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 = '188C') 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.
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 = '188C') ORDER BY s.status = 'Current' DESC, s.stc_number
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC SA1060GLInstallation of Norton Radome Kit4306CX.STC SA1081SOIncrease in fuel weight from86,000 pounds to 92,340 pounds.STC SA1149SWInstallation of a hot water heater.STC SA1150SWInstallation of Litton LTN 51 inertial navigation system.STC SA1178WECockpit voice recorder.STC SA1206WEBeta range override control switch.STC SA132CEOverspeed warning system.STC SA133SOCockpit voice recorder.STC SA1495SOModification of Flight Equip. and Engrg. double passenger seat model650L to attach a double shoulder harness/lap belt assembly.STC SA1506GLRebuilt alternate flap drive torque tube assembly P/N 807723-R, rebuilt Lockheed P/N 807723 with 4130 tubing and type design end fittings.STC SA1506GL;Rebuilt alternate flap drive torque tube assembly P/N 807723-R, rebuilt Lockheed P/N 807723 with 4130 tubing and type design end fittings.STC SA158SOOverwing emergency escape ropes.STC SA1637WEInstallation of cargo door approximately 80 inches high by 144 inches long in left side of fuselage forebody.STC SA1754WEInstallation of cargo doors, cargo floor and other changes. (188A, 188C Aircraft SN 1070 and higher are eligible.)STC SA1779WEInstallation of Heathair AC-10194, AC-10195 pallets and Heathair AC-10196, AC-10197 nets on Lockheed electra model 188C cargo freighter.STC SA1833SOInstallation of an aft cargo door and cargo compartment interior.STC SA1834SOInstallation of a forward cargo door and cargo compartment interior.STC SA1982WEInstallation of luggage barrier.STC SA1984WEInstallation of inflatable slide for right rear emergency exit and for left rear service door; also International Inflatables emergency light No. 68555.STC SA2012SOInstallation of a divider and a courier seat.STC SA2043SOInstallation of dual Sperry SPI-402, flight director system.STC SA2092WEInstallation of Heath 54 x 88-inch cargo pallet AC-10528-1 and net AC-10657-101.STC SA2152WEInstallation of Heath 88 x 108 inch cargo pallet AC-10527-1 and net AC-10196-1.STC SA2187WEModification of inflatable slide International Inflatables emergency escape chute kit#KP 684.STC SA218WETurbine installation GTC 85-90E or GTCP 85-291E.STC SA2197WEInstallation of Brownline modified cargo restraint system.STC SA2301WEInstallation of emblem light.STC SA2324WEInstallation of spraymat ice protection system on L-188 propeller spinner, Hamilton Standard P/N 553546, replacing Hamilton Standard heater blanket.STC SA2405WEInstallation of PICO Division pressure regulator P/N 3001 on automatically inflatable emergency evacuation slides in lieu of International Inflatables pressure regulator P/N 68240 and 70003.STC SA240SOOil separator B500-2.STC SA2456WEInstallation of Collins Model860E-2 and dual DME system.STC SA2559WEInstallation of H. Koch & Sons beverage cart P/N 601-710315-1 on stowage mushroom plate assembly.STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC SA2694WEModification for installation of: nose and wingtip instrumentation boom provisions; research apparatus mounting provisions; dropsonde dispenser; increased breathing oxygen provisions and research electrical system.STC SA2695WEModification for installation of: nose instrumentation boom and wingtip instrumentation boom. Modification per STC SA2694WE is required prior to this modification.STC SA2889WEConversion of Lockheed Model 188A and 188C into all cargo configuration by installation of cargo door, cargo floor and cargo lining. (188A s/n 1035 and up)STC SA2963WEIncrease maximum zero fuel weight to 90,000 pounds by modifying aircraft. (188A s/n 1035 and up)STC SA2974WEModification for installation of aft galley and forward galley rework.STC SA2991WEInstallation of passenger compartment interior arrangement in aft fuselage.STC SA3-596Waste-King 5424-200 Flight Recorder SystemsSTC SA3059WEMaximum landing weight substantiated to 98,102 pounds(from 95,650 pounds). (188A s/n 1035 and up)STC SA3084WEInstallation of Collins FPC-75 ground proximity warning system computer.STC SA3098WEStructural modifications. (188A s/n 1035 and up)STC SA3117SOInstallation of an engine reduction gearbox electrical/magnetic chip detector system.STC SA3118SOInstallation of fuel flowmeters and a fuel management system.STC SA3120WEModification consisting of installation of cargo pallet restraint system. (188A s/n 1035 and up)STC SA3141WEInstallation of AiResearch GTCP85-98, -98C or -98CK auxiliary power unit to supply starting air and 400400 HZ power.STC SA3148WEInstallation of Collins FPC-75 ground proximity warning system.STC SA3152WEInstallation of cargo door only.STC SA3159WEInstallation of cargo floor and interior. (188A s/n 1035 and up)
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