N852V
STCs that may be installed · 200
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 = '3023508'
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.
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 = '3023508'
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_numberRun 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.
Airframe · Douglas DC-10-40
STC SA3278SOInstallation of a modified smoke barrier in Class E cargo compartment.STC SA2779CEInstallation of Collins TCAS II traffic alert and collision avoidance system.STC SA3335WEInstallation of stretcher carrier AM2003.STC ST00232ATInstallation of tray carriers.STC ST4CHInstallation of replacement oven door.STC SA1447GLInstallation of on-board engine analyzer system.STC SA3970SW-DInstall a Litton LTN-2001 global positioning satellite sensor unit(GPSSU) with dual wiring provisions.STC SA5214NMInstallation of AMI model 2055 cabin attendant seat.STC SA398NEInstallation of Auto-Vac-2 manifold vacuum system per certain engine STC's.STC SA3864SWRelocate passenger emergency oxygen from seatback to center console between passengers.STC SA3929SW-DReplace the single Litton LTN-51 INS with a LTN-72STC SA2437NMInstallation of fixed primary nozzlesSTC SA3699SWInstallation of Plumly airborne floor proximity lighting system.STC SA2728WEIncorporation of Holcombe Industries HI-LITE SYSTEM P/N 50-1001 for emergency evacuation slide lighting. (707 AIRPLANES EQUIPPED WITH BOEING P/N 65-11685 AND 65-68862 FORWARD THRUST REVERSER DOORS)STC SA5881SWInstallation of class divider.STC SA1258EAInstallation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584)STC SA1391SOInstallation of in-flight video systems.STC SA1342SOInstallation of Aero Systems CD-3000 fuel management computer.STC SA4566SWInstallation of inner pane, accoustic cabin window.STC SA4186WEInstallation of Stowe Corp. liquor cart, P/N 10051-3.STC SA4138WEInstallation of cabin window plug assembly.STC SA372GLInstallation of Honeywell P/N HG280BD80 digital airdata computer in the number three position per NWA project 1-34-40300 in place of the Honeywell P/N HG280D5 presently used in this position for data collection purposes only.STC SA108NWInstallation of Mark IV visual entertainment system.STC SA132NWInstallation of Sundstrand Visual Entertainment SystemSTC SA285NWFactory installation of Xenon light in Sundstrand Visual Entertainment System installations.STC SA88GLInstallation of Bendix GPW-83 ground proximity warning systems.STC SA2893WEInstallation of Hermes LD-3 Kool- flite refrigerated cargo container.STC SA969EAInstallation of Inflight movie projection assembly P/N 10270, Super 8mm IMPAK system.STC SA2783WEInstallation of wheeled refrigerated module, P/N730l4000-101. (747-251B)STC SA3918SW-DInstallation of Hughes-Avicom audio/game entertainment system.STC ST00743LA-DInstallation of control column and rudder pedal, position sensors for Flight Data Recorder Expanded Parameters.STC ST00757LA-DInstallation of Rockwell Collins alternate part number SVHS Video Tape Player.
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.STC SE00024ENInstallation of oil tank filler neck check valve.STC 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.STC SE00402NYInstallation of corrosion resistant steel replacement Chip Detectors.STC SE497NEInstallation of oil tank filler neck check valve assembly.STC SE00054AT-DModification of the turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment.STC SE00047AT-DModification of turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment.STC SE00046AT-DState 1 LPC Stator: Provide a seamless one piece rubber airflow surface at the inner shroud.STC 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.STC SE2888SO-DModify turbine exhaust case to incorporate Model -20 mount features.STC SE593NEInstallation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List)STC SE435NEInstallation of an oil tank filler opening shuttle valve.STC 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 SERIESSTC SE133NEIncorporation of Hamilton Standard EDM 110-3 Engine Data MultiplexerSTC SE118NEThrust reverser system P/N 221D0065, consisting of 4 major installations.STC SE1141CERemoval of 15th stage bleeds and surge detector system.STC SE33NEIncorporation of improved combustor and turbine components which permit operation at increased EGT limits.STC SE11CEInstallation of aircraft integrated data system components on engine.