N628VA
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
L2 DOOR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED EPSU 13WL IAW AMM 33-51-38,OPS CHECK OK
LOSS OF YELLOW HYDRAULIC SYSTEM AT CRUISE. REPLACED HYDRAULIC LINE, UNION, AND PACKINGS.
TORSION BOX LOWER SIDE SHELL STR15 L FASTENER HOLE IS CRACKED IN PRESSURE PLATE, 5TH HOLE FROM AFT, PER SB A320-53-1251, FIG A-GDAAA VIEW D. GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/17/2019 AND EC 5331.000001 CONFIG. 1LH
TORSION BOX LOWER SIDE SHELL STR15 R FASTENER HOLE IS CRACKED IN PRESSURE PLATE 2ND HOLE FROM AFT PER SB A320-53-1251 FIG. A-GDAAA VIEW D GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/17/2019 AND EC 5331.000001 CONFIG. RH
EVIDENCE OF CORROSION FOUND ON THE AFT LAVATORY VENT OUTLET SKIN CUTOUT GROUNDED - YES. REPAIRED SKIN PER A320 SRM 53-41-11-300-004
EVIDENCE OF CORROSION FOUND ON THE AFT LAVATORY VENT OUTLET SKIN CUTOUT GROUNDED - YES. REPAIRED SKIN PER A320 SRM 53-41-11-300-004
EVIDENCE OF CORROSION FOUND ON THE INTERNAL SURFACE COMMON TO THE AFT LAVATORY VENT FLANGE AND FUSELAGE SKIN GROUNDED - YES. REMOVED AND REPLACED INTERNAL DOUBLER PER A320 SRM 53-41-11-300-004, CORROSION TO SKIN WAS REPAIRED ON CUST CARD P063684
EMERGENCY LIGHT EPSU 11WL FAILS CAPACITY CHECK GROUNDED - YES. REMOVED & REPLACED 11WL BATTERY S/N 792862. OPS CHECK GOOD. A320 AMM 33-51-00, 33-51-38.
RT FLOORBEAM FR66 - FR68 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-42-11 AND DWG D53472172.
CABIN FWD WET AREA, SEAT TRACK CORRODED FR20 BS Y8077 RBL30, RBL-Y14 GROUNDED - YES. REMOVED DAMAGE ON SEAT TRACK, MATL REMOVED 0.015, MAX ALLOWABLE 0.012 FOUND TO BE OUT OF LIMITS PER SRM 53-00-15-283-001 FIG 001. REMOVED SEAT TRACK, SPLICE PLATE AND LIGHT ASSY PER SRM 51-42-11, INSTALLED NEW SEAT TRACK PER SRM 51-42-11.
CABIN FWD WET AREA FLOOR LONGITUDIANL BEAM CORRODED AT SCREW HOLE FR16 BS X7087, LBL22, BL+4560 GROUNDED - YES. REMOVED CORROSION AND FOUND CORROSION ON FWD CABIN WET AREA LONG BEAM DAMAGE EXCEEDED SERVICEABLE LIMITS IAW SRM 53-11-14. REMOVED FLOOR PANEL 211KF IAW SRM 51-42-11. REMOVED AUTOTRANSFORMER TRAY AND BEAM PER SRM 51-42-11, LOCATED AND DRILLED NEW BEAM PER SRM 53-11-14. INSTALLED NEW BEAM AND AUTOTRANSFORMER TRAY PER SRM 51-42-11, INSTALLED FLOOR PANEL 211KF PER SRM 51-42-11 AND AMM 53-12-11.
AFT CABIN FR68 AT RBL 30 THE FLOOR SUPPORT HAS CORROSION AROUND 2 CLIP NUTS. GROUNDED - YES. REMOVED DAMAGE, MAT LOSS 0.021 (0.016 MAX ALLOWABLE) AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-14. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-42-11 AND DWG 53472040.
