TCDS A10CE

STCs approved under this data sheet · 1,102

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 = 'A10CE')
  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 ST02985NYInstallation of a Honeywell CAS 66A TCAS 1 Installation on a Learjet inc. Model 31, in accordance with Bombardier Aerospace Master Drawing List BAS31010032 Revision NC, dated September 12, 2007, or later approved revision.Amtech Aeronautical LimitedSTC ST02982NYAircell ST3100 Satcom installation in accordance with Bombardier Inc. Master Document List BAS31010034 Revision N/C, Transport Canada approved September 12, 2007, or later Transport Canada approved revision.Amtech Aeronautical LimitedSTC SA996EAInstallation of Shaw Aero fuel filler cap P/Ns 457-2, -266, -370, 431, -9R, -125, -1251.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 ST01620WI-DInstallation of a new DC-to-DC Dual Boost Power Converter on a Learjet 60XR aircraft in accordance with Learjet Inc. Master Document List M100543ICT, revision (C), dated February 4, 2011, FAA approved February 4, 2011, or later FAA approved revision. Instructions for Continued Airworthiness, M100543ICT-ICA-001, revision (NC), dated January 17, 2011, FAA accepted February 4, 2011, or later FAA accepted revision, are required for MDL M100543ICT-001 configuration.Learjet 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 ST01614WI-DInstallation of Airfield Technology, Inc., (ATI) AT-950 Flight Inspection System (FIS) with a Crossbow Technology, Inc., Attitude Heading Reference System (AHRS). Data Required: (1) Duncan Aviation Inc., Document List No. 100325015, Revision A, dated December 03, 2010, (2) FAA Approved Airplane Flight Manual Supplement, Duncan Aviation Inc., Document No. 100219044, Revision A, dated December 03, 2010, or later FAA Approved Revisions to (1) or (2).Duncan Aviation IncSTC SA225NWInstallation of the Mark II performance system, including recontoured wing leading edge, recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements.Avcon Industries IncSTC SA232NWInstallation of the Mark II performance system, including recontoured wind leading edge, recontoured flap leading edge, wind vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1082 dated November 16, 2010, or later FAA approved revision. 350 Knot Vmo authorized if equipped in accordance with Avcon Master Drawing List No. 1082 dated November 16, 2010, or later FAA approved revision. An FAA approved airplane flight manual supplement is required for each model.Avcon Industries IncSTC SA253NWInstallation of the Mark II performance system, including recontoured wing leading edge, recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1084 dated November 16, 2010, or later FAA approved revision. 350 Knot Vmo authorized if equipped in accordance with Avcon Master Drawing List No. 1084 dated November 16, 2010 or later FAA approved revision. An FAA Approved Airplane Flight Manual Supplement is required for each model.Avcon Industries IncSTC SA841NWInstallation of the Mark II performance system, including recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1085 dated November 16, 2010, or later FAA approved revision. 350 Knot Vmo authorized if equipped in accordance with Avcon Master Drawing No. 1085 dated November 16, 2010, or later FAA approved revision. An FAA approved Airplane Flight Manual Supplement is required for each model.Avcon Industries IncSTC SA900NW: Installation of the Mark II performance system, including recontoured wing leading edge, recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1086 dated November 16, 2010, or later FAA approved revision. An FAA approved Airplane Flight Manual Supplement is required for each model.Avcon Industries IncSTC SA1489CERemoval of 24-inch wide executive door and installation of 36-inch wide cargo door per AVCON Drawing List 36000 stamped FAA Approved with a date of May 8, 1979, July 3, 1980, November 15, 2010, or later approved revision for Learjet Models 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A, 36, and 36A.Avcon Industries IncSTC ST09488AC-DInstallation of Multi-Mode Receiver, GNLU-930.Aviation System Standards Aircraft Maintenance and Engineering Division, AJW-344STC ST00646WI-DInstallation of AlliedSignal Enhanced Ground Proximity Warning System.Learjet IncSTC ST00390WIInstallation of MTR-101 reeling machine on one of both wings.AVT CorporationSTC ST00858WI-DInstallation of Collins