N215BZ
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, 2023-09-24 – 2026-01-19.
Part: UNKNOWN — ODOR (CABIN) · airframe 10,159 hrs · 4,466 cycles
DURING SERVICE FAS REPORTED WEIRD SMELL IN CABIN. TECH INSPECTED VENTS AND ONLY FOUND MINOR DUST. PERFORMED INSPECTION OF AREA WITH NO DEFECTS NOTED. PERFORMED AIR CONDITIONING SYSTEM OPERATION TEST. NO SMELLS OR DEFECTS NOTED. NO EMERGENCY DECLARED, AND NO MEDICAL ATTENTION NEEDED FOR PAX OR CREW.
Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
AFT SERVICE DOOR UNDERNEATH SCUFF PLATES, FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062
Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FWD PASSENGER DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FOUND DURING HEAVY CHECK - AFT CARGO DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FOUND DURING HEAVY CHECK - REAR BARREL FR 79 STGR 34L FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FWD SERVICE DOOR UNDERNEATH SCUFF PLATES, FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062
Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FOUND DURING HEAVY CHECK - FWD PASSENGER DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062
Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,075 hrs · 3,390 cycles
FOUND DURING HEAVY CHECK - AFT PASSENGER DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 2,837 hrs · 1,163 cycles
MAJOR REPAIR PERFORMED TO AIRCRAFT FUSELAGE DUE TO CONTACT WITH JETBRIDGE.- DOUBLER REPAIR OF DENT #1 ON FORWARD LH FUSELAGE BETWEEN FR24 AND FR26 AND ON STGR 23 AND DENT #2 ON FR24 AND STGR 24