Mooney M20B
STCs that may be installed · 274
In force first, then newest. The registry doesn’t record which STCs an aircraft has.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('5870206')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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 s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('5870206')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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.
STC SA315CHInstallation of McCauley propeller model B3D36C424/74SA-0.STC SA676GLInstallation of a Shadin Company Fuel Flow Indicating SystemSTC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.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 SA10372SCInstallation of a Chelton Aviation Corp (CAC) AP-3C autopilot in accordance with the Master Drawing List No ST7893SC-A-12, Rev. B, dated January 7, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. ST7893SC-A-14, Rev. I.R., dated January 19, 2005, or later FAA approved revision is required.STC SA01660LAInstallation of Air-Tec Alternator kit. Descriptive data pertaining to this design change are considered inadequate for duplication in other aircraft. This approval is limited to the installation on Mooney M20B, S/N 1900 only.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 SA00071SECockpit sun visor installation.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA2168NMInstallation of the Precise Flight stand-by vacuum system (SVS).STC SA2174NMInstallation of Precise Flight speedbrake system.STC SA4342NMInstallation of Precise Flight 100 or 2000 Series Speedbrake System.STC SA5708NMInstallation of Precise flight manual control speedbrake.STC 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 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 SA3275WEInstallation of George M. Adams DGA-2000 or Bodell BMI-2000 wheels and Bodell Mfrg. BMI-252 brakes.STC ST02547ATInstallation of a voice alert system.STC SA00117DEInstallation of Oilamatic Preoiler system per FAA approved Oilamatic, Inc. Drawing List No. M20400, initial release, dated 6/1/94 or later FAA approved revisions.STC SA00165BOInstallation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.STC SA02549ATModification of engine exhaust system for improved engine performance.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA1156WEInstallation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A1A or O-360-A1D engine.STC SA7609SWInstallation of composite wing tipsSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA5844NMInstallation of an electronic digital engine tachometer, Model P-1000, P/N P100030- .STC SA02431ATInstallation of a BAE-14/28 Air Driven Alternator on a Mooney M20 AircraftSTC SA09470SCInstallation of Starter Indicator light system.STC SA02168AKInstallation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.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 SA09309AC-DInstallation of S-TEC System 30 ALT Altitude Hold System, Model ST-746.STC SA5211SW-DInstallation of S-TEC system 40/50, single and two axis automatic flight guidance systems, model ST-193-40/50.STC SA09308AC-DInstallation of S-TEC system 20/30 single and two axis automatic flight guidance systems.STC SA71GLInstallation of air filtersSTC SA01310ATInstallation of a Mooney One-Piece Lower Fuselage Skin, P/N 310322-501, and related attachment structure.STC SA2986WEInstallation of Pathfinder autopilot systems. (M20 SERIES see MDL No. 77-030-1 for approved models)STC SA00511SEInstallation of a type 7308 lamp.STC SA01553ATModify the side windows by replacing the existing 3/16 inch thick glass with 1/4 inch thick glass.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA1111SOInstallation of an adjustable trim tab on the left aileron.STC SA4023WEInstallation of flap gap fairings, flap hinge fairings, fuselage fairing at the tail cone, and a plexiglass landing light fairing.STC SA4382WPInstallation of wheel well doors.STC SA4453NMInstallation of dorsal fin. (M20A w/metal tail)STC SA4474NMInstallation of wing tips similar to those for Mooney Model M20J, M20K, or earlier models.
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