TCAS-94 TCAS II systemDuncan Aviation IncSTC ST01586WI-DInstallation of a FMS-5000 Flight Management System W/GPS-4000S (WAAS W/LPV) on a Learjet 60XR aircraft.Learjet IncSTC ST01585WI-DInstallation of a new floorplan on a Learjet 60XR aircraft.Learjet IncSTC ST01579WI-DInstallation of a Rockwell Collins DBU-5000 Data Loader on the Learjet 60XR aircraft.Learjet IncSTC ST00952SE-DGroup aircraft approved for Reduced Vertical Separation Minimum (RVSM).Learjet IncSTC ST01587WI-DUpgrade of a single Universal Avionics Systems Corporation (UASC) UNS-1C Flight Management System (FMS) to UNS-1Ew FMS with Wide Area Augmentation system (WAAS) and Localizer Performance with Vertical guidance (LPV) Monitor.Duncan Aviation IncSTC SA1553NMInstallation of one or two 90 US gallons fuselage auxiliary fuel tank(s), in accordance with Branson List of Drawings and Documents, No. 61A000, Revision B, FAA approved May 16, 1983, or later FAA approved revision.Avcon Industries IncSTC SA2446SWInstallation of cabin door closing system in accordance with Drawing List No. 34 dated 3/17/80 or later FAA approved revision.Avcon Industries IncSTC SA2715SWInstallation of access doors in engine nacelle according to Drawing 375201, Revision A, dated 1/13/78, or later FAA approved revision.Avcon Industries IncSTC SA5516SWInstall Sperry SPZ500LR Automatic Flight Control System in accordance with Dee Howard Drawing List No. 46, Rev. D, dated 8/26/83 or later FAA approved revision.Avcon Industries IncSTC ST01551WI-DActivation of the Wireless Local Area Network (WLAN) for Satcom System on a Learjet 60XR aircraftLearjet IncSTC ST09476AC-DInstallation of dual Universal UNS-1F Flight Management System.Aviation System Standards Aircraft Maintenance and Engineering Division, AJW-344STC ST01527WI-DInstallation of Microwave Oven in the Right Hand Forward Galley on Learjet 60XR aircraftLearjet IncSTC ST00013WI-DInstallation of a modified engine bleed air mixing valve regulated air source.Duncan Aviation IncSTC ST03065AT-DInstallation of a Single Universal UNS-1C+ or UNS-1E Flight Management SystemLearjet IncSTC ST01564WI-DModification of a Rockwell Collins, Inc. RAC-870 Radio Altimeter Converter installation.Rockwell Collins IncSTC SA2755CE-DInstallation of Collins TCAS-94 Traffic and Collision Avoidance System with Collins TDR-94D Mode-S Transponder (2 ea).Duncan Aviation IncSTC ST01542WI-DModification of a Rockwell Collins, Inc. AFD-3010 and AFD-3010E Adaptive Flight Display Installation in Part 25 Aircraft.Rockwell Collins IncSTC ST00032MCInstallation of the Rockwell Collins AHC-3000S Attitude Heading Reference System.Learjet Inc.STC ST03828ATInstallation of Runway Awareness and Advisory System (RAAS)Stevens Aviation Inc.STC ST00510WIInstallation of tip tank baggage compartments.Avcon Industries IncSTC ST00031MCInstallation of the Universal Avionics Sytems Corporation Vision-1 System.Learjet Inc.STC ST00034MCInstallation of (a) the Universal Avionics Systems Corporation UNS-1LW & UNS-1FW Flight Management System with a Wide Area Augmentation System and (b) the Trimble Model TA-12 Global Positioning System.Learjet Inc.STC ST02710CHThis design change is valid only for Learjet 60 aircraft, serial numbers 002 through 0248. Installation of an L-3 Communications Avionics Systems GH-3100 Electronic Standby Instrument System (ESIS)West Star Aviation IncSTC ST02766CHInstallation of dual Universal Avionics Systems Corporation UNS-1Ew Flight Management SystemsWest Star Aviation IncSTC ST00077WI-DInstallation of a Sundstrand Mark VII Ground Proximity/Windshear Warning System.Duncan Aviation IncSTC ST00317WI-DInstallation of an Allied-Signal Mark V Ground Proximity Warning System (GWPS).Duncan Aviation IncSTC ST00318WI-DInstallation of an Allied Signal Sundstrand Mark VII Ground Proximity Warning System (GPWS).Duncan Aviation IncSTC ST00550WI-DInstallation of Universal Avionics, Inc., UNS-1D Flight Management System (Dual).Duncan Aviation IncSTC ST00581WI-DInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS).Duncan Aviation IncSTC ST00702WI-DUpgrade of the existing AlliedSignal MK-V GPWS with Windshear to Enhanced (EGPWS) capabilities with display in the Learjet Model 60 Airplanes.Duncan Aviation IncSTC ST01024WI-DInstallation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).Duncan Aviation IncSTC ST01480NY-DInstallation of a Universal Avionics Terrain Awareness System (TWAS).Duncan Aviation Inc
Back to TCDS A10CE