N161UW
Registered owner: AMERICAN AIRLINES INC, TX (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: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THE LOSS OF GREEN HYDRAULIC PRESSURE IN FLIGHT FOLLOWED BY YELLOW HYDRAULIC SYSTEM OVERHEAT. THE AIRCRAFT LANDED SAFELY AT DFW AND WAS TOWED TO THE GATE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
AIRCRAFT WAS NOT GROUNDED: MUTLIPLE FAULT MESSAGES FOR THE EMERGENCY POWER SUPPLY UNIT SYSTEM AS WELL AS INOPERATIVE EMERGENCY LIGHTS AT SEATS 14 ABC AND 15 ABC WERE NOTED DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 (AALA202603306873) AND THE L1 DOOR SLIDE PER JOB CARD 26L00025010 (AALA202603308202) WHICH CLEARED THE FAULT MESSAGES. MAINTENANCE FOUND A BROKEN WIRE ON THE WALL CONNECTOR FOR SEAT 14 ABC AND 15 ABC WHICH WAS REPAIRED PER ESPM 20-48-00. (AALA202603308199) A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED WITH NO FAULTS OR ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: MUTLIPLE FAULT MESSAGES FOR THE EMERGENCY POWER SUPPLY UNIT SYSTEM AS WELL AS INOPERATIVE EMERGENCY LIGHTS AT SEATS 14 ABC AND 15 ABC WERE NOTED DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 (AALA202603306873) AND THE L1 DOOR SLIDE PER JOB CARD 26L00025010 (AALA202603308202) WHICH CLEARED THE FAULT MESSAGES. MAINTENANCE FOUND A BROKEN WIRE ON THE WALL CONNECTOR FOR SEAT 14 ABC AND 15 ABC WHICH WAS REPAIRED PER ESPM 20-48-00. (AALA202603308199) A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED WITH NO FAULTS OR ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: MUTLIPLE FAULT MESSAGES FOR THE EMERGENCY POWER SUPPLY UNIT SYSTEM AS WELL AS INOPERATIVE EMERGENCY LIGHTS AT SEATS 14 ABC AND 15 ABC WERE NOTED DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 (AALA202603306873) AND THE L1 DOOR SLIDE PER JOB CARD 26L00025010 (AALA202603308202) WHICH CLEARED THE FAULT MESSAGES. MAINTENANCE FOUND A BROKEN WIRE ON THE WALL CONNECTOR FOR SEAT 14 ABC AND 15 ABC WHICH WAS REPAIRED PER ESPM 20-48-00. (AALA202603308199) A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED WITH NO FAULTS OR ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED AISLE EMERGENCY LIGHT DOES NOT ILLUMINATE AT SEAT 8C. MAINTENANCE FOUND SEAT 8C EMERGENCY EXIT LIGHT TERMINAL PULLED FROM CONNECTOR 7261VC3, RETERMINATED CONTACT PER ESPM 20-53-55 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED A LANYARD HANGING OUT OF L4 DOOR, CATERING UNABLE TO OPEN. MAINTENANCE OPENED L4 DOOR AND SECURED NYLON LANYARD STRAP PER AMM 52-13-00.
AIRCRAFT WAS GROUNDED: FLOOR EMERGENCY LIGHT AT SEAT ROW 31C IS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AT P2 CONNECTOR AT SEAT 31C, REPLACED EMERGENCY LIGHT HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER CMM 25-21-61.
AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND #2 RH EMERGENCY EXIT DOOR DAMPERS. MAINTENANCE SERVICED #2 RH EMERGENCY EXIT DOOR DAMPERS IAW AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AND SEATBELT SIGN AND NO PORTABLE DEVICES SIGNS AND ALL LIGHTS INCLUDING EMERGENCY LIGHTS COME ON AND START FLASHING WITH SOME SORT OF HIGH PITCH ALARM WITH NO CREW INPUT. CABIN LIGHTS GO TO FULL BRIGHT AND CAN NOT BE CONTROLLED BY CREW. NO FLIGHT DECK INDICATION OF ANY ALARMS ARE NOTICEABLE IN-FLIGHT DECK BUT THE ECAM DOES FLASH THE SEATBELT AND NP DEVICES AS THE ARE GOING ON AND OFF IN THE CABIN. MOVING THE FLIGHT DECK SWITCHES DOES NOT STOP THEM FROM CYCLING. LASTED ABOUT 8 MINUTES AND THEN STOPPED. THEN STARTED AGAIN 5 MINUTES LATER FOR ANOTHER TWO MINUTES THEN LIGHTS AT MAX BRIGHTNESS AND SIGNS ON FOR REMAINDER OF FLIGHT. MAINTENANCE CONFIRMED THE FAILURE OF THE CABIN ASSIGNMENT MODULE WAS CAUSING THE CIDS LIGHT TO BE ON THE FLIGHT ATTENDANTS PANEL AND REPLACED IT PER AMM 23-73-19. MAINTENANCE ALSO FOUND #2 ENGINE IDG WAS OPERATING OUT OF RANGE AND REPLACED IT PER TASK CARD. 26L40024001. (AALA202509174386) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES OR FAULTS NOTED.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AND SEATBELT SIGN AND NO PORTABLE DEVICES SIGNS AND ALL LIGHTS INCLUDING EMERGENCY LIGHTS COME ON AND START FLASHING WITH SOME SORT OF HIGH PITCH ALARM WITH NO CREW INPUT. CABIN LIGHTS GO TO FULL BRIGHT AND CAN NOT BE CONTROLLED BY CREW. NO FLIGHT DECK INDICATION OF ANY ALARMS ARE NOTICEABLE IN-FLIGHT DECK BUT THE ECAM DOES FLASH THE SEATBELT AND NP DEVICES AS THE ARE GOING ON AND OFF IN THE CABIN. MOVING THE FLIGHT DECK SWITCHES DOES NOT STOP THEM FROM CYCLING. LASTED ABOUT 8 MINUTES AND THEN STOPPED. THEN STARTED AGAIN 5 MINUTES LATER FOR ANOTHER TWO MINUTES THEN LIGHTS AT MAX BRIGHTNESS AND SIGNS ON FOR REMAINDER OF FLIGHT. MAINTENANCE CONFIRMED THE FAILURE OF THE CABIN ASSIGNMENT MODULE WAS CAUSING THE CIDS LIGHT TO BE ON THE FLIGHT ATTENDANTS PANEL AND REPLACED IT PER AMM 23-73-19. MAINTENANCE ALSO FOUND #2 ENGINE IDG WAS OPERATING OUT OF RANGE AND REPLACED IT PER TASK CARD. 26L40024001. (AALA202509174386) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES OR FAULTS NOTED.
AIRCRAFT WAS GROUNDED: EMERGENCY LIGHTS AND SEAT BELT SIGN & NO PORTABLE DEVICES SIGNS & ALL LIGHTS INCLUDING EMERGENCY LIGHTS COME ON AND START FLASHING WITH SOME SORT OF HIGH PITCH ALARM WITH NO CREW INPUT. CABIN LIGHTS GO TO FULL BRIGHT & CAN NOT BE CONTROLLED BY CREW. NO FLIGHT DECK INDICATION OF ANY ALARMS ARE NOTICEABLE IN-FLIGHT DECK BUT THE ECAM DOES FLASH THE SEATBELT AND NP DEVICES AS THE ARE GOING ON AND OFF IN THE CABIN. MOVING THE FLIGHT DECK SWITCHES DOES NOT STOP THEM FROM CYCLING. LASTED ABOUT 8 MINUTES AND THEN STOPPED. THEN STARTED AGAIN 5 MINUTES LATER FOR ANOTHER TWO MINUTES THEN LIGHTS AT MAX BRIGHTNESS AND SIGNS ON FOR REMAINDER OF FLIGHT. (OPEN)
AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT HAND DOOR 842 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT IN BASE MAINTENANCE: WHILE PERFORMING EMERGENCY LIGHT TEST, FAULT "EPSU BATTERY MID R" WAS DISPLAYED ON THE PTP PANEL. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT IN BASE MAINTENANCE: ON PTP PANEL 110RH EMERGENCY LIGHT SYSTEM TEST RETURNED: ATA 33-51-38 "EPSU BATTERY EXIT L" AND "EPSU ATTERY EXIT R" FAULT MESSAGE. REPLACED THE BATTERIES FOR EMERGENCY POWER SUPPLY UNIT 11WL (AALA202507082534) AND 12WL (AALA202507083117) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
AIRCRAFT IN BASE MAINTENANCE: ON PTP PANEL 110RH EMERGENCY LIGHT SYSTEM TEST RETURNED: ATA 33-51-38 "EPSU BATTERY EXIT L" AND "EPSU ATTERY EXIT R" FAULT MESSAGE. REPLACED THE BATTERIES FOR EMERGENCY POWER SUPPLY UNIT 11WL (AALA202507082534) AND 12WL (AALA202507083117) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557 HARNESS WIRING EGT, AALA202507099554 HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. A REVIEW OF THE DFDR DATA RESULTED IN THE DETERMINATION THAT THERE WAS AN EGT INDICATION ISSUE. MAINTENANCE REPLACED ALL OF THE EGT THERMOCOUPLES AND LEADS PER AMM 77-21-10. (AALA202506265557) HARNESS WIRING EGT, AALA202507099554, HARNESS WIRING EGT, AALA202507095688 HARNESS WIRING EGT, AALA202507099096 HARNESS WIRING EGT, AALA202507099743 HARNESS UPPER EGT, AALA202507098423 HARNESS LOWER EGT, AALA202507097894 COUPLING EGT)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVER LIMIT ON TAKEOFF. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED SAFELY AT PHX WHERE IT TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR LATCH CATCHING WHILE ATTEMPTING TO OPEN. LUBRICATED DOOR MECHANISM.
AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY 12WL FAULT. REMOVED AND REPLACED EPSU BATTERY 12WL.
AIRCRAFT WAS IN BASE MAINTENANCE: DONT WORK CORRECTLY EPSU-EMERGENCY POWER SUPPLY UNIT 14WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 14WL (AALA202409107071) INCLUDING BATTERY (AALA202409104806) IN PASSENGER CABIN IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. PERFORMED BITE TEST, TEST IS OK IAW AMM 33-51-00-710-001-A.
AIRCRAFT WAS IN BASE MAINTENANCE: DONT WORK CORRECTLY EPSU-EMERGENCY POWER SUPPLY UNIT 14WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 14WL (AALA202409107071) INCLUDING BATTERY (AALA202409104806) IN PASSENGER CABIN IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. PERFORMED BITE TEST, TEST IS OK IAW AMM 33-51-00-710-001-A.
AIRCRAFT WAS IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 12WL DOESNT WORK CORRECTLY INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202409100500) AND BATTERY (AALA202409107420) IN PASSENGER CABIN PER AMM 33-51-38-000-001-A.
AIRCRAFT WAS IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 12WL DOESNT WORK CORRECTLY INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202409100500) AND BATTERY (AALA202409107420) IN PASSENGER CABIN PER AMM 33-51-38-000-001-A.
AIRCRAFT WAS IN BASE MAINTENANCE: WHEN CLOSE DOOR 842 NO SHOW MESSAGE IN ECAM PAGE. TARGET WAS FOUND DIRTY PERFORMED CLEAN.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801.
AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION SLIDE PACK ASSEMBLY PASSENGER CREW DOOR 831 IN PASSENGER CABIN. REPLACED SLIDE PACK ASSEMBLY.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AR FR 35.2 BETWEEN S41L AND S42L. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 68 AND FR 69 AT -Y1162.5. REPLACED FLOOR SUPPORT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT FITTING AFT ATTACHMENT BRACKET WORN AT RIB 13 . REPLACED BRACKET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON FORWARD ATTACHMENT FITTING OUTBOARD UPPER SLEEVE / PIN BETWEEN PYLON RIBS 4 AND 5. REPLACED SLEEVE / PIN PER TASK CARD 26C41554028.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON FORWARD ATTACHMENT FITTING OUTBOARD LOWER SLEEVE / PIN BETWEEN PYLON RIBS 4 AND 5. REPLACED SLEEVE / PIN PER TASK CARD 26C42554028.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON FORWARD ATTACHMENT FITTING OUTBOARD UPPER SLEEVE / PIN BETWEEN PYLON RIBS 4 AND 5. REPLACED SLEEVE / PIN PER TASK CARD 26C42554028.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR 68 LEFT-HAND AT LEVEL STR 23L IN AFT GALLEY AREA. REPLACED CORNER FITTING AND FASTENERS PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: RIGHT AFT GALLEY CORNER FITTING WORN AT FR 68 AND S23R. REPLACED AFT CORNER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT FITTING AFT ATTACHMENT BRACKET WORN AT RIB 13 . REPLACED BRACKET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED ON FR 66 AT LEVEL STR 23L IN AFT GALLEY AREA. REPLACED CORNER FITTING PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT JACK FITTING BETWEEN WS 070 AND WS 141 BETWEEN RIBS 2 AND 3. REPAIRED LANDING GEAR RETRACTION ACTUATOR ATTACHMENT JACK FITTING PER EA 356779.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK # 6 LOWER AFT BOLT BETWEEN WS 6132 AND WS 6699, BETWEEN RIBS 11 AND 12. REPLACED BOLT PER AMM 27-84-64 AND TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK # 10 UPPER FORWARD BOLT BETWEEN WS 11198 AND WS 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66 AND TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK # 10 UPPER AFT BOLT BETWEEN WS 11198 AND WS 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66 AND TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK # 8 UPPER AFT BOLT BETWEEN WS 8744 AND WS 9235, BETWEEN RIBS 16 AND 17. REPLACED BOLT PER AMM 27-84-65 AND TASK CARD 26C61057005.
AIRCRAFT WAS IN BASE MAINTENANCE: CRACK HANDLE SLIDING WINDOW F/O SIDE IN COCKPIT. REPLACED HANDLE SLIDING WINDOW F/O SIDE IN COCKPIT.
AIRCRAFT WAS IN BASE MAINTENANCE: CRACK HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPIT. REPLACED HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPIT.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 AND AT STR 23R IN AFT GALLEY AREA. REPLACED LOWER SILL PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT COVER SHEET BETWEEN FR 52A AND FR 56, BETWEEN S39R AND S41R. REPAIRED COVER SHEET PER EA 202761A
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE / CLEAT AT FR 35.4 BETWEEN S40R AND FR 41R. REPLACED SHEAR TIE / CLEAT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR WEB AT FR 16 AND S23L. REPLACED WEB PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 AND STR 23L IN AFT GALLEY AREA. REPLACED LOWER SILL PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY SEAT TRACK AT FR 20 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA DUMMY RAIL BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #3 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY AREA SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP FITTING 7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 LEFT AND DOOR STOP FITTING #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ON FA DISPLAY PANEL ILLUMINATED. FOUND L3 EMERGENCY DOOR DAMPENER LOW PRSSR. SERVICED L3 DOOR DAMPENER.
AIRCRAFT WAS GROUNDED: SUSPECTED COMPRESSOR STALL ON ENGINE #2. SHORTLY AFTER TAKEOFF WE FELT AND HEARD 3 SUCCESSIVE BOOMS. FIRST OFFICER NOTICED A SLIGHT DECREASE IN N1. IT WAS A TOGA TAKEOFF, APU BLEED ON. ALL PARAMETERS WERE NORMAL AT CLIMB POWER, NO ECAMS RECEIVED. CALLED MOC INFLIGHT,NO ABNORMALITIES NOTED. DURING A REVIEW OF THE DFDR DATA IT WAS NOTED THAT THERE WAS A 3 SECOND UNCOMMANDED ROLL BACK OF N1 ON THE #2 ENGINE. IT WAS ALSO NOTED THAT THE EGT HAD EXCEEDED 970 AND MAINTENANCE ACCOMPLISHED A BORESCOPE OF THE HPT1 AND LPT1. MAINTENANCE FOUND DAMAGE TO THE LPT BLADES THAT WAS WITHIN LIMITS BUT LIMITED TO 10 FH OR 5 FC BEFORE REPLACING THE ENGINE. MAINTENANCE REPLACED THE #2 ENGINE PER TASK CARD 26L40071001.
