Cessna T337D
STCs that may be installed · 192
In force first, then newest. The registry doesn’t record which STCs an aircraft has.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2075719')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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 s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2075719')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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.
STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA638GLInstallation of a Shadin Co. 910516 fuel flow indicating system.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA00729SEInstallation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760, Revision -, dated 7/20/99, or later FAA approved revision.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 SA03100ATInstallation of Wing Auxiliary Fuel Tanks.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.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 SA02307ATInstallation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, or later FAA approved revisions.STC SA02308ATInstallation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions.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 ST01548LAInstallation of external landing gear position verification mirrors and aft engine cowl observation mirrors.STC SA1823NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.STC SA02700ATInstallation of Air Conditioner SystemSTC SA02686ATInstallation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions, dated June 15, 2003, or later FAA approved revision.STC SA02055ATInstallation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.STC SA01215SEInstallation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.STC ST02547ATInstallation of a voice alert system.STC SA4961NMInstallation of a NSA sunvisor system for the pilot and copilot.STC SA02527ATInstallation of a landing gear in-transit warning light in 337 models that are equipped with an electric motor to retract landing gear instead of engine driven hydraulic pump.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA02510ATInstallation of a rear firewall engine accessory access door.STC SA01091ATManufacture of mechanical cowl flap control system.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA71GLInstallation of air filtersSTC SA02056ATInstallation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.STC SA02023ATInstallation of a fuel transfer system to transfer fuel from a wing tip extension fuel tank to the main wing fuel tank.STC SA01985ATInstallation of a fuel jettison system.STC SA09419AC-DInstallation of S-TEC System 20/30 single and two axis automatic flight guidance systems, Model ST-869-20/30.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA3863NMInstallation of American intercooled engines as modified by STC SE3864NM.STC SA1877NMInstallation of Hoskins Model CFS-2000A, -2001A, FT-200, fuel flow indicating system.STC SA02095AKInstallation of hourmeter airspeed switch.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA01093ATManufacture of short takeoff and landing (STOL) kit and tail boom to vertical fin fairings.STC SA01090ATManufacture of flap gap seals.STC SA01094ATManufacture of modified Lightning Wingtips.STC SA00061LAInstallation of JPI digital tachometer.STC SA2492SOInstallation of Appalachian Accessories stainless steel brake discs, P/N 75-25A.STC SA1801CEInstallation of Total Flood Corporation fire extinguishing system in the cabin and/or fire extinguishant system in engine compartments.STC SA5656NMInstallation of burglar alarm system.STC SA00409ATInstallation of Cessna 02A entry door (P/N 1517080-1) and wind deflector.STC SA00410ATDesign, fabrication and installation of upper and lower windshield retaining gussets.STC SA3240SORemoval of main landing gear wheel doors and actuators, which are replaced with a fixed composite panel containing a cutout for gear passages.STC SA5926NMInstallation of manifold pressure instrument.
Back to Cessna T337D