TCDS 3A19
STCs approved under this data sheet · 448
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 = '3A19') 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 = '3A19') 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 SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA1809WEInstallation of one twelve-gallon auxiliary fuel tank in each outboard wing panel.STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA8150SWInstallation of VENTUBE pilot/co-pilot overhead fresh air valves. (195 SERIES LC-126A; LC-126B; LC-126C)STC SA02277AKInstallation of FMK Light Emitting Diode (LED) Instrument Panel Lights.STC SA02137ATInstallation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA00812CHReplace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.STC SA01119CHReplace Cessna Sun visor assemblies with Aircraft Recycled Flying controls tinted Sun Visor AssembliesSTC SA03204ATModification of passenger cabin front Doorpost AssemblySTC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA01323WIInstallation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.STC SA01324WIInstallation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 115-1 is derived from Drawing List 115-1 Revision D and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA01436SECockpit sunvisor retrofit kit.STC SA01389SEInstallation of 8-gallon extended range wing fuel tanksSTC SA01944CHModify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.STC SA633GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA789GLSuperseded by STC SA01944CH. Installation of Lycoming O-235-L2C engine modified in accordance with STC SE790GL in combination with propellers: Sensenich 72CK-S6-0-54 or McCauley 1A103/TCM6958. This allows airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA865GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA2846SWConversion from trigear to conventional gear configurationSTC SA3788NMInstallation of Sensenich 74DM6S5 Propeller; Elano Exhaust System, P/N EL 099001-063 and -060; and Cessna Muffler, P/N 0454011-1, in accordance with FAA Approved ACT Report No. 104, dated February 10, 1992, or later FAA approved revisions. STC SA4795SW for the installation of Lycoming 0-320-E2D engine is required as part of this installation.STC SA4795SWInstallation of an Avco Lycoming O-360 or O-320 engine and increase airplane gross weight.STC SA5733SWInstallation of Long Range Wing Fuel Tanks in accordance with Custom Aircraft Conversions, Inc. Drawing List No. C1502-000, revised 05/10/84 and Revision B, dated 02/24/96, or later FAA Approved revision.STC SA1814NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window plexiglass 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 SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA2105NMModification of the landing gear system form a tricycle to a convetional (tail dragger).STC SA4906NMConversion of tricycle landing gear to conventional tailwheel landing gear.STC SA01077SEInstallation of fluoropolymer film.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC SA01243SEInstall a 14.6 gallon auxiliary fuel tank in the baggage compartmentSTC SA2382NMInstallation of Aileron and Flap Gap Seals.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC SA4-394Installation of George M. Adams DGA-2000 wheels and Bodell Mfg Model BMI-252 brakes.STC SA326EAWet-to-dry vacuum pump conversion kit 300-3.STC SA00168BOInstallation of Aero Ski Model M1800 main skis and T3000 tail ski. Modification limited to installation on 150L, serial number 15073301 ONLY.STC SA3688NMCockpit sun visor installation.STC SA09643SCModification to remove the Standard Airworthiness Certificate and placing them in 'Special Airworthiness Certificate-Primary Category' to allow the pilot-owner to perform preventative maintenance beyond what is allow under Part 43, Appendix A.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 SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA01125SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2171, Revision IR, dated July 17, 2002, and Installation Manual MA2172, Revision IR, dated September 6, 2002, or later FAA approved revision of either of these documents.
NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.STC SA1005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.STC SA839NEInstallation of William C. Roberts stainless steel brake discs P/N 201-195 SS 201-260 SS, 201-440 SS, 201-40 SS in lieu of Cessna, carbon steel brake discs, Cessna P/N B-30195, C164-26A, C-30440, C164-40 respectively.
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