# N282VA: 2023 Costruzioni Aeronautiche Tecna P2010 TDI - Status: Valid registration - Airframe: [Costruzioni Aeronautiche Tecna P2010 TDI](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2010-tdi) (registry code 0330403, 4 seats) - Engine: [Cont TAE125-02-125](https://openairdocs.org/engine/cont-tae125-02-125) (registry code 59309) - Data sheets: [TCDS A00066CE](https://openairdocs.org/tcds/A00066CE) (Costruzioni Aeronautiche Tecnam S.P.A.), [TCDS E00069EN](https://openairdocs.org/tcds/E00069EN) (Continental Aerospace Technologies GmbH) (OpenAirDocs) - Serial number: 254/US - Year built: 2023 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Standard, normal - Airworthiness date: January 19, 2024 - Certificate issued: October 9, 2024 - Expires: October 31, 2031 - Mode S code: A2D745 - Registered owner: [Switchback Aviation LLC](https://openairdocs.org/faa-owner/SWITCHBACK%20AVIATION%20LLC) - Location: [Red Lodge, MT](https://openairdocs.org/faa-place/MT/Red%20Lodge) - Owner type: LLC - Owner's area on the map: 45.0876° N, 109.5584° W: Placed by OpenAirDocs at the center of ZIP code 59068, 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=282VA - Page: https://openairdocs.org/aircraft/N282VA 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): 2 in force ### Matched by airframe (Costruzioni Aeronautiche Tecna P2010 TDI) - [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 (Cont TAE125-02-125) - [AD 2025-20-18](https://openairdocs.org/ad/2025-20-18): Coolant Servicing · Continental Aerospace Technologies TAE 125-02-125. Effective Oct 30, 2025 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N282VA. ## FAA accident and incident reports None matched to N282VA. ## 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 N282VA not matched to an aircraft (38) They name N282VA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASAA2021092036032](https://openairdocs.org/sdr/ASAA2021092036032), Sep 20, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHT BITE CHECK FAILS GROUNDED - YES. REMOVED AND REPLACED EPSV 10WE IAW A320 AMM 33-51-38. OPS CHECKS GOOD IAW A320 AMM 33-51-38-740-053-A - [SDR ASAA2021082535881](https://openairdocs.org/sdr/ASAA2021082535881), Aug 25, 2021: SKIN. PUNCTURED. ITEM 782 - LEFT ELEVATOR UPPER SURFACE HAS A SMALL DENT/PUNCTURE 3'-6" OUTBD OF FUSELAGE & 8" FROM TRAILING EDGE GROUNDED - YES. REPAIRED LEFT ELEVATOR UPPER SU - [SDR ASAA2021082735780](https://openairdocs.org/sdr/ASAA2021082735780), Jul 28, 2021: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR BEAM HAS CORROSION -Y500 AT FR 69 AND FR 70. GROUNDED - YES. FLOOR "L" BEAM Y-500 AT FR69- FR70, CORROSION DEPTH .035", ALLOWABLE MAX. DEPTH IS - [SDR ASAA2021072735779](https://openairdocs.org/sdr/ASAA2021072735779), Jul 27, 2021: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR BEAM CORRODED -Y160 FR68, GROUNDED - YES. FLOOR BEAM AT Y-160 FR 68 CORRODED BEYOND ALLOWABLE