N651GT

STCs that may be installed · 18

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 = '138513B'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52054')
    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.

Engine · Pratt & Whitney JT9D series

STC SE2338SOInstallation of an oil tank safety cap adapter which prevents oil loss in the event of loss or damage to the filler cap.Jet Avion Corporation · Lists JT9D-20STC SE00024ENInstallation of oil tank filler neck check valve.Helicopter Support Inc Services Div · Lists JT9D-3ASTC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.Cook Airtomic · Lists JT9D-20STC SE00402NYInstallation of corrosion resistant steel replacement Chip Detectors.Vickers IncSTC SE497NEInstallation of oil tank filler neck check valve assembly.Aviation Components Support · Lists JT9D-3ASTC SE00054AT-DModification of the turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment.Aero Component Technologies · Lists JT9D-7R4DSTC SE00047AT-DModification of turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment.Aero Component Technologies · Lists JT9D-20STC SE00046AT-DState 1 LPC Stator: Provide a seamless one piece rubber airflow surface at the inner shroud.Aero Component Technologies · Lists JT9D-20STC SE00045AT-DModify -59A LPT case to reduce the thickness of four bosses to eliminate interference with the turbine case cooling manifold installed on -7Q engines. This modification permits use of the -59A LPT case on-7Q engines.Aero Component Technologies · Lists JT9D-59ASTC SE2888SO-DModify turbine exhaust case to incorporate Model -20 mount features.Aero Component Technologies · Lists JT9D-7ASTC SE593NEInstallation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List)Basken Valve CorporationSTC SE435NEInstallation of an oil tank filler opening shuttle valve.Stockbridge William D · Lists JT9D-20JSTC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIESRolls Royce, IncSTC SE133NEIncorporation of Hamilton Standard EDM 110-3 Engine Data MultiplexerUnited Technologies · Lists JT9D-7R4D1STC SE118NEThrust reverser system P/N 221D0065, consisting of 4 major installations.Pratt & Whitney · Lists JT9D-7R4D1STC SE1141CERemoval of 15th stage bleeds and surge detector system.Trans World Airlines Inc · Lists JT9D-7ASTC SE33NEIncorporation of improved combustor and turbine components which permit operation at increased EGT limits.Pratt & Whitney Aircraft Grp · Lists JT9D-7FSTC SE11CEInstallation of aircraft integrated data system components on engine.Trans World Airlines Inc · Lists JT9D-3A
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