N128AN
Registered owner: BANK OF UTAH 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
AIRCRAFT WAS GROUNDED: EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE ON ROWS 17ABC AND 18ABC. MAINTENANCE REPAIRED BROKEN WIRE ON HARNESS UNDER 17ABC PER ESPM 20-43-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: DOOR 4R HAS 4 INCH STRAP HANGING OUT. MAINTENANCE SECURED DOOR 4R SLIDE STRAP PER AMM 25-62-44.
AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 10WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.
AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 15WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.
AIRCRAFT WAS NOT GROUNDED: LIFE VEST MISSING AT SEAT 15B. MAINTENANCE INSTALLED LIFE VEST PER AMM 26-66-52.
AIRCRAFT WAS NOT GROUNDED: GREEN CORD HANGING FROM BOTTOM OF L1 DOOR. MAINTENANCE ACCOMPLISHED VISUAL INSPECTION L1 DOOR SLIDE GROUND CHECK GOOD AND RESTOWED EXCESS STRAP PER AMM 25-62-44.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS STRAP HANGING OUTSIDE OF FORWARD PASSENGER ENTRY DOOR (L1) DURING FLIGHT. ALL DOORS INDICATED CLOSED, NO ISSUE WITH CABIN PRESSURIZATION. MAINTENANCE INSTALLED MISSING BUCKLE ON L1 DOOR SLIDE PER AMM 25-62-44 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: DURING LEFT HAND FORWARD SLIDE CHANGE, EMERGENCY POWER SUPPLY UNIT SYSTEM TEST RESULTED IN FAULT MESSAGE. LEFT/EMERGENCY POWER SUPPLY UNIT (12WL) EXTERNAL RIGHT FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT (12WL).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ATL DUE TO A BURNING SMEEL IN THE REAR OF THE AIRCRAFT. THE AIRCRAFT LANDED SAFELY AT ATL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUNF THE AVIONICS VENT BLOWER FAN MOTOR 20HQ MAKING EXCESSIVE NOISE WITH A BURNING SMELL ALONG WITH A ECAM VENT BLOWER FAULT MESSAGE. MAINTENANCE REPLACED THE AVIONICS VENT BLOWER FAN MOTOR 20HQ PER AMM 21-26-51. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: SEATS 11, 12, 13 ABC EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 11,12,13 ABC PER SWPM 20-10-13.
AIRCRAFT WAS GROUNDED: EMERGENCY LIGHTS ON SEATS ABC ROWS 24 AND 25 ARE INOPERATIVE. 7261VC7A HAS BEEN REPLACED AND WIRES RE-TERMINATED
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INSIDE DOOR CUTOUT FORWARD EDGE STIFFENER LOCATED AT FR 71 BETWEEN STRINGERS 27R AND 31R. REPLACED FRAME ANGLE SUPPORT PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BOTH ENDS OF VIASAT CENTER DOUBLER BLANKING PLATE. REPLACED VIASAT CENTER DOUBLER BLANKING PLATE PER SRM 51-42-11.
AIRCRAFT WAS IN BASE MAINTENANCE: DURING EPSU SYSTEM TEST, EPSU (10WL) FWD L - DETECTED. REMOVED CEILING PANEL 221BC. REMOVED BATTERY (P/N#3214-31) OF EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL IAW A321 AMM 33-51-38-000-002-A. INSTALLED BATTERY (P/N#3214-31) OF EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL.
AIRCRAFT WAS IN BASE MAINTENANCE: DURING EPSU SYSTEM TEST, (13WL) AFT L FAULT IS DETECTED. DISPLACED EMERGENCY OXYGEN CONTAINER FROM THE SERVICE CHANNEL OF THE AFT UTILITY AREA IAW A321 AMM 35-21-41-000-001-A REMOVED THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) (13WL), INSTALLED SERVICEABLE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) (13WL). REINSTALLED EMERGENCY OXYGEN CONTAINER FROM THE SERVICE CHANNEL OF THE AFT UTILITY AREA.
AIRCRAFT WAS GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER BELOW SERVICE LIMITS. SERVICED DAMPER PER AMM 52-22-00.
AIRCRAFT WAS GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER BELOW SERVICE LIMITS. SERVICED DAMPER PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: 1:40 INTO FLIGHT, LEVEL AT FL 320-TWO, 1 SECOND IN DURATION ECAMS- SMOKE FORWARD CARGO SMOKE. SELF RESOLVED. MAINTENANCE ACCOMPLISHED SMOKE DETECTOR TEST WITH NOT FAULTS NOTED PER TSM 26-16-00-810.