DURING CLIMB, AN UNUSUAL ODOR WAS PRESENT IN THE FWD GALLEY, LAVATORY AREA. ALL SYSTEMS NORMAL, DISCONNECTED IFE AND ODOR DISSIPATED AFTER APPROX 20-30 MINUTES TOTAL. BOTH LAVATORY AND GALLEY AREA FULLY INSPECTED FOR SOURCE, NONE NOTED IFE REMAINED OFF FOR FLIGHT. MX ACCOMPLISHED TSM 05-50-00-81-08-31A, UNABLE TO DUPLICATE ODOR, TURNED ON IFE AND NO ODOR NOTED.
ON ARRIVAL, A BURNING ODOR FROM FWD GALLEY OVEN. MX INSPECTED AND DISCOVERED LT CABIN FAN FAULT ON ECAM AND SPLY CB X18 TRIPPED. PERFORMED INSPECTION IAW TSM 055000810831 AND FOUND LT CABIN FAN INOP WHICH CAUSED A BURNING SMELL AT FWD GALLEY OVEN. FWD GALLEY OPS CHECK GOOD AND OK FOR SERVICE. LT CABIN FAN AMBER ON ECAM. ITEM PLACED ON MEL 212101, MCC NOTIFIED. THIS OPENS MDDR 42992. MEL LIST UPDATED. PLACARD INSTALLED. INOPERATIVE LT CABIN FAN CAUSED ODOR AT FWD GALLEY OVEN AS A RESULT, REF LP 1071134 ITEM NR. FAN IS SCHEDULED TO BE REPLACED NEXT MX OPPORTUNITY. NO FURTHER REPORTS OF ODOR WERE NOTED ON THE SUBSEQUENT FLIGHTS.
AIRCRAFT EXPERIENCED A LOW CREW OXYGEN WARNING DURING CRUISE, THE ACFT DIVERTED FOR REPAIR. DURING TROUBLESHOOTING THE TECHS FOUND AN OXYGEN LEAK FROM THE LOW PRESSURE LINE FITTING AT THE OXYGEN BOTTLE PRESSURE REGULATOR. THE LINE WAS SECURED AND THE OXYGEN BOTTLE WAS REPLACED, NO FURTHER LEAKS WERE NOTED. MAINTENANCE CONTROL CREATED A WATCH ITEM TO MONITOR THE OXYGEN PRESSURE ON SUBSEQUENT FLIGHTS, TO DATE NO ABNORMAL OXYGEN PRESSURE HAS BEEN NOTED.
SHORTLY AFTER REACHING CRUISE ALTITUDE, THE CREW RECEIVED A CABIN PRESSURE NR 1 SYSTEM STATUS MESSAGE (CAB PR 1) DISPLAYED ON ECAM WITH AN ASSOCIATED CABIN PRESSURE "BUMP". IAW FCOM PRO-ABN-21 15/24 THE CREW CONTINUED TO DESTINATION. AFTER APPROXIMATELY 1 HR THE CREW RECEIVED A "CAB PRESSURE EXCESS CAB ALT ECAM" WARNING. THE CREW INITIATED A DESCENT TO FL100 AND DIVERTED. UPON ARRIVAL, LOCAL MAINTENANCE MET THE ACFT AND ACCOMPLISHED THE FOLLOWING AMM PROCEDURE AMM 21-31-00-710-002-A. THE NR 1 CABIN PRESSURE CONTROLLER WAS FOUND FAULTY AND DEACTIVATED IAW MEL 21-31-01-2. THERE WAS NO REPORT OF ACTUAL CABIN PRESSURE LOSS DURING THE EVENT. THE ACFT DEPARTED AND CONTINUED TO ITS FINAL DESTINATION WITHOUT ANY FURTHER FAULTS. THE NR 1 CABIN SYSTEM CONTROLLER WAS REPLACED AND THE SYSTEM WAS REACTIVATED.
