N184WW
STCs that may be installed · 241
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 = '2730105'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '29001')
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 = '2730105'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '29001')
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 · Dassault-Breguet MYSTERE FALCON 20-F5
STC ST01335WI-DModification of a Collins CDU-5000/6100/6200 Control Display Unit(s) installation.STC ST274CH-DInstallation of a Honeywell CAS 67 TCAS II System.STC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationSTC ST00600WI-DInstallation of Collins Pro Line 4 Avionics System.STC ST01527SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Dassault Mystere Falcon 20-F5, Serial Number 430 only. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM).STC ST02100CHInstallation of dual Computer Instruments Corporation Air Data Computers with Innovative Solutions & Support Air Data Interface.STC ST02102CHInstallation of an L3 Communications (Goodrich) GH-3100 Electronic Standby Instrument System (ESIS).STC ST02030CH-DInstallation of a dual Innovative Solutions and Support (IS&S) altimetry system.STC ST01277WI-DModification of a Collins Flight Management System (FMS) Installation
in Part 25 Aircraft in accordance with Collins Drawing Index as listed on AML No. ST01277WI-D, Revision -, or later FAA approved revisions.STC ST02020CH-DInstallation of a Rockwell Collins Copilot's ADC-80K Air Data computer, ALI-80A Altimeter with FCS-80/85 Interface and Standby Pneumatic Altimeter.STC ST02941ATInstallation of a Honeywell KGP-860 Enhanced Ground Proximity Warning System (EGPWS).STC ST01464SENon-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM)STC ST02901ATInstallation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS) in accordance with Jet Aviation Master Drawing List (MDL) F20-20311-010, Revision IR, Dated May 21, 2004, or later FAA approved revision.STC ST00002NYInstallation of a baggage compartment (vacated by the relocation of APU).STC ST00827NYInstallation of a Sundstrand T-62T40-C9 APU.STC ST00017NYInstallation of Garrett GTCP 36-150(W) APU.STC ST01295SEGroup aircraft approval for Reduced Vertical Separation Minimum Qualification Document.STC ST02844ATManufacture of electrically powered window shades for the passenger cabin in accordance with Aerospace Technologies Group (ATG) Master Drawing List No. ATG- WS- 1204DL, Revision D, dated March 3, 2004, or later FAA approved revision. Installation of window shades in accordance with ATG Drawing No. ATG-IP-1204, dated March 3, 2004, or later FAA approved revision.STC ST10193SCInstallation of a vapor cycle (Freon, R-134a) air conditioning system for ground and in-flight cooling.STC ST01884CHInstallation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System with Terrain Display.STC ST01358CH-DInstallation of aircraft interior furnishings, cabinetry and entertainment system. Approved for installation on serial number 408 ONLY.STC ST01146WIInstallation of Wing to Fuselage Upper Fairing Assemblies.STC ST01355CH-DInstallation of a MagnaStar C-2000 digital airborne telephone system. Aproved for serial number 408 ONLY.STC SA980GL-DInstallation of a P/N M45-170093-501 or M45-170093-502 Master Warning Panel.STC ST01314CH-DInstallation of provisions for future installation of Universal Avionics Terrain Avoidance Warning System (TAWS).STC ST01579CH-DInstallation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).STC ST01575CH-DInstallation of ARTEX 110-406 NAV Emergency Locator Transmitter with an ELT/NAV Interface Unit.STC ST01421CH-DAlterations to existing Auto Throttle System. Must have STC ST1020NY installed.STC ST01580CH-DInstallation of Universal Avionics Terrain Awareness and Warning System (TAWS) with Video Display on an optional Universal Avionics Multi-Function Display (MFD).STC ST01127CH-DInstallation of provisions for the future installation of Universal Avionics flat Panel Electronic Engine Indicators.STC ST00775CH-DInstallation of an AlliedSignal Avionics MK-V, enhanced ground proximity warning system.STC ST00777CH-DModification of the aircraft inverter system, reducing the inverter system from three (3) inverters to two (2) inverters due to the reduced aircraft S.C. electrical load.STC ST01362VCH-DInstallation of a Dual Universal Avionics UNS-1K Flight Management System with GPS as a primary means of navigation.STC ST01316CH-DInstallation of Collins Proline II Communication, navigation, pulse system with Baker B1035 cockpit audio system.STC ST01420CH-DInstallation of Standard Alterations Required for Installation of Collins EFIS-85B(12), EFIS-85C(14)/APS-85 Avionics. STC SA2157CE must be installed previously or concurrently.STC ST00782CH-DInstallation of a Dual Honeywell Avionics FMZ-2000, flight management system with GPS as a primary means of navigation.STC ST01052CH-DInstallation of an AlliedSignal Avionics CAS 67A traffic alert and collision avoidance system (TCAS II) with Rockwell Collins TDR-94D mode s transponders.STC ST09940SCInstallation of a vapor cycle (Freon, R-134a) air conditioning system for ground and inflight cooling with optional electrical heating.STC ST01319CH-DInstallation of Dual Davtron Cockpit clocks.STC ST01364CH-DInstallation of Safe Flight 1501 Series Angle of Attack System.STC ST01422CH-DInstallation of Safe Flight 6502 Series Windshear Warning System.STC ST01400CHInstallation of Universal Avionics Systems Model 640 flat panel electronic engine and systems instrument display system.STC ST00938WI-DModification of Collins GPS-4000 Global Positioning Sensor installation to a Collins GPS-4000A Global Positioning Sensor installation in a part 25 aircraft per Collins Installation INstructions as listed in AML No. ST00938WI-D, latest revision.STC ST01315CH-DStandard Alterations required for installation of Colins Proline IV Avionics Suite. This mod requires concurrent installation of Collins Proline IV Avionics Suite per STC ST00600WI-D.STC ST01317CH-DInstallation of Collins TCAS-4000 Traffic and Collision Avoidance System (TCAS II).STC ST01318CH-DInstallation of a Terra Jet Call Selective Calling System (SELCAL).STC ST01356CH-DInstallation of Universal Avionics CVR-30B cockpit voice recorder (CVR) system.STC ST01357CH-DInstallation of BFGoodrich WX-1000E stormscope Series II system IAW Garrett drawing list #70-0766-001 dtd 11/10/00 or later FAA approved revision.STC ST00931WIInstallation of Honeywell MK-V Enhanced Ground Proximity Warning System (EGPWS).STC ST00932CH-DInstallation of an AlliedSignal Avionics MK-VII Enhanced Ground Proximity Warning System.