N668UP
Registered owner: UMB BANK NA 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.
3 reports on file, 2026-04-12 – 2026-07-21.
Part: FLAP SYSTEM — NO DISCREPANCY · airframe 4,570 hrs · 3,594 cycles
FLAP FAIL AT 1 AFTER TAKEOFF ( EMERGENCY DECLARED ) ARRIVED AT ACFT & FOUND FLAPS SET TO FIRST NOTCH (1). POWERED ACFT & SELECTED 0 DEGREES (STOW) POSITION. FLAPS RETRACTED & STOWED WITH NO DISCREPANCIES OR CAS MESSAGES POSTED. PERFORMED SEVERAL ADDITIONAL FLAP EXTEND/RETRACT CYCLES WITH NO DISCREPANCIES NOTED. PERFORMED CMC DOWNLOADS & SUBMITTED FILES TO CONTACT CENTER. WHILE WAITING FOR TROUBLESHOOTING RECOMMENDATIONS FROM CONTACT CENTER, A NEW OEM DIAGNOSTICS SD CARD WAS MADE & CMC WAS INTERROGATED FOR ADDITIONAL DIAGNOSTIC DATA. WHILE MONITORING FLAP SENSOR DATA, IN FLAP SYS MONITOR PAGE IN CMC, PERFORMED SEVERAL ADDITIONAL EXTEND/RETRACT CYCLES, NOTING NO ABNORMAL READINGS BETWEEN POSITION TRANSMITTER DATA. NEW OEM DIAGNOSTICS CARD WAS PLACED IN SD CARD HOLDER BOX ATTACHED TO ACFT LAPTOP CASE. IAW RECOMMENDATIONS OF CONTACT CENTER, PERFORMED SATIS OPS CHECK OF FLAP SYS, NO DISCREPANCIES NOTED. WORK PERFORMED IAW AMM, 27-50-00.
Part: LEVER — FAILED (FLAPS) · airframe 4,204 hrs · 3,356 cycles
ON DEPARTURE FROM KEGE WHEN SELECTING THE FLAPS FROM 1TO 0 WE RECIEVED A FLAPS FAIL CAS AND THE FLAPS REMAINED AT 1. AIRSPEED WAS MAINTAINED BELOW 180 KNOTS AND MAXIMUM ALTITUDE WAS 17000'. THE QRH WAS UNABLE TO RESOLVE THE CONDITION. NORMAL LANDING FOLLOWED AT 16,100 LBS. ( EMERGENCY DECLARED ) INSTALLED CUSTOMER SUPPLIED REPAIRED FLAP SELECT LEVER P/N 780501-9 S/N 3273 IAW PH300 AMM 27-53-01 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. REF PH300 AMM 27-50-00-710-801A. UNIT REMOVED P/N 780501-9 S/N 1827.
Part: FLAP SYSTEM — FAULTED · airframe 4,182 hrs · 3,341 cycles
FLAPS FAILED IN NR 1 POSITION RIGHT AFTER TAKE OFF. ( EMERGENCY DECLARED) POWERED UP AIRCRAFT TO FIND FLAP3 FAIL AMBER CA3 MESSAGE DISPLAYED. GAINED ACCESS TO OEM DIAGNOSTICS BY CONFIGURING A CMC CONFIGURATION CARD AND VIEWING ACTIVE AND HISTORICAL FAULTS REF EMB-505 AMM CH 45-45-00. NO ACTIVE FAULTS PRESENT AT THIS TIME. HISTORICAL EVIDENCE SHOWED FAULT 743 I FCS FLAP DISAGREE, CODE 27523800. FOLLOWED FIM TASK 27-53-00-810-818-A TO FIND THIS AS A TRANSITORY CONDITION. RESET FLAPS CLEARING FLAPS FAIL CAS MESSAGE AND PERFORMED MULTIPLE OPS CHECKS REF EMB 505 AMM CH 27-50-00 WITH NO FURTHER DEFECTS OR RELATED MESSAGES.