CREW REPORTED AT INITIAL ACCELERATION, CLIMBING THRU 10000 FT, BLUE HYD OVERHEAT AND FAULT W/ASSOCIATED BLUE FLT CONTROL LOSS. CREW RETURNED TO DEPARTURE AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT AND TAXIIED TO THE GATE UNDER POWER. PROBLEM WAS TROUBLESHOT TO BLUE ELECTRIC PUMP FAILURE AND PUMP WAS REPLACED AS WELL AS CASE DRAIN FILTER IAW AMM 29-12-43. OVERWEIGHT LANDING INSPECTION ALSO PERFORMED IAW AMM 05-51-11-200-004-B WITH NO DEFECTS NOTED. NO REPORTS OF ANY ISSUES ASSOCIATED TO BLUE SYSTEM HYDRAULICS ON SUBSEQUENT FLIGHTS.
LEFT OVERWING EMERGENCY EXIT DOORS ARE NOT INDICATING ARMED. MAINTENANCE RESET THE OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-11-04, NO FURTHER DISCREPANCIES NOTED AFTER SEVERAL FLIGHTS.
DURING CLIMB, INFLIGHT TEAM REPORTED ELECTRICAL BURNING ODOR IN CABIN. SHUTDOWN THE IFE SYSTEM. ODOR DISSIPATED AND NO OTHER ISSUES WERE NOTED. RETURNED TO DEPARTURE, LANDED UNEVENTFULLY. MX ACCOMPLISHED TSM 24-00-00-810-823A FOR ELECTRICAL BURNING ODOR OR FUMES. NO ODOR NOTED FROM RELATED ACFT SYSTEMS. IFE SYSTEM POWER RESTORED AND OPERATED. ENGINES WERE RUN THERE WERE NO ASSOCIATED ODORS NOTED. A NR 2 ENGINE WASH WAS ACCOMPLISHED DUE TO PREVIOUS BIRD INGESTION. ACFT RELEASED TO SERVICE, NO FURTHER ISSUES NOTED.
ON ARRIVAL, L1 DOOR WAS OPENED AND NOTED THE L1 DOOR GUST LOCK WOULD NOT ENGAGE. MX REMOVED L1 DOOR LINER. CLEANED GUST LOCK MECHANISM, ROD SEAL INTO ITS NORMAL POSITION AND OPS CHECKED GOOD IAW AMM 52-11-21.
DISCOVERED THE L1 DOOR GUST LOCK WOULD NOT ENGAGE. MX RESECURED THE GUST LOCK ROD SEAL AND OPS CHECKED OK IAW AMM 52-11-21.
DURING APPROACH AT 1815Z, CREW NOTED A F/CTL SLATS FAULT WITH NO MOVEMENT OF THE SLATS IN THE SELECTED FLAP SETTING. MC NOTED AN ASSOCIATED SLT 1 AND 2 SYS JAM CHECK SLT MECH DRIVE MESSAGE. DECLARED AN EMERGENCY. UNEVENTFUL LANDING. THE F/CTL SLATS FAULT MESSAGE WAS CLEARED WITH A RESET OF THE SFCC 1 AND 2 CB`S IAW TSM 24-00-00. MX CHECKED THE TRAVEL RANGE OF THE SLATS OFR OBSTRUCTIONS AND CLEARANCE THEN CYCLED THE FLAPS THROUGH THE FULL RANGE SEVERAL TIMES- SYS CHECKED OK IAW AMM 27-84-00-710-001. THE ACFT WAS RETURNED TO SERVICE. FLIGHT WAS OPERATED WITH NO ISSUES NOTED. A FOLLOW UP REQUEST TO DO A COMPLETE OPS CHECK AND VISUAL INSP OF THE SLAT SYS. IT WAS ACCOMPLISHED WITH NO FINDINGS. ACCORDING TO THE OPERATORS RECORDS, ALL AD, SB, STC`S AND PMA`S ARE IN FULL COMPLIANCE WITH THE TYPE DESIGN CERTIFICATE AND ASSOC REGULATORY REQUIREMENTS.
