N6830P
STCs that may be installed · 420
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 = '7102404'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41532')
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 = '7102404'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41532')
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 · Piper PA-24-250
STC SA7180SW-DInstallation of S-TEC System 65 two axis automatic flight guidance system Model ST-443.STC SA6069SW-DInstallation of S-TEC manual electric trim system, Model ST-358.STC SA6059SW-DInstallation of S-TEC system 60 single axis automatic flight guidance system Model ST-020.STC SA4390SWInstallation of single or dual toe brakes.STC SA2844CEInstallation of a plastic cap enclosure over the anti-collision strobe light system.STC SA5205SW-DInstallation of S-TEC System 60 pitch stabilization system Model ST-057.STC SA5208SW-DInstallation of S-TEC system40/50 single and two axis automatic flight guidance systesm, model ST-195-40/50.STC SA6053SW-DInstallation of S-TEC System 60 two axis automatic flight guidance system, Model ST-021, with Optional automatic electric trim systemSTC SA2713CEInstallation of PRONAV global positioning system, GPS-100 navigator.STC SA1178EAInstallation of Silver Instruments fueltron IG or IP or Fuelgard digital fuel flow indicating systemSTC SA4-666Installation of a Grimes D-7080-1-12 rotating beacon.STC SA1531GLInstallation of on-board engine analyzer system.STC SA4958NMInstallation of a hand control for the rudder.STC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA4721NMInstallation of SynCon alarm system.STC SA317NEInstallation of Auto-Vac-2 manifold vacuum system.STC SA2549CEInstallation of a Webco door latch kit.STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.STC SA2487CEInstallation of rudder, aileron, flap, and stabilator trim tab gap sealsSTC SA2485CEInstallation of side windows with an increase of thickness from 1/8 inch to 1/4 inch.STC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.STC SA660WEInstallation of HRD-type fire extinguishing system. (AND STC SA111WE)STC SA3559NMInstallation of ARNAV systems FC-10 or FT-10 digital fuel flow indicating system. (PA-24-260 with fuel injected normally aspirated engine)STC SA3550NMInstallation of Hartzell / HC-C2YK-1BF/F8477D-5R . propellerSTC SA1455NMInstallation of a flame proof auxiliary heater-dryer, Model12-1600.STC SA921GLInstallation of a Shadin Company fuel flow indicating system.STC SA2541NMInstallation of fiberglass wing tips.STC SA191NEReplace original brake discs with discs modified in accordance with Roland Longarzo procedure.STC SA1027SWInstallation of manual electric pitch trim AK267.STC SA808SWInstallation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW.STC SA838SWInstallation of Mitchell glide slope coupler Model 1C493.STC SA576SWInstallation of Mitchell automatic flight system model AK186 consisting of Piper altimatic IIIB autopilot radio coupler, and automatic aileron stabilizer model AK179.STC SA581SWInstallation of Mitchell Automatic Aileron Stabilizer Model AK179.STC SA662SWInstallation of Mitchell automatic flight system model AK220 consisting of Century III autopilot with option automatic pitch trim, automatic aileron stabilizer and radio coupler.STC SA756SWInstallation of Mitchell automatic flight system model AK236, consisting of Century II autopilot with optional radio coupler.STC SA3045SW-DInstallation of Mitchell automatic flight system model AK519 consisting of Century IIB autopilot with optional radio coupler.STC SA3074SW-DMitchell automatic flight system AK547 consisting of Century I autopilot with optional omni tracker.STC SA2272NMInstallation of fiberglass window mouldings. (PA-24-260 24-1 thru 24-4299)STC SA2190NM PAGE 1Installation of electronics International Digital Volt/Amp Gauges and Accessories.STC SA4401SWInstallation of S-TEC system 60 single axis automatic flight guidance system, Model ST-020STC SA1667NMInstallation of a Shadin "Digiflo" digital fuel flow indicator systemSTC SA4317SWInstallation of S-TEC system 60 two axis automatic flight guidance system, Model ST-021 with optional autotrim systemSTC SA4581SWInstallation of S-TEC system 60, Pitch Stabilization System Model ST-507 with optional autotrim system.STC SA1268NWInstallation of a Hoskins FT-101 computerized fuel systemSTC SA334SWInstallation of InterAv Alternator.STC SA1167NWInstallation of an updated instrument panelSTC SA928NWAeroquip high temperature hydraulic hoses and fittings between oil cooler and engine.STC SA463GLInstall instrument panel and instruments. (PA-24-250 24-2299 and above) (PA-24-260 24-3642, 24-4000 thru 24-4802) (PA-24-400 26-2 and above)STC SA2944SWAddition of Hydro Seal Fluid Additive to landing gear shock struts.STC SA3451WEInstallation of Hartzell HC-A3VK4/V7636D-0 or V7636N-0 constant speed propeller.