Learjet 24B

STCs approved for this model · 69

Current certificates 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 model_key = '24B')
  ORDER BY s.status = 'Current' 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 SA01213CHInstall air ambulance conversion in accordance with Spectrum Aeromed Inc. Drawings as listed on AML SA01213CH, or later FAA approved revision.Spectrum Aeromed LLC dba Spectrum AeromedSTC SA01452CHInstallation of an air ambulance conversion kit.Med-Pac Inc.STC SA1170CEStretcher installation in cabin area.Med-Flite of Midamerica IncSTC SA1170GLExcept Model 55: Install Egan Aviation air ambulance stretcher P/N 125 using installation kit P/N 803, inverter/pump kit No. 808, 809, or 810. For Model 55, install air ambulance stretcher P/N 125 using installation kit P/N 804, medical oxygen system kit P/N 807, inverter/pump kit No. 808, 809, or810.Paul/ Lanna Egan LLCSTC SA1639GLInstall air ambulance conversion.Spectrum Aeromed LLC dba Spectrum AeromedSTC SA1670SWInstallation of engine thrust reversers.The NORDAM Group LLCSTC SA1RMInstallation of cargo restraint systemAvcon Industries IncSTC SA2304SWReplacement of plunger type landing gear squat switch with rotary type switch.Sierra 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 SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)Precise Flight Inc.STC SA2661SWInstallation of Ray Model 7507A battery monitoring systemZee Company, IncSTC SA2726SWInstallation of 6-pole rotary squat switches.Sierra Industries, IncSTC SA2788SWInstallation of tail-stringer antenna housing.Sted-Mac CoSTC SA2876WEInstallation of vertical tail floodlights on the horizontal stabilizer.DeVore Aviation Corporation of America, a New Mexico CorporationSTC SA30GLInstallation of electronic engine synchronizer system.Ontic Engineering and Manufacturing Inc.STC SA3249WEInstallation of dual Collins ADF Systems.Learjet IncSTC SA3264WEInstallation of Global GNS-500A VLF navigation system.Learjet IncSTC SA3328WEInstallation of flight data recorder Sundstrand Model FA542.Learjet IncSTC SA3899WEInstallation of Collins F1S-84 Flight Instrument System.Learjet IncSTC SA4059NMInstallation of emergency medical system.Milam International IncSTC SA4060NMInstallation of emergency medical system.Mayo Aviation IncSTC SA412CEInstallation of Woodward Electronic Engine synchronizer system.Ontic Engineering and Manufacturing Inc.STC SA4218WEInstallation of Radio Corporation of America Primus-300SL Color Weather Radar System.Learjet IncSTC SA4403NMInstallation of third attitude indicator that meets the requirements of FAR 121.305(j).Learjet IncSTC SA4999NMInstallation of lifeport patient loading and support system.LifePort LLCSTC 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 SA944NWInstallation of the XR Drag Reduction SystemAvcon Industries IncSTC SA996EAInstallation of Shaw Aero fuel filler cap P/Ns 457-2, -266, -370, 431, -9R, -125, -1251.Parker Hannifin Fluid Systems DivisionSTC ST00016WIInstallation of Electric Floorboard HeatersLearjet IncSTC ST00098IBIntroduction of ADS-B OutSTC Twenty One LimitedSTC ST00361DEInstallation of Puritan Bennett or B/E Aerospace Sweep on 2000 or Zodiac Intertechnique EROS crew oxygen mask.West Star AviationSTC ST00462LAModification of the engine exhaust system.Rooke Corporation dba Aviation EquipmentSTC ST00738WIIncreased service life. Data required.Phoenix Air Group Inc.STC ST00814WILanding Gear Life Extension.Phoenix Air Group Inc.STC ST00835DEInstallation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensorPeregrineSTC ST01138DEInstallation of MidContinent MD23 standby altimeter and/or attitude indicatorsButler National CorporationSTC ST01195WIInstallation of Rosemount Pitot/Static Probes, altimeters, and associated equipment in Learjet 20 series aircraft to obtain Reduced Vertical Separation Minimum approval.Avcon Industries IncSTC ST01733WIInstallation of the Quiet Lear Hushkit or Avcon Noise SuppressorButler National CorporationSTC ST01734WIInstallation of an Emergency Pneumatic Reservoir Assembly, EAS P/N 1260001-02EAS CorporationSTC ST01842SEInstallation of a Sandel Avionics Horizontal Situation Indicator (HSI) and Attitude Direction Indicator (ADI)Butler National CorporationSTC ST01904CHInstallation of IS&S Air Data Display Units 9D-80130-15, Analog Interface Unit 9B-81040-30, and Rosemount model 0856NA pitot-static probes. Limited to Learjet 24 models with MKII wings, 300 kts Vmo airspeed limitation, and JET FC-110 autopilot. Excludes serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.Royal Air IncSTC ST01930LAInstallation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI)Sandel Avionics LLCSTC ST01936WIInstallation of LED lightsAeroLED's Holdings LLCSTC ST01946NYCockpit voice recorder replacement with Universal CVR 30B or CVR120.MidCanada Mod CenterSTC ST02004WIInstallation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI)PeregrineSTC ST02016CHCertification for Reduced Vertical Separation Minimum (RVSM) operational capability. Excluding serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.Royal Air IncSTC ST02097SEInstallation of replacement circuit boards for the FC-110 autopilotSymetric Industries, DBA Extant AerospaceSTC ST02121CHCertification for Reduced Vertical Separation Minimum (RVSM) operational capability and installation of dual Honeywell AM-250 Altimeters and Rosemount model 0856NA Pitot-Static ProbesFlight Test Aerospace, IncSTC ST02230SEThe installation of dual Garmin GTX-33ES Mode-S transponders and single or dual Garmin GTN 650/750 panel mounted navigation and global positioning system (GPS) units, or dual Garmin GTX-335R and/or GTX-345R Mode-S transponders and single or dual Garmin GTN 650/750/625/725 panel mounted navigation and GPS unitsButler National CorporationSTC ST02265CHInstallation of Thrust Reverser Hydraulic System Modifications that were previously installed by STC SA1731SW, SA1669SW or SA1670SWLeading Edge Designs LLC
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