# N733TA: 2026 Costruzioni Aeronautiche Tecna P2010 - Status: Valid registration - Airframe: [Costruzioni Aeronautiche Tecna P2010](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2010) (registry code 0330402, 4 seats) - Engine: [Lycoming IO-390-C3B6](https://openairdocs.org/engine/lycoming-io-390-c3b6) (registry code 42710) - Data sheets: [TCDS A00066CE](https://openairdocs.org/tcds/A00066CE) (Costruzioni Aeronautiche Tecnam S.P.A.), [TCDS E00006NY](https://openairdocs.org/tcds/E00006NY) (Lycoming Engines) (OpenAirDocs) - Serial number: 337/US - Year built: 2026 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Standard, normal - Airworthiness date: July 14, 2026 - Certificate issued: July 1, 2026 - Expires: July 31, 2033 - Mode S code: A9D7DA - Registered owner: [Tecnam US Inc](https://openairdocs.org/faa-owner/TECNAM%20US%20INC) - Location: [Sebring, FL](https://openairdocs.org/faa-place/FL/Sebring) - Owner type: Non-citizen corporation - Owner's area on the map: 27.5033° N, 81.3677° W: Placed by OpenAirDocs at the center of ZIP code 33870, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=733TA - Page: https://openairdocs.org/aircraft/N733TA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 3 in force ### Matched by airframe (Costruzioni Aeronautiche Tecna P2010) - [AD 2026-07-05](https://openairdocs.org/ad/2026-07-05): Engine Exhaust System · Costruzioni Aeronautiche Tecnam P2010. Effective Apr 20, 2026 - [AD 2025-03-09](https://openairdocs.org/ad/2025-03-09): Rudder Control System · Costruzioni Aeronautiche Tecnam P2010 and P2010 TDI. Effective Mar 3, 2025 ### Matched by engine (Lycoming IO-390-C3B6) - [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 ## Information bulletins (advisory) (1 in force) - [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019 ## NTSB investigations None matched to N733TA. ## FAA accident and incident reports None matched to N733TA. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N733TA not matched to an aircraft (5) They name N733TA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DJFA2007138](https://openairdocs.org/sdr/DJFA2007138), Dec 2, 2007: HEATER. SMOKE. AT FL 400 CREW REPORTED SMOKE AND FUMES IN THE COCKPIT APPROX 3 MINS AFTER ACTIVATING/OPENING FLIGHT DECK HEAT VALVE. SMOKE WENT AWAY AFTER HEAT VALVE WAS CLOSE - [SDR DJFA2007112](https://openairdocs.org/sdr/DJFA2007112), Oct 1, 2007: CONNECTOR. BURNED. CREW REPORTED SMELL OF SMOKE FROM THE LAV AND BAGGAGE FIRE ILLUMINTATED. AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERED A BURNED PIN IN THE LAV WATER TANK CONNE - [SDR DJFA2006256](https://openairdocs.org/sdr/DJFA2006256), Jun 2, 2006: BRAKE ASSY. DRAGGING. CREW REPORTED THAT THE RT BRAKE PEDAL WENT TO THE FLOOR WITH VERY LITTLE BRAKING POWER ON THE RT SIDE. MAINTENANCE INSPECTED AND SERVICED EACH MASTER CYLINDER T - [SDR DJFA2006226](https://openairdocs.org/sdr/DJFA2006226), Apr 2, 2006: COALESCER BAG. SATURATED. WHEN MAIN AIR VALVES WERE OPENED TO PRESSURIZE AIRCRAFT AFTER TAKEOFF CREW REPORTED THAT SMOKE BEGAN TO COME INTO CABIN. CREW DONNED OXYGEN MASKS, AND TURNED TH - [SDR DJFA2005150](https://openairdocs.org/sdr/DJFA2005150), Oct 16, 2005: ENGINE. LEAKING. UPON CLIMB-OUT FROM KTEB, LT ENGINE OIL PRESS GAUGE FLUCTUATED BETWEEN 30 AND 40 PSI, AND RT OIL PRESS GAUGE REMAINED STEADY AT 37 PSI. APPROX 30 TO 40 MINS INT ## STCs that may be installed (OpenAirDocs) (13) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Costruzioni Aeronautiche Tecna P2010) - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA001410BO](https://openairdocs.org/stc/SA001410BO) (historical): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation ### Approved for the engine (Lycoming IO-390-C3B6) - [STC SE00825WI](https://openairdocs.org/stc/SE00825WI): Installation of Specialty Products Spin-on oil filter on Lycoming Engines. B & C Specialty Products Inc - [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd - [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp - [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc ## Earlier aircraft with N733TA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N733TA before. - [Cancelled 1989-01-30](https://openairdocs.org/deregistered/N733TA-1989-01-30): Cessna 172N, S/N 17268525. Triennial form not returned ## Related - Other Costruzioni Aeronautiche Tecna P2010 aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2010/aircraft.md - The Lycoming IO-390-C3B6 engine: https://openairdocs.org/engine/lycoming-io-390-c3b6.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.