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 SA5467SWInstallation of dual camera port.STC ST01617WI-DONE ONLY STC; SN 5456: Installation of Interior Alteration. Data Required: (1) Duncan Aviation Inc., Document List No. 100930014, Revision A, dated December 20, 2010, (2) FAA Approved Airplane Flight Manual Supplement, Duncan Aviation Inc., Document No., 100907003, Revision A, dated December 20, 2010, or later FAA Approved Revisions to (1) or (2).STC ST01882SE-DInterior reconfiguration of Boeing Model 777-300ER series airplanes in accordance with Jamco America, Inc. Master Drawing List (MDL) No. MDL1269-1, Revision L, dated December 14, 2010, or later Federal Aviation Administration (FAA) approved revision.STC SR03847ATInstallation of APC Starter Generator on the Bell 206L-1, 206L-4 and 407 Series Helicopter in accordance with Certification Services Master Data List R24-AEV-001, Revision A, Dated March 07, 2010, or later FAA approved revision.STC SA00702ATInstallation of a Basic Type BAE-14/28 Model 2025 deployable air driven alternator system.STC SR00714DE-DInstallation of Public Address System in accordance with Master Drawing List, Air Methods Corporation Document Number 721-9040, revision IR dated 11/22/2010, or later FAA approved revisions.STC ST04222AT-DINSTALL AN AIRCELL ATG-5000 WITH WLANSTC SA02098SEInstallation of vortex generators on the wings and tail surfaces and strakes on the engine nacelles.STC SH1007SWModify tail rotor pitch change mechanism to add duplex bearing, (P/N 47-641-131-1) in place of single row bearing. Approved for Bell models 47D1, 47G, and 47G-2 with 47-640-044 tail rotor gear box assembly.STC SH1170SWInstallation of tail rotor gear box no. 47-640-065-31 and tail rotor hub and blade assembly no. 47-640-071-3. Eligible on Bell model 47G with Franklin 6V4200-C32, 6V335-A, or 6V350-A engines installed. STC SH479SW required.STC SH909SWInstallation of Franklin 6V-350-A engine, derated to 200 HP. Limited to installation on serial number 1355 ONLY.STC SH963SWInstallation of Bell Model 47G-2A-13-place wide cabin on the Bell Model 47G-5, retaining the 47G-5 instruments and pedestal. Limited to installation on serial number 7808 ONLY.STC SR01811SEInstallation of General Electric Model CT58-140-2 enginesSTC SA02874CH-DInstallation of Hartzell HC-E2YR-2BTF/FC7693F(B)+1 propellersSTC ST03900ATInstallation of Avionica, Inc. satLINK system to provide voice and data communications over the Iridium satellite network (SATCOM).STC ST02161SE-DInstallation of an interior reconfigurationSTC SA02376AKReplacement of tricycle landing gear with conventional (tail-wheel) landing gearSTC ST00145SEONE ONLY STC; S/N 24896: Interior reconfiguration involving galleys, lavatories, video installation and seats.STC ST02096SEONE ONLY, SN 49670: Installation of Olympic Aero Services Transient Suppression Devices on aircraft equipped with auxiliary fuel systemSTC ST02900CHInstallation of Rosemount Aerospace 8700E1-4 Series Electronic Flight Bag (EFB) SystemSTC ST01913LAInstallation of TopSeries I-4000 In-Flight Entertainment System.STC ST01486SE-DGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM).STC ST00055MCInstallation of Combat Systems Officer System.STC ST01614WI-DInstallation of Airfield Technology, Inc., (ATI) AT-950 Flight Inspection System (FIS) with a Crossbow Technology, Inc., Attitude Heading Reference System (AHRS). Data Required: (1) Duncan Aviation Inc., Document List No. 100325015, Revision A, dated December 03, 2010, (2) FAA Approved Airplane Flight Manual Supplement, Duncan Aviation Inc., Document No. 100219044, Revision A, dated December 03, 2010, or later FAA Approved Revisions to (1) or (2).STC ST01893SE-DInstallation of an interior reconfiguration on Boeing Model 777-200 series aircraft in accordance with Jamco America, Inc. Master Drawing List MDL1498-1, Revision B, dated December 3, 2010, or later Federal Aviation Administration (FAA) approved revision.STC