N761KB
STCs that may be installed · 479
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.
Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2073451'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '17040')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, s.status = 'Current' DESC, s.status_date DESC, s.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 m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2073451'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '17040')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, s.status = 'Current' DESC, s.status_date DESC, s.stc_numberRun 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.
Airframe · Cessna T210M
STC SA02768CHInstallation of Teledyne Continental Motors IO-520-A & -F (as modified by STC SE03704AT) or IO-550 F (as modified by STC SE03705AT) and Hartzell Propeller (P)HC-(C or J)3YF-1RF/F8468(B,K) 3 bladed metal propeller, or McCauley Propeller models D3A34C401/90DFA-() or D3A34C402/90DFA-()STC SA2390NMInstallation of Turboplus Intercooler System No. 15000 or 15000-AD.STC SA00606NYInstallation of O & N Aircraft Modifications low fuel warning device.STC SA01194NYInstallation of a Freon-Type electric motor driven Air Conditioning SystemSTC SA1003NEConfiguration 1: Installation of an Allison 250-B17F Turboprop Engine (450Hp), (TCDS. E10CE) Hartzell HC-B3TF-7A/
T9212NK-2, Constant Speed reversing propeller, and, a 27.7 gallon Auxiliary Fuel Tank in the fuselage aft, baggage compartment.
Configuration 2: Installation of a Rolls Royce Corporation, 250-B17F/2 engine (450Hp), (TCDS. E10CE). and Hartzell HCB3TF-
7A/T9212NK-2, Constant Speed reversing propeller.STC SA3753NMInstallation of stiffening ribs in the aileron and rudder surfaces and redistribution of the mass balance in the aileron, rudder and elevator surfaces.STC SA515NEInstallation of an aft baggage compartment auxiliary fuel tank and transfer system to the right wing tank.STC SA00353BOInstallation of an auto lean systemSTC SA02276AKInstallation of AMSAFE Aviation Inflatable RestraintsSTC SA00352BO PAGE 1Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),STC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA02918CHReplace original Teledyne Continental Motors (TCM) TSIO-520 engine with TCM IO-550-P model aircraft engine; turbo normalized not to exceed the rating of 310 BHP Maximum Continuous Power for both the aircraft and engineSTC SA00780SEInstallation of the True Lock Safety Retention Axle Lock Nut SystemSTC SA01118WIInstallation of the Concorde FLA or VRSLA RG series batteriesSTC SA09857ACInstallation of an ISTART Starting Enhancement SystemSTC SA01816WIInstallation of an ADS-B compliant system, comprised of a Garmin GTX 330 Mode S Transponder and a Free Flight 1201
GPS receiver.STC SA11172SCInstallation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antennaSTC SA00149BOInstallation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1STC SA02547ATInstallation of a Voice Alert System.STC SA03658ATInstallation of a Voice Alert System to incorporate as primary annunciators for stall and gear warningsSTC SA02119SE PAGE 1Installation of Garmin GDL 88 ADS-B UAT Transceiver SystemSTC SA01969SEInstallation of a Mid-Continent MD302 Standby Attitude ModuleSTC SA01107SERMD Aircraft Lighting high intensity discharge wingtip lightSTC SA3685NMInstallation of fiberglass wing tips; each tip having a 100 watt recognition light and a clear plastic lens.STC SA01229SE PAGE 1Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radiosSTC SA00172WIInstallation of TKS anti-icing system components, with placard stating 'Flight into known icing conditions is prohibited.'STC SA02442AK PAGE 1Approval of the L-3 Communications NGT 2000/2500 ADS-B systemSTC SA01933LA-D PAGE 1Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
SystemSTC SA01669CHInstallation of Challenger Reusable Air FilterSTC SA02930NYInstallation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) InstrumentsSTC SA2162NMInstallation of the Precise Flight stand-by vacuum system (SVS)STC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA2107AT-DInstallation of a Teledyne Continental Motors IO-550-P engine and Hartzell PHC-J3YF-1RF/F7691() propellerSTC SA01744WIInstallation of an Induction Manifold Fuel Drain Line FilterSTC SA3531NMInstalling copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP)STC SA02121SEInstallation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic SystemSTC SA00269BOInstallation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.STC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleSTC SA02015SE-DInstallation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.STC SA1305WEInstallation of Brittain Model PCA-1 Pitch Assist with Altitude HoldSTC SA245WEInstallation of Brittain/Clarkson AutopilotSTC SA469WEInstallation of Brittain Model PC-1 Pitch Assist and Model AH-1 Altitude Hold (optional)STC SA662WEInstallation of Brittain Industries, Inc., Model B1-400 Hi-Lo Sensitivity AdaptorSTC SA1343WEInstallation of Brittain Industries Model B-4 Flight Control System.STC SA618WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA627WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA674WEInstallation of Brittain Model B-4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA1609WEInstallation of Brittain Industries Model B-5 flight control system.STC SA1672WEInstallation of Brittain Industries Model B-5 Flight Control System