TCDS 1A4
STCs approved under this data sheet · 276
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 = '1A4') 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 = '1A4') 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 SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA02280AKInstallation of a Maule Fuel Selector Valve.STC SA01715SEONE-ONLY STC: Replacement of existing Control wheels on Piper PA-20, serial number 20-279 with PA-16 Type Conttrol Stick configuration.STC SA1-157McCauley fixed pitch MET-L-PROP1A170/GM7450 with Lycoming O-290-D engine.STC SA1-24McCauley fixed pitch MET-L-PROP Models 1A170/GM7455 and 1A170/ GM7453 with Lycoming O-290-D2 engine.STC SA1-89Installation of McCauley Propeller Systems fixed pitch MET-L-Prop models 1A170/GM7452 and 1A170/GM7454STC SA01063CHInstallation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring.STC SA1-167Lycoming O-320 150 hp engine, Sensenich M-74DM propeller, Piper PA-22-150 engine baffles, and and Harrison AP13SJ03-01 oil cooler.STC SA4-977Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons.STC SA4008NMInstallation of removable panels on the battery box slides.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 SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.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 SA00097SEInstallation of a vortex generator kit.STC SA384ALInstallation of rudder centering device in lieu of ventral fin.STC SA5-65Installation of Goodyear 25 x 11.0 - 4 Type IV tires with tubes on Goodrich Model 841696 4-inch wheels on main landing gear, using Alaskan Aircraft Equipment Supply Model A-1 rim adaptersSTC 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 SA948GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).STC SA01770NYInstallation of CAM 556-643.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest 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 SA3217WEInstallation of George M. Adams DGA-2000 or Bodell BMI-2000 wheels and Bodell BMI-252 brakes.STC SA1008WEInstallation of Poly-Fiber covering material.STC SA351NEAirframe modification for installation of modern instrument panel.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA1067GLSurrendered and incorporated into STC SA00478CH.STC SA00932SEInstallation of the Stewart wing tip assemblySTC SA09470SCInstallation of Starter Indicator light system.STC SA00851SEInstallation of Rudder Trim System.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA71GLInstallation of air filtersSTC SA11RMInstallation of modified axles, wheels and brakesSTC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA1558NMInstallation of Jensen Aircraft fuel valve plug No. 011-1.STC SA1586NMInstallation of replacement long-life lift strut.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA02093AKInstallation of hourmeter airspeed switch.STC SA12RMInstallation of Light Plane Components landing gear vee assembly.STC SA00393SEInstallation of the G/S 2500 and G/S2500R Aircraft Security Alarm System.STC SA666NWInstallation of Teflon control yoke bail or control yoke bushings.STC SA573SWInstallation of Plane Booster wing tip kit 101-250.STC SA00061LAInstallation of JPI digital tachometer.STC SA2508SOReplacement of Cleveland brake discs, No. 164-67 or 164-167, with Appalachian Accessories' stainless steel brake discs, Part No. 73-67.
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