N2BZ
STCs that may be installed · 266
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 = '7630410'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41533')
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 = '7630410'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41533')
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 · Rockwell International 500-S
STC SA2478SWInstallation of Lycoming IO-720- B1B engine and increase take-off and landing weight to 7800 lbs.STC SA2691WEInstallation of Lycoming IO-720-B1B or B1BD turbocharged engineSTC SA529WEInstallation of turbosupercharged Lycoming IO-540 series engines.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA917EAInstallation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail, P/N 30-0555-( ).STC SA20GLInstallation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO)STC SA250CEInstallation of Woodward electronic propeller synchraphaser system.STC SA01754SEInstallation of the Merlyn Products Inc. remote oil filterSTC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA01695SEInstallation of an antennaSTC SA01170NYInstallation of NPX138N-XXX FM Transceiver.STC ST01468CHInstallation of various SMR Technologies electrical propeller deicer models.STC SA00729SEInstallation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760, Revision -, dated 7/20/99, or later FAA approved revision.STC SA00812NYInstallation of Technisonic Industries Limited TFM-138, A, and B (does not include TFM-138, s/n 1540 and up, TFM-138B, s/n 1500 and up).STC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA1-143Installation of Chamberlain 2001X series radome kits.STC SA01314WIReplace the original equipment oil temperature, oil pressure, and fuel pressure 3-in-1 gauges and dual cylinder head temperature gauge with oil temperature, oil pressure, and cylinder head temperature 3-in-1 gauges and dual fuel pressure gauge.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA2826SWInstallation of auxiliary fuel tank according to Report No. MDL 60700 Master Drawing List revised 7/27/78, or later FAA approved revision.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.STC ST02547ATInstallation of a voice alert system.STC SA09530AC-DInstallation of S-TEC System 55X Two-Axis Automatic Flight Guidance System, Model ST-904.STC SA8597SWInstallation of P/N DF062-507, upper center fuel tank bladder cells as a replacement for original bladder P/N 5630062-507.STC SA71GLInstallation of air filtersSTC SA00169SEInstall Lycoming IO-540-M1C5 engine and Hartzell HC-C3YR-2UF/FC8468()-6R propeller.STC SA1017EAInstallation of vertical tail floodlightsSTC SA00874WIInstallation of elevator and rudder trim actuator.STC SA798SWRadome nose extension.STC SE01840ATInstallation of Naceele Mounted Recognition Lights.STC SA1158GLReplace standard wing tip assembly with winglet tip assembly.STC SA1566GLInstallation of flap gap wing fairings.STC SA00105SEModify Flap Pulleys.STC SA01444ATInstallation of an Enviro Systems AirConditioner.STC SA01820ATInstallation of Exhaust Deflectors.STC SA01677ATInstallation of Electrosystems 90 Amp Alternators.STC SA00529SEModification, inspection, and repair of the wing to fuselage attachment straps, wing leading edge close outs, and wing station 24.0 ribs.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA3143SW-DInstallation of Century automatic flight system.STC SA5969NMInstallation of Lycoming TIO-540- J2B(d) engine, Hartzell HC-C3YR-2UF/FC8468D-6R, or HC-C4YR-2/ FC6660 propeller and optional Merlyn Products MPI 98-1005-519 turbocharger.STC SA00387SEModification of the existing fuel system to increase its capacity by the installation of additional fuel tanks and associated hardwareSTC SA8705SWInstallation of R25V0N Alternator Control Unit or R2510N Alternator Control Unit or V2510A Over Voltage Sensor.STC SA00061LAInstallation of JPI digital tachometer.STC SA7187SW-DInstallation of S-TEC Manual Electric Trim System, Model ST-129.STC SA2903SWInstallation of wing flap gap seals.STC SA3492WEReplacement installation of vertical tip assembly.