N367P

STCs that may be installed · 347

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 = '7102302')
    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.

Airframe · Piper PA-23

STC SA4008NMInstallation of removable panels on the battery box slides.Bogert AviationSTC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.Garmin AT Inc.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.Aero Enhancements Inc.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.Avidyne CorporationSTC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.Garmin AT Inc.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.Garmin AT Inc.STC SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.JAARS Inc.STC SA00743SEInstallation of vortex generators on the wing leading edge, underside of the horizontal stabilizer, and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117, Revision IR, dated July 14, 1999, and Installation Instructions MA2118, Revision IR, dated September 21, 1999, or later FAA approved revisions to either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthyMicro AeroDynamics IncSTC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemPS Engineering IncorporatedSTC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.Aero Holdings Ltd. a Texas limited partnershipSTC SA01077SEInstallation of fluoropolymer film.Columbia Pacific AirlinesSTC SA4-994Installation of Firestone Model DFA-233 wheel assemblies, Model CFA-299 brake assemblies and6.50x8 6-ply tires.Skybound Manufacturing Inc.STC SA1008WEInstallation of Poly-Fiber covering material.Poly-Fiber Inc.STC ST02547ATInstallation of a voice alert system.Aircraft Components IncSTC SA00448DEInstallation of Oilamatic preoiler system.Oilamatic IncSTC 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.Avidyne CorporationSTC SA00695SEReplacement of certain Rotomaster and Rayjay scavenge pumpsMachen IncSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemAircraft & Rotorcraft Products (ARP) IncSTC SA2357CEInstallation of LH and RH main fuel tank bladder cells, P/N's DF054-320 and DF054-321, as replacements for original bladders.Floats & Fuel CellsSTC SA1480WEInstallation of an integral 24 gallon auxiliary fuel tank in each wing tip.Met-Co AireSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA00621LAInstallation of an electronic digital engine tachometer, horizon model P-1000.Horizon Instruments IncSTC SA02410ATReplace existing Auxiliary Electric Standby Fuel Pump with PMA Products, Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v), 1A15-s/n 24-3642, 24-4000 through 24-4782, 24-4784 through 24-4803, 2A13-s/n 28-7690001 through 28-7990626, 28-8090001 and up(14v)PMA Products, Inc.STC SA2-21Installation of landing lights in outer wing leading edge.Gulfstream Aerospace CorporationSTC SA3-334Installation of aerial camera provisions. Limited to Restricted Category with camera installed.Gulfstream Aerospace CorporationSTC SA01349NYInstallation of oil temperature coupler kit, P/N ALH-I-005, with Airparts Installation Drawing List as listed on AML No. Sa01349NY.Airparts of Lock HavenSTC SA2914WEInstallation of improved rudder trim tab actuating rod.Aviation Research CorporationSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA01058ATInstallation of Composite spinner.TCB Composite Co.STC SA01263ATInstallation of Composite Spinner.TCB Composite Co.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)D & K AviationSTC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'Advanced Aero Safety Inc.STC SA71GLInstallation of air filtersBrackett Aero Filters Inc.STC SA1306SWInstallation of Lycoming IO-360-C1C engines with Hartzell HC-C2YK-2/C7666A-4 propellers with gross weight increase.Apache Modification Aircraft CorporationSTC SA597SWExtended nose with baggage compartment.Apache Modification Aircraft CorporationSTC SA598SWInstallation of wheel well doors.Apache Modification Aircraft CorporationSTC SA599SWInstallation of fiberglass engine nose cowls.Apache Modification Aircraft CorporationSTC SA600SWInstallation of narcelle and wing root fairings.Apache Modification Aircraft CorporationSTC SA612SWInstallation of square wing tips.Apache Modification Aircraft CorporationSTC SA613SWInstallation of dorsal fin and square tip fin and rudder.Apache Modification Aircraft CorporationSTC SA697SWInstallation of one-piece windshield.Apache Modification Aircraft CorporationSTC SA698SWInstallation of Rear picture window.Apache Modification Aircraft CorporationSTC SA774SWInstallation of Franklin 64-350-C1 engines with McCauley 2AF31C10/84SF-8 propeller increase gross weight 3675 lbs. takeoff for Piper Model PA-23, and increase in gross weight to 3992 lbs take-off for Piper model PA-23-160Apache Modification Aircraft CorporationSTC SA779SWInstallation of auxiliary tanks in the nacelle over top of wingApache Modification Aircraft CorporationSTC SA803SWDual brake installationApache Modification Aircraft CorporationSTC SA894SWInstallation of nacelle saddleback.Apache Modification Aircraft CorporationSTC SA897SWInstallation of fiberglass propeller spinners.Apache Modification Aircraft CorporationSTC SA898SWRevised engine cowling installationApache Modification Aircraft CorporationSTC SA7815SW-DInstallation of S-TEC System 60 two axis automatic flight guidance system, Model ST-486, with optional automatic electric trim system.S-TEC Corporation
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