N636SW
STCs that may be installed · 347
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 = '7102406')
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 = '7102406') 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
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.
Airframe · Piper PA-24-260
STC SA03708ATReplacement of the Main Landing Gear HousingSTC SA4172NMInstallation of Aviation Development oil filter.STC SA01201ATInstallation of left hand side and right hand side auxiliary tank fuel cell assemblies.STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA00484WIInstallation of shoulder harness for two front seats.STC SA00746WIInstallation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901)STC SA01834CHInstallation of the High Intensity Discharge Light Assembly Kit.STC SA00769CHInstallation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540, AEIO-540 and HIO-540 engines.STC SA270GLInstallation of forward windows, P/N's W-, W/T-, WG-2058-187 or-250 and W-, W/G-20599-187 or -250.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC 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 SA5925SWInstallation of auxiliary instrument air system.STC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.STC SA01695SEInstallation of an antennaSTC SA208GLInstallation of one piece windshield.STC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA4008NMInstallation of removable panels on the battery box slides.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 SA4-955Fiberglass vertical fin mount for either Grimes or Whelen WRM rotating beacons.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning 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 SA00927ATInstallation of composite propeller spinner.STC SA01421ATInstallation of an OCEM AP-3C autopilot. (PA-24-180)STC SA00954ATInstallation of composite bulkhead.STC SA01299SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to either of these documents.STC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).STC SA4150NMInstallation of Precise Flight Series 100 Speedbrake System.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.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 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 ST02547ATInstallation of a voice alert system.STC ST02651ATReplace rudder balance weight kit #760705 with new advanced design used by Piper on PA-24-400 Model aircraft for rudder balance in accordance with Southland Aviation Drawing 24-001, dated April 17, 2003.STC SA00175DEInstallation of Oilamatic Preoiler system.STC SA5983NMCockpit sun visor installation.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA434NEInstallation of William C. Roberts' steel brake discs P/N 201-19-SS dated 6/29/85, in lieu of Piper carbon steel brake discs, Piper 754-530.STC SA2652CEInstallation of main fuel cell bladders as replacements for original bladders.STC SA01352LAReplacement of Piper Battery box part numbers 20659-00, 21524-00, 21524-02, 25338-00, or 26240-00 and venting battery, with Riley Aircraft Battery Box, part number 1001TR, and Gill manifold battery Model G-35M.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA6019NMInstallation of an electronic digital engine tachometer.STC SA02410ATReplace existing Auxiliary Electric Standby Fuel Pump with PMA Products, Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v), 1A15-s/n 24-3642, 24-4000 through 24-4782, 24-4784 through 24-4803, 2A13-s/n 28-7690001 through 28-7990626, 28-8090001 and up(14v)STC SA3565WEInstallation of single piece windshield.STC SA09470SCInstallation of Starter Indicator light system.