N65ML

STCs that may be installed · 107

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 = '7630107'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '29001')
    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.

Airframe · Rockwell International NA-265-65

STC ST00605WIInstallation of Universal Avionics Systems dual UNS-1K, UNS-1L, or UNS-1Lw Flight Management System with dual GPS.Sabreliner Aviation LLCSTC ST00614WIInstallation of L3 Systems S703-1000-00 solid state digital flight data recorder.Sabreliner Aviation LLCSTC ST00788WIInstallation of the Honeywell CAS 67A TCAS II System with TPU 67A Processor, Dual MST 67A Mode S Transponders, and Dual IVA-81A or IVA-81D TA/RA/VSI Indicators.Sabreliner Aviation LLCSTC ST00969WIInstallation of Honeywell Mark VIII Enhanced Ground Proximity Warning SystemSabreliner Aviation LLCSTC ST00995WIInstallation of ARTEX 110-406 MHz Emergency Locator Transmitter.Sabreliner Aviation LLCSTC ST01054WIInstallation of a Universal Corp Terrain Awareness Warning System (TAWS)Sabreliner Aviation LLCSTC 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 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.Rockwell Collins IncSTC ST01256WI-DModification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision.Rockwell Collins IncSTC ST01518WIInstallation of Eyebrow and Upper Aft Cockpit Window Plugs in place of the existing Cockpit Windows.Aviation Maintenance & Technical SupportSTC ST01965CH-DInstallation of Honeywell N1 Digital Electronic Engine Controls (DEEC)Honeywell International IncSTC ST00699CH-DInstallation of an AlliedSignal Aerospace TFE731-3DR-1D Turbofan Engine.Honeywell International IncSTC 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 ST1344CH-DInstallation of dual Honeywell Enhanced GNS-XLS Flight Management Systems.Honeywell International 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 ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationRockwell Collins IncSTC ST01134SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM). Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to the Rockwell International Model NA-265-65 (Sabreliner 65) only.AeroMech IncorporatedSTC ST01941CHInstallation of a Honeywell CAS-67A Traffic Alert and Collision Avoidance System (TCAS II).Spirit Avionics LTDSTC ST00728WIInstallation of either a Honeywell Inc. TCAS-2000 TCAS II System or a L3 Communications TCAS 2000 TCAS II System.Aviation Maintenance & Technical SupportSTC SA1637NMStair and handrail modification.Rosen Sunvisor Systems LLCSTC SA1256SOInstallation of Utah Research and Development Company Model126BC101 battery charging system.Aviall Services, Inc.STC ST00050DE-DInstallation of Bendix/King CAS-81 TCAS II system.Learjet IncSTC ST00943WIInstallation of Universal Avionics System Corporation terrain awareness system (TAWS).Aviation Maintenance & Technical SupportSTC SA2878SWInstall two two-place side facing couches.Aviation Fabricators IncSTC ST00933SEThis approval is limited to the Sabreliner 265-65, Serial Number 465-74. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-SL65-0101, Revision "New," dated June 14, 2001.AeroMech IncorporatedSTC ST00664WIInstallation of dual Universal Avionics UNS-1K flight management systems as a GPS primary means of navigation for oceanic/remote operations.Aviation Maintenance & Technical SupportSTC ST00921WI-DInstallation of a dual collins AHS-3000A Atttitude Heading Reference System.Rockwell Collins IncSTC ST00919WI-DInstallation of a single Collins GNLU-930 Multi-Mode Receiver System.Rockwell Collins IncSTC SA1724SWInstallation of freon air conditioner.Signature Flight Support CorporationSTC SA4456SWInstallation of Dual Global GNS-500A series III Omega navigation system with Vandling Model NDB-2 navigation data bank.Signature Flight Support CorporationSTC SA3052WEInstallation of Vertical Tail Floodlights on horizontal stabilizerDeVore Aviation Corporation of America, a New Mexico CorporationSTC SA2642CEInstallation of Collins Traffic Alert and Collision Avoidance System, TCAS II.Rockwell Collins IncSTC ST00698WIReduction in the maximum seating configuration from 10 to 9 by removal of the seat belt from the forward lavatory passenger seat and installing a placard 'DO NOT OCCUPY DURING TAKE-OFF AND LANDING' above the seat back. One-Time only STC for S/N 465-42.Executive Aircraft CorporationSTC ST00891CHInstallation of Fairchild F-800 digital flight data recorder.ElectroSonicsSTC ST01622ATModification is for an electrical change to the fuel transfer system.Jet Harbor, IncSTC ST00844CHInstallation of dual Universal UNS-1K Flight Management Systems.ElectroSonics Div of AiRadio CorporationSTC ST01294ATInstallation of Concorde RG-380E/40 valve regulated sealed lead-acid battery as replacement of installed Ni-Cad Battery.Jet Harbor, IncSTC ST00667CHInstallation of Dual AlliedSignal GNS-XLS flight management systems as primary means of navigation for oceanic and remote airspace.ElectroSonics Div of AiRadio CorporationSTC ST1031SOReplace existing nickel-cadmium batteries with Teledyne Gill BB638/T series lead-acid type batteries.Teledyne Battery Products · Lists NA-265 SeriesSTC SA1972SWInstallation of BKM 100-265 nose wheel steering control.Aviation Material and Technical SupportSTC SA2997SWInstallation of nose wheel steering transfer test switch.Aviation Material and Technical SupportSTC SA4223SWInstallation of Hydraulic fluid level warning and hydraulic pump run advisory system.Aviation Material and Technical SupportSTC SA4373SWInstallation of BKM 78-2610-1 nose wheel steering feedback potentiometer assembly.Aviation Material and Technical SupportSTC SA8976SWReduce maximum passenger seating configuration from 10 to 9 by removing the seat belt and installing a placard by the forward lavatory passenger seat.Jet East, IncSTC ST00241NY-DInstallation of a Single Bendix/King CAS-66A TCAS I system, and Single TA/IVSI.Delta EngineeringSTC SA2745CEInstallation of the Universal Navigation Corp. CVR-80 cockpit voice recorder.Rockwell Collins IncSTC SA2544CEInstallation of single or dual hydraulic starting system.Midcoast Aviation IncSTC SA1121GLInstallation of Dorne and Margolin DMN 4-17() VOR/ILS antenna on vertical stabilizer.Butler Aviation-Pal-Waukee IncSTC SA1998CEInstallation of Scott/EROS quick donning mask and regulator.Sabreliner Corp
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