TCDS 3A23
STCs approved under this data sheet · 294
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 = '3A23') 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 = '3A23') 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 SA03406ATInstall McCauley model 2A34C209/78[X]-4E propeller.STC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.STC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA01923LAInstallation of the P-1000 Digital Electronic Tachometer.STC SA09539AC-DInstallation of S-TEC System 20/30 Automatic Flight Guidance Systems.STC SA02256AKInstallation of F. Atlee Dodge weld on float fittings.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA241CHInstall Ceconite 101 fabric.STC SA2963SOAdd the following approved fuel: leaded and unleaded automotive gasoline per ASTM specification D-439.STC 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 SA03124ATHorizontal stabilizer finlets for installation on Maule M-7-235, serial number 12001C ONLY.STC SA01412CHInstallation of Wipaire Model 3000 Amphibian/Seaplane Floats and Parts Kit No. W-PMA112.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.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 SA02034CHModify cabin doors in accordance with the Blackhawk Aircraft Maintenance Maule Extended Cabin Door Opening Modification Manual, dated May 1, 2004, or later FAA approved revisions.STC SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.STC SA02024CHInstallation of an S-TEC System 55x Two Axis Automatic Flight Guidance System (autopilot) with Flight Director, ST645 Annunciator, and altitude alter/pre-select.STC 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 SA945GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01259SEInstallation of aerial survey equipment in accordance with I. T. Industrial Group installation drawing D-1, dated August 15, 2003, or later FAA approved revision. This modification must be maintained in accordance with I. T. Industrial Group report number IT-3, "Installation and Removal Instructions and Instructions for Continued Airworthiness," Revision A, dated September 2, 2003, or later FAA approved revision.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 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 SA1008WEInstallation of Poly-Fiber covering material.STC ST02547ATInstallation of a voice alert system.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 SA00170SEInstallation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics drawings and installation instructions specified on the attached FAA AML No. SA00170SE dated November 12, 1997, or later FAA approved revision.
NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.STC SA131CHInstallation of Model M2000 and M3000H fixed skis.STC SA130CHInstallation of Model R2800 retractable skis.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA1160SOInstallation of Weldon, P/N 6005-2A, aircraft engine driven fuel pump in lieu of diaphram type pump.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.STC SA1145GLSurrendered and incorporated into STC SA00478CH.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA09518AC-DInstallation of S-TEC System 20/30 single and two-axis automatic flight guidance systems, Model ST-892-20/30STC SA8905SW-DInstallation of S-TEC System 55 two axis automatic flight guidance system, Model ST-573, with optional autotrim system.STC SA09443AC-DInstallation of S-TEC System 55/55X Two Axis, System 65 Two Axis, System 60 Single Axis, System 60 Two Axis, System 60 Pitch Stabilization System, System 40/50 Single and Two Axis Systems, System 20/30 Single and Two Axis Systems, System 30 ALT Altitude Hold System, and Manual Electric Trim System, Model ST-873,STC SA09138AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-620,STC SA09512AC-DInstallation of S-TEC System 55X Two Axis Automatic Flight Guidance System, Model ST-890STC SA09470SCInstallation of Starter Indicator light system.STC SA09439AC-DInstallation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-872-20/30.STC SA09352AC-DInstallation of S-TEC System 20/30 single and two-axis automatic flight guidance systems, Model ST-810-20/30.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.
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