ACFT WAS OPERATING FLIGHT, AFTER MAKING A NORMAL DEPARTURE AT 00F8Z (3 MIN LATE DUE TO NON-MX ISSUES) AND TOOK OFF AT 0106Z AIRMAN REPORTED A HYD Y RSVR OVHT ALONG WITH A HYD Y ENG 2 PUMP LO PR AND SYS LO PR MESSAGE AT 0111Z. AN ACARS WAS SENT BY THE CREW AT 0118Z NOTING THEY HAD THE MESSAGE AND THEY HAD COMPLIED WITH ECAM ACTIONS. AN AIRCELL CALL WAS PLACED BY THE CREW TO THE MX. THE CREW WAS REFERRED TO FCOM 3.02.29 FOR ACTION. THE CREW MADE THE DECISION TO RETURN AFTER CONFERRING WITH MX. AN EMERGENCY WAS DECLARED BY THE CREW. THE ACFT MADE AN UNEVENTFUL LANDING AT 0152Z AND SET BRAKES AT 0157Z. MX MET THE ACFT. UPON ACCOMPLISHING TSM 29-13-00-810-802, IT WAS FOUND THAT THE CHECK VALVE, 3083GM, PN ZCV63-6-1, HAD FAILED INTERNALLY. REF IPC 29-13-03-15B ITEM 100. THE RESERVOIR STILL HAD APPROX 205 GALLONS OF FLUID REMAINING. THE CHECK VALVE WAS REPLACED ALONG WITH THE Y-SYSTEM PRESSURE FILTER, LP FILTER AND CASE DRAIN FILTER PRECAUTIONARY. THE SYS WAS CHECKED WITH NO FURTHER ISSUES AND RETURNED TO SERVICE AT 1200Z ON THE 21ST. ACFT HAS HAD NO FURTHER REPORTS OF Y SYS FAULTS.
FUSELAGE DETAIL INSP OF CABIN FLOOR STRUCTURE BELOW AFT GALLEY WAS ACCOMPLISHED. DURING THE INSP, CORROSION WAS FOUND ON 1 LONGERON BEAM (Y=464.8) WHICH EXCEEDED SRM 53-00-14 ALLOWABLE LIMITS. LONGERON BEAM (PN D53472284008) WAS REPLACED.
ACFT WAS IN FOR OVERNIGHT SCHEDULED MX. DURING THE WEEKLY CHECK, IT WAS NOTED THAT THE LAST 3 ROWS OF COACH SEATS, 24, 25, AND 26 ABC, EXIT PATH LIGHTING WOULD NOT ILLUMINATE. UPON TROUBLESHOOTING, LINE MX FOUND THAT THE CONNECTOR FIN 7260VC10 HAD BROKEN WIRES ON THE SEAT SIDE OF THE HARNESS WHERE IT ENTERS THROUGH THE LOWER SIDEWALL AREA. CAUSE OF DAMAGE UNKNOWN. THESE EXIT POINTS ARE USUALLY COVERED BY A PROTECTIVE COVER, PN D9241160000200, WHIC IS SECURED IN 2 PLACES TO THE SIDEWALL. THE COVER IN THIS POSITION WAS MISSING. WORKING WITH MX CONTROL, IT WAS DETERMINED THAT REPAIRING THE HARNESS WAS NOT AN OPTION. A HARNESS ASSY, PN 8008-40-60-60, REF IIPC 33-51-09-20G, ITEM 80, WAS OBTAINED AND REPLACED ALONG WITH A NEW COVER. SYSTEM CK OK AND ULTIMATELY TOOK A 3 MINUTE DELAY FOR THE COMPLETION OF THIS TASK. ACCORDING TO THE OPERATOR`S RECORDS, ALL AD`S, SB`S, STC`S AND PMA`S ARE IN FULL COMPLIANCE WITH THE TYPE DESIGN CERTIFICATE AND ASSOCIATED REQUIREMENTS.