N877KB
STCs that may be installed · 225
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 = '2076802'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '01518')
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 = '2076802'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '01518')
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 · Cessna 650
STC SA1292GLInstall Egan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 802.STC ST00716WIInstallation of shoulder harness kit.STC ST01328CHInstall Air Ambulance Conversion.STC ST00881WI-DModification of a TCAS II system installation to Change 7.0 or Change 7.1STC ST00796DEInstallation of Teledyne Battery Products P/N 7638-44T Lead-Acid BatterySTC ST01577LAA replacement of the Honeywell Model AZ-840 Air Data Computers (ADCs), P/N 7014700-901, that were previously installed by Honeywell Supplemental Type Certificate SA6046NM, with new Model AZ-840 ADCs, P/N 7014700-615STC ST01399WIInstallation of Honeywell DL-950 Data Loader.STC ST00800DEModification of a TCAS II system installation to Change 7.1STC ST04238ATUpgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1STC SA2158CEInstallation of the Universal UNS-1 Flight Management System With Version 14.x software with heading select limited to headings which intercept the active leg between waypoints.STC ST09978SCInstallation of Honeywell Integrated Hazard Avoidance System (IHAS) 8000 Class A Traffic Alert System and Class B Terrain Awareness Warning SystemSTC ST01548WIInstallation of seat headrest assembliesSTC ST00892CHInstallation of an AlliedSignal Mark VII Ground Proximity Warning System or AlliedSignal Mark VII Enhanced Ground Proximity Warning System.STC ST02127LAInstallation of a Crane Aerospace & Electronics Tire Sensor AssemblySTC ST03256NYHoneywell MARK VII Enhanced Ground Proximity Warning System (EGPWS) installationSTC ST03216NYInstallation of L3 Communications FA2100 Cockpit Voice Recorder (CVR) SystemSTC ST03217NYInstallation of P-RNAV compliance on the installed Honeywell GNS-XLS Flight Management SystemSTC ST01145CH-DInstallation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II) with MOPS 6.04A or MOPS 7.STC ST01202WI-DModification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision.STC ST00673WI-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 ST00682WI-DModification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I 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 in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.STC ST00064WI-DInstallation of Keith Products Freon Air Condition System.STC ST02810CHInstallation of dual Universal Avionics Systems Corporation UNS-1Lw Flight Management Systems with display on existing Universal Avionics EFI-890R Electronic Flight Instrument Systems (EFIS)STC ST02795CHInstallation of dual Universal Avionics Systems Corporation UNS-1Lw Flight Management Systems with display on existing Honeywell (Sperry) EDZ-601 Electronic Flight Instrument Systems (EFIS)STC SA2110CE-DInstallation of Garrett Model GTCP36-150(W) Auxiliary Power Unit operating as a nonessential electrical and bleed air source for on board electrical and environmental systems.STC ST00703WI-DInstallation of an Allied Signal Enhanced Ground Proximity Warning Systems (EGPWS).STC ST02745CHInstallation of Universal Avionics Systems Corporation Dual UNS-1Espw Flight Management SystemSTC SA519NERemove existing starter-generator and install Aircraft Parts Corp. starter-generator P/N 400SG111Q-4.STC ST01900CHInstallation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System with Terrain Display.STC ST02540AT-DInstallation of replacement fuel tank sealant systemSTC ST02146NYInstallation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX).STC ST00605CH-DInstallation of Honeywell Traffic Alert and Collision Avoidance System (TCAS II).STC ST00606CH-DInstallation of dual Universal Navigation Corp UNS-1CSP Flight Management Systems.STC ST01507CH-DInstallation of Universal Avionics Systems Corporation terrain awareness warning system (TAWS), software control number (SCN) 10.X and Universal Avionics Systems Multi-Function Display (MFD).STC ST604CH-DInstallation oof AlliedSignal Mark VII ground proximity warning system with windshear detection system.STC ST01646CH-DInstallationof Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS) with -011 Application Software and Optional Terrain Display.STC ST02248NYInstallation of EMS HSD-64, HSD-128, HSD-HCM, and HSD-XSTC ST01756CH-DInstallation of Honeywell N1 Digital Electronic Engine Control (DEEC).STC ST01142WI-DModification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head.STC ST00844WI-DModification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter.STC ST01394WI-DModification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation.STC ST00467WI-DInstallation of Rockwell Collins, Inc. TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II).STC ST00554DEInstallation of a Co-Pilot's Digital Air Data Display Unit and relocation of Standby Pneumatic Altimeter. For installation on models 650, Citations III and Citation VI.STC ST02206NYDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Cessna 650, Serial Number 6500042. Installation of Sandel ST3400 TAWS.STC ST00751NYInstallation of a Dual AlliedSignal GNS-XLS flight management system.STC ST01484SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-C650-0415 Rev. New, dated December 3, 2004 or latest FAA approved revision.STC SA2746CE-DInstallation of Bendix/King CAS-81 Traffic Alert and Collision Avoidance System.STC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationSTC ST01946NYCockpit voice recorder replacement with Universal CVR 30B or CVR120.STC ST01262WIInstallation of a 1, 2, or 3 place side facing seat.