AIRCRAFT WAS NOT GROUNDED: ENGINE 1 FUEL FILTER CLOGGED ECAM AT 1500 AGL ON DEPARTURE. FLIGHT CREW REPORTED TAKEOFF WAS MAX-IMP, APU-ON. ECAM SELF CLEARED WITHOUT PILOT ACTION. MAINTENANCE REPLACED FUEL FILTER AND ACCOMPLISHED A SATISFACTORY LEAK CHECK.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL; #2 BETWEEN RIBS 10 AND 11. REPAIRED LEFT WING UPPER SKIN PANEL PER EA 349927.
AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLIGHT ATTENDANT FIRST CLASS FLASHLIGHT.
AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ON FORWARD FLIGHT ATTENDANTS PANEL. MAINTENANCE FOUND DAMPER AND EMERGENCY OPERATION CYLINDER SERVICING VALVE LEAKING AND REPLACED IT PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: DURING PUSHBACK - VERY ROUGH PUSH, VERY LOUD SOUND FROM THE NOSE DURING TAXI - ONLY DURING LEFT TAXI TURNS AND DURING BRAKING. MAINTENANCE CONFIRMED THAT WHEN TURNING THE NOSE LANDING GEAR TO THE LEFT AND TO THE RIGHT WITH THE WHEELS INSTALLED A GRINDING NOISE OCCURS. MAINTENANCE DISCONNECTED THE WHEELS AND THEY WERE ABLE TO TURN THE NOSE LANDING GEAR SLLEVE. MAINTENANCE DETERMINED THE INTERNAL PORTION OF THE GEAR WAS CAUSING THE ISSUE AND REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY PER TASK CARD 26L71032003.
AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ILLUMINATED ON FLIGHT ATTENDANT CONTROL PANEL. SERVICED LEFT AFT DOOR ASSSIT BOTTLE AND ERSET THE CIDS WHICH CLEARED THE FAULT LIGHT.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT LIGHT INOPERATIVE AT ROW 21ABC. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT LIGHT INOPERATIVE AT ROW 21ABC. **SUPPLEMENTAL REPORT FOR AALA202307177936: MAINTENANCE REPAIRED WIRING HARNESS FOR SEAT 21ABC EMERGENCY PATH LIGHT PER SWPM 20-10-13 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. ** (CLOSED)
DURING PERIODIC SERVICE, PERFORMED CIDS BITE AND FOUND FAULT "EPSU BATTERY EXIT L"
AIRCRAFT WAS NOT GROUNDED: DURING CIDS BITE CHECK MAINTENANCE FOUND EMERGENCY POWER SUPPLY UNIT BATTERY EXIT LEFT FAULT. REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL.
AIRCRAFT WAS GROUNDED: SHORTLY AFTER TAKEOFF ENGINE #1 FUEL FILTER CLOG ECAM MESSAGE DISPLAYED. ECAM MESSAGE CLEARED AFTER 15 MINUTES. MAINTENANCE REPLACED #1 ENGINE FUEL FILTER PER AMM 73-11-10. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: 3L FLIGHT ATTENDANT SEAT FLASHLIGHT MISSING. MAINTENANCE INSTALLED FLASHLIGHT PER AMM 25-35-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION FOR DOOR ASSIST BOTTLE L3 LOW. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: CAUTION RED LIGHTS ON FLIGHT ATTENDANTS PANEL ARE ILLUMINATED. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-10-00 AND CAUTION LIGHTS EXTINGUISHED.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS OVERWING EXIT LIGHTS AT DOOR 2R ARE ILLUMINATED INFLIGHT. MAINTEANCE REPLACED EMERGENCY POWER SUPPLY UNIT 15WL BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON FORWARD FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED L3 DOOR ASSIT BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED MID LAVATORY DOOR ALL CHECKS NORMAL PER AMM 52-00-00.
