# N314TL: 2019 Perry Diclemente TUCANO REPLICA - Status: Valid registration - Airframe: [Perry Diclemente TUCANO REPLICA](https://openairdocs.org/model/perry-diclemente-tucano-replica) (registry code 056379N, 2 seats) - Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572) - Serial number: TR1703 - Year built: 2019 - Type: Fixed wing single engine - Engine type: 4 cycle - Kit: Flying Legend Italia Srls TUCANO REPLICA - Airworthiness: Experimental, amateur built - Airworthiness date: June 13, 2019 - Certificate issued: July 28, 2021 - Expires: July 31, 2028 - Mode S code: A35761 - Registered owner: [Schaaf Rodney B](https://openairdocs.org/faa-owner/SCHAAF%20RODNEY%20B) - Location: [Bowman, ND](https://openairdocs.org/faa-place/ND/Bowman) - Owner type: Individual - Owner's area on the map: 46.1608° N, 103.4236° W: Placed by OpenAirDocs at the center of ZIP code 58623, within about 13 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314TL - Page: https://openairdocs.org/aircraft/N314TL 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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Perry Diclemente TUCANO REPLICA) None in force. ### Matched by engine (Rotax 912ULS series) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N314TL. ## FAA accident and incident reports None matched to N314TL. ## 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 N314TL not matched to an aircraft (9) They name N314TL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 9JLA2014122905065](https://openairdocs.org/sdr/9JLA2014122905065), Sep 14, 2014: STEP. FAILED. DURING PAX DEPARTURE FROM ACFT THAT THE LOWER STEP OF THE MAIN ENTRY STAIRS FAILED. THE LOWER STEP & SUPPORT CONTROLLER WAS REPLACED WITH NEW. - [SDR 9JLA2014091005063](https://openairdocs.org/sdr/9JLA2014091005063), Sep 5, 2014: SERVO. WEAK. AN INTERMITTENT YAW DAMPENER FAULT, INDICATING THAT THE AUTO PILOT WOULD TRIP OFF WHILE IN TURBULENCE. TROUBLESHOOTING FOUND THE RUDDER SERVO PN 622-6717-104 SN - [SDR 9JLA2014012404246](https://openairdocs.org/sdr/9JLA2014012404246), Jan 4, 2014: PRESSURE SWITCH. DEFECTIVE. CREW REPORTED AN ANTI-ICE BLEED AIR DUCT FAILURE WARNING IN FLIGHT. TROUBLESHOOTING FOUND THE WING ANTI-ICE CONTAINMENT DUCT PRESS SWITCH HAD FAILED. THE SWITCH - [SDR 9JLA2013090504239](https://openairdocs.org/sdr/9JLA2013090504239), Aug 30, 2013: ACTUATOR. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE RT RETRACTABLE LANDING LIGHT WOULD NOT RETRACT AND STOW. TROUBLESHOOTING IDENTIFIED THE LANDING LIGHT ACTUATOR AS DEFECTIVE. R - [SDR 9JLA2013052204235](https://openairdocs.org/sdr/9JLA2013052204235), Apr 19, 2013: ADC. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE NR 1 PDF INDICATED THE LOSS OF IAS AND ALT ON THE CAPTAINS SIDE WHILE ENROUTE. TROUBLESHOOTING INDICATED THE NR 1 ADC DEFECTIV - [SDR 9JLA201271904219](https://openairdocs.org/sdr/9JLA201271904219), Jun 20, 2012: MOTOR. DEFECTIVE. CREW REPORTED THAT THE AIR CONDITIONING WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE AIR CON COMPRESSOR MOTOR AS DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED, F - [SDR 9JLA2012071704219](https://openairdocs.org/sdr/9JLA2012071704219), Jun 20, 2012: MOTOR. OVERHEATED. THE CREW REPORTED THE AIR CONDITIONING SYSTEM INOPERATIVE. TROUBLESHOOTING FOUND THE AIR CONDITIONER COMPRESSOR MOTOR DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED. - [SDR 9JLA2012071704216](https://openairdocs.org/sdr/9JLA2012071704216), Apr 18, 2012: INVERTER. DEFECTIVE. CREW REPORTED THE LT INVERTER FAILED IN FLIGHT. FOUND THE LT AC INVERTER TO BE DEFECTIVE. INSTALLED AN O/H UNIT, FUNCTIONAL CHECKED SATISFACTORY. - [SDR DIXA200700001](https://openairdocs.org/sdr/DIXA200700001), Feb 22, 2007: ELECTRICAL SYS. ODOR. FLIGHT CREW REPORTED HEARING A POPPING SOUND FROM BEHIND THE COCKPIT LT SIDEWALL AREA FOLLOWED BY A SLIGHT ELECTRICAL ODOR FOR A PERIOD OF 15 SECONDS. NO SYSTEM ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Perry Diclemente TUCANO REPLICA aircraft: https://openairdocs.org/model/perry-diclemente-tucano-replica/aircraft.md - The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.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.