TCDS A6CE
STCs approved under this data sheet · 275
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 = 'A6CE') 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.
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 = 'A6CE') ORDER BY s.status = 'Current' DESC, s.status_date 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 SA1823NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.STC SA02700ATInstallation of Air Conditioner SystemSTC SA8533SW-DInstallation of a Century Automatic Flight System Model AK1055 consisting of a Century 2110/2130/2131/2150/2151 AutopilotSTC SA02686ATInstallation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions, dated June 15, 2003, or later FAA approved revision.STC SA02055ATInstallation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.STC SA01215SEInstallation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.STC ST02547ATInstallation of a voice alert system.STC SA4961NMInstallation of a NSA sunvisor system for the pilot and copilot.STC SA00165BOInstallation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.STC SA00419NYInstallation of cockpit utility light.STC SA02527ATInstallation of a landing gear in-transit warning light in 337 models that are equipped with an electric motor to retract landing gear instead of engine driven hydraulic pump.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA02510ATInstallation of a rear firewall engine accessory access door.STC SA2832SOInstallation of a combination radio/throttle/gust lock.STC SA01179ATInstallation of an external cargo Pod.STC SA01091ATManufacture of mechanical cowl flap control system.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA01280CHInstallation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404)STC SA71GLInstallation of air filtersSTC SA5090NMInstallation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip.STC SA02056ATInstallation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.STC SA02023ATInstallation of a fuel transfer system to transfer fuel from a wing tip extension fuel tank to the main wing fuel tank.STC SA01985ATInstallation of a fuel jettison system.STC SA02017ATInstallation of a Wescam FLIR System, NSI Microwave System and an Operator's Console.STC SA09419AC-DInstallation of S-TEC System 20/30 single and two axis automatic flight guidance systems, Model ST-869-20/30.STC SA01888ATInstallation of a composite structure baggage door in RH side of the fuselage.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA3863NMInstallation of American intercooled engines as modified by STC SE3864NM.STC SA2619WEInstallation of Pathfinder Model P1-( ) autopilot system.STC SA2620WEInstallation of Pathfinder Model P2-( ) autopilot system.STC SA8008SWInstallation of Zeftronics alternator control units P/N's R25101 (27.7V systems) or R25102 (28.8V systems).STC SA1877NMInstallation of Hoskins Model CFS-2000A, -2001A, FT-200, fuel flow indicating system.STC SA02095AKInstallation of hourmeter airspeed switch.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA01093ATManufacture of short takeoff and landing (STOL) kit and tail boom to vertical fin fairings.STC SA01344ATInstallation of a baggage door on the aft right side of the fuselage.STC SA157NEInstallation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent.STC SA01090ATManufacture of flap gap seals.STC SA01094ATManufacture of modified Lightning Wingtips.STC SA2242SOInstallation of external fuselage insecticide spray tank and associated dispersal equipment.STC SA00061LAInstallation of JPI digital tachometer.STC SA2492SOInstallation of Appalachian Accessories stainless steel brake discs, P/N 75-25A.STC SA1801CEInstallation of Total Flood Corporation fire extinguishing system in the cabin and/or fire extinguishant system in engine compartments.STC SA00556ATInstallation of Appalachian Accessories carbon steel brake discs, P/N AA-27A.STC SA00199ATInstallation of carbon steel brake discs that have melonite surface treatment, P/N AA-25A.STC SA8922SWInstallation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126, S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT)STC SA5656NMInstallation of burglar alarm system.STC SA00409ATInstallation of Cessna 02A entry door (P/N 1517080-1) and wind deflector.STC SA00410ATDesign, fabrication and installation of upper and lower windshield retaining gussets.
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