N206FR
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.
22 reports on file, 2010-04-30 – 2026-04-22.
Part: COMPUTER — ABNORMAL (SLAT CONTROL) · airframe 48,830 hrs · 23,820 cycles
DURING FLAP/SLAP RETRACTION Â AT TAKEOFF F7CTL SLTAS LOCKED WING TIP BRK IAW AMM 27-51-34-000-001A AND 27-51-34-400-001A REV 76 01/FEB 2026 SFCC 22CV WAS REPLACED IN NORMAL CONDITION BITE TEST SATISFACTORY. IAW AMM 27-80-00-869-004A THE REST OF THE WING TIP BRAKE OF SLAT SYS WAS PERFORMED SATISFACTORY. OPS TEST OF SLAT SYS IAW AMM 27-84-00-710-001. SATISFACTORY Â DRIVE STATION CHK PERFORMED IAW AMM 27-84-00-210-001. TORQUE LIMITERS OF ACTUATOR 6085CM FOUND TRIPPED, APU CHK PERFORMED, IN GOOD CONDITION WITHOUT WATER FPPU CHK PERFORMED ZERO DATUM MARK, Â FOUND ALIGNED BY MCC REQUEST IS NECCESARY REPLACE ATUACTOR 6085CM IAW AMM27-84-49-000-001-A/400-001-A THE ACTUATOR TYPE B FIN 6085 CM R & R. OPS TEST OF SLAT POWER -TRASMISSION, FOUND SATISFACTORY.
Part: COMPUTER — FAULTED (FLAP SYSTEM) · airframe 23,664 hrs · 48,589 cycles
AFTER TAKE OFF FLAPS LOCKED. IAW AMM 27-51-00-740-002-A BITE TEST SLAT AND FLAP CONTROL COMPUTER, IAW AMM 27-50-00-869-006-A RESET OF WING TIP BRAKE WAS PERFORMED, SATISFACTORY, IAW AMM 31-36-00-000-001-A PCMCIA MEMORY CARD WAS DOWNLOADED. IAW TSM TASK 27-51-00-810-855-A WTB/POB TEST PERFORMED UNSUCCESSFULLY OR TEST ABORTED. AND AMM 27-51-00-710-001-A / 27-51-00-810-855-A REV 76 REV DATE 01 FEB 2026 WAS PERFORMED . THE SFCC 2 WAS REPLACED. NO HELP, BITE TEST AND W.T.B/ P.O.B OF TWO SYS FLAP AND SLATS WERE PERFORMED SEVERAL TIMES TO CONFIRM FAULT. THE WTB FLAP LT WERE FOUND WITH FOLLOW MESSAGE FLP LT WTB YEL SOLENOID 33CV FAULT AND FLP LT WTB BLUE SOLENOID 33CV FAULT. PENDING REPLACED OF THE WTB FLAP LH 33CV AND MANAGE THE COMPONENT SFCC COMPUTER. IAW AMM 27-51-51-000/400-001-A THE WING-TIP BRAKE (33CV) WAS REMOVED AND REPLACED.TEST SATISFACTORY.
Earlier reports · 2010–2022 · 20 reports
2022
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
DISCREPANCY: REFERENCE NR 12197.0547 AFT WET AREA FR 68 FLOORBEAM Y765 CORRODED. CORRECTIVE ACTION REMOVED AND REPLACED FLOORBEAM Y765 AT FR68 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
DISCREPANCY: REFERENCE LP 12197.0534 BEAM Y919 HAS CORROSION AROUND HOLE AT FRAME C66. CORRECTIVE ACTION: EVALUATED, REMOVED AND REPLACED FLOOR BEAM Y919 AT FR 66 IAW A320 SRM 53-00-14-283-002, 51-42-11 AND 51-75-12-911-002//END
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
DISCREPANCY: REFERENCE NR 12197.0545 AFT WET AREA FR 66 FLOORBEAM-Y1292 CORRODED. CORRECTIVE ACTION REMOVED AND REPLACED FLOORBEAM-Y1292 AT FR66 IAWA320 SRM 51-72-11
Part: RETAINER — CORRODED (R1 GIRT BAR) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
R1 DOOR AREA BELOW GIRT BAR RETAINERS, CORROSION ON WEB FWD AND AFT RETAINER AREA. EVALUATED AND REPAIRED R1 DOOR SILL WEB FWD AND AFT RETAINER AREAS IAW A320 SRM 53-11-14-283-005
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
CORROSION ON MULTIPLE AREAS ON RH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED RH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
CORROSION ON MULTIPLE AREAS ON LH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED LH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW A320 SRM 51-42-11. PERFORMED PERATIONAL TEST OF VOR 1 AND 2 SYSTEMS IAW AMM 34-55-00-740-002-A. BITE TEST GOOD
Part: BEAM — CORRODED (R2 DOOR SILL) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
AFT R2 DOOR SILL BEAM PREVIOUS REPAIR CORRODED. REMOVED AND REPLACED CORRODED R2 DOOR SILL IAW SRM 51-42-11
Part: BEAM — CORRODED (L1 DOOR SILL) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
