N203BZ
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
9 reports on file, 2024-09-09 – 2026-05-15.
Part: ENGINE — VIBRATION · airframe 11,980 hrs · 5,003 cycles
INTERMITTENT ENGINE VIBRATION DECENDING THROUGH 10000 FEET. SECOND TIME WE HAD AN ENGINE FAULT INDICATION AS WELL. VIBRATION COULD BE FELT ON THE RUDDER PEDALS WITH ADDED THRUST ON THE LEFT ENGINE. PERFORMED VIBE ANALYSIS. VIBES REMAIN IN ALLOWABLE LIMITS DURING ENGINE RUNS. NO FUALTS PRESENT DURING ENGINE RUNS.
Part: SPINNER — LEAKING (RT ENGINE) · airframe 11,180 hrs · 4,589 cycles
CABIN ODOR - RIGHT ENGINE SPINNER COVERED IN OIL, OIL SPLATTER IN COWLING. OIL SMELL IN FLIGHT DECK AND CABIN ON DESCENT AROUND 10K FEET. COMPLIED WITH FIM TASKS IN REFERENCE TO A220 AMM 71-00-00. FOUND NO OIL LEAK, FLUID FOUND TO BE DE-ICING FLUID. NO SMELL OF OIL IN CABIN NOR FLIGHT DECK DURING ENGINE RUN. AIRCRAFT GOOD FOR CONTINUED SERVICE. NO EMERGENCY DECLARED.
Part: LINE — BROKEN (RH ENGINE) · airframe 8,883 hrs · 3,434 cycles
R ENG FIRE MESSAGE IN FLIGHT. ENGINE SHUTDOWN AND 1 BOTLE DEPLOYED. PERFORMED INSPECTION AND FOUND NO EVIDENCE OF FIRE ON RH ENGINE. FOUND DAMAGED LINE THAT WAS IN VICINITY OF THE TR FIRE DETECTION LOOP. REPLACED LINE, AND REPLACED BLOWN FIRE BOTTLE.
Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL SYS) · airframe 7,439 hrs · 2,845 cycles
FUEL LEAK CAUTION MESSAGE APPEARED IN CRUISE AFTER 3 HOURS OF FLYING. FUEL BURN CONFIRMED, AND MESSAGE CLEARED AFTER 3 MINUTES. PERFORMED VISUAL INSPECTION OF FUEL SYSTEM WITH NO LEAKS FOUND.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,891 hrs · 2,623 cycles
FWD FUS RH LWR SKIN UNDERNEATH SCUFF PLATES, SERVICE DOOR, FWD FUS RH LWR SKIN UNDERNEATH SCUFF PLATES CORROSION FOUND ON SKIN. CORROSION REMOVED REPAIRED AS PER REO500-53-21-954----FOUND DURING HEAVY CHECK.
Part: ACCESS DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,891 hrs · 2,623 cycles
AFT LWR FUS WASTE ACCESS 146BR, AFT LWR FUS WASTE ACCESS 146BR FOUND CORROSION ON INNER SIDE, WASTE AREA, CORROSION REMOVED/REPAIRD S PER REO 500-52-47-129- HEAVY CHECK SDR SUBMISSION.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,891 hrs · 2,623 cycles
AFT WASTE DOUBLER REAR BARREL FUSELAGE, AFT WASTE DOUBLER INNER DOUBLER AT FR75 ST6R35 CORROSION, CORROSION REMOVED/REPAIR AS PER REO 500-53-61-1438
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,891 hrs · 2,623 cycles
RH SKIN FUSELAGE LWR SKIN FR 30A... RH SKIN TUS LOW3ER SKIN AT FR 30A/ST6R31 R FOUND CORROSION. CORROSION REMOVED/REPAIRED PER REO500-53-31-257
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,891 hrs · 2,623 cycles
FWD CARGO LWR SKIN UNDERNEATH SCUFF PLATES, CORROSION FOUND AROUND ATTACHMENT HOLES, CORROSION REMOVED/REPAIRED AS PER REO 500-52-21-100