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 SA01328LAModification of right hand side door to provide an openable window.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA01951NY-DInstallation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.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 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 SA02007NYInstallation of SMR Technologies pneumatic deicer models.STC SA10285SCInstallation of a Chelton Aviation Corp (CAC) AP-3C autopilot.STC SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.STC SA01436SECockpit sunvisor retrofit kit.STC SA2456CEInstallation of fuel inlets and and caps. (210R S/N 21058819 THRU 21064950) (P210R S/N P21000001 THRU P21000867) (T210R S/N T210-0198 THRU 21064950)STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA4473NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.STC SA5467NMInstallation of acrylic window liners. (206 SERIES 402B0301 AND ON)STC SA2602NMInstallation of Precise Flight, Inc. 100 Series Speedbrake System in accordance with Precise Flight, Inc. Speedbrake Installation Drawing No. 210S006A, dated October 17, 1988, and Drawing List No. 210S008A, dated October 20, 1988, or later FAA approved revisions. Or Installation of Precise Flight, Inc. Speedbrake 2000 System in accordance with PreciseSTC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01077SEInstallation of fluoropolymer film.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC SA2382NMInstallation of Aileron and Flap Gap Seals.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC SA2559CEAdd provisions to disable aileron servo for KFS-200 autopilot.STC ST02547ATInstallation of a voice alert system.STC SA3696NMCockpit Sun Visor installation in accordance with FAA approved Rosen Drawing List Number RCS-00DL, dated December 17, 1986, or later FAA approved revisions.STC SA2577CEInstallation of main fuel cell bladders as replacements for original bladders. (T210 SERIES SPECIFIC SERIAL NUMBERS AFFECTED)STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.STC SA01074WIInstallation of McFarlane Aviation Flap Roller Assembly Service Kit MCSK100STC SA5821NMInstallation of an electronic digital engine tachmoter, Model P-1000.STC SA3596SWInstallation of induction manifold sniffle valve system, revised oil breather system, and battery box vent system.STC SA3728SWInstall vacuum pump cooling shroud.STC SA4578SWInstallation of an auxiliary engine driven vacuum pump system.STC SA00455DEInstallation of a large vertical left hand side window and/or an optional Del Air One Passenger Observation Rear Seat Assembly.STC SA00941SEInstallation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.STC SA09470SCInstallation of Starter Indicator light system.STC SA00425DEInstallation of model FB-02 'Fixed Arm' Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System.STC SA00426DEInstallation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.STC SA8896SW-DInstallation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-566, with Optional Autotrim System.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA01590ATInstallation of Composite Spinner.STC SA01280CHInstallation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404)STC SA71GLInstallation of air filtersSTC SA3312WEInstallation of recognition lights on horizontal stabilizer.STC SA09447AC-DInstallation of S-TEC System 40X/50X Single and Two Axis Automatic Flight guidance Systems, Model ST-788-40X/50XSTC SA3226NMInstallation of 16.25 gallon usable fuel-containing lightning resistant wing tips.STC SA4300WEInstallation of a 16.25 gallon usable fuel-containing wing tips.STC SA00368DEInstallation of an Aircraft Noise Control System.STC SA00846WIInstallation of B&C Specialty products BC 425-1 standby alternator.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA00367DEInstallation of an Oilamatic Preoiler system.