TCDS A3SO

STCs approved under this data sheet · 445

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 = 'A3SO')
  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 ST02547ATInstallation of a voice alert system.Aircraft Components IncSTC SA01143WIInstallation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft.Laminar Flow Systems IncSTC 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 SA01161SEApproval of this change in type design applies to the airplane models listed above, only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.Micro AeroDynamics IncSTC SA00261NYInstallation of Aviation Services, Inc. Model 1201 Cockpit Utility Light.Burns Richard GSTC ST01125WIInstallation of Garmin GTX 330 Mode S Transponder with Traffic Information System Capability. Limited to installation on PA-32-260, serial number 32-7100002.Garmin International IncSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemAircraft & Rotorcraft Products (ARP) IncSTC SA02579ATInstallation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware.PMA Products, Inc.STC SA00705WIInstallation of Garmin GNS 430 VHF Communication Transceiver/VOR/ILS Receiver/GPS Receiver.Garmin International IncSTC SA00801WIInstallation of GARMIN GNC 420 or GNC 420A.Garmin International IncSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA09524SCConversion of existing Piper air conditioning system from R12 to R134a refrigerant.Steinbach & Associates, Inc.STC SA5843NMInstallation of an engine electronic digital tachometer.Horizon Instruments IncSTC SA00710WIInstallation of Garmin GMA 340 audio panel.Garmin International IncSTC SA09160AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-640,S-TEC CorporationSTC SA09470SCInstallation of Starter Indicator light system.Texas Skyways IncSTC SA00800WIInstallation of GARMIN GPS 400 with (1) Garmin Dwg No. 005-C0084-00, Rev B, dtd 6/17/99, "Master Dwg List, GPS 400 Installation in Piper PA32," and (2) FAA Approved Flight Manual Supplement (AFMS) for Piper PA32 "Garmin GPS 400 Receiver" Rev A, dtd 7/6/99, or later FAA approved revisions of (1) or (2).Garmin International IncSTC SA8392SW-DInstallation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-534S-TEC CorporationSTC SA09491SCInstallation of a low voltage warning system.Stark's AviationSTC SA02168AKInstallation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.Avalaska IncSTC SA2253WEInstallation of Edo Model FD-3500-21 amphibious floats.Sea Emperor, Inc.STC SA364GLFor 'T' tail configuration - installation of Norton radome kit No. 4229X. For conventional tail configuration - installation of Norton radome kit No. 4229XC.Saint-Gobain Performance Plastics CorpSTC SA514GLInstallation of Norton radome kit No. 4262X.Saint-Gobain Performance Plastics CorpSTC SA8396SW-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-536S-TEC CorporationSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA00923ATInstallation of composite propeller spinner.TCB Composite Co.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)D & K AviationSTC SA1486SOInstallation of speed enhancement kit.Laminar Flow Systems IncSTC SA1801SOInstallation of Laminar landing gear fairing additions.Laminar Flow Systems IncSTC SA693CEReplace existing engine induction air filter with AC Spark Plug filter.Brackett Aero Filters Inc.STC SA71GLInstallation of air filtersBrackett Aero Filters Inc.STC SA09454AC-DInstallationo f S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems, Model ST-791-40X/50XS-TEC CorporationSTC SA00870WIInstallation of GTX 327 transponder.Garmin International IncSTC ST09524SCPiper conversion of air conditioning systems from using R12 to R134a refrigerant on aircraft models listed. For PA-31-300 s/n 31-660, 31-712 thru 31-900, 31-7300901& up. For PA-31-325 sns 31-7400990 & up. PA-31-350 sns, 31-5001& 31-5003, 31-7305005 upSteinbach & Associates, Inc.STC SA1123EAInstallation of Devore vertical tail floodlights on upper surface of horizontal stabilator.DeVore Aviation Corporation of America, a New Mexico CorporationSTC SA1159EAInstallation of DeVore 'Tel-Tail' lights on lower surface of horizontal stabilator.DeVore Aviation Corporation of America, a New Mexico CorporationSTC SA1105CHInstallation of a Hartzell HC-C3YR-1RF/F7693F propeller and 835-52(P) or C3535-1(P) spinnerHartzell Propeller IncSTC SA00801WI-DInstallation of the Garmin GNC 420 or GNC 420AGarmin International IncSTC SA3181NMInstallation of Hartzell HC-E3YR-1()F/F7673DR-0 three-blade propeller on a Lycoming TIO-540-SIAD engine.Hartzell Propeller IncSTC SA8530SW-DInstallation of a Century Automatic flight system, Model AK1052 consisting of a Century 2010/2030/2031/2050/2051 autopilot.Century Flight Systems IncSTC SA01831AT-DInstallation of FFC engineering order P28-2810-001.Floats & Fuel CellsSTC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsJ P InstrumentsSTC SA01224ATInstallation of wheel hub cabs with valve stem access door.LoPresti Speed MerchantsSTC SA00639WIInstallation of the GARMIN GPS 155XL GPS Receiver.Garmin International IncSTC SA00640WIInstallation of GARMIN GNC 300XL VHF Communication Transceiver/GPS Receiver.Garmin International IncSTC SA3774WEInstallation of Hoskins Model CFS-1000, -1001, FT-100, or FT-101 fuel flow indicating system.Sandia Aerospace CorporationSTC SA09333AC-DInstallation of S-TEC system 30 alt altitude hold system.S-TEC CorporationSTC SA09331AC-DInstallation of S-TEC System 30 ALT Altitude Hold System, Model ST-734.S-TEC CorporationSTC SA00079BOInstallation of Meriden GS-22 glide slope antenna.Meriden Electronics CorporationSTC SA5925NMInstallation of oil pressure/temperature instrument.Electronics International
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