TCDS A2WE

STCs approved under this data sheet · 346

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 = 'A2WE')
  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 SA4296SWInstallation of Global Navigation Inc GNS-500A Series III VLG/Omega Navigation System.Signature Flight Support CorporationSTC SA4456SWInstallation of Dual Global GNS-500A series III Omega navigation system with Vandling Model NDB-2 navigation data bank.Signature Flight Support CorporationSTC ST02114ATInstallation of AlliedSignal CAS-66 TCAS 1 System.C E AvionicsSTC SA7080NMInstallation of General Electric (GE) CF700-2D-2 engines modified with a new fan exit guide vane assembly, Part Number (P/N) 6078T97G01.Noise Reduction Engineering, Inc.STC SA3052WEInstallation of Vertical Tail Floodlights on horizontal stabilizerDeVore Aviation Corporation of America, a New Mexico CorporationSTC SA1418SWSeat installation.Sierra Industries, IncSTC SA1460SWModification of 2-place aft couch installed under SA172CE to 3-place couch and addition of one oxygen dropout mask and associated changes to the oxygen systemSierra Industries, IncSTC SA2642CEInstallation of Collins Traffic Alert and Collision Avoidance System, TCAS II.Rockwell Collins IncSTC ST00847LAInstallation of the folding jump seat.Naval Air Systems Command PMA-207STC ST00370WIIncrease Fuselage life limit via Damage Tolerance Analysis.Centurion InvestmentsSTC ST00698WIReduction in the maximum seating configuration from 10 to 9 by removal of the seat belt from the forward lavatory passenger seat and installing a placard 'DO NOT OCCUPY DURING TAKE-OFF AND LANDING' above the seat back. One-Time only STC for S/N 465-42.Executive Aircraft CorporationSTC ST00891CHInstallation of Fairchild F-800 digital flight data recorder.ElectroSonicsSTC ST01622ATModification is for an electrical change to the fuel transfer system.Jet Harbor, IncSTC ST00844CHInstallation of dual Universal UNS-1K Flight Management Systems.ElectroSonics Div of AiRadio CorporationSTC ST01294ATInstallation of Concorde RG-380E/40 valve regulated sealed lead-acid battery as replacement of installed Ni-Cad Battery.Jet Harbor, IncSTC ST00667CHInstallation of Dual AlliedSignal GNS-XLS flight management systems as primary means of navigation for oceanic and remote airspace.ElectroSonics Div of AiRadio CorporationSTC ST1031SOReplace existing nickel-cadmium batteries with Teledyne Gill BB638/T series lead-acid type batteries.Teledyne Battery ProductsSTC SA1907SWInstallation of hot air mixing valve position indicator.Aviation Material and Technical SupportSTC SA1946SWInstallation of engine fuel shut down system.Aviation Material and Technical SupportSTC SA1957SWInstallation of additional hydraulic pressure switch.Aviation Material and Technical SupportSTC SA1960SWInstall engine oil pressure low caution light cutoff switches.Aviation Material and Technical SupportSTC SA1961SWInstallation of Entrance door counterbalance system.Aviation Material and Technical SupportSTC SA1972SWInstallation of BKM 100-265 nose wheel steering control.Aviation Material and Technical SupportSTC SA2341SWInstallation of No. 2 hydraulic pump.Aviation Material and Technical SupportSTC SA2382SWChange nose gear linkage and stop assembly to provide increased steering capability from 35 degrees to 45 degrees.Aviation Material and Technical SupportSTC SA2388SWInstall diode across coil of hydraulic pump relay.Aviation Material and Technical SupportSTC SA2701SWRelocation of hydraulic pressure.Aviation Material and Technical SupportSTC SA2789SWInstallation of Foxboro fuel management system.Aviation Material and Technical SupportSTC SA2838SWInstallation of recognition lights.Aviation Material and Technical SupportSTC SA2997SWInstallation of nose wheel steering transfer test switch.Aviation Material and Technical SupportSTC SA4024SWInstallation of BKM anti-skid brake monitor system.Aviation Material and Technical SupportSTC SA4096SWInstallation of a bleed air engine fuel manifold purge system.Aviation Material and Technical SupportSTC SA4137SWInstallation of engine starter inhibit circuit.Aviation Material and Technical SupportSTC SA4223SWInstallation of Hydraulic fluid level warning and hydraulic pump run advisory system.Aviation Material and Technical SupportSTC SA4373SWInstallation of BKM 78-2610-1 nose wheel steering feedback potentiometer assembly.Aviation Material and Technical SupportSTC ST494CHInstallation of fiber optic lighting system, P/N AV11001.Avtec, IncSTC SA67GLInstall B.F. Goodrich pneumatic de-icer system listed on Master Drawing List Report No. 74-04-047B.BF Goodrich AerospaceSTC SA8976SWReduce maximum passenger seating configuration from 10 to 9 by removing the seat belt and installing a placard by the forward lavatory passenger seat.Jet East, IncSTC SA8944SWModification of thrust reverser flexure plates.Bizjet International Sales & Support IncSTC ST00241NY-DInstallation of a Single Bendix/King CAS-66A TCAS I system, and Single TA/IVSI.Delta EngineeringSTC SA2114SW-ACInstallation of Advanced Navigation Model 7000 Loran C navigation system with interface into the autopilot and pilot's flight director system.Federal Aviation AdministrationSTC SA2745CEInstallation of the Universal Navigation Corp. CVR-80 cockpit voice recorder.Rockwell Collins IncSTC SA2120SW-ACSubstantiate satisfactory operation in the RNAV lateral axis of the Parker/Gull aerea navigation system utilizing a Gull navigation computer unit with software program P/N 555-050-001 Rev. E and a Honeywell inertial reference system.FAA Aviation System Standards AVN-300STC SA2070SW-ACSubstantiate satisfactory operation of ARMA Area Inertial Navigation System (A-INS) in the RNAV lateral axis only.FAA Aviation System Standards AVN-300STC SA2547CEInstall palletized Collins TCAS II Evaluation/Demonstration System (one only)Rockwell International Collins Commercial AvionicsSTC SA1290CEInstallation of Avcon Industries stretcher P/N 4006-103 or 4006-104.Med-Flite of Midamerica, IncSTC SA7756SWInstallation of Aerex Group fuel flow interface unit.AEREX Group IncSTC SA2544CEInstallation of single or dual hydraulic starting system.Midcoast Aviation IncSTC SA1353GLInstallation of Fairchild Model 501 flight data recorder.ElectroSonics Div of AiRadio CorporationSTC SA2112SWInstallation of Bendix Model 20A microwave landing system modified for flight inspection interface into the flight inspection console, autopilot, pilot, and copilot flight directors.Federal Aviation Administration
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