N641LB

STCs that may be installed · 71

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 = '3027377'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '03013')
    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 · Mcdonnell Douglas Helicopter 600N

STC SA800EAInstallation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power suppliesWhelen Aerospace TechnologiesSTC SR01050LAInstallation of main rotor blades P/N 500P2300-501/503/505Helicopter Technology CompanySTC SR00862LAInstallation of aft belly utility mount.Airfilm Camera Systems LLCSTC SR01078LAInstallation of right side dual utility mount, in accordance with FAA Approved Aero Pacific Master Drawing List for Right Side Dual Utility Mount, MDL 6003, dtd 4/15/00 or later FAA approved revision.Airfilm Camera Systems LLCSTC SH2735NMInstallation of pneumatic door actuators.Dart Aerospace USA Inc.STC SR02808LAInstallation of MD500 Side Pull KitAerocraft IncorporatedSTC SH5206NMInstallation of two underfuselage jacking hard points.Dart Aerospace USA Inc.STC SR09178RCInstallation of a vapor-cycle air conditioning system with a belt driven compressor.MD Helicopters LLCSTC SR00314ATInstallation of engine firewall in Hughes 369 model helicopterThoroughbred Aviation Maintenance IncSTC SR00450ATInstallation of a seat pan inspection panel.Thoroughbred Aviation Maintenance IncSTC SR01839ATInstallation of cyclic friction leversThoroughbred Aviation Maintenance Inc.STC SR02693LAInstallation of a redundant system for the primary Cargo Hook system when conducting Human External Cargo (HEC) external loads operationsOnboard Systems International LLCSTC SH4908NMFabrication of Onboard Systems Model 200-034-00, 200-034-01, and 200-034-02 Load Weigh KitsOnboard Systems InternationalSTC SR00525SEFabrication of Onboard Systems Model 200-231-00 and 200-231-01 Cargo Hook Attach Point Kit and installation of these Cargo Hook Attach Point KitsOnboard Systems InternationalSTC SR00892SEFabrication of Onboard Systems International Model 200-264-00, 200-264-01, and 200-264-02 Cargo Hook Kits.Onboard Systems InternationalSTC SR02001SEFabrication and installation of Model 72448 locking fuel cover assemblyTimberline Aerospace LLCSTC SR02704SEInstallation and maintenance of the Sunspot 36 and 46 series lightsAeroLED's Holdings LLCSTC SR01343NYInstallation of main rotor blade tie down tips.VIH Aerospace IncSTC SR02124SEInstallation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;Garmin International IncSTC SR02728NYInstallation of Quick Release Mounting Provisions on the right or left sideDart Aerospace LimitedSTC SA615EAInstallation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.Whelen Aerospace TechnologiesSTC SR00359BOInstallation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.Whelen Aerospace TechnologiesSTC SH2554NMInstallation of Modified front window canopy.The NORDAM Group LLCSTC SR02586LAInstallation of Freeflight Systems Radar Altimeter RA-4000 or RA-4500 System with optional FTG-410 Tone GeneratorPrecision Heli-Support, LLCSTC SR00864DEInstallation of Concorde Battery Corporation 24 Ah VRLA Main BatteryConcorde Battery CorporationSTC SR02487AKInstallation of L-3 Communications Avionics Systems ESI-500 Standby Instrument SystemADS-B Technologies, LLCSTC SR02493SEInstallation of a cargo hookMechanical Specialties LLCSTC SR02470AKInstallation of the L-3 Communications NGT -1000/2000/2500 ADS-B SystemADS-B Technologies, LLCSTC SR02471AKInstallation of the L-3 Communications NGT -9000/9000R ADS-B SystemADS-B Technologies, LLCSTC SH4909NMReplace the aft engine compartment heat blanket with a stainless steel firewall.Cascade STC LLCSTC SR01635SEInstallation of a Supplemental Lighting SystemAviation Specialties Unlimited Inc.STC SR02394AKReplacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting systemSeaplanes North LLCSTC SR00877SEInstallation of an engine inlet air filtration systemAerometalsSTC SR02310SEInternal structural provisionBrim AviationSTC SR09640RCInstallation of Night Vision Goggle (NVG) Compatible Lighting SystemAero Dynamix Inc.STC SH1383SOManufacture of Nightscanner searchlight kit.Bell Helicopter Textron Inc.STC SR02255SEInstallation of external cargo racksBrim AviationSTC SH7404SWInstallation of a crew door window.Bell Helicopter Textron Inc.STC SR01960LAInstallation of removable seat pansAerometalsSTC SR00088ATInstallation of replacement windshield and windows.Bell Helicopter Textron Inc.STC SH207WEInstallation of range extension fuel tank in cargo area.ROBERTSON FUEL SYSTEMS LLCSTC SR02232LAInstallation of Garmin Model 400W / 500W Series GPS-WAAS Navigation SystemGarmin AT Inc.STC SR02011SEFabrication of Aerometals, LLC, Transmission Oil Seals in accordance with Master Drawing List Aero-MDL-004, dated November 9, 2009, or later FAA-approved revision; and installation in accordance with the corresponding Aerometals Installation Instructions, as referenced on the continuation page.AerometalsSTC SR02043SEFabrication of Aerometals, LLC, Transmission Oil Seals in accordance with Master Drawing List Aero-MDL-004, dated November 9, 2009, or later FAA-approved revision; and installation in accordance with the corresponding Aerometals Installation Instructions, as referenced on the continuation page.AerometalsSTC SR02062SEFabrication of a replacement Aerometals Heater Control Valve Assembly in accordance with Aerometals Master Drawing List No. Aero-MDL-007, Revision A, dated February 17, 2010, or later FAA-approved revision; and installation of this assembly in accordance with Aerometals Installation Instructions No. Aero-Inst-008, Revision NC, dated March 27, 2009, or later FAA-accepted revision.AerometalsSTC SR01996SEFabrication and installation of an oil tank filler cap assembly in the above model rotor craftAerometalsSTC SR02007SEInstallation of a Brim Aviation cargo rack in accordance with McClenahan Engineering Master Drawing List and Installation Instructions number DM0916-3, revision IR, dated April 21, 2009, or later FAA-approved revision. This modification must be maintained in accordance with Brim Aviation Instructions for Continued Airworthiness number DM0916-9, revision N/C, dated June 17, 2009, or later FAA-accepted revision.Brim AviationSTC SR02008SEInstallation of a Tech Tools 369/500 bubble window in accordance with Brim Aviation Master Drawing List number BR600-010, revision NC, dated June 1, 2009, or later FAA-approved revision. This modification must be maintained in accordance with Brim Aviation Instructions for Continued Airworthiness number BR600-008, revision N/C, dated June 17, 2009, or later FAA-accepted revision.Brim AviationSTC SR02009SEInstallation of Brim Aviation tundra pads in accordance with McClenahan Engineering Master Drawing List and Installation Instructions number DM0916-3, revision IR, dated April 21, 2009, or later FAA-approved revision. This modification must be maintained in accordance with Brim Aviation Instructions for Continued Airworthiness number DM0916-8, revision N/C, dated June 17, 2009, or later FAA-accepted revision.Brim AviationSTC SR01924LAInstallation of a Platinum Aviation cockpit pedestal slant panelIntegrated Flight Systems
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