AIRCRAFT WAS GROUNDED: UPON ARRIVAL (CABO). SJD ON POST FLIGHT INSPECTION FOUND ENGINE #1 OIL SERVICE DOOR HAD SEPERATED FROM COWLING WITH MULTIPLE GASHES IN COWLING AFT OF SERVICE AREA. REPLACED #1 ENGINE LEFT FAN COWL PER TASK CARD 26L00071006.
AIRCRAFT WAS GROUNDED: DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND EMERGENCY FLOOR PROXIMITY LIGHT ON SEAT 9C, 10C, AND 11C INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AT SEAT 11C, REPAIRED WIRES PER ESPM 20-43-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK FOR ALL SEAT LOCATIONS PER AMM 33-51-00 WITH NO DEFECTS NOTED.
AIRCRAFT WAS NOT GROUNDED: R3 DOOR DAMPER PRESSURE LOW. MAINTENANCE SERVICED DAMPER PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER PRESSURE LOW. MAINTENANCE SERVICED DAMPER PER AMM 52-22-00.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO A SLATS LOCKED AT 0 MESSAGE IN FLIGHT UPON ARRIVAL TO DFW. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE TORQUE LIMITER TRIPPED ON RIGHT WING #5 SLAT ACTUATOR 6091CM AND REPLACED THE ACTUATOR PER AMM 27-84-49.
AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ECAM DURING CRUISE LASTED A FEW SECONDS THEN WENT OUT ON ITS OWN FLIGHT ATTENDANTS REPORTED NO EVIDENCE OF SMOKING/VAPING. MAINTENANCE ACCOMPLISHED LAVATORY SMOKE DETECTOR SYSTEM OPERATIONAL CHECK PER AMM 26-17-00 WITH NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: VENT AVIONICS SYSTEM FAULT ON ECAM. CREW FOLLOWED ECAM ACTIONS AND AIRCRAFT WOULD NOT PRESSURIZE SUFFICIENTLY. (ORIGINAL ECAM WAS VENT SKIN VALVE FAULT). AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SFO WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53-00-002-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-26-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE INOPERATIVE. MAINTENANCE RE-SECURED DOOR HANDLE KNOB AT FORWARD LAVATORY DOOR, AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 14WL BATTERY FAULT DURING EMERGENCY LIGHT TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAULT DURING EMERGENCY LIGHT TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203245267: REPLACED LEFT WING SLAT #1 ACTUATOR 6013CM (AALA202203245267) AND RIGHT WING SLAT #1 ACTUATOR 6063CM (AALA202203262014) PER TSM TASK 27-81-00-810-810-A.** (CLOSED)
AIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203245267: REPLACED LEFT WING SLAT #1 ACTUATOR 6013CM (AALA202203245267) AND RIGHT WING SLAT #1 ACTUATOR 6063CM (AALA202203262014) PER TSM TASK 27-81-00-810-810-A.** (CLOSED)
AIRCRAFT WAS GROUNDED: ODOR IN FLIGHT DECK DESCENDING THOUGH 18,000 FEET UNTIL TAXI IN. OCCURRED IN FLIGHT DECK FIRST, THEN NOTICED IN CABIN ALSO BY 1ST FLIGHT ATTENDANT. SMELL REPORTED AS DIRTY/CHEMICALLY. ACCOMPLISHED CARD 26L00021001 SMOKE/TROUBLESHOOTING, FOUND HYDRAULIC FLUID IN KEEL BEAM AREA AND FOUND YELLOW SYSTEM HYDRAULIC DRAIN VALVE LEAKING. CLEANED HYDRAULIC FLUID IN AREA AND REMOVED AND REPLACED YELLOW HYDRAULIC SYSTEM RESERVOIR DRAIN VALVE IAW AMM 29-13-41.
AIRCRAFT WAS GROUNDED. R1 DOOR WILL NOT ARM. ARMING LEVER OUT OF RIG. ACCOMPLISHED ADJUSTMENT OF INTERLOCK MECHANISM OF EMERGENCY ESCAPE HANDLE, PER AMM 52-11-22-820-001-A AND TRIPLE LEVER RIGGING. PERFORMED INTERLOCK MECHANISM TEST, PER AMM 52-10-00-710-002-A. OPERATIONS CHECK GOOD. SUPPLEMENTAL REPORT TO ADD AIRCRAFT TIMES AND CYCLES TO SECTION 3.
