TCDS A13CE

STCs approved under this data sheet · 328

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 = 'A13CE')
  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 SA01205WI-DInstallation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.Honeywell International IncSTC SA10005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.Plane Plastics Ltd.STC SA01105WI-DInstallation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).Honeywell International Inc.STC SA02446CHInstallation of the Courtesy Light Kit.Knots 2U Ltd.STC SA01442WIInstallation of Lycoming IO-360-A1B6D engine, McCauley B2D34C207/78TCA propeller, and associated systems modifications.Vanderhoof ChadSTC SA917EAInstallation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail, P/N 30-0555-( ).Honeywell International Inc.STC SA5701SWInstallation of electrically driven vacuum pump as a standby auxiliary pump to the existing instrument.Aero Safe CorporationSTC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.K S Avionics IncSTC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.K S Avionics IncSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)Aviation Development CorporationSTC SA01170NYInstallation of NPX138N-XXX FM Transceiver.Northern Airborne Technology LtdSTC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.Insight Instrument CorporationSTC SA00812CHReplace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.Vantage Plane Plastic LtdSTC SA00230BOInstallation of Lycoming Model O-360-A1F6 engine to replace existing Lycoming O-360-F1A6 engine. This approval is limited to the installation made in Cessna Model 177, Serial Number 17700380 ONLY.Catallozzi Edmund JSTC SA477CHInstallation of McCauley Propeller model B3D36C428/82NPA-6.McCauley Propeller SystemsSTC 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.Garmin AT Inc.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA01548SEInstallation of a Lycoming O-320-E2D engine modified by STC SE3692SW.Gold Coast Aviation Service IncSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.Aero Enhancements Inc.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.Avidyne CorporationSTC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.Electronics International Inc.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.Garmin AT Inc.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.Garmin AT Inc.STC SA01889NYFabrication and installation of an FRP Lower Cowl Fairing.Sobchuk RoySTC SA01436SECockpit sunvisor retrofit kit.Rosen Sunvisor Systems LLCSTC SA02208AKInstallation of Lycoming O-320-E2D modified engine. Limited to installation on model 177, serial number 01049 ONLY.Hot Springs AviationSTC SA2457CEInstallation of fuel inlets and caps. (177B S/N 17700001 THRU 17702752)Hartwig Aircraft Fuel Cell RepairSTC 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.Experimental Aircraft Association Inc.STC SA803GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, STC SE800GL approves, 87 minimum antiknock index.EAA Aviation FoundationSTC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemPS Engineering IncorporatedSTC SA10222SCInstallation of a Chelton Aviation Corp (CAC) AP-3C autopilot in accordance with Master Drawing List No. MS-005-12, Rev. F, dated February 3, 2004, or later FAA approved revision. FAA approved Airplane Flight Manual MS-005-14, Rev. I. R., dated February 5, 2004, or later FAA approved revision is required.Chelton Aviation CorporationSTC SA02674ATModification of engine exhaust system for improved engine performance by installation of Power Flow Systems, Inc. Tuned Exhaust System per Master Drawing List, PFS-13740-00, Revision, IR, dated: 06/05/03 or Master Drawing List, PFS-13741-00, Revision, IR, dated: 11/26/03 and Installation Instructions Report, PFS-13750-00, Revision A, dated: 08/30/02 or Installation Instructions contained in Report PFS-13751-00, Revision, IR, dated: 11/26/03 or later FAA approved revision.Power Flow Systems IncSTC SA2166NMInstallation of the Precise Flight stand-by vacuum system (SVS).Precise Flight IncSTC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.Aero Holdings Ltd. a Texas limited partnershipSTC SA01077SEInstallation of fluoropolymer film.Columbia Pacific AirlinesSTC 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.J P InstrumentsSTC 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.Aerospace Logic Inc.STC ST02547ATInstallation of a voice alert system.Aircraft Components IncSTC SA4964NMInstallation of a NSA sunvisor system for the pilot and copilot.Rosen Sunvisor Systems LLCSTC 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.Avidyne CorporationSTC SA00419NYInstallation of cockpit utility light.Burns Richard GSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemAircraft & Rotorcraft Products (ARP) IncSTC SA01386NYInstallation of Fibre Glass Reinforced Plastic Nacelle Fairing, Trade Name 'Exhaust Fairing".Maple Leaf Aviation LtdSTC SA1005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.Soros, IncSTC 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.Flight Life, Inc.STC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.Trevor Burward-HoySTC SA00895LAInstallation of instrument panel.Trevor Burward-HoySTC SA6023NMInstallation of an electronic digital engine tachometer, Model P-1000.Horizon Instruments IncSTC SA01033SEInstallation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2162, Revision IR, dated November 1, 2001, and Installation Manual MA2163, Revision IR, dated December 3, 2001, or later FAA approved revisions. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Micro AeroDynamics Inc
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