AIRCRAFT WAS GROUNDED: AISLE OVERHEAD EXIT SIGN AFT SIDE WILL NOT ILLUMINATE AT SEAT ROWS 23 AND 24. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202211014520) AND BATTERY (AALA202211017792) PER AMM 33-51-38. ALSO REPLACED EMERGENCY POWER SUPPLY UNIT 13WL BATTERY (AALA202211017659) PER AMM 33-51-38. A SATISFACTORY OPEATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: AISLE OVERHEAD EXIT SIGN AFT SIDE WILL NOT ILLUMINATE AT SEAT ROWS 23 AND 24. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202211014520) AND BATTERY (AALA202211017792) PER AMM 33-51-38. ALSO REPLACED EMERGENCY POWER SUPPLY UNIT 13WL BATTERY (AALA202211017659) PER AMM 33-51-38. A SATISFACTORY OPEATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: AISLE OVERHEAD EXIT SIGN AFT SIDE WILL NOT ILLUMINATE AT SEAT ROWS 23 AND 24. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202211014520) AND BATTERY (AALA202211017792) PER AMM 33-51-38. ALSO REPLACED EMERGENCY POWER SUPPLY UNIT 13WL BATTERY (AALA202211017659) PER AMM 33-51-38. A SATISFACTORY OPEATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ILLUMINTATED FOR R4 DOOR. MAINTENANCE SERVICED R4 DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-614-001-A.
AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ILLUMINTATED FOR L3 DOOR. MAINTENANCE SERVICED L3 DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-614-001-A.
AIRCRAFT WAS GROUNDED: WITH EMERGENCY LIGHTS SWITCH IN ARMED POSITION THE EMERGENCY EXIT LIGHTS IN THE CABIN KEEP FLICKERING ON AND OFF. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT L3 DOOR PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT FORWARD FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED DOOR DAMPER AT L3 EMERGENCY EXIT DOOR PER AMM 52-22-00-614-002-A. CAUTION LIGHT ON FORWARD FLIGHT ATTENDANT PANEL WENT OUT.
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION PANEL LIGHT ILLUMINATED. MAINTENANCE FOUND DOOR DAMPER PRESSURE LOW. SERVICED DOOR DAMPER PER AMM 52-22-00. ACCOMPLISHED BITE OF CIDS PER AMM 23-73-00 NO LIGHTS ILLUMINATED ON CIDS PANEL. CHECKED GOOD NO FAULTS NOTED AT THIS TIME.
AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION DOOR BOTTLE LOW. CIDS BITE DOOR BOTTLE EXIT LEFT. MAINTENANCE ACCOMPLISHED CHARGING OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00-614-002.
AIRCRAFT WAS GROUNDED: FUEL LEFT WING TANK OVERFLOW MESSAGE ECAM IN FLIGHT TURNED CENTER TANK LEFT TRANSFER OFF NO FUEL IN CENTER TANK. EMERGENCY CANCELED NUISANCE ECAM. **SUPPLEMENTAL REPORT FOR AALA202205111913: REPLACED THE LEFT-WING HIGH-LEVEL SENSOR AND THE LEFT-WING OVERFLOW SENSOR (AALA202205120992) PER AMM 28-46-15. A SATISFACTORY BITE CHECK WAS ACCOMPLISHED PER AMM 28-4600-740-001 ** (CLOSED)
AIRCRAFT WAS GROUNDED: FUEL LEFT WING TANK OVERFLOW MESSAGE ECAM IN FLIGHT TURNED CENTER TANK LEFT TRANSFER OFF NO FUEL IN CENTER TANK. EMERGENCY CANCELED NUISANCE ECAM. **ORIGINAL REPORT WAS AALA202205111913** REPLACED THE LEFT-WING HIGH-LEVEL SENSOR AND THE LEFT-WING OVERFLOW SENSOR (AALA202205120992) PER AMM 28-46-15. A SATISFACTORY BITE CHECK WAS ACCOMPLISHED PER AMM 28-4600-740-001.