AIRCRAFT IN BASE MAINTENANCE. INOPERATIVE PASSENGER SEAT EMERGENCY EXIT LIGHT AT SEAT ROW 36 LEFT IN PASSENGER CABIN (1 EA). PERFORMED CLEANING OF PASSENGER SEAT EMERGENCY EXIT LIGHT AT SEAT ROW 36 LEFT, PER ESPM 20-55-20-0201-01 IN PASSENGER CABIN (1 EA).
AIRCRAFT IN BASE MAINTENANCE. LOW PRESSURE PASSENGER CREW DOOR 832 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT AFT GALLEY AREA. REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 832, PER AMM 52-13-14-400-001-B.
AIRCRAFT IN BASE MAINTENANCE. LOW PRESSURE PASSENGER CREW DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT FORWARD GALLEY AREA. REPLACED CYLINDER DOOR DAMPER ON PASSENGER CREW DOOR 831 AT FORWARD GALLEY AREA, PER AMM 52-11-14-400-001-B.
AIRCRAFT IN BASE MAINTENANCE. DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA. REPLACED SLIDE RAFT PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA.
AIRCRAFT IN BASE MAINTENANCE. FOUND WEAR ON SUPPORT ARM PASSENGER CREW DOOR 841 UPPER FITTING ASSEMBLY FRAME TO ARM AT FORWARD GALLEY AREA. REPLACED UPPER SUPPORT ARM FITTING ON PASSENGER CREW DOOR 841, IAW AMM 52-11-31-400-002-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND WEAR ON SUPPORT ARM PASSENGER CREW DOOR 831 UPPER FITTING ASSEMBLY FRAME TO ARM AT FORWARD GALLEY AREA. REPLACED UPPER SUPPORT ARM FITTING ON PASSENGER CREW DOOR 831, IAW AMM 52-11-31-400-002-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 3 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 2 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 1 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM FITTING 6 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 5 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE FITTING 4 LEFT, IAW AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. LOW PRESSURE PASSENGER CREW DOOR 841 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT FORWARD GALLEY AREA. REPLACED CYLINDER DOOR DAMPER ON PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA, IAW AMM 52-11-14-400-001-B.
AIRCRAFT IN BASE MAINTENANCE. FOUND CORRODED AREA ON LOWER SILL BETWEEN FR 67 AND FR 68 AT STR 23L IN AFT GALLEY AREA, MEASURING L=1.005 INCH W=0.914 INCH D=0.040 INCH. PERFORMED PERMANENT REPAIR ON LOWER SILL, IAW A321 SRM 53-41-14-300-001 FIGURE 001, REPAIR PRINCIPLE 5.
AIRCRAFT IN BASE MAINTENANCE. FOUND L=0.863 INCH CRACK ON SHEAR PLATE AT FR 69 TO FR 70 AND STR 23L. REPLACED SHEAR PLATE, IAW SRM A321 51-72-11-911-001, 51-42-11-801 AND DWG D53474180.
AIRCRAFT IN BASE MAINTENANCE. FOUND L=0.927 INCH CRACK ON SHEAR PLATE FR 69 TO FR 70 AND STR 23R AT AFT GALLEY AREA. REPLACED SHEAR PLATE, IAW A321 SRM 51-42-11-801 & DWG D53474180.
AIRCRAFT IN BASE MAINTENANCE. FOUND CORRODED AREA ON CENTER FITTING AT STR 23R AND FR 16 TO FR 20 IN AFT GALLEY AREA MEASURING L=0.915 INCHES W=0.584 INCHES D=0.089 INCHES. REPLACED CENTER FITTING, IAW A321 SRM 51-72-11-911-001, 51-42-11-801 AND DWG D53135145.
AIRCRAFT WAS GROUNDED. DOOR 1L SLIDE WILL NOT ARM. REMOVED AND REPLACED DOOR 1L SLIDE/RAFT.
