TCDS A7EU
STCs approved under this data sheet · 562
Current certificates first, most recently changed first.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A7EU') 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 FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A7EU') ORDER BY 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.
STC SA2614NMCockpit sun visor installation per FAA approved Rosen Drawing List Number RF 50/200-00DL, dated 5/15/1984 or later FAA approved revision.STC SA2652NMCockpit Sun Visor installation.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 SA1996SWInstallation of auxiliary landing lights.STC ST01570NYLimit passenger seating capacity to a maximum of 9 persons. Approved for installation on model Mystere-Falcon 200, serial number 494 ONLY.STC ST01571NYLimit passenger seating capacity to a maximum of 9 persons.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 ST09983SCRestricted to a maximum nine-passenger seatSTC 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 SA2772NMInstallation of dual Universal UNS-1A Flight Mgmt. System with VLF/Omega and Inertial NAV Sensors.STC SA92RMInstallation of a Global Navigation System Model GNS-500A VLF/OMEGASTC 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 ST01423CH-DInstallation of aircraft interior furnishings, cabinetry and entertainment system. Approved for installation on serial number 267 ONLY.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 SA3394WEReplacement of cargo barrier net installed per STC SA1467SW with a rigid cargo barrier partition.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 ST01287NYInstallation of a Safe FLight Ram Air Temperature indicator/engine pressure ratio computer.STC ST01351CH-DInstallation of Dual Universal UNS-1K Flight Management 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.STC ST274CHInstallation of a Bendix/King CAS67TCAS II system with dual MST-67 Mode S transponders.STC SA1016SWInstallation of Collins AL-101 radio altimeter.STC SA1389SWInstallation of auxiliary power unit Solar T62T-39 and Hamilton Standard simple/bootstrap air cycle unit Model R70-3W.STC SA4067SWInstallation of Freon air conditioner compressor/condensor package in aft fuselage tail section.STC SA730SWRelocation of one 750VA inverter, installation of two 2500 VA inverters, and removing one1500 VA and one 750 VA inverter.STC SA753SWInstallation of Class D baggage compartment.STC ST491CHInstallation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I).STC SA1200SWInstallation of AP-104/FD-109F/FD-109H autopilot/flight director control system.
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