N206BZ
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.
7 reports on file, 2024-12-04 – 2026-07-22.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,841 hrs · 5,121 cycles
HEAVY CHECK, REAR BARREL WASTE DOUBLER FOUND CORRODED, WASTE DOUBLER REPAIRED.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,841 hrs · 5,121 cycles
HEAVY CHECK - FWD MID FUSELAGE SKIN BETWEEN FR 34/FR35, STGR 36L 36R, FOUND CORRODED. CORROSION REMOVED AND DAMAGE REPAIRED
Part: SUPPORT — CORRODED (ZONE 100) · airframe 11,841 hrs · 5,121 cycles
HVY CHECK SUBMISSION - CORROSION FOUND AT FR 57/FR58 ON WTBF SUPPORT ANGLE UNDER FAIRING 195KB. ANGLE REPLACED.
Part: NUT PLATE — BROKEN · airframe 10,545 hrs · 4,483 cycles
FACILITY FOR REPAIR - (HVY) - HD LO QTY - WHILE PERFORMING MX FOR HYD LEAK, FOUND LWR VS TE PANEL BOTTOM NUT PLATE BRACKET BROKEN OFF. VS TE LOWER CLOSURE RIB PN C01953501-005 AND VS TE HINGE #1 ASSY REPLACED PER CATA-55EA-02533.
Part: FUEL FILTER — CLOGGED (ZONE 100) · airframe 10,420 hrs · 4,416 cycles
LT AND RT FUEL FILTER CAUTION MESSAGE APPEARED SHORTLY AFTER TAKEOFF WHEN PASSING THROUGH 7000 FEET. BEGAN RUNNING QRH AND MESSAGED DIESAPPEARED. FUEL FLOW AND SYNOPTIC PAGE LOOKED NORMAL AND MESSAGE DID NOT ILLUMINATE AGAIN. DECLARED EMERGENCY FOR PRIORITY SPACING AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED FUEL FILTER ON LH AND RH ENGINES. LEAK CHECKED GOOD. OPERATIONAL CHECKS GOOD. SMALL AMOUNTS OF CONTAMINATES SEND OUT FOR EXAMINATION.
Part: RUDDER CONTROL — MALFUNCTIONED (ZONE 300) · airframe 8,620 hrs · 3,547 cycles
UNCOMMANDED RUDDER INPUTS OR YAW MOTION INFLIGHT. BECOMING LARGER DURING DESCENT THROUGH 10000 AND COINCIDING WITH SPEED REDUCTION (AUTOPILOT IN CONTROL). PERFORMED AUTOFLIGHT CONTROL SYSTEM TEST, WITH NO ANNOMOLIES NOTED AND NO FAULTS.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 7,381 hrs · 2,977 cycles
AFT LWR WASTE ACCESS CUTOUT AT FR 75 FOUND CORROSION. PERFORMED REPAIR.