AIRCRAFT WAS NOT GROUNDED: MID FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERY DRAINED. REMOVED AND REPLACED MID FLIGHT ATTENDANT SEAT BATTERY PACK (AALA202008139005) & FLASHLIGHT AALA202008139004 PER AMM 25-65-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: MID FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERY DRAINED. REMOVED AND REPLACED MID FLIGHT ATTENDANT SEAT BATTERY PACK (AALA202008139005) & FLASHLIGHT AALA202008139004 PER AMM 25-65-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE - EPSU (EMERGENCY POWER SUPPLY UNIT) SYSTEM TEST, ERROR MESSAGE: BAT/EPSU (14WL) MID R. TROUBLESHOOTING PER TSM 33-51-00. REMOVED AND REPLACED EPSU 14WL PER AMM 33-58-00, OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF, UNDER 80 KNOTS, AFTER AMBER CAUTION DISPLAYED AND LEFT ENGINE WAS SLOW TO ACCELERATE. MAINTENANCE FOLLOWED TSM 73-00-00-810-880-A 13 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 71-00-00-700-011-B 13. NO FAULTS NOTED.
DURING TAXI OUT ALL CREWMEMBERS EXPERIENCED AN ACRID DE ICE LIQUID SMELL, SOMEWHAT OF A DIRTY SOCK SMELL, WENT AWAY AND DECISION WAS MADE TO DEPT. THEN GOING THRU APPROX16,000 AGAIN THE SMELL EVEN HEAVIER AND DECIDED TO RETURN TO ORD. NO EMERGENCY DECLARED, 10,000 LBS UNDER MAX A321 LANDING WEIGHT. RNWY 10R NO ARFF REQ
AIRCRAFT WAS NOT GROUNDED: R8 DOOR SLIDE ASSIST BOTTLE BELOW LIMITS. MAINTENANCE SERVICED DOOR SLIDE ASSIST BOTTLE TO PROPER PRESSURE PER MM 52-13-14.
AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY CYLINDER/ACCUMULATOR LOW. MAINTENANCE SERVICED DOOR EMERGENCY CYLINDER/ACCUMULATOR PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: ETOPS CARGO COMPARTMENTS CHECK FOUND SPONGY FLOOR PANELS 151QF, 151MF, 151QG AFT CARGO. MAINTENANCE REPLACED 151QF (SEE AALA201910029018), 151MF, 151QG FLOOR PANELS PER AMM 53-42-14.
AIRCRAFT WAS GROUNDED: ETOPS CARGO COMPARTMENTS CHECK FOUND SPONGY FLOOR PANELS 151QF, 151MF, 151QG AFT CARGO. MAINTENANCE REPLACED 151QF, 151MF (SEE AALA201910029019), 151QG (SEE AALA201910029020) FLOOR PANELS PER AMM 53-42-14.
AIRCRAFT WAS GROUNDED: ETOPS CARGO COMPARTMENTS CHECK FOUND SPONGY FLOOR PANELS 151QF, 151MF, 151QG AFT CARGO. MAINTENANCE REPLACED 151QF (SEE AALA201910029018), 151MF, 151QG FLOOR PANELS PER AMM 53-42-14.
AIRCRAFT WAS GROUNDED: PILOT REPORTS APU WONT START. MAINTENANCE FOUND POSITIVE CABLE AT APU STARTER BURNT OFF. PULLED CB L42 AND L41 ON PANEL 121VU FOR SAFETY. REPLACED WIRE TERMINALS TO APU STARTER, REPLACED APU STARTER IAW AMM 49-42-51. CONNECTED AND TORQUED WIRES TO APU STARTER. APU OPERATION CHECKS GOOD.
AIRCRAFT IN BASE VISIT: EPSU (12WL) FAILED CIDS1 EPSU SYSTEM TEST DURING T/C 26L00025011. REMOVED AND REPLACED EPSU (12WL) IAW AMM 33-51-38 OPS CHECK. GOOD OK FOR SVC IAW AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: 4R DOOR EMERGENCY OPERATING CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: 2R DOOR EMERGENCY OPERATING CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: 4R DOOR EMERGENCY OPERATIONAL CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY ACCUMULATOR (CYLINDER) AT 4R HAD LOW PRESSURE. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.
HAD AN ELECTRICAL ODOR AND VIBRATION. DIVERTED, EMERGENCY DECLARED, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AVIONICS VENT BLOWER FAN 20HQ CAUSING THE VIBRATION AND ODOR. REMOVED AND REPLACED THE BLOWER FAN IAW AMM 21-26-51. NO FAULTS NOTED. NO FURTHER ODOR OR VIBRATION IN THE CABIN.
R4 DOOR EMERGENCY CYLINDER PRESSURE WAS LOW, 1450 PSI, AT 71 DEGREES F. SERVICED THE CYLINDER IAW AMM 52-10-00.
L1 DOOR SLIDE DIFFICULT TO ARM AND DISARM. FOUND FOD IN THE AFT GIRT BAR RECEIVER LATCH. REMOVED THE FOD AND OPS CHECKED GOOD IAW AMM 52-00-00.
R4 DOOR OPERATION CYLINDER PRESSURE WAS LOW. 1200 PSI AT 76 DEGRESS F. SERVICED THE DOOR CYLINDER IAW AMM 52-10-00.
R4 DOOR DAMPER BOTTLE PRESSURE WAS LOW, 1400 PSI. SERVICED R4 DOOR DAMPER BOTTLE IAW AMM 52-13-11.
R4 DOOR EMERGENCY OPERATING CYLINDER PRESSURE LOW. MAINTENANCE SERVICED THE CYLINDER IAW AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
R1 DOOR EMERGENCY OPERATING CYLINDER PRESSURE LOW, 1400 PSI AT 80 DEGREES FARENHEIT. SERVICED THE R1 DOOR EMERGENCY OPERATING CYLINDER IAW AMM 52-10-00.
R4 DOOR DAMPER EMERGENCY OPERATION CYLINDER AT 1400 PSI AT 79 DEGREES F. SERVICED THE CYLINDER IAW AMM 52-10-00-614-001-A.
R4 DOOR DAMPER PRESSURE IS LOW. SERVICED THE DOOR DAMPER IAWCARD 52-93-01.
R4 DOOR WOULD NOT ARM. FOUND DEBRIS IN DOOR SEAL.
AIRCRAFT GROUNDED. SEAT 34C EMERGENCY LIGHT IS INOPERATIVE. SPLICED BROKEN WHITE WIRE BETWEEN SEATS 33ABC AND 34ABC PER ESPM 20-43-11 AND AWM 33-51-08. OPERATIONS CHECK OKAY.
AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE SHOWING ZERO PRESSURE. SERVICED L1 DAMPER TO PROPER PRESSURE PER AMM 52-11-14.
AIRCRAFT WAS NOT GROUNDED: LOOSE L1 SLIDE. REPLACED L1 SLIDE PER MCM 25-94-03.
R4 ENTRY DOOR AFT ASSIST HANDLE WAS MISSING UPPER HALF. REPLACED THE UPPER HALF OF THE R4 ENTRY DOOR AFT ASSIST HANDLE.
AIRCRAFT WAS NOT GROUNDED: EPSU SYSTEM TEST FAILS 13WL BATTERY PACK WHEN TESTING CIDS 1 SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED. BROKEN EMERGENCY PATH LIGHT LENS COVER AT LAVATORY D. REPLACED LIGHT LENS ASSEMBLY PER MM 33-51-19-400.
AIRCRAFT WAS NOT GROUNDED. BROKEN EMERGENCY PATH LIGHT LENS / COVER AT LAVATORY L. REPLACED LIGHT LENS ASSEMBLY PER MM 33-51-19-400.
AIRCRAFT WAS NOT GROUNDED. PERFORMED EMERGENCY POWER SUPPLY UNIT TEST, FOUND EMERGENCY BATTERY POSITION 13WL FAULT. REPLACED BATTERY PACK 13 WL (AFT) PER MM 33-50-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED. FOUND R1 DOOR EMERGENCY EXIT HOLDER BROKEN. REPLACED R1 DOOR EMERGENCY EXIT LIGHT PER AMM 33-51-13. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
R4 DOOR DAMPER PRESSURE BELOW LIMIT. SERVICED R4 DOOR DAMPER IAW AMM 52-10-00.
CRACKED LOWER EMERGENCY LIGHT AT R4 DOOR. REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-51-13.
CRACKED LOWER EMERGENCY LIGHT AT L1 DOOR. REPLACED EMERGENCY LIGHT ASSEMBLY BY L1 DOOR IAW MM 33-51-13.
DURING ETOPS INSPECTION FOUND AFT CARGO FLOOR PANEL 151LF DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS GROUNDED. DURING ETOPS INSPECTION FOUND AFT CARGO FLOOR PANEL 151LF DELAMINATED. REPLACED FLOOR PANEL 151LF PER AMM 53-42-14.
AIRCRAFT WAS NOT GROUNDED. R1 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. R1 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
DURING TAKEOFF ROLL CAPTAIN`S PFD SHOWED NO AIRSPEED. TAKEOFF ABORTED AT 105 KNOTS. FOUND INGESTED BUGS IN ALL PITOT PROBE. R & R CAPTAIN`S PITOT TUBE IAW AMM 34-11-15.