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.

Airframe · Piper PA-24-260

STC SA03708ATReplacement of the Main Landing Gear HousingAeronautical Design Service Pty Ltd TheSTC SA4172NMInstallation of Aviation Development oil filter.Aviation Development CorporationSTC SA01201ATInstallation of left hand side and right hand side auxiliary tank fuel cell assemblies.FFC ManufacturingSTC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.Electronics International Inc.STC SA00484WIInstallation of shoulder harness for two front seats.PHILL-Air Inc.STC SA00746WIInstallation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901)PHILL-Air Inc.STC SA01834CHInstallation of the High Intensity Discharge Light Assembly Kit.Knots 2U Ltd.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.Champion Aerospace LLCSTC SA270GLInstallation of forward windows, P/N's W-, W/T-, WG-2058-187 or-250 and W-, W/G-20599-187 or -250.Great Lakes Aero Products IncSTC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.M-20 Oil Separators LLCSTC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeGarmin AT Inc.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemPrecise Flight IncSTC 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-( ).Honeywell International Inc.STC SA5925SWInstallation of auxiliary instrument air system.Aero Safe CorporationSTC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.K S Avionics IncSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA208GLInstallation of one piece windshield.Great Lakes Aero Products IncSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)Aviation Development CorporationSTC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.Insight Instrument CorporationSTC SA4008NMInstallation of removable panels on the battery box slides.Bogert AviationSTC 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.Garmin AT Inc.STC SA4-955Fiberglass vertical fin mount for either Grimes or Whelen WRM rotating beacons.Univair Aircraft Corporation · Lists PA-24 SeriesSTC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.Aero Enhancements Inc.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.Avidyne CorporationSTC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.Electronics International Inc.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.Garmin AT Inc.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.Garmin AT Inc.STC SA00927ATInstallation of composite propeller spinner.TCB Composite Co.STC SA01421ATInstallation of an OCEM AP-3C autopilot. (PA-24-180)Chelton Aviation CorporationSTC SA00954ATInstallation of composite bulkhead.TCB Composite Co.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.Micro AeroDynamics IncSTC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).Precise Flight IncSTC SA4150NMInstallation of Precise Flight Series 100 Speedbrake System.Precise Flight IncSTC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.Aero Holdings Ltd. a Texas limited partnershipSTC 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.J P InstrumentsSTC 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.Aerospace Logic Inc.STC ST02547ATInstallation of a voice alert system.Aircraft Components IncSTC 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.Hanson NolanSTC SA00175DEInstallation of Oilamatic Preoiler system.Oilamatic IncSTC SA5983NMCockpit sun visor installation.Rosen Sunvisor Systems LLCSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemAircraft & Rotorcraft Products (ARP) IncSTC 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.Flight Life, Inc.STC SA2652CEInstallation of main fuel cell bladders as replacements for original bladders.Floats & Fuel CellsSTC 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.Riley Aircraft of ArizonaSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA6019NMInstallation of an electronic digital engine tachometer.Horizon Instruments IncSTC 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)PMA Products, Inc.STC SA3565WEInstallation of single piece windshield.Cee Bailey's Aircraft PlasticsSTC SA09470SCInstallation of Starter Indicator light system.Texas Skyways Inc
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