TCDS A16SW
STCs approved under this data sheet · 194
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 = 'A16SW') 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 = 'A16SW') 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 SA2745NMInstallation of aft fuselage fuel tank fill system.STC ST02371LAAlteration of a Beechcraft Corporation 400A airplane, to replace Pratt & Whitney JT15D-5 series engines with Williams International FJ44-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Config. A) and (/or) the installation of Nextant Winglets (Config. B)STC ST03110CHInstallation ofL3 Communications Digital Flight Data RecorderSTC ST03389CHInstallation of Honeywell KHF-950 High Frequency Communication System with Optional Avtech CSD-714 SelCal DecoderSTC ST03473CHInstallation of the Safe Flight AutoPower Automatic Throttle System (ATS)STC ST03960ATInstallation of Rockwell Collins Venue In-Flight Entertainment(IFE), Aircell Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN) Astronics 115VAC 60HZ Cabin Inverter, and Emteq LED Cabin Lighting SystemSTC ST04214CHInstallation of Automatic Dependent Surveillance Broadcast (ADS-B) Out transponderSTC ST00959ATConsolidate STC's SA3320SO,ST00141AT, ST00244AT, ST00245AT, AND ST00667AT. (400 S/N RJ-61 ONLY)STC ST09775ACModification of the nose landing gear strut and the addition of pressure tubing and fittings to the nose gear for servicing of the oleo strut.STC ST01637WIActivation of the Wireless Fidelity (WiFi) capabilities of previously installed router(s) and Aircraft Transmitting Portable Electronic Devices (T-PEDs) Tolerance TestingSTC SA2501SOInstallation of Whelen Flashing Anticollision Light P/N 90033.STC ST02619ATInstallation of a Battery Low Voltage Warning/Shutoff System per Master Drawing List MDL RAF01106A dtd 6/10/02 or later FAA approved revision.STC ST01641WI-DInstallation of Rockwell Collins, Inc. Aircraft Information Management (AIM) SystemSTC ST00344ATInstallation of emergency lighting system improvement modification.STC ST00425ATInstallation of a Pulse Lighting System.STC ST00533WIInstallation of Safe Flight Instrument Corporation N1 Computer System, P/N 6810-1 MOD A.STC ST00600ATInstallation of alternate cabin lighting.STC ST00667ATInstallation of Collins Avionics bravo enhancement package.STC ST00737ATInstallation of Autopower System.STC ST00793ATInstallation of External Power Overvoltage. Protection SystemSTC ST00966ATInstallation of pilot and co- pilot seat crotch belt.STC ST01478ATInstall cockpit window sunvisor monorail systemSTC ST02251ATInstallation of a cockpit speaker and aural warning muting system.STC ST02506ATInstallation of an Increased Ampere-Hour Recombinant Gas (RG) Lead acid battery.STC ST02620ATInstallation of a LED Tail Position Navigation Light ReplacementSTC ST02784ATInstallation of dual Innovative Solutions and Support (IS&S) Air Data Display Units (ADDU) and a single Analog Interface Unit (AIU)STC ST02851ATCertification of Reduced Vertical Separation Minimum (RVSM) Operational CapabilitySTC ST00235WI-DModification of a single Collins AMS-850 Avionics Management SystemSTC ST09573SCModification of Collins Avionics VHF Communications Radio systems with 8.33 kHz frequency spacing capability.STC SA2188CEIncorporate aircraft interior improvements.STC SA2205CEInstallation of second Collins ADF-60A system.STC SA2215CEInstallation of Fairchild Model F-800, digital flight data recorder.STC SA2216CEInstallation of Fairchild Model A100A cockpit voice recorder.STC SA2217CEInstallation of Sperry Instrument monitor system, Model CM-400.STC SA2218CEInstallation of copilot flight director, Sperry FZ-500.STC SA2219CECategory II certification.STC SA2220CEInstallation of King Radio Corporation High Frequency Communication System Model KHF-950.STC SA2222CEIncorporate aircraft interior improvements, including provisions for use of lavatory seat for take-off and landing operations.STC SA2338CEInstallation of Sperry three tube electronic flight instrument system, EDZ-805.STC SA2339CEInstallation of Sperry Primus 650radar system.STC SA2340CEInstallation of second Collins distance measuring equipment DME-42A and indicator IND-42A system.STC SA2341CEModification of cockpit pedestal to make provisions for additional equipment.STC SA2356CEInstallation of Honeywell Flight Management System, FMZ-610.STC SA2358CECategory II certification.STC SA2369CEInstallation of an optional interior configuration, including a ninth seat.STC SA2374CEAddition of Collins DDA-42 DME distance adapter to an existing/single Collins DME-42.STC ST00693WI-DModification of dual Collins AMS-5000 avionics management system, dual Collins APS-4000 autopilot system, and PFD-MFD-PFD (3-tube) or PFD-MFD-MFD-PFD (4-tube) EFIS display installations.STC ST00723WI-DInstallation and Modification of dual Collins AMS-5000 Avionics Management System, dual Collins APS-4000 Autopilot System and Collins PFD-MFD-PFD (3 tube) or Collins PFD-MFD-MFD-PFD (4 tube) EFIS Display Pro Line 4 Avionics System.STC ST00780WI-DModification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation.STC ST00812SEGroup airplane approval for Reduced Vertical Separation Minimum (RVSM).
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