N603AX

STCs that may be installed · 382

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 = '3023501')
    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 DC-10-30

STC ST01347LAInstallation of a lower lobe anti-rollout latch Telair part number 92036-1, -2Telair International LLCSTC ST02489LAInstallation of Telair International Inc. light weight LD3 (NAS3610 / SAE36100 - 2K2) cargo container P/N LD3100-31000ZZZTelair International LLCSTC SA2684WEInstallation of Tridair Industries main deck baggage container system.Telair US LLCSTC ST02524LAInstallation of TCAS version 7.0Aviation Communication and Surveillance Systems (ACSS) LLCSTC SA1359NMInstallation of Stowe Corporation Closet P/N 12535-1.Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA IncSTC SA3892WEInstallation of Stowe Corp. service carts.Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA IncSTC SA3901NMInstallation of a Coatroom.Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA IncSTC ST01870LAInstallation of an external tank, associated systems and support structure for the aerial dispersant of liquids.10 Tanker-STC LLCSTC ST03483ATInstallation of a Portable Beverage Dispensing System, P/N B43-FA-001.Dynamo Beverage Company, USA, L.L.C.STC ST00503LAInstallation of Securaplane Model No. BC-1302 Battery Charger, Battery Temperature Sensor Model No. BTS-1302 and Remote Display Unit Model No. DU-1302 as a form, fit, and functional replacement for the existing General Electric Battery Charger System.Securaplane TechnologiesSTC ST02050LAInstallation of Goodrich-Hella Anticollision Recognition Lighting System (ARLS)GoodrichSTC ST00526WI-DModification of Collins VHF COMM Receiver InstallationRockwell Collins IncSTC SA2955SOReplacement of existing electromechanical fuel quantity indicators with Smiths Industries digital fuel quantity indicatorsOntic Engineering and Manufacturing Inc.STC SA5016NMInstallation of cargo containers.Satco IncSTC ST00337LAInstallation of Teledyne Controls' Optical Quick Access Recorder (OQAR)Teledyne ControlsSTC SA3415NMInstallation of a main cabin cargo handling system.Ancra International LLCSTC ST03944ATInstallation of Avionica, Inc. satLINK System to provide voice and short burst data communications over the Iridium satellite Communications network (SATCOM), with Wi-Fi voice over IP (VoIP) cordless phone in accordance with Archeion Holdings LLC Master Data List 102810-MDL, Revision D, Dated January 17, 2012, or later FAA approved revisions.Archeion Holdings LLCSTC SA1135NW-DInstall fireproof blankets on the Engine Fan Reverser Intermediate Fireseal, in lieu of Fireproof Intumescent Coating, in accordance with United Air Lines DAS-1-WE, Approved Drawing List No. 1135 dated March 23, 1982, or later FAA approved revisions.United Airlines IncSTC SA1144NW-DInterchangeable cart installations.United Airlines IncSTC SA1935NW-DCabin configuration changed to 24 F/C/72 business/141 coach seats. Installed two double closets, one single closet and the foldable crew rest berth in the door 2 area. Installed video in zones A, B & C. Removed centerline overhead storage compartments in zone A. Relocated lights and emergency oxygen supply to suit new cabin configuration. Replaced emergency evacuation alarm system with one similar to 747 system. This reconfiguration is accomplished according to United Air Lines, DAS-1-WE, Approved Drawing List No. 1935 dated June 16, 1983, or later approved revisions.United Airlines IncSTC SA1936NW-DInstallation of DC-10-10 yaw damper computers on DC-10-30 aircraft per COA 3-2958. This change order will replace Bendix yaw computers P/N 3757082-7 with Bendix yaw computers P/N 3757091-9 with mod "H" accomplished. The installation will be in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 1936 dated June 7, 1983 or later FAA approved revisions.United Airlines IncSTC SA1947NM-DTraining requirements, special limitations, and installation of required provisions, including communications and equipment, to permit occupancy of the lower galley during taxi in accordance with FAA approved United Air Lines, Inc. Drawing List No. 1947 or later approved revisions and United Air Lines Approved Flight Manual Supplement dated September 10, 1984, to FAA Approved Airplane Flight Manual MDC-J5830.United Airlines IncSTC SA1948NM-DCabin configuration will be changed to accommodate 40 first class and 230 coach passengers. One each clothes closet will be installed aft of RH and LH Door 1. Cart stowage units will be installed aft of RH and LH Door 2. Miscellaneous and emergency equipment will be relocated as required. Projection Video System will be installed. See Approved Drawing List dated October 1, 1984.United Airlines IncSTC SA1949NM-DInstallation of DC-10-10 roll & pitch computers on DC-10-30 aircraft per COA 3-3047. This change order will replace Bendix roll computer P/N 3757319-7 and pitch computer P/N 3757320-7 with Bendix roll computer P/N 3757087-9 and pitch computer 3757121-9. The installation will be in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 1949 dated October 9, 1984, or later FAA approved revisions and approved Airplane Flight Manual Supplement MDCJ5830 dated September 24United Airlines IncSTC SA2700NM-DCabin configuration changed to accommodate 40 first class and 230 coach passengers. Crew rest facility located forward of Door 2RH and closet located at Door 2LH removed.United Airlines IncSTC SA2705NM-DCabin configuration changed to accommodate 40 F.C. and 245 coach passengers. Coat closet installed aft of LH & RH Door 1.United Airlines IncSTC SA2711NM-DModifies the aircraft to install an emergency escape path lighting system. The