N22708

STCs that may be installed · 356

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 = '2071818'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '17020')
    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 · Cessna 150H

STC SA6037SW-DInstallation of S-TEC System 40/50, single and two axis automatic flight guidance system, Model ST-298-40/50.S-TEC CorporationSTC SA4005NMPrecise Flight Inc. Pulselite Control SystemPrecise Flight IncSTC SA01205WI-DInstallation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.Honeywell International IncSTC SA01105WI-DInstallation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).Honeywell International Inc.STC SA06037SW-DInstallation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems.S-TEC CorporationSTC SA02446CHInstallation of the Courtesy Light Kit.Knots 2U Ltd.STC 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 SA3659SWInstallation of Jetton Alert II alarm system.Jetton AircraftSTC SA1809WEInstallation of one twelve-gallon auxiliary fuel tank in each outboard wing panel.Flint Aero IncSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)Aviation Development CorporationSTC SA8150SWInstallation of VENTUBE pilot/co-pilot overhead fresh air valves. (195 SERIES LC-126A; LC-126B; LC-126C)Soros Inc. a Texas CorporationSTC SA02277AKInstallation of FMK Light Emitting Diode (LED) Instrument Panel Lights.Forest KirstSTC SA02137ATInstallation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051Lord CorporationSTC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.Insight Instrument CorporationSTC SA00812CHReplace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.Vantage Plane Plastic LtdSTC 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 SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA01323WIInstallation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.Aircraft Development CoSTC SA01324WIInstallation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 115-1 is derived from Drawing List 115-1 Revision D and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.Aircraft Development CoSTC 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 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 SA01436SECockpit sunvisor retrofit kit.Rosen Sunvisor Systems LLCSTC SA01389SEInstallation of 8-gallon extended range wing fuel tanksDel-AirSTC SA01944CHModify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.Experimental Aircraft Association Inc.STC SA633GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.EAA Aviation FoundationSTC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemPS Engineering IncorporatedSTC SA2846SWConversion from trigear to conventional gear configurationDel-AirSTC SA3788NMInstallation of Sensenich 74DM6S5 Propeller; Elano Exhaust System, P/N EL 099001-063 and -060; and Cessna Muffler, P/N 0454011-1, in accordance with FAA Approved ACT Report No. 104, dated February 10, 1992, or later FAA approved revisions. STC SA4795SW for the installation of Lycoming 0-320-E2D engine is required as part of this installation.Del-AirSTC SA4795SWInstallation of an Avco Lycoming O-360 or O-320 engine and increase airplane gross weight.Del-AirSTC SA1814NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window plexiglass 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.G & D Aero Products Inc.STC SA01077SEInstallation of fluoropolymer film.Columbia Pacific AirlinesSTC 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 SA2382NMInstallation of Aileron and Flap Gap Seals.Knots 2U LtdSTC 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 SA326EAWet-to-dry vacuum pump conversion kit 300-3.Parker Hannifin CorpSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemAircraft & Rotorcraft Products (ARP) IncSTC SA1005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.Soros, Inc · Lists 150 SeriesSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.Trevor Burward-HoySTC SA01065SEInstallation of vortex generators on the wings and vertical tail surfaces of the above model aircraft per Drawing Package MA2081, Revision IR, dated January 15, 2002, and Installation Manual MA2082, Revision IR, dated February 13, 2002, or later FAA approved revision of either of these documents.NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Micro AeroDynamics IncSTC SA572CEInstallation of Lycoming 150 or 160 hp Model O-320 engine.Williams Robert or BarbaraSTC SA09470SCInstallation of Starter Indicator light system.Texas Skyways IncSTC SA09491SCInstallation of a low voltage warning system.Stark's AviationSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.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)D & K AviationSTC SA00270WIInstallation of fiberglass replacement wing tips.Aircraft Development CoSTC SA71GLInstallation of air filtersBrackett Aero Filters Inc.
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