AIRCRAFT WAS GROUNDED: FUEL LEFT WING TANK OVERFLOW MESSAGE ECAM IN FLIGHT TURNED CENTER TANK LEFT TRANSFER OFF NO FUEL IN CENTER TANK. EMERGENCY CANCELED NUISANCE ECAM. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: IN FLIGHT, LOST FLIGHT DIRECTOR 1 AND 2, AUTOPILOT 1 AND 2. AUTOTHROTTLE INOPERATIVE AND NO FLIGHT MODE ANNUNCIATOR. FLIGHT DECLARED AN EMERGENCY LANDING SAFELY AT PHX. RESET #1 FMGC. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS OF FLIGHT DIRECTOR, AUTOPILOT, AND AUTOTHROTTLE SYSTEMS PER AMM 22-97-00-710-001-A.
AIRCRAFT WAS GROUNDED: LANDING GEAR SHOCK FAULT ECAM DISPLAYED AFTER TAKE OFF. LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO ABQ LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS GROUNDED: ÿ½AUTO FLT A/THR OFFÿ½ ECAM DISPLAYED AFTER TAKEOFF. AUTO THROTTLE WOULD NOT RE-ENGAGE. BOTH FLIGHT DIRECTORS FAILED AND WOULD NOT RESET. FLIGHT RETURNED TO ABQ LANDING SAFELY. ACCOMPLISHED SATISFACTORY AUTOMATIC FLIGHT SYSTEM TEST AS PER AMM 22-96-00-710-001-A. NO FAULT HISTORY.
AIRCRAFT WAS GROUNDED: LANDING GEAR SHOCK FAULT ECAM DISPLAYED AFTER TAKE OFF. LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO ABQ LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203165880: REPLACED NLG SHOCK ABSORBER PER JOB CARD 26L71032001.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON PANEL. L3 DOOR ASSIST BOTTLE PRESSURE SHOWING LOW PRESSURE. SERVICED BOTTLE PER JOB CARD 26L80052003.
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT INOPERATIVE AT DOOR 4L. REPLACED FLASHLIGHT WITH SERVICEABLE UNIT, OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: CABIN DOOR 1L SLIDE NOT INDICATING ARMED ON ELECTRONIC CENTRAL AIRCRAFT MONITOR WHEN SLIDE ARMING LEVER PHYSICALLY MOVED TO THE ARMED POSITION. CORRECTLY FOLDED GIRT ASSEMBLY PER AMM 25-62-44.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING SLAT 2 TRACK 6 SPHERICAL BEARING ATTACHMENT FITTING BUSHING CRACKED. REPLACED SLAT 2 PER JOB CARD 26C62057009.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.
AIRCRAFT WAS GROUNDED: DURING L2 SLIDE CHANGE EMERGENCY POWER SUPPLY UNIT TEST FAILED (EXIT AND INT LOAD FORWARD LEFT). TROUBLE SHOT PER TSM 33-51-00-810-808A. (EXIT FAULT) CLEANED BREAK-AWAY CONNECTOR INTEGRAL TO R1 SLIDE. FAULT CLEARED.
AIRCRAFT WAS NOT GROUNDED: SMOKE DETECTOR IN LAVATORY E WENT OFF WITH THE APPROPRIATE CHIMES, LAVATORY WAS SEARCHED WITH NO SOURCE DETECTED. FLIGHT ATTENDANTS NOTED SMOKE AROUND THE AFT GALLEY 4R READING LIGHT AND TURNED IT OFF . MAINTENANCE RELAMPED THE READING LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: R1 DOOR REQUIRES SERVICING OF THE DOOR ASSIST ACCUMULATOR. SERVICED R1 DOOR PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: ENGINE 1 NUMBER 1 EXHAUST GAS TEMPERATURE, NUMBER 2 AND FUEL FLOW FLUCTUATIONS IN DESCENT TO CLT. FOUND PS3 LINE WITH PIN HOLE AND WITH WATER AND DEBRIS. REPLACED THE FLEX LINE OF THE PS3 AND PURGED THE LINE PER AMM 75-00-00. PERFORMED ENGINE RUN WITH NO DEFECTS NOTED AT THIS TIME.
