N342JC
STCs that may be installed · 102
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 = '7850100'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '30031')
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 = '7850100'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '30031')
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 · Saab-Fairchild 340A
STC SA2470CEInstallation of B&D Instruments & Avionics, Inc. Electronic Propeller Gear Box Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7330-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7330-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2471CEInstallation of B&D Instruments & Avionics, Inc. Electronic Engine Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7380-003-024, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7380-003-024, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2472CEInstallation of B&D Instruments & Avionics, Inc. Electronic Gas Generator Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7320-003-011, dated January 23, 1989, or later FAA Approved revision; for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7320-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (2) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7321-004-011 dated September 12, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2473CEInstallation of B&D Instruments & Avionics, Inc. Electronic Torque Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7300-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7300-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7301-003-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.STC SA2493CEInstallation of B&D Instruments & Avionics, Inc. Electronic Interturbine Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision A, dated March 13, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision D, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2494CEInstallation of B&D Instruments & Avionics, Inc. Electronic Propeller Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7310-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7310-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7311-004-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.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 SA2180CE-DInstallation of Garrett Model GTCP-150(W) Auxiliary Power Unit operating as a nonessential electrical and bleed air source for on board electrical and environmental systems.STC SA367NEInstallation of GE CT7-5A2 engines.STC SA4217NM-DEngine air-intake duct modification.STC SA829NERemove existing starter-generators and install APC starter-generator P/N 400SG112Q.STC SA2736CE-DInstallation of Bendix/King CAS-81 traffic alert and collision avoidance system and MST-67A mode-S transponder (2 each).STC SA984GL-DInstallation of a Bendix TCAS II system comprised of the following model numbers: TPA-81A, TCAS Processor, two MST-67A, Mode S transponders, KFS-578A, TCAS control, two IVA-81A, TA/VSI indicators, two ANT-81A, TCAS antennas, and two Dorne and Margolin DMNI 70-2, mode S antennas.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 ST09384SCInstallation of a single Universal Avionics UNS-IK Flight Management System with integrated GPS.STC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationSTC ST00545DEInstallation of a Tropospheric Airborne Meteorological Data Reporting (TAMDAR) system.STC ST00093NYInstallation of APC Generator Control Unit GCSG505-5.STC ST23BOInstallation of a Collins TCAS-94 traffic collision avoidance system(TCAS-II).STC SA3681NMCockpit sun visor installation.STC ST00814ATInstallation of replacement floorboards.STC SA3667SWInstallation of a freon air conditioning system.STC SA7971SWInstallation of freon air conditioning using Enviro Systems, Inc. components.STC SA8114SWInstallation of a cabin auxiliary heater system (electric), ground use only.STC ST01176NYInstallation of replacement floor panels in the cabin and cargo compartment.STC SA7485SWInstallation of DeVore Tail Floodlights.STC ST00341LAInstallation of Nasco Aircraft Brake or SGL Carbon Composites brake stack kit P/N 3001049, in Aircraft Braking Systems brake assembly p/n 5012589-1 or 5012589-2.STC ST01115CHInstallation of Model 1200 Galley Unit Numbers 1, 2, and 3.STC SA8979SWRecore of Hamilton Standard P/N 779215 heat exchanger with a new core.STC ST09277SCInstallation of an Improved Transmissivity Radome.STC ST00848ATReplacement of high maintenance open terminal with a closed switching assembly for the engine anti-icing sensor.STC SA8941SWInstallation of retrofit engine inlet icing protective system.STC ST181CHInstallation of a landing light pulsing system.STC SA2666CEInstallation of Collins TCAS-94 traffic alert and collision avoidance system.STC SA2483CEReplace either one or both of the original ventilation blowers with Advanced Ind. Inc., BC112A blower assembly.STC ST60CHInstallation of PN 4881X.STC ST32CHInstallation of parking brake cable.STC SA2736CEInstallation of Bendix/King CAS-81 traffic alert and collision avoidance system and MST-67A mode-S transponder (2 each).STC SA1444GLInstallation of MAPCO Model 1075 liquid container module in Metair left side galley (P/N 38-94-1).STC SA2615CEInstall dual Collins TDR-94D Mode S transponders.STC SA2180CEInstallation of Garrett Model GTCP46-150(W) auxiliary power unit, operating as a non-essential electrical and bleed air source for on board electrical and environmental systems.STC SA3584SWInstallation of ONI Loran C Model 7000 navigation system.STC SA5966SWInstallation of wingtip recognition lights.STC SA5969SWInstallation of Baker M2000 passenger auto briefing system.STC SA5970SWInstallation of Eldec fuel used and fuel remaining system.STC SA5976SWInstallation of Global GNS-1000 flight management system.STC SA5978SWRelocation of aisle to center from left to center.STC SA5979SWService port installation.STC SA5980SWInstallation of thermal and acoustical insulation.