N110LL
STCs that may be installed · 320
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 = '7103902'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41509')
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 = '7103902'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41509')
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-39
STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA00670ATInstallation of an OCEM AP-2C or AP-3C autopilot system in accordance with Automatic Flight Systems OCEM AP-2C, AP-3C Installation Manual for Aircraft Piper Models PA-30 and PA-39 dated February 15, 1995, or later FAA Approved revisions.STC SA00733ATInstallation of composite aft spinner bulkhead and/or composite spinner.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA01252SEInstallation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document.STC SA428NEInstallation of William C. Roberts brake discs P/N 202-22SS in lieu of Piper brake discs P/N 754-554.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA00027SEInstallation of CAPCO Auxiliary Nacelle Fuel TanksSTC ST02547ATInstallation of a voice alert system.STC SA5983NMCockpit sun visor installation.STC 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.STC SA00786SEInstallation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30, Revision G, dated August 1, 2002, or later FAA approved revision.STC SA2652CEInstallation of main fuel cell bladders as replacements for original bladders.STC SA5841NMInstallation of an engine electronic digital tachometer.STC SA01571CHInstallation of modified nose cone.STC SA01349NYInstallation of oil temperature coupler kit, P/N ALH-I-005, with Airparts Installation Drawing List as listed on AML No. Sa01349NY.STC SA8891SW-DInstall S-TEC System 55, 2 axis automatic flight guidance system, Model ST-562, with optional autotrim system.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA01280CHInstallation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404)STC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'STC SA693CEReplace existing engine induction air filter with AC Spark Plug filter.STC SA71GLInstallation of air filtersSTC SA00763SEInstallation of vortex generators on the wing leading edge, and vertical fin surfaces.STC SA1153SWSquare wing tips with dual navigation lights.STC SA557GLInstallation of Hartzell Propeller Models HC-E2YL-2BSF/F7663-6Q and HC-E2YL-2BLSF/FJ7663-6Q and Hartzell D-5749(P) or D-5749(P) spinners.STC SA3336WEInstallation of single piece windshield.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA516GLInstallation of aileron, flap, flap to fuselage, rudder gap seals, wing root fairings, dorsal fin, and engine nacelle fairing.STC SA1111SWInstallation of outer wing integral auxiliary fuel tanks including gross weight increase of 180 pounds.STC SA1112SWInstallation of dorsal fin.STC SA1113SWInstallation of extended nose with baggage compartment of 130 lbs capacitySTC SA1114SWInstallation of nacelle baggage compartments of 75 lbs capacity each sideSTC SA1115SWDual brakes.STC SA1151SWInstallation of Lycoming IO-360-C1C engine (200 hp) with Hartzell HC-C2YK-2/ C7666A-4 propeller.STC SA1152SWInstallation of one-piece windshield.STC SA1239SWInstallation of Rajay turbosupercharges and Lycoming IO-360-C1C or IO-360-C1F engines.STC SA1254SWInstallation of electrothermal propeller de-icing system. Aircraft must be placarded: WARNING. THIS AIRPLANE NOT APPROVED FOR FLIGHT INTO KNOWN ICING CONDITIONS.STC SA1337SWInstallation of pneumatic de-icing system.STC SA1341SWInstallation of nose taxi light.STC SA09363AC-DInstallation of S-TEC system 30 alt altitude hold system Model ST-817STC SA01224ATInstallation of wheel hub cabs with valve stem access door.STC SA1007NWInstallation of a low thrust detector system.STC SA02096AKInstallation of hourmeter airspeed switch. (PA-23-250 Navy UO-1)STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA00726CHReplace lower cabin door sill.STC SA00676CHReplace existing spinner with either Hartzell spinner P/N D-5749L or D-5749LP.STC SA1662GLInstallation of rudder fin cap fairing, with or without a strobe.