstallation of Cockpit Sun Visor.STC ST03041ATThis is an installation for a Honeywell ARINC 717 Flight Data Acquisition Management System in accordance with General Aerospace Master Drawing List No. GA67-DFDR-MDL, Revision A, dated October 1, 2004, or later FAA approved revisions.STC ST03042ATHoneywell Aircraft Communication Addressing and Reporting Systems (ACARS).STC SA01698LAInstallation of interior sidewall/armrest panels per drawing DT1-1-02, Revision B, dated December 6, 2004, and later FAA approved revisions as listed on AML No. SA01698LA.STC SE01805NYInstallation of Fuel Nozzle Adapters using studs and nuts.STC ST00211BOInstallation of Aircell ST 3120 Satellite Transceiver System in accordance with BBAS Master Document List BAS63017004, Revision A, dated February 8, 2005, or later FAA approved revision.STC ST01509SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-MU-0413, Rev. NEW, dated February 4, 2005 or latest FAA approved revision.STC ST10297SC-DS/N 103 ONLY: Installation of an executive cabin interior.STC ST10380SCThe right hand #1 & #2, and left hand #2, #3, #7 & #8 low back wide seats with hidden extendable headrests will be replaced with high back wide seats with exposed flex wing style extendable headrestsSTC SA2505NMInstallation of Pheromone aerial application system. (AT-400A RESTRICTED CATEGORY)STC SA4428NMInstallation of Schweizer Phermone aerial application system model No. P.A.A.S. 82.STC ST01714LA-DInstallation of a Honeywell MST-67A Transponder Upgrade for Elementary Surveillance Mode S Transponders (Flight ID).STC SR00576DEInstallation of a Roll-on Littler System.STC SR02057NYUpgrade of the S6135-20600 series main gearbox by replacing input free-wheeling units in accordance with Carson drawing. IFWU INSTL Carson S-61 No. CHI-R-001, no revision, dated 12-15-04 and Carson Installation Instructions Report CHI-R-INSTALL, no revision, dated 12-14-04.STC SR02055NYInstallation of Fuel Purge Canister to be done in accordance with Transport Canada approved DART Aerospace Ltd. Installation Instructions, IIN-D412-706, Revision A, dated November 30, 2004, or later Transport Canada approved revision.STC SR02056NYInstallation of Helicopter Performance Monitoring System is to be done in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332101, Revision 1, dated July 25, 2003, or later Transport Canada approved revision. Audio option is to be installed in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332102, dated April 2, 2003, or later Transport Canada approved revisions.STC ST02054NYInstallation of Fin-Cap Camera System to be completed in accordance with Aero Consulting Services Ltd. Modification Data Summary Number E181000, Revision N/C, or later Transport Canada approved revision.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA01981NYInstallation of a Universal Avionics Terrain Awareness Warning System (TAWS).STC ST416CH-DInstallation of a Honeywell Ground Proximity Warning System (GPWS) or Enhanced Ground Proximity Warning System (EGPWS).STC ST01506SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-BJ400-0412 , Rev. NEW, dated January 28, 2005, or later FAA approved revisions.STC SA10351SCInstallation of decorative fiberglass fairing in accordance with Texas Skyways, Inc. Master Drawing No. TSFG-100-1, dated November 18, 2004, or later FAA approved revisions.STC SA5810NMInstallation of Flite-Tronics static inverter model No. PC-3Y-500.STC SH8801SW-DFabrication and installation of Simplex Model 301 fire attack system.STC ST01496SECockpit Sun Visor installation in accordance with Federal Aviation Administration (FAA) approved Rosen Sunvisor Systems Drawing List 1570000-DL, Revision E, dated
December 28, 2004, or later FAA approved revision.STC ST01505SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Hawker Siddeley DH.125 Series 400A, Serial Number NA742 only. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM).STC ST02045CH-DInstallation of an Aft Lavatory with shower.STC ST10379SCInstallation of a Universal Avionics Systems Multi-Function Display.STC ST10377SCInstallation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) upgrade.STC ST10378SCInstallation of a Universal Avionics Systems Multi-Function Display.STC ST01502SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Dassault Mystere-Falcon 20-D5, Serial Number 202 only. Non-Group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM).STC ST01740LAInstallation of ACSS T2CASSTC ST02053NYInterior installation in accordance with Transport Canada approved Cascade Engineering Order 3410 Rev. Nil, dated January 13, 2005, or later Transport Canada approved revisions.STC SA01301WIInstallation of Jacobs R-755B2 or R-755B2M engine modified for fuel injection in accordance with STC SE01288WI, J.P. Instruments Fuel Flow meter in accordance with STC SA00432SE, and electric fuel boost pump. Data required: (1) Radial Engines Master Drawing List Report REL1003-13, Revision (IR), dated October 4, 2004, (2) Radial Engines Limited Instruction for Continued Airworthiness Report REL1003-12, Revision (IR), dated October 4, 2004, and (3) FAA Approved Airplane Flight Manual Supplement REL1003-5, Revision (IR), dated January 21, 2005 or later FAA Approved revisions to (1), (2), or (3).STC SA02078CHInstallation of a Hartzell Propeller Inc. 75 diameter three-blade propeller model (P)HC-C3YF-1RF/F7392 with A-2295-1(P) spinner or model (P)HC-G3YF-1RF/F7392 with C-4582-(P) spinner on a Cessna R172K (Hawk XP) Landplane aircraftSTC ST01500SEDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Raytheon Model HS125-700A Serial No. NA0322. Divian and PSU assembly installation.STC ST01501SEInstallation of Air Traffic Control Mode S Transponders with Elementary/Enhanced Surveillance in Boeing 767-200 airplanes in accordance with Northwest Aerospace Technologies, Inc. (NAT) Master Drawing List N0221-D10, Revision A, dated December 16, 2004, or later Federal Aviation Administration (FAA) approved revisions.STC SA01175WIInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS).STC SA01176WIInstallation of Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS-II).STC ST01128CH-DInstallation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system.STC ST01382SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM). Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 31, Serial Numbers 033, 033A, 033C, and 033D only.STC ST01498SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 55, Serial Number 085 only.STC ST01707LAInstallation of ACSS T2CASSTC ST10294SC-DInstallation of cockpit center pedestal extension.STC ST10295SC-DS/Ns 52 and up ONLY: Installation of 3rd Collins FMS 6100 Flight Management System.STC ST10296SC-DS/N 102 ONLY: Installation of an executive cabin interior.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.STC ST00795ATApproval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only).STC ST01043ATApproval of increased operating weights.