LIMITS, DEPTH OF CORROSION .032" MAX. ALLOWABLE . - [SDR ASAA2021072735778](https://openairdocs.org/sdr/ASAA2021072735778), Jul 27, 2021: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR BEAM CORRODED Y765 FR68. GROUNDED - YES. REMOVED CORROSION ON FLOOR BEAM Y765 FR 67-70. CORROSION DEPTH= .028" MAX ALLOWABLE DEPTH = .016" BEAM - [SDR ASAA2021072735660](https://openairdocs.org/sdr/ASAA2021072735660), Jul 27, 2021: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR BEAM CORRODED -Y765 FR 68 GROUNDED - YES. REMOVED CORROSION ON LONGITUDIONAL BEAM FR68 -Y765. CORROSION DEPTH=.080Ï¿½ MAX ALLOWABLE = .016Ï¿½ B - [SDR ASAA2020021033106](https://openairdocs.org/sdr/ASAA2020021033106), Feb 3, 2020: FIRE LOOP. UNKNOWN. DURING PRE-FLT INOP SYS ENG 2 LOOP B GROUNDED - YES. DEFERRED - [SDR ASAA20191231708](https://openairdocs.org/sdr/ASAA20191231708), Dec 27, 2019: WARNING MESSAGE. ILLUMINATED. WING ANTI-ICE FAULT INDICATION DURING DESCENT AND IN LEVEL FLIGHT, GROUNDED - YES. OPEN. - [SDR ASAA2019121331583](https://openairdocs.org/sdr/ASAA2019121331583), Dec 13, 2019: ANTI-ICE SYSTEM. FAULTED. PILOT REPORTS WING A. ICE SYS FAULT GROUNDED - YES. PFR SHOWS R WAI VALVE (10DL). R WING AI VALVE OPS OK (USING APU AIR) REF AMM 30-11-00-810-803A REQUIRES OPS - [SDR ASAA2019120961517](https://openairdocs.org/sdr/ASAA2019120961517), Dec 6, 2019: THERMOSTAT. FAILED. R/H WING ANTI-ICE FAULTED DURING DESCENT. GROUNDED - YES. BMC2 LOGGED 36-11-00 PRESS REG-V 4001HAZ OR SOL 10HAZ OR SENSE LINE. BMC2 BITE CK NORMAL, REF MM 36-11 - [SDR ASAA2019091930810](https://openairdocs.org/sdr/ASAA2019091930810), Sep 19, 2019: WARNING SYSTEM. FALSE ACTIVATION. AIR PACK 1 REGUL FAULT GROUNDED - YES. PERFORMED SYSTEM RESET IAW AMM 21-61-00-718-001, OPS CHECK GOOD FAULTS RESET. - [SDR ASAA2019091930809](https://openairdocs.org/sdr/ASAA2019091930809), Sep 19, 2019: WARNING SYSTEM. FALSE ACTIVATION. AUTO FLIGHT FCU 1 FAULT GROUNDED - YES. PERFORMED AFS TEST IAW AMM 22-96-00-710-001-A . TEST OK . OPS CHECK GOOD - [SDR ASAA2019061769698](https://openairdocs.org/sdr/ASAA2019061769698), Jun 16, 2019: LEVER. STICKING. ENGINE 2 THRUST LEVER STICKS IN REVERSE WHEN COMING BACK TO IDLE THRUST GROUNDED - YES. PERFORMED PFR CHECK NO FAULTS NOTED OPERATIONAL CHECK IAW 78-31-00-710-0 - [SDR ASAA2019052629515](https://openairdocs.org/sdr/ASAA2019052629515), May 26, 2019: WARNING SYSTEM. FALSE ACTIVATION. WING ANTI-ICE FAULT DURING DESCENT GROUNDED - YES. PERFORMED WING ANTI-ICE BITE TEST PER AMM 30-31-00-710 TEST OK. - [SDR ASAA2019052329451](https://openairdocs.org/sdr/ASAA2019052329451), May 23, 2019: UNKNOWN. MALFUNCTIONED. AP2 INOP GROUNDED - YES. PERFORMED RESET OF FMGC 1 AND 2 IAW AMM 22-83-00. OK FOR SERVICED. NO FAULTS NOTED. - [SDR ASAA2019052229449](https://openairdocs.org/sdr/ASAA2019052229449), May 22, 2019: ECU. FAULTY. ENGINE 1 FADEC A FAULT GROUNDED - YES. R&R ENG 1 ECU PER AMM 73-21-60-400-001-B OPS TEST