L1 DOOR SILL BEAM, FWD AND AFT FASTENER HOLES CORRODED. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-42-11
Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 40,690 hrs · 16,821 cycles
MAIN CABIN L/H FLOOR SUPPORT Y1292 HAS CORROSION ON UPPER FLANGE STA 16-STA20. REMOVED AND REPLACED Y1292 FLOOR SUPPORT STA 16-20 IAW A320 SRM 51-72-911-002
2021
Part: CLAMP — LEAKING (APU) · airframe 40,097 hrs · 16,566 cycles
STRONG ODOR DURING APPROACH TO LANDING. LP172678 APU LEAKING OIL AT FAN ASSY. CLAMP / REMOVED AND REPLACED PACKINGS AND CLAMP IAW AMM 49-52-51-400-002-A, NO LEAKS NOTED AT THIS TIME. A/C OK TO CONTINUE
Part: UNKNOWN — ODOR (CABIN) · airframe 39,491 hrs · 16,293 cycles
LP177985 DISCREPENCY ITEM 1 -- FUME EVENT IN DESCENT AT 14000' TO LANDING SMELLED LIKE DIRTY SOCKS. FOUND OIL LEAKING FROM APU OIL DRAIN PLUG REPAIR PLUG LEAK CHECK GOOD REF LP177989 FOR ENGINE AND APU RUNS FOR TWO HOURS AMM 05-50-816-831
Part: DRAIN — LEAKING (APU) · airframe 39,488 hrs · 16,291 cycles
AFT FA'S REPORTED FEELINGS TINGELS AND SMELLED DIRTY SOCKS . C/W INSPECTION TO ID CAUSE OF FUME EVENT FOUND TO BE TYPE 3 ENG 2 & C/W DECONTAMINATION OF ECS. PER TSM T/S MANUAL 05-50-500-810-831-A. PLACED ENG 2 BLEED AIR SYSTEM ON MEL 36-11-01ACNTL # 1175494 DD 10-14-21 PER MCC TH 411864 A/C OK FOR SERVICE FOUND AND FIXED LEAK IN APU DRAIN PLUG. PERFORMED APU AND ENGINE WITH PACKS RUNNING. NO ODORS NOTED AT THIS TIME. AMM 05-50-00-810-831-A
Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 38,606 hrs · 15,859 cycles
DISCREPANCY: FUME EVENT (SMELLED LIKE ACFT OIL) ON APCH TO CUN. C/W QRH, MASKS ON, SWITCHED OFF LH PACK. A4FTER LANDING, FA'S SAID NO ODOR IN CABIN, BUT THEY COULD SMELL IT ON FLIGHT DECK. PLACED #1 PACK ON MEL# 25-52-01F. CORRECTIVE ACTION: REFERENCE MEL 21-52-01F - REACTIVATED PACK 1 FLOW CONTROL VALVE. PERFORMED TSM 05-50-00-810-831-0-A, COULD NOT DUPLICATE ODOR, NO ODOR PRESENT AT THIS TIME. OPS CHECK GOOD. THIS ACTION CLEARS MEL,PLACARDS REMOVED, AC OK FOR SERVICE. IAW TSM 05-50-00-810-831-0-A.
2017
Part: NUT — LOOSE (ENGINE MOUNT) · airframe 27,477 hrs · 11,057 cycles
NR 1 ENGINE AFT MOUNT INBD LINK UPPER SHEAR PIN, NUTS ARE LOOSE. REMOVED AND REPLACED THE NR 1 ENGINE AFT MOUNT I/B LINK UPPER SHEAR PIN NUT IAW AMM 71-72-11-400-043-A.
Part: NUT — LOOSE (ENGINE MOUNT) · airframe 27,477 hrs · 11,057 cycles
NR 1 ENGINE AFT MOUNT OTBD LINK UPPER SHEAR PIN NUT LOOSE. REMOVED AND REPLACED THE AFT MOUNT NUT IAW AMM 71-22-11-400-043-A.
2016
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,460 hrs · 9,504 cycles
LEFT EMERGENCY EXIT POWER SUPPLY BATTERY FAULT. REPLACED THE BATTERY PACK, OPS CHECKED OK. IAW AMM 33-51-38 PB 401.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,591 hrs · 8,354 cycles
DURING C CHECK INSPECTION NOTED L2 DOOR SILL CORRODED AROUND FASTENER HOLE AT FRAME 68. REPAIRED L2 DOOR SILL AT FRAME 68 IAW SRM 53-41-14 FIGURE 201.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,591 hrs · 8,354 cycles
DURING C CHECK INSPECTION, NOTED THE R2 DOOR SILL CORRODED AROUND FASTENER HOLE AT FRAME 68. REPAIRED R2 DOOR SILL AT FRAME 68 IAW SRM 53-41-14 FIGURE 201.
Part: HYDRAULIC LINE — BURST (RT MLG) · airframe 20,580 hrs · 8,349 cycles
HYD GREEN RSVR LOW LEVEL ECAM. R & R AFT HYD LINE RT MLG DOOR IAW AMM 32-31-39PB401. NO LEAKS NOTED AT THIS TIME. SERVICED GREEN HYD SYS.
2010
Part: EPSU — FAULTY (EMERGENCY LIGHTS) · airframe 15 hrs · 1 cycles
DISCOVERED DURING OVERNIGHT MX REF LOG PAGE 523605. EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL FAULTS. R & R EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL OPS CHECK GOOD IAW AMM 33-51-38 PB 401.