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.
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_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 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 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 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 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 SA5090NMInstallation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip.STC 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 SA02095AKInstallation of hourmeter airspeed switch.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 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 SA1626NM PAGE 1Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)STC SA7808SW-DInstallation of S-TEC system 60 Pitch Stabilization System Model ST-478 with Optional Automatic Electric Trim SystemSTC SA5176NMInstallation of an ADC Corporation Model 5001A engine pre-oiler systemSTC SA1546GLInstallation of on-board engine analyzer system.STC SA7774SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems, model ST-317-40/50.STC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA7209SW-DInstallation of S-TEC System 60 Two Axis Automatic /Flight Guidance System with Optional Autotrim System Model ST-314.STC SA7203SW-DInstallation of S-TEC System 65 Two axis Automatic Flight Guidance System, Model ST-313.STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.STC SA4024NMReplace the standard Cessna oil drain plug with a Bogert Aviation quick drain.STC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.STC SA4166NMInstallation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506.STC SA1455NMInstallation of a flame proof auxiliary heater-dryer, Model12-1600.STC SA1418SOReplacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations)STC SA2190NM PAGE 1Installation of electronics International Digital Volt/Amp Gauges and Accessories.STC SA1558SWInstallation of vortex generators, wing leading edge cuffs, wing tips, fairings, de-icing boots and stall strips.STC SA1356CEChrome-plated brake disc installation.
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