N44708
STCs that may be installed · 449
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 = '7102808'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41514')
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 = '7102808'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41514')
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-28-180
STC SA03209ATInstallation of Gomolzig Quietflight low noise silencer P/N PA-28-606503.STC SA4008NMInstallation of removable panels on the battery box slides.STC 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.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA00072SECockpit sun visor installation.STC SA2660CEOperation of airplane on leaded and unleaded automotive gasoline, 91 minimum antiknock index(RON+MON)/2. Intermixing with aviation gasoline also approved. (PA-28-181 SN 28-671 to 28-5859, 28-7105001 to 28-7505261, 28-7690001 to 28-8590001 and up)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 SA02022CHInstallation of Pneumatic Luggage Door Strut Kit.STC SA01100ATInstallation of Composite Spinner.STC SA2213WEConversion of Lycoming O-360-A3A engine to Model O-360-A1A engine and installation of Hartzell HC-C2YK1-B/7666A-0 propeller.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA5053NMInstallation of acrylic window liners in accordance with FAA approved Gale R. Calhoon Report No. 3, no revision, dated September 1, 1990, or later FAA approved revision.STC SA02770ATInstallation of Aeronautical Electronics Corporation Electronic Checklist Models AEC-ECTO, AEC-ECTS or AEC-APWS.STC SA3332NMThe Model 702 VHF Communication Radio, P/N 430-0049-0 ( )-0( ), is installed on the Piper Model PA-28-180 airplane, in accordance with II Morrow, Inc. Installation Report No. 48, dated November 26, 1985.STC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01077SEInstallation of fluoropolymer film.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC ST02547ATInstallation of a voice alert system.STC SA09623ACInstallation of Century Flight Systems Model AK1069 Triden autopilotSTC SA01143WIInstallation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft.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 SA00261NYInstallation of Aviation Services, Inc. Model 1201 Cockpit Utility Light.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA09166AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-642,STC SA8548SW-DInstallation of a Century yaw damper system.STC SA330NEReplace original brake discs w/William C. Roberts stainless steel discs, P/N 201-120-SS. (M20M s/n 27-0001 thru 27-0116)STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA02454ATInstallation of a shoulder harness restraint system.STC SA09524SCConversion of existing Piper air conditioning system from R12 to R134a refrigerant.STC SA01174LAInstallation of supplemental baggage compartment below existing rear baggage compartment.STC 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)STC SA09470SCInstallation of Starter Indicator light system.STC SA09491SCInstallation of a low voltage warning system.STC SA525GLInstallation of Norton Radome kit, No. 4229XC.STC SA00849SEInstallation of vortex generators on wings and tail surfaces.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA00178ATInstallation of composite spinner and/or spinner bulkheads.STC SA00945ATInstallation of composite forward bulkhead.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 SA1487SOInstallation of speed enhancement kit.STC SA1800SOInstallation of Laminar landing gear fairing additions.STC SA693CEReplace existing engine induction air filter with AC Spark Plug filter.STC ST09524SCPiper conversion of air conditioning systems from using R12 to R134a refrigerant on aircraft models listed. For PA-31-300 s/n 31-660, 31-712 thru 31-900, 31-7300901& up. For PA-31-325 sns 31-7400990 & up. PA-31-350 sns, 31-5001& 31-5003, 31-7305005 upSTC SA09414AC-DInstallation of S-TEC System 40X/50X single and two axis automatic flight guidance systems, model ST-867-40X/50X.STC SA5136SW-DS-TEC System 60 single axis automatic flight guidance system ST-136.