TCDS A52EU

STCs approved under this data sheet · 128

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 = 'A52EU')
  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.

STC SA3538SWInstallation of Refuel Panel Door Switch GuardM7 Aerospace LLCSTC SA3540SWInstallation of 16 place executive interiorM7 Aerospace LLCSTC SA3657SWInstallation of a 19 place executive interiorM7 Aerospace LLCSTC SA5965SWInstallation of rechargeable flashlights.M7 Aerospace LLCSTC SA5968SWInstallation of Dual Davtron Digital ClocksM7 Aerospace LLCSTC SA5971SWInstallation of J.E.T. Standby Gyro-HorizonM7 Aerospace LLCSTC SA5972SWInstallation of TAI-80A SAT-TAS-TAT IndicatorsM7 Aerospace LLCSTC SA5973SWInstallation of IDC Standby Airspeed and Standby AltimeterM7 Aerospace LLCSTC SA5974SWInstallation of Copilot s IDC Airspeed, Vertical Speed and Rad-Bar AltimeterM7 Aerospace LLCSTC SA5975SWInstallation of Flight Fone V Communication SystemM7 Aerospace LLCSTC SA5977SWInstallation of 14 place executive interior.M7 Aerospace LLCSTC ST03135NYActivation of Free Directional Gyro ModeACS-NAI LimitedSTC SA3583SWInstallation of IDC Pneumatic Encoding Altimeter.M7 Aerospace LLCSTC SA5967SWInstallation of Collins CTL Proline II (CTL-22/22/32/62/92, CAD62, BD136, and IND42C).M7 Aerospace LLCSTC 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.Teledyne ControlsSTC 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.Teledyne ControlsSTC 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.Teledyne ControlsSTC 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.Teledyne ControlsSTC 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.Teledyne ControlsSTC 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.Teledyne ControlsSTC 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.Rockwell Collins IncSTC 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.Rockwell Collins IncSTC 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.Duncan Aviation IncSTC SA367NEInstallation of GE CT7-5A2 engines.General Electric CoSTC ST02357AKLimit the maximum passenger seating capacity to 19Peninsula Airways IncSTC SA4217NM-DEngine air-intake duct modification.GKN Aerospace Transparency Systems Inc.STC SA829NERemove existing starter-generators and install APC starter-generator P/N 400SG112Q.Skurka Aerospace Inc.STC SA2736CE-DInstallation of Bendix/King CAS-81 traffic alert and collision avoidance system and MST-67A mode-S transponder (2 each).Duncan Aviation IncSTC ST02349AKLimit the maximum passenger seating capacity to 30Peninsula Airways IncSTC ST02540AT-DInstallation of replacement fuel tank sealant systemFFC ManufacturingSTC 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.Standard AeroSTC 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.Rockwell Collins IncSTC 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.Rockwell Collins IncSTC ST01394WI-DModification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation.Rockwell Collins IncSTC ST09384SCInstallation of a single Universal Avionics UNS-IK Flight Management System with integrated GPS.New SystemsSTC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationRockwell Collins IncSTC ST01697LAIncrease maximum zero fuel weight.Altair Holdings LimitedSTC ST00545DEInstallation of a Tropospheric Airborne Meteorological Data Reporting (TAMDAR) system.FLYHT Inc.STC ST00093NYInstallation of APC Generator Control Unit GCSG505-5.Aircraft Parts CorporationSTC ST02685ATInstallation of a FA2100CVR Cockpit Voice Recorder (CVR).Chippewa Aerospace, Inc.STC ST23BOInstallation of a Collins TCAS-94 traffic collision avoidance system(TCAS-II).Wiggins AirwaysSTC SA3681NMCockpit sun visor installation.Rosen Sunvisor Systems LLCSTC ST00814ATInstallation of replacement floorboards.TMG AirpairsSTC SA3667SWInstallation of a freon air conditioning system.AAR Airframe and Accessories GroupSTC SA7971SWInstallation of freon air conditioning using Enviro Systems, Inc. components.AAR Airframe and Accessories Group IncSTC SA8114SWInstallation of a cabin auxiliary heater system (electric), ground use only.AAR Airframe and Accessories Group IncSTC ST01176NYInstallation of replacement floor panels in the cabin and cargo compartment.Comtek Advanced Structures Ltd.STC SA7485SWInstallation of DeVore Tail Floodlights.DeVore Aviation Corporation of America, a New Mexico CorporationSTC ST09615SCInstallation of Model 925 passenger seats, manufactured by B/E Aerospace under TSO C39b, in lieu of the existing series 121 seats.American Eagle Airlines IncSTC 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.NASCO Aircraft Brake Inc
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