ST02864NYInstallation of Universal Avionics 1408-00-1/-2 Solid State Data Transfer Unit in accordance with Field Aviation East Limited Master and Data List No. DDL-1198, Revision IR, dated October 21, 2009, or later Transport Canada approved revision.STC ST09702AC-D777-200 50J/226Y Reconfiguration, Aircraft 019 & 020 in accordance with Continental Airlines Master Drawing List 2500DA12085, Rev A, dated December 1, 2010 or later FAA approved revision.STC SA00855SEInstallation of BAS, Inc. duel belt shoulder harness with inertia reel in accordance with BAS Report 1002, dated April 1, 2000, or later FAA approved revision.STC SA01085SEInstallation of BAS, Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE, dated May 13, 2002, or later FAA approved revision.STC SA01256SEInstallation of BAS, Inc. shoulder harness with inertia reelSTC SA01370SEInstallation of BAS, Inc. Shoulder Harness in accordance with BAS, Inc. Drawing List, which includes Installation Instructions, and Instructions for Continued Airworthiness, listed on FAA AML SA01370SE, dated January 26, 2004, or later FAA approved revision.STC SA01643SEInstallation of BAS, Inc. shoulder harness with inertia reelSTC SA3812NMInstallation of a BAS tail pull handle in the aft fuselage.STC SA3813NMInstallation of a BAS tail pull handle in the aft fuselage.STC SA3814NMInstallation of BAS, Inc. tail pull handle in the aft fuselage.STC SA3815NMInstallation of BAS tail pull handle in the aft fuselage.STC SA3816NMInstallation of a BAS, Inc., tail pull handle in the aft fuselage.STC SA3851NMInstallation of a BAS tail pull handle in the aft fuselage.STC SA5658NMInstallation of a BAS, Inc. tail pull handle in the aft fuselage.STC ST02160SE-DInstallation of an interior reconfigurationSTC ST02775CHInstallation of Aircraft Passenger Cabin ModificationsSTC ST04220AT-DInstallation of a Broad Band Multi-link (BBML) System.STC SH5764NMIncrease in maximum ground idle speed.STC ST336CH-DInstallation of an AlliedSignal Avionics Mark VII Ground Proximity Warning System with Windshear.STC SE91WERemoval of General Electric 'EGT cable and conduit assembly,' P/N9037M17P03 or 9037M17P04, and replacement with Co-Operative Industries P/N 66615.STC ST01455SE-DUpper deck stowage bin and closet modification of 747-400 series airplanes in accordance with Jamco America, Inc. Master Drawing List IA-104MDL, Revision L, dated November 23, 2010, or later Federal Aviation Administration (FAA) approved revision.STC SR03895ATInstallation of a Lead Acid Battery as a replacement for the existing Nickel-Cadmium Battery.STC ST02548NYConfiguration A: Seasonal Bin Fixed Physical Provisions Only
Installation of seasonal bin fixed provisions in accordance with Voyageur Airways Limited Design Change Summary DCS 07-001, Rev N/C dated June 27, 2007 or later Transport Canada approved revisions.
Instructions for Continued Airworthiness are contained in Voyageur Airways Limited MMS 07-0001, Rev B, dated January 28, 2008 or later Transport Canada accepted revisions.
Configuration B: Seasonal Bin Installation
Installation of seasonal bin shall in accordance with Voyageur Airways Limited Design Change Summary DCS 07-001, Rev B dated October 16 2007 or later Transport Canada approved revisions.
Operation must be in accordance with Voyageur Airways Limited Flight Manual Supplement AFMS 07-0001, Rev A, dated May 1, 2008 or later Transport Canada approved revisions.
Instructions for Continued Airworthiness are contained in Voyageur Airways Limited MMS 07-0001, Rev B, dated January 28, 2008 or later Transport Canada accepted revisions.STC ST02562NYThe installation of Battery Powered Refuel System to be done in accordance with Voyageur Airways Limited Design Change Summary DCS 07-003, Rev. N/C, dated April 10, 2008, or later Transport Canada approved revision.STC ST02902CH-DInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS) Software Upgrade and Activation of Runway Awareness & Advisory System (RAAS).