N50TP
STCs that may be installed · 105
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 = '7102504')
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 = '7102504') 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
Run 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-25-235
STC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lightsSTC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01147WIInstallation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes.STC SA1892WEInstallation of hydraulic systemSTC SA521WESwathmaster dust and spray attachment.STC SA7965SWApplication of fabric and polyurethane finishing system.STC SA01757WITo allow the use of UL91 or UL94 (minimum) grade aviation fuelSTC SA02532ATInstallation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.STC SA01435LAInstallation of engines modified with Firewall Forward Technologies LLC modified camshaftSTC SA00954WIInstallation of Concorde RG Series Batteries in Piper Single Engine Airplanes.STC SA01967WIUse of GAMI G100UL High Octane Unleaded AvgasSTC SA04776NYThe HIPEC Covering and Finishing System must be performed and maintainedSTC SA1151NWInstallation of the Flight Grip Model 135 Control Stick GripSTC SA01831WITo allow the use of UL91 (minimum) grade aviation fuelSTC SA03286CHInstall an electronic engine ignition systemSTC SA04032CHInstall rocker switch assembliesSTC SA00344BO PAGE 1Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.STC SA615EAInstallation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.STC SA04112CHInstallation of Appareo Systems, LLC Stratus ESG ADS-B transponderSTC SA04424ATInstallation of Continental Motors, Inc. (CMI) Shower-of-Sparks Starting Vibrator Booster SystemsSTC SA00024NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.STC SA02212AKReplacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systemsSTC SA2586NMInstallation of J.P. Instruments temperature monitoring systems.STC SA02428SEInstallation of an Air Stream Switch for an electric time recording device on non-pressurized aircraftSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA441SWInstallation of Flexsteel Landing GearSTC SA00780SEInstallation of the True Lock Safety Retention Axle Lock Nut SystemSTC SA00149BOInstallation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1STC SA03658ATInstallation of a Voice Alert System to incorporate as primary annunciators for stall and gear warningsSTC SA4305WEInstallation of GAR-AERO wheel adapters and tundra type tires on the main landing gearSTC SA00992ATInstallation of a wing forward spar fuselage attachment cluster and cross tube.STC SA10682SCInstallation of alternator and voltage regulatorSTC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA3531NMInstalling copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP)STC SA01154ATInstallation of the wing forward spar fuselage attachment assembly reinforcement.STC SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA01026SEImproved fuel gascolator assembly.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemSTC SA2515NMInstallation of Hoffmann HO 4/27 BHM-185 fixed pitch propeller in accordance with FAA Mile High Gliding, Inc. Report No. 2501 dated June 18, 1984, or later FAA approved revision. FAA Approved Airplane Flight Manual supplements are required for normal category as listed in the Approved Model List.STC SA316BOModification of a fuel system by the installation of a fuel pump and auxiliary fuel tank for the transfer of fuel from the auxiliary tank to the main tank.STC SA1315WEInstallation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA01085LAInstallation of the VNS 1000 Voice Navigation System.STC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA00769CHInstallation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540, AEIO-540 and HIO-540 engines.STC SA02139LAONE ONLY STC, S/N 25-7556161: Installation of a 38 gallon fuselage tank and selector valve.