installation is in accordance with DAS-1-WE Approved United Air Lines Drawing List 2711 dated August 10, 1986, or later FAA approved revisions.United Airlines IncSTC SA2726NM-DInstallation of an ARINC Communication Addressing and Reporting System (ACARS).United Airlines IncSTC SA2751NM-DModifies the outboard flap actuator, or actuators, incorporating a UA design piston. The installation is in accordance with DAS-1-WE Approved United Air Lines Drawing List No. 2751, dated August 17, 1988, or later FAA approved revision.United Airlines IncSTC SA2794NM-DThe activation of the Windshear function of the Sundstrand Mark VII Dual Function Ground Proximity/Windshear Warning System Computer. The installation is in accordance with United Air Lines DAS 1 WE Approved Amended Drawing List No. 2794 dated April 29, 1993 or later FAA approved revision. United Air Lines Approved Flight Manual Supplement to FAA Approved Flight Manual No. MDC-J5830 dated April 26, 1993 or later FAA approved revision is required as part of this modification.United Airlines IncSTC SA2795NM-DInstallation and activation of a Collins Radio TCAS Processor and Collins Radio TCAS Type Weather Radio Indicators, on aircraft that have been previously equipped with full TCAS provisions, in accordance with United Air Lines DAS-1WE Approved Drawing List 2795 dated October 7, 1991 or later FAA approved revision. United Air Lines Airplane Flight Manual Supplement to FAA Approved Flight Manual Number MDC-J5830, dated October 8, 1991, or later FAA approved revision, is required as part of this modification.United Airlines IncSTC SA2817WE-DTwo additional serving cart tie down fittings are installed at Fus. Sta. 1289.0, Butt Line 86.20 left and right. Two cart tie down fittings are relocated from Fus. Sta. 816.00 to Sta. 821.75, Butt Line 86.20 left and right. Installations in accordance with DAS-1-WE United Air Lines Drawing List 2817 dated October 1, 1974 or later FAA approved revision.United Airlines IncSTC SA2830WE-DInstallation of Collins FPC-75, P/N 622-2615-012 or -011, Rev. N or P/N 622-2615-212 or -211 in accordance with DAS-1-WE Master List of drawings and documents for United Air Lines Change Order Authorization Nos. 3-1719, 3-1863, and 3-1864, dated February 26, 1979 or later FAA approved revisions. One of the following is required as part of this installation: United Air Lines FAA Approved Airplane Flight Manual Supplement dated March 30, 1976, or later FAA approved revisions to McDonnell Douglas Airplane Flight Manual Document No. MDC-J1010; United Air Lines FAA Approved Flight Manual Supplement dated June 19, 1976, or later FAA approved revision to McDonnell-Douglas DC-10-30 Airplane Flight Manual Document No. MDC-J1030.United Airlines IncSTC SA3031WE-DFour additional serving cart tie-downs are installed on main deck;United Air Lines Inc.STC SA4843NMInstallation of Kaiser ElectroPrecision Lavatory Auto-Dump Kit System, installation on DC-10, Main Deck Lavatory positions 1, 2, 3, 4, 5, 6, 7, C and D, in accordance with FAA Approved Kaiser ElectroPrecision Drawing RYY509-027, Revision "A", dated February 7, 1990, or later FAA approved revision.Rockwell Collins Inc.STC ST00700WIInstallation of Penny & Giles Recording Exhaust-Gas Temperature Indicator 65009-004 EGT in accordance with: (1) Penny & Giles Aerospace, Inc. Recording EGT Model 65009 Installation Manual Document #65009-004-011, Revision -, dated May 1, 1998; and (2) Penny & Giles Aerospace, Inc. Airplane Flight Manual Supplement (AFMS) Drawing #65009-004-013, Revision "original", dated August 19, 1998; or later FAA Approved Revisions to (1) or (2).Teledyne ControlsSTC ST00759WIReplace existing engine instruments with the Penny & Giles Aerospace, Inc. Engine Instruments Display System (EIDS). Model 94002, in accordance with (1) Installation Data referenced on Continuation Sheet 2; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Continuation Sheet 2; or later FAA Approved Revisions to (1) or (2). (see continuation sheet 2 of 2)Teledyne ControlsSTC ST03046ATInstallation of an ADAM Communication and Information Management System with IRIDIUM SATCOM System and three Class 2 Electronic Flight Bags in accordance with Avionics Support Group, Inc. Master Drawing List 24652-MDL, Revision H, dated July 12, 2011, or later FAA approved revision.Avionics Support Group IncSTC SA2914NMInstallation of Centerline Stow Bins.Aim Aerospace IncSTC SA3313NMInstallation of a class divider.AIM Aviation IncSTC SA3698NMInstallation of Centerline Stow Bins.AIM Aviation IncSTC SA713NWInstallation of Class Divider.AIM Aviation IncSTC ST00634SEInstallation of sidewall panels.Aim Aerospace IncSTC ST00991AT-DInstallation and operation of The Shaw Aero Devices, Inc. 331 & 332 Series Waste Drain and 580 Series Lavatory Rinse/Fill Values.Parker Hannifin - Fluid Systems DivisionSTC 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 ST02622NYAFIRS 220 Automated Flight Information Reporting System Installation with Optional Global Voice Satellite Communications to be installed in accordance with FLYHT - AeroMechanical Services Installation Instructions 151-0037, Revision B, dated March 26, 2009, or later Transport Canada approved revision.AeroMechanical Services LtdSTC SA2043NMInstallation of Delco Performance Management SystemBoeing CompanySTC ST02857CHInstallation of Electronic Flight Bag provisions and Aircraft Wireless LAN UnitCanard Aerospace CorporationSTC SA339CHInstallation of replacement Immersion Heater.Aircraft Food Service Equipment RepairSTC ST01338CHInstallation of an Auxiliary Power Unit Door Actuator System.Woodward MPC
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