N261GL

STCs that may be installed · 243

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.

Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
  FROM (
    SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
    FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '7150005'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52032')
    GROUP BY stc_number
  ) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
  ORDER BY m.side, 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.

Airframe · Raytheon 1900D

STC SA01622CHInstallation of an SEI Quick Access Recorder.Systems & Electronics Inc. (SEI)STC ST02815ATInstallation of a cockpit door and modification of the forward bulkhead in accordance with U. S. Technical Master Drawing List Document No. 4099-25-000, revision G, dated March 4, 2004, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement (AFMS), U.S. Technical Document No. U10-0127, dated March 8, 2004, or later FAA approved revision, is a required part of this modification. Instructions for Continued Airworthiness can be found in U. S. Technical Document No. U10-0129, release 1, dated March 4, 2004, U. S. Technical Document U10-0128, release 1, dated March 4, 2004, and U. S. Technical Document U10-0130, release 1, dated March 4, 2004.U.S. TechnicalSTC SA00948CHInstallation of various de-icer wire harnesses. (E90 modified by STC SA3593NM, F90 modified by STC SA4131NM, B200 modified by STC SA2698NM-S, DHC-6 Series modified by STC SA3532NM)SMR Technologies IncSTC SA01852NYInstallation of a Communicator System. Limited to installation on serial number UE-227.Northeast Engr & Dev LtdSTC SA01873CHReplacement of certain Goodrich pneumatic deicer boots.SMR TechnologiesSTC 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 SA01126WIReplacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632DER Associates Ltd.STC SA00110ATInstallation of a Marathon KSP 400 battery.Aviall Services, Inc.STC ST00021DE-DInstallation of GPWS system.Learjet IncSTC ST00022DE-DInstallation of Bendix/King CAS-66A TCAS I System.Learjet IncSTC ST00141DE-DInstallation of AlliedSignal CAS-67A TCAS II System.Learjet IncSTC SA01467NYSubstitution of Incandescent Light Bulbs with Light Emitting Diodes for Warning Annunciator Panel and Caution/Advisory Annunciator Panel.Aero Consulting Services LtdSTC SA09863SCInstallation of Avionics Specialties, Inc. power analyzer and recorder number SL17029.Aviation Ventures, Inc.STC SA1022WIInstallation of a second Bendix/King KLN 90B GPS navigation system. Data Required: 1. Raytheon Aircraft Services Top Drawing No. 148-100480, Revision A, dated August 16, 2001, or later FAA approved revision. 2. Raytheon Aircraft Services Airplane Flight Manual Supplement, number RAS1900E032, dated November 23, 2001, or later FAA approved revision.Raytheon Aircraft Services IncSTC SA00845WI-DModification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II receiver transmitter.Rockwell Collins IncSTC SA09854SCInstallation of Ultra Electronics Controls Division Hub Integrated Power and Switching System (HIPSS) propeller deice system.Celsius Aerotech, Inc.STC SA8811SWInstallation of an engine cowling safety clip.Sugar Land Jet Center, A Texas CorporationSTC SA7361SWInstallation of tail floodlights.DeVore Aviation Corporation of America, a New Mexico Corporation · Lists 1900 SeriesSTC SA02150AK-DFabrication and installation of Aero Twin, Inc. single place folding seat P/N ATFS1-01K.Aero Twin, IncSTC ST00917NYInstallation of Ground Utility Winterization Kit consisting of engine heaters, a battery warmer, cockpit heaters and a cabin outlet for a cabin heater.Field Aviation East LimitedSTC SA000873CHInstallation of an Auxiliary Annunciator SystemAstral Aviation Inc.STC SA00873CHInstallation of an Auxiliary Landing Gear Annunciator System.Astral Aviation, IncSTC SA00749ATModification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent)Aero Trim, IncSTC SA09242ACInstallation of provisions for a New Systems P/N NS20004-1Air Call system.New SystemsSTC SA00638CHModification of aircraft to authorize landing with a flap setting of 17 .Barnhart Aviation ServiceSTC SA09317SCNew Systems P/N NS20004-1 Air Call(Selcal) unit installed.New SystemsSTC SA00775ATInstallation of a Bendix/King KLN90B Global Positioning System.Piedmont Avn Services, IncSTC SA00776ATInstallation of a Dual Bendix/King Mode S Transponder, Traffic Alert and Collision Avoidance System and Sundstrand Mark VI Ground Proximity Warning SystemPiedmont Avn Services, IncSTC SA5656NMInstallation of burglar alarm system.Thompson Harold SSTC SA187CHInstallation of a Flight Visions FV-2000/KA head- up display.Flight Visions, IncSTC SA8694SWInstallation of a Sundstrand Mark VI GPWS system.New SystemsSTC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.Electronics InternationalSTC SA2190NM PAGE 1Installation of electronics International Digital Volt/Amp Gauges and Accessories.Electronics InternationalSTC ST12400WIInstallation of Garmin Avionics Modernization PackageAlpine Aviation, Inc.STC SA00281BO PAGE 2Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000Avidyne CorporationSTC SA01933LAInstallation of Garmin Model 400W / 500W Series GPS-WAAS Navigation SystemGarmin AT Inc.

Engine · Pratt & Whitney PT6A series

STC SE12225ACThis STC will incorporate P&W 1700 rpm propeller reduction gearbox on P&WC engines to allow 1700 rpm propeller installationHigh Cotton Aircraft Conversions, LLC · Lists PT6A-41STC SE00010ENInstructions for Continued Airworthiness for the PT6A-25, and, -25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-25STC SE000010ENInstructions for Continued Airworthiness for the PT6A-25 and PT6A-25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company, Inc. · Lists PT6A-25STC SE000011ENInstructions for Continued Airworthiness for the PT6A-25C engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company, Inc. · Lists PT6A-25CSTC SE00001ENEngines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 2, 8/16/95.MORE Company Inc · Lists PT6A-38STC SE00002ENInstructions for Continued Airworthiness for the PT6A-34, -34AG, -34B, -36, -114, -114A, -116, -135, and -135A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-114STC SE00003ENInstructions for Continued Airworthiness for the PT6A-6/C20, -20, -20A and, -20B engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-20STC SE00004ENInstructions for Continued Airworthiness for the PT6A-11, -11AG, -15AG, -110 and-112 engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-11STC SE00006ENInstructions for Continued Airworthiness for the PT6A-45A, -45B, and, -45R engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-45ASTC SE00011ENInstructions for Continued Airworthiness for the PT6A-25C engine model that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.MORE Company Inc · Lists PT6A-25CSTC SE000ENEngines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 4, dated 8/16/95.MORE Company Inc · Lists PT6A-21STC SE10947SCThe conversion of the Pratt & Whitney Canada, Model PT6A-21 to a PT6A-28 turboprop enginePrime Turbines · Lists PT6A-21STC SE00482SEIncorporation of turbine engine into a twin power section turboprop assembly.Fifty-Ten-Yankee LLC · Lists PT6A-114ASTC SE10552SCConversion of Pratt & Whitney Canada Corp. Model PT6A-27 or -28 to a Model PT6A-34 turboprop engine.Prime Turbines LLC · Lists PT6A-27
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