Cessna T337H-SP

STCs that may be installed · 160

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 ('2073015')
    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.

STC SA03100ATInstallation of Wing Auxiliary Fuel Tanks.Aviation EnterprisesSTC 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 SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.Electronics International Inc.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.Aviation EnterprisesSTC 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.Aviation EnterprisesSTC 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 SA02700ATInstallation of Air Conditioner SystemAviation EnterprisesSTC 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.Aviation EnterprisesSTC 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.Aviation EnterprisesSTC 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.Micro AeroDynamics IncSTC SA4961NMInstallation of a NSA sunvisor system for the pilot and copilot.Rosen Sunvisor Systems LLCSTC 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.Aviation EnterprisesSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA02510ATInstallation of a rear firewall engine accessory access door.Aviation Enterprises · Lists 337 SeriesSTC SA01091ATManufacture of mechanical cowl flap control system.Aviation Enterprises · Lists 337 SeriesSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA71GLInstallation of air filtersBrackett Aero Filters Inc.STC SA5090NMInstallation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip.Flint Aero IncSTC 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.Aviation EnterprisesSTC SA02023ATInstallation of a fuel transfer system to transfer fuel from a wing tip extension fuel tank to the main wing fuel tank.Aviation Enterprises · Lists 337 SeriesSTC SA01985ATInstallation of a fuel jettison system.Aviation Enterprises · Lists 337 SeriesSTC SA09419AC-DInstallation of S-TEC System 20/30 single and two axis automatic flight guidance systems, Model ST-869-20/30.S-TEC CorporationSTC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsJ P InstrumentsSTC SA02095AKInstallation of hourmeter airspeed switch.Avalaska IncSTC SA01093ATManufacture of short takeoff and landing (STOL) kit and tail boom to vertical fin fairings.Aviation Enterprises · Lists 337 SeriesSTC SA01090ATManufacture of flap gap seals.Aviation Enterprises · Lists 337 SeriesSTC SA01094ATManufacture of modified Lightning Wingtips.Aviation Enterprises · Lists 337 SeriesSTC SA00061LAInstallation of JPI digital tachometer.J P InstrumentsSTC SA5656NMInstallation of burglar alarm system.Thompson Harold SSTC SA00409ATInstallation of Cessna 02A entry door (P/N 1517080-1) and wind deflector.RT Aerospace Corp · Lists 337 SeriesSTC SA00410ATDesign, fabrication and installation of upper and lower windshield retaining gussets.RT Aerospace Corp · Lists 337 SeriesSTC SA3240SORemoval of main landing gear wheel doors and actuators, which are replaced with a fixed composite panel containing a cutout for gear passages.RT Aerospace CorpSTC SA1626NM PAGE 1Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)Electronics InternationalSTC SA7808SW-DInstallation of S-TEC system 60 Pitch Stabilization System Model ST-478 with Optional Automatic Electric Trim SystemS-TEC CorporationSTC SA5176NMInstallation of an ADC Corporation Model 5001A engine pre-oiler systemACD CorporationSTC SA1546GLInstallation of on-board engine analyzer system.Masten Products IncSTC SA7774SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems, model ST-317-40/50.S-TEC CorporationSTC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesElectronics InternationalSTC SA7209SW-DInstallation of S-TEC System 60 Two Axis Automatic /Flight Guidance System with Optional Autotrim System Model ST-314.S-TEC CorporationSTC SA7203SW-DInstallation of S-TEC System 65 Two axis Automatic Flight Guidance System, Model ST-313.S-TEC CorporationSTC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.Electronics InternationalSTC SA4024NMReplace the standard Cessna oil drain plug with a Bogert Aviation quick drain.Bogert AviationSTC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.Electronics InternationalSTC SA4166NMInstallation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506.Malkasian PaulSTC SA1455NMInstallation of a flame proof auxiliary heater-dryer, Model12-1600.Thermal, IncSTC SA1418SOReplacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations)Aircraft Products Supply Co Inc · Lists T337 SeriesSTC SA2190NM PAGE 1Installation of electronics International Digital Volt/Amp Gauges and Accessories.Electronics InternationalSTC SA1558SWInstallation of vortex generators, wing leading edge cuffs, wing tips, fairings, de-icing boots and stall strips.Williams Barbara or BobSTC SA1356CEChrome-plated brake disc installation.Engineering Plating & Processing, Inc. · Lists T337 Series
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