N201FR
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
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, 2009-05-24 – 2021-07-30.
Part: INTAKE — CONTAMINATED (APU) · airframe 44,984 hrs · 17,668 cycles
DISCREPANCY: STRONG BURNING RUBBER SMELL MID-FLIGHT ROWS 13-14 DURING DESCENT. / PERFORMED TSM 05-50-00-810-831-A DECISION TABLE MOST PROBABLE CAUSE APU. PERFORMED AMM 49-00-00-200-812-A. FOUND OIL ON INTAKE FLAP CLEANED AREA, OPENED APU AND INSPECTED, NO OTHER DEFECTS NOTED, RAN EACH PACK INDIVIDUALLY, NO ODOR NOTED.
Earlier reports · 2009–2019 · 21 reports
2019
Part: SLIDE — FAILED (L1 DOOR) · airframe 39,731 hrs · 15,366 cycles
DISCREPANCY: REFERENCE LOG PAGE LP1148549 ITEM 3, EPSU TEST FAILURE WITH MULTIPLE MX MESSAGES. AFTER FURTHER TROUBLE SHOOTING L1 DOOR SLIDE FOUND TO BE CAUSE. L1 DOOR SLIDE REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE REFERENCE AMM 25-62-44-012-A AND 011A. TEST OK./END/
2018
Part: NOT REPORTED — MALFUNCTIONED (RUDDER) · airframe 38,775 hrs · 14,963 cycles
ABORTED TAKE-OFF FOR RUDDER JAM/DIFFICULT DIRECTIONAL CONTROL. THE AIRCRAFT WAS GROUNDED DUE TO THE EVENT. MX PERFORMED YAW DAMP SYS TEST AMM 22-63-00-710-001-A, ADIRS SYS TEST AMM 34-14-00-740-004-A, AFS TEST AMM 22-91-00-710-001-A, AUTO CHANGEOVER FUNCTION AMM 22-60-00-710-002-A, RUDDER TRAVEL LIMITING FUNCTION AMM 22-61-00-710-001-A, AND ALL TESTS PASSED. FLIGHT CREW PERFORMED A HIGH SPEED TAXI AND AN OCF, BOTH SUCCESSFUL.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
LT FWD EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
RT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
LT AFT EMERGENCY EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
LT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
LT AFT EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 38,613 hrs · 14,897 cycles
RT AFT EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
MAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, FR16-FR18 BL 8.5+Y. REMOVED AND EVALUATED CORROSION OF FLOORBEAM AT Y8.5 FR16-18. MAX ALLOWED REMOVAL IS .031" MAT. REMOVED .038 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-44-11, 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
MAIN CABIN FLOORBEAM TOP CAP, CORRODED 1292, FR16. REMOVED CORROSION AND EVALUATED FLOORBEAM 1292 FR16. REMOVED .0185 MATERIAL, FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, 52-11-15 AND 51-44-11.
Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
MAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, Y+503.2, FR16. REMOVED AND EVALUATED CORROSION ON MAIN CABIN LONGITUDINAL FLOORBEAM AT Y+503.2 FR16. MAT REMOVED .082", MAX ALLOWED .047" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004 FIG 006 SHEET 1, REMOVED AND REPLACED DUMMY RAIL Y+503.2 FR 12-16 IAW SRM 51-42-11, 51-44-11 AND 51-72-11.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
L2 DOOR SILL CORRODED AT THE FWD AND AFT BLANKING PLATE FASTENER HOLES. REMOVED AND REPLACED THE L2 DOOR SILL IAW SRM 53-41-14-300-001, 51-72-11-911-001, 51-42-11 AND AMM 38-30-00.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
FLOORBEAM -Y765 CORRODED FR66. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 64 TO FS 66 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
R2 DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FWD SECTION. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001, 53-41-14-283-002, 51-42-11 AMM 38-30-00.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,613 hrs · 14,897 cycles
FLOORBEAM -Y765 CORRODED FR 68. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 67 TO FS 70 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.
2017
Part: SKIN — CORRODED (FRAME 70) · corrosion level 2 · airframe 32,344 hrs · 12,399 cycles
AFT RIGHT FUSELAGE LAVATORY BACKING SYSTEM EXHAUST VENT SKIN CUT-OUT SEPERATING AND CORRODED JUST FORWARD OF FRAME 70. REPAIRED THE SKIN.
2014
Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 23,855 hrs · 9,071 cycles
GREEN SYS HYD LINE FAILED, FLUID LOSS, RETURNED TO THE FIELD. R & R THE LINE ASSEMBLY IAW AMM 32-31-39-400-001-A. OPERATIONS IAW AMM 32-31-00-710-002-A01 & LEAK CHECKED NORMAL. LOG PAGE 911844 2.
2013
Part: SKIN — DENTED (NR 1 SLAT) · airframe 19,195 hrs · 6,990 cycles
ACFT OUT OF SERVICE DURING C4/S1 CHECK. LT WING L/E NR 1 SLAT DAMAGED OTBD END. REPAIRED IAW SRM 57-40-00, PB201.
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,195 hrs · 6,990 cycles
DURING C4/S1 CHECK. CABIN RT AFT SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6.B.(1)-(8). ACFT OUT OF SERVICE.
2010
Part: WIRE HARNESS — FAILED (COFFEEMAKER) · airframe 8,886 hrs · 2,942 cycles
SMOKE REPORTED IN AFT GALLEY. POWER WAS SHUTOFF AND BREAKERS PULLED, PERFORMED VISUAL INSP BEHIND AFT GALLEY UNIT, POWER CONTROL PANEL FOR COFFEE MAKERS, OVEN, INSPECTED WIRING HARNESS NO BURN MARKS, NO BURN MARKS ON PLUMBING LINES, FOUND AFT OVEN VENT FILTERS CLOGGED AND BLOCKED, NO VENTILATION, CLEANED FILTERS AND REINSTALLED VENT FILTERS, AFT GALLEY NR1 COFFEE MAKER WAS REMOVED AND FOUND BURN MARKS AROUND POWER SUPPLY. INSTALLED SERVICEABLE COFFEE MAKER AMM 25-35-15 PB401 OPS, CHECK GOOD.
2009
Part: ATTACH FITTING — BROKEN (ZONE 300) · airframe 4,374 hrs · 1,368 cycles
DURING DAILY CHECK, DEN MAINTENANCE NOTED THE LEFT INBOARD ELEVATOR SERVO CONTROL ATTACH POINT ANTI-ROTATION LUG WAS BROKEN. MAINTENANCE PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A REPAIR LUG TO THE LEFT HAND ELEVATOR INBOARD SERVO CONTROL FITTING PER AIRBUS SRM 55-26-47.