GOOD. A/C OK FOR SERVICE. - [SDR ASAA2019032228763](https://openairdocs.org/sdr/ASAA2019032228763), Mar 22, 2019: WARNING SYSTEM. FALSE ACTIVATION. SMOKE CARGO FWD & AFT INDICATION DURING CRUISE. EACH INDICATION WAS ABOUT 3 SEC LONG AND SHOWED UP TWICE ON EICAS. NO FURTHER INDICATIONS AFTER THE TWO REPORTED - [SDR ASAA2019032028708](https://openairdocs.org/sdr/ASAA2019032028708), Mar 20, 2019: WARNING SYSTEM. ACTIVATED. ENGINE 2 IGN B FAULT GROUNDED - YES. ON DEFERRAL. - [SDR ASAA2019030828570](https://openairdocs.org/sdr/ASAA2019030828570), Mar 8, 2019: WARNING SYSTEM. ACTIVATED. WING ANTI ICE FAULT ECAM MESSAGE. GROUNDED - YES. DEFERRED PER MEL 30-11-01-01 - [SDR ASAA2019022728401](https://openairdocs.org/sdr/ASAA2019022728401), Feb 27, 2019: WARNING SYSTEM. FALSE ACTIVATION. WING ANTI ICE ECAM ON FINAL APPROACH GROUNDED - YES. PERFORMED TEST OF WING ANTI ICE PER AMM 30-11-00. TEST OK. A/C OK FOR SERVICE - [SDR ASAA2019021228166](https://openairdocs.org/sdr/ASAA2019021228166), Feb 12, 2019: WARNING SYSTEM. FALSE ACTIVATION. WING ANTI ICE SYSTEM FAULT (3) GROUNDED - YES. PERFORMED TSM 30-11-00-810-803-A, SUBTASK 30-11-00-710-052-A, A (B) 1, REF. TSM 36-11-00-810-810. BITE TEST OF TH - [SDR ASAA2018121437375](https://openairdocs.org/sdr/ASAA2018121437375), Dec 13, 2018: SENSOR. FAILED. PACK 1 REGUL FAULT IN FLIGHT GROUNDED - YES. REMOVED AND REPLACED PACK 1 COMPRESSOR OUTLET TEMP SENSOR 12HH. REF AMM 21-61-11. GRD CHECK OK. P/N OFF 9105A0005-0 - [SDR ASAA2018121097254](https://openairdocs.org/sdr/ASAA2018121097254), Dec 9, 2018: WARNING MESSAGE. FALSE ACTIVATION. AIR PACK 2 REGUL FAULT ECAM MSG GROUNDED - YES. DEFERRED. ETOPS RESTRICTED - [SDR ASAA2018121087253](https://openairdocs.org/sdr/ASAA2018121087253), Dec 8, 2018: WARNING MESSAGE. FALSE ACTIVATION. ECAM PACK 1 REGUL FAULT GROUNDED - YES. PERFORMED OPERATIONAL TEST OF THE PACK 1. OPS CHECK GOOD. NO FAULTS FOUND. REF AMM 21-61-00 - [SDR ASAA2018102626604](https://openairdocs.org/sdr/ASAA2018102626604), Oct 22, 2018: CONTROLLER. FAILED. NR 1 BLEED HEAT EXCHANGER DURING FLIGHT TEMP WAS IN AMBER INDICATING HALF TEMP OF NUMBER 2 BLEED HEAT EXCHANGER NO ECAM. GROUNDED - YES. R/R NR 1 ENG. THEROSTAT - [SDR ASAA2018061425056](https://openairdocs.org/sdr/ASAA2018061425056), Jun 14, 2018: WARNING SYSTEM. FALSE ACTIVATION. AIR BLEED 1 FAULT GROUNDED - YES. ENG BLEED RESET SUCCESSFUL. PERFORMED BITE TEST OF BMC NR 1 REF AMM 36-11-00 PB 501:OK: NO HISTORY IN PREVIOUS LOGPAGE OF JUN - [SDR ASAA2018052184712](https://openairdocs.org/sdr/ASAA2018052184712), May 18, 2018: INDICATOR. MALFUNCTIONED. HORIZONTAL AMBER LINES SHOWING ACROSS FUEL USED INDICATION NUMBERS. ACFT GROUNDED. PERFORMED AN ENGINE RUN ON ENGINES 1 & 2 IAW TSM 28-42-00-810-883-A. FAULTS C - [SDR ASAA2018041524267](https://openairdocs.org/sdr/ASAA2018041524267), Apr 15, 2018: REGULATOR. FAULTED. NR 1 A/C PACK REGULATOR FAULTED. ACFT GROUNDED. RESET THE A/C PACK TEMP CONTROL SYSTEM IAW AMM 21-61-00. OPS CHECKED GOOD. NO FAULTS. - [SDR ASAA2018041024208](https://openairdocs.org/sdr/ASAA2018041024208), Apr 10, 2018: SENSOR. FAULTY. NR 1 A/C PACK REGULATOR FAULTED. ACFT GROUNDED. ACCOMPLISHED COMPUTER RESET IAW TSM 24-00-00-810-818, AIRCRAFT OK FOR SERVICE. REMOVED AND REPLACED THE P1 COMP - [SDR ASAA2018032624045](https://openairdocs.org/sdr/ASAA2018032624045), Mar 26, 2018: RADAR. MALFUNCTIONED. NR 2 RADAR IS INOPERATIVE IN ALL MODES. ACFT GROUNDED. ACCOMPLISHED A BITE CHECK, ALL SYSTEMS NORMAL IAW AMM 31-41-00-740-002, OK FOR SERVICE. - [SDR ASAA2018032424037](https://openairdocs.org/sdr/ASAA2018032424037), Mar 24, 2018: PROXIMITY SWITCH. OUT OF ADJUST. AFT CARGO DOOR OPEN INDICATION, ACFT GROUNDED. AIR TURNBACK, ACCOMPLISHED RMA 2112 TO CLEAN AND ADJUSTED THE PROXIMITY SWITCH 32 WV AFT CARGO COMPARTMENT IAW IA - [SDR ASAA2018030823785](https://openairdocs.org/sdr/ASAA2018030823785), Mar 8, 2018: FCU. MALFUNCTIONED. NR 1 FCU INOPERATIVE ACFT GROUNDED. RESET THE NR 1 FCU IAW AMM 22-81-00, OPS CHECKED OK. FAULT CLEARED. - [SDR ASAA2018030123755](https://openairdocs.org/sdr/ASAA2018030123755), Mar 1, 2018: PCU. FAULTED. SLAT SYS 2 FAULT. ACFT GROUNDED. REMOVED AND REPLACED SLAT SYS 2 PCU IAW AMM 27-84-51. SLAT PCU HOSE INSTALLED, DRIVESHAFT INSTALLED AND FINAL TORQUE ACCOMPLISH - [SDR ASAA2018022523695](https://openairdocs.org/sdr/ASAA2018022523695), Feb 25, 2018: INTERFACE UNIT. FAILED. NR 2 ENGINE EIU FAULT. ECAM ENG-2 APPROACH IDLE ONLY. A/THR INOPERATIVE, REV 2 INOPERATIVE. ACFT GROUNDED. R & R THE NR 2 ENGINE EIU (ENGINE INTERFACE UNIT) IAW - [SDR ASAA2018012123258](https://openairdocs.org/sdr/ASAA2018012123258), Jan 21, 2018: WARNING LIGHT. FALSE ACTIVATION. AFT CARGO DOOR ECAM INDICATION AT 2,000 FT AFTER TAKEOFF. ACFT GROUNDED. PERFORMED AN OPS CHECK IAW AMM 52-71-12-400-002-(E). OPS OK. - [SDR VQI2018F00020](https://openairdocs.org/sdr/VQI2018F00020), Oct 11, 2017: UNKNOWN. MALFUNCTIONED. REPORTED THE FOLLOWING DEFECT ON THE GROUND IN SFO. APU DID NOT START ON FIRST TWO ATTEMPTS. CHECKED APU OPERATION IAW AMM 491000, APU CHECKED OK. NO FURTHER IS - [SDR VQI2017F00021](https://openairdocs.org/sdr/VQI2017F00021), Jun 29, 2017: IDG. FAILED. THE FLIGHT CREW REPORTED A NR 1 GENERATOR FAULT INFLIGHT, COMPLIED WITH ECAM, SUCCESSFUL RESET. R & R NR 1 IDG IAW AMM 24-21-51. OPS CHECKED GOOD, - [SDR VQIA2017080900037](https://openairdocs.org/sdr/VQIA2017080900037), Feb 26, 2017: PUMP. FAILED. THE FLIGHT CREW ON ACFT REPORTED THE LEFT FUEL TANK NR 1 FAULT. R & R FUEL PUMP AT FIN NR 21QA IAW AMM 282151, PB401. OPS CHECKED GOOD. NO FURTHER ISSUES REPORT ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Costruzioni Aeronautiche Tecna P2010 TDI aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2010-tdi/aircraft.md - The Cont TAE125-02-125 engine: https://openairdocs.org/engine/cont-tae125-02-125.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.