Supplemental type certificates
49,109 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 SA01454CHInstallation of Butterfield Industries Oil Residue Collection System, kit Part Number BI 8030-1STC SA01596SEInstallation of Butterfield Industries Oil Residue Collection System, kit P/N BI 3401-1.STC SA01800CHInstallation of Butterfield Industries Oil Residue Collection System, kit Part Number BI 2001-1STC SA02215SEFabrication of Inspection Panel Kit BI 9501-001STC SA02473SEInstallation of Raisbeck/Hartzell Swept Blade Turbofan PropellersSTC SA02559SEInstallation of Raisbeck/Hartzell Five-Blade Swept Turbofan PropellersSTC SA02620SEInstallation of Butterfield Industries Air/Oil Separator System, kit Part Number BI 8055-1STC SA1668NMInstallation of new main landing gear doorsSTC SA1783NMInstall Mark VI system.STC SA2116NMInstallation of Raisbeck fully enclosed main landing gear doorsSTC SA2133NMInstallation of fully enclosed main landing gear doorsSTC SA2623NMInstallation of fully enclosed main landing gear door system and associated actuation mechanismSTC SA2905NMInstallation of Butterfield Industries Flow Through Anti-Ice Kit Part Number BI 1001-1STC SA2939NMInstallation of nacelle overwing storage lockers and lower flap fairing.STC SA3366NMInstallation of the Ram Air Recovery System.STC SA3532NMInstallation of Hartzell/Raisbeck Quiet Turbofan Propeller System. Suitable for DHC-6-300 airplanes with PT6A-27 engines.STC SA3591NMInstallation of lower aft fuselage strakes.STC SA3593NMInstallation of Raisbeck/Hartzell Quiet Turbofan Propellers or Swept Turbofan Propellers, and optional Increased Gross WeightSTC SA3683NMInstallation of exhaust stack fairings.STC SA3819NMInstallation of nacelle overwing stowage lockers and lower flap fairing.STC SA4010NMInstallation of lower aft fuselage strakes.STC SA4130NMInstallation of lower aft fuselage strakes.STC SA4131NMInstallation of Hartzell/Raisbeck Quiet Turbofan PropellerSTC SA4362NMInstallation of Butterfield Industries Oil Residue Collection System Kit Part Number BI 1011-1STC SA4733NMInstallation of lower aft fuselage strakes.STC SA4734NMInstallation of nacelle overwing storage lockers and lower flap fairing.STC SA4940NMInstall engine fluids collection tank.STC SA4944NMInstallation of fully enclosed main landing gear door system for high-flotation-gear-equipped aircraftSTC SA4952NMInstallation of main landing gear door system for high flotation gear equipped aircraft.STC SA5151NMInstallation of dual aft body strakes.STC SA5152NMInstallation of nacelle wing lockers.STC SA5661NMInstallation of turbofan propellers.STC ST00179SEInstallation of an aft fuselage stowage locker.STC ST00352SEInstallation of an aft fuselage stowage locker.STC ST00399SEThe above boeing model which has incorporated Raisbeck Commercial Air Group Inc Master Drawing List 96B-1001, Revision D, dated September 2, 1997, or later FAA approved revision, complies iwth FAR Part 36, Stage 3 noise limits.STC ST00448SEThe above Boeing model which has incorporated Raisbeck Commercial Air Group, Inc, Master Drawing List 97B-7001, Revision C, dated July 14, 1997, or later FAA approved revision, complies with FAR Part 36, Stage 3 noise limits.STC ST00553SEIncorporation of the Raisbeck Commercial Air Group inlet acoustical treatment and associated structure on certain engine nose cowlsSTC ST00555SEModification in the leading edge slat and flap configurationsSTC ST01182LAInstallation of an interior modification.STC SA1098WEInstallation of Roto-Master (Rajay) turbocharged Continental IO-470-E or IO-470-S engine.STC SA1252WEInstallation of Rajay turbocharged Continental - Teledyne O-470-G-C1 and/or IO-470C, -J, -K, -N engines.STC SA125SOInstallation of Turbocharged Lycoming G0-480- G1D6 engine (STC SE124SO)STC SA1260WEInstallation of turbocharged Lycoming O-360-A1A or A1D engines.STC SA136SOInstallation of Turbosupercharged GO-480-D1A engines.STC SA153SOInstallation of Turbocharged Lycoming O-360-A1A, IO-360-B1A, or IO-360-B1B enginesSTC SA1557WEInstallation of turbocharged Lycoming O-540-E4B5 engineSTC SA156SOInstallation of Turbocharged Lycoming G0-480-G1D6 engine (STC SE124SO) per FAA Sealed Roto-Master (Rajay/Riley) drawing List R0018. FAA approved Flight Manual Supplement, dated November 24, 1965 or later, FAA approved revision and Roto-Master (RAJAY/Riley) Turbo Owner s Manual required with this installation.STC SA1592WEInstallation of automatic fuel mixture control.STC SA181SOInstallation of Turbosupercharged Continental IO-470- U enginesSTC SA193SOInstallation of turbocharged Lycoming GO-480-C1B6 or GO-480-G1B6 engines, per STC SE124SO.