AIRCRAFT WAS NOT GROUNDED. CABIN INTERCOMMUNICATION DATA SYSTEM CAUTION LIGHT ILLUMINATED ON FORWARD FLIGHT ATTENDANT PANEL. SERVICED L-3 DOOR ASSIST BOTTLE, PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. FOUND EMERGENCY LIGHTS AT DOOR R3 NOT WORKING. REMOVED AND REPLACED 3 RT DOOR EMERGENCY POWER SUPPLY UNIT (AALA202010279004) AND BATTERY (AALA202010279009), IAW AMM33-51-38- 000-001-A &33-51-38-400-001-A.
AIRCRAFT WAS NOT GROUNDED. FOUND EMERGENCY LIGHTS AT DOOR R3 NOT WORKING. REMOVED AND REPLACED 3 RT DOOR EMERGENCY POWER SUPPLY UNIT (AALA202010279004) AND BATTERY (AALA202010279009), IAW AMM33-51-38-000-001-A &33-51-38-400-001-A.
AIRCRAFT NOT GROUNDED: SMOKE DETECTOR {MID-LAV} AURAL ALERT SOUNDED FOR APPROX. 10 SECS, THEN STOPPED . NO EVIDENCE OF FIRE OR SMOKE.REPLACED MID LAV FILTER PER AMM 26-22-00,
AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY CYLINDER PRESSURE WAS LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER #2 ENG START (W/IN 60 SECONDS) "F/CTL-FALP SYSTEM 1 FAULT" ILLUMINATED. WHILE ON TELCOM WITH US MOC, ECAM MSG EXTINGUISHED ON ITS OWN. AFTER FLAP RETRACTION (+ 1 MIN) "F/CTL-FLAP SYS 2" (REPEAT 2) ILLUMINATED ON ECAM WITH FLAP POSITION INDICATOR TURNED AMBER. ECAM THEN DISPLAYED "FLAP FAULT" W/OUT ANY NUMBER DISPLAYED. LATER SYSTEM 1 FAULT RETURNED. ACCOMPLISHED ECAM PROCEDURE, (GPWS FLAP MODE PRESSED) BUT WITHIN 2 MINUTES ALL ECAM WARNINGS EXTINGUISHED. DE-SELECTED GPWS FLAP MODE (BACK TO NORMAL POSITION). PLEASE NOTE EXTENSIVE HISTORY OF FLAP FAULTS. AT T.O. +28 MINS, ECAM MSG "F/CTLFLAP SYS 1 FAULT" RETURNED. AT T.O. +33 MINS AND THEN RETURNED. FLAP OPERATED NOMINALLY ON ARRIVAL - NO ECAM MESSAGE. FLAPS 3 LANDING. MAINTENANCE REMOVED AND REPLACED FLAP 2 PCU VALVE BLOCK IAW 27-54-53 OPS AND LEAK CHECKED GOOD.
AIRCRAFT WAS GROUNDED: DURING THE OPERATIONS CHECK OF THE EPSU BY BITE CHECK, THE CHECK FAILED. MAINTENANCE REPLACED L1 DOOR SLIDE PER JOBCARD #26L00025010.
AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING DESCENT ECAM ANNUNCIATED FUEL CTR R XFR FAULT. NO FUEL IN CENTER TANK AT THE TIME OF FAULT. MAINTENANCE TROUBLESHOT IAW TSM 28-26-00-810-805A. REMOVED AND REPLACED FUEL CONTROL VALVE ACTUATOR (12QL) IAW AMM 28-26-51. ACCOMPLISHED FUEL TRANSFER IAW AMM 28-25-00. OPS GOOD, NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON DECENT DUE TO ECAM MSG F/CTL FLAPS FAULT. MAINTENANCE ADJUSTED INTERCONNECTING STRUT PROX SWITCH IAW AMM 27-51-15. FLAP SYSTEM OPS CHEKS NORM.
AIRCRAFT WAS NOT GROUNDED: L3 DOOR OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK