N235FR
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
REFERENCE LP147381 #2 EMERGENCY POWER SUPPLY UNIT L (11WL) FAULT. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED MAINTENANCE VISIT. REPLACED EPSU FIN 11WL REF AMM TASK 33-51-38-000-001-A, AMM 33-51-38-400-001-A. BITE TEST OK, AC OK FOR SERVICE. /END/.
AC WAS OOS DUE TO DEFECT. FUME REPORT SEAT PLASTIC SMELL IN FLIGHT-PERFORMED TSA 05-05-00-810-831-A. IDENTIFICATION OD THE CAUSE FOR THE CABIN ODOR, SMOKE OR FUME. DURING INSPECTION FOUND ODOR COMING FROM COCKPIT PRINTER. CORRECTIVE ACTION: PERFORMED DEACTIVATION OF COCKPIT PRINTER AND PULL AND COLLARD CIRCUIT BREAK J21 IAW EA# A2-31R-39133. MEL 31-30+08A REMAINS OPEN.
FAULT HAPPENED DURING RON MAINTENANCE, SO DID NOT CAUSE A FLIGHT DELAY. DISCREPANCY: LP1263893 ITEM 3; DURING EPSU SYS TEST UNIT 11WL FAULTED. AFTER RESET OF UNIT 11WL, PERFORMED OPS CHECK OF EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK PER AMM 33-51-00-710-001-A. OPS CHECK GOOD AT THIS TIME, A/C OK FOR SERVICE.
DISCREPANCY: REFERENCE PEMCO N/R # 12704.0310 AFT CABIN AFT WET AREA R/H FLOOR BEAM AT THRESHOLD AREA HAS CORROSION AT ATTACHMENT HOLES AT FR 68. CORRECTIVE ACTION: CLEANED, EVALUATED & REPAIRED AFT CABIN WET AREA R/H FLOORBEAM AT THRESHOLD AREA ATTACHEMENTS HOLES AT FR 68 I.A.W. A320 SRM 53-41-300-001 REPAR CAT A, NO FURTHER ACTION REQUIRED
DISCREPANCY: REFERENCE PEMCO N/R#12704.0281 FWD FUSELAGE BELOW FLOOR BOARDS BETWEEN FR 16 AND FR 21 L/H L-1 DOOR THRESHOLD AREA LOWER O/B ATTACHMENT HOLES CORRODED (9EA) CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SILL FR 16 TO 20 CENTER SCUFF PLATE FITTING IAW A320 DRM 51-72-11, 51-42-11//END
DISCREPANCY: REFERENCE PEMCO N/R#12704.0309 AFT CABIN AFT WET AREA R/H SHEAR PLATE CRACKED UNDERNEATH FWD END CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN AFT WET AREA R/H SHEER PLATE IAW A320 SRM 51-42-11 PARA 2 E AD PARA 2L.//END//
DISCREPANCY: REFERENCE PEMCO N/R#12704.0308 AFT CABIN AFT WET AREA L/H SHEAR PLATE CRACKED UNDERNEATH FWD END. CORRECTIVE ACTION: REMOVED & REPLACED AFT CABIN AFT WET AREA L/H SHEER PLATE IAW A320 SRM 51-42-11
DISCREPANCY: REFERENCE PEMCO N/R#12704.0285 FWD FUSELAGE BELOW FLOOR BOARDS AT FR 15 Y503 HAS SURFACE CORROSION AT FLOOR BEMAFT END ATTACHMENTS HOLES CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM AT FR15 Y503 IAW A320 SRM 51-42-11///END//
DISCREPANCY: REFERENCE LP 251998 ITEM 1; PASSENGER / CREW DOOR L1 ARMED PLATE FELL OFF. CORRECTIVE ACTION: RESECURED PASSENGER / CREW DOOR L1 ARMED PLATE IAW AMM 52-11-22-420-054-B. A/C OK FOR SERVICE. TORQUE WRENCH STS 0236 DD 13 JUL 2022.
DISCREPANCY: REFERENCE LP151647 ITEM 1, PRECAUTIONARY: REPLACE LEFT FRONT DOOR SLIDE ARMED INDICATING LIGHT. CORRECTIVE ACTION: REMOVED AND REPLACED LEFT FRONT DOOR SLIDE ARMED INDICATING LIGHT PER AMM 52-73-21-000-001-A AND AMM 52-73-21-400-001-A. OPS CHECK GOOD NO FAULTS AT THIS TIME.
DISCREPANCY: REFERENCE LP151644 ITEM 1, LEFT FRONT DOOR INDICATES SLIDE ARMED EVEN THOUGH IT IS DISARMED. CORRECTIVE ACTION: R&R EMERGENCY BATTERY PACK AT EPSU (10WL), OPS CHECK GOOD REF. AMM 52-73-21-00-710.
11WL. FAILED EPSU SYS TEST, BATTERY WAS DUE TO EXPIRE 01/JUNE/2021. R&R EPSU UNIT, TEST OK AT THIS TIME REF AMM 33-51-38-04 CONF 00
DISCREPANCY: EPSU (13WL) POWER SUPPLY UNIT FAILED EPSU TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU PSU 13WL, PER AMM 33-51-18 PB401. OPERATIONS CHECK GOOD.
ONTINUED TROUBLESHOOTING, IAW A320 TSM 25-62-00-810-819H. FOUND CONNECTOR 2872 VC LOOSE, AFTER RECONNECTING OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001. 08/20/2020-SUPPLEMENT-CORRECTIVE ACTION: TROUBLESHOOTING PERFORMED IAW A-320-33-07-00-810-860. REMOVED AND REPLACED EPSU 13WL, IAW AMM A-320-0357-38-000-001. REMOVED AND REPLACED L2 DOOR SLIDE, IAW AMM A-320-25-62-44-400-006. DISCREPANCY: DURING HEAVY SERVICE CHECK, OPERATIONAL CHECK OF EMERGENCY LIGHTS FAILED. FAULTING EPSU (13WL) AFT L/ DEU B (300RH7). CORRECTIVE ACTION: PLACED L2 DOOR SLIDE ON MEL 25-61-02A CONTROL NR 1162136 DD 04/14/2020 PER TSM.
DISCREPANCY: REFERENCE LP1205537-1, APPROXIMATELY LAST 10-12 MINUTES OF FLIGHT DESCENDING BELOW 16,000 FEET, VIBRATION FELT ALONG WITH HUMMING/WHINING NOISE FLT DECK & FORWARD GALLEY FLOOR. NOTICED BY BOTH PILOTS AND FLIGHT ATTENDANTS. PLEASE INSPECT AVIONICS BAY. ALONG WITH VIBRATION & UNUSUAL NOISE, NOTICED A VERY FAINT SMELL POSSIBLY ELECTRICAL SMOKE. NO OTHER INDICATIONS OF FIRE WERE NOTICED. CORRECTIVE ACTION: REFERENCE LP1205537-1, AIRCRAFT WAS GROUNDED DUE TO DISCREPANCY. MX INSPECTED AIRCRAFT PER TSM 05-50-00-810-831-A FOR A TYPE 9 CAUSE. TESTED AEVC PER AMM TASK 21-26-00-710-001, EXTRACT FAN FAILED, PLACED EXTRACT FAN ON MEL 21-26-02C, CONTROL # 1148699, DUE 04/05/2019. MAINTENANCE PROCEDURE COMPLIED WITH AND VALVE VERIFIED OPEN. REFERENCE LP1205539-2, R&R AV EXTRACT BLOWER 18HQ OPS CK OK REF AMM 21-26-51-PB401 TW-F9T01840 06-19 P/N OFF: EVT3454HC S/N OFF 164907155 P/N ON: EVT3454HC S/N ON 164906426./END/
AIRSPEED DISCREPANCY ON INITIAL CLIMBOUT. CAPTAIN`S AIRSPEED 180, FIRST OFFICER'S 240. REMOVED AND REPLACED THE AIR DATA MODULE AT POSITION 19FP2 IAW AMM 34-11-17-000-001-A, AND 34-11-17-400-001-A. PERFORMED AN OPS TEST OF THE NR 2 ADR IAW AMM 34-13-00-740-003-A. OPS CHECKED GOOD.
NR 2 ENGINE FUEL RETURN VALVE LEAKING AT UNION. REMOVED AND REPLACED THE FUEL RETURN VALVE IAW AMM 73-11-50-400-002-A. LEAK AND OPS CHECKED GOOD.
SKIN DENTED FRAMES 8-9. PERFORMED A PERMANENT REPAIR IAW EA A2-53R-33747, REV C AND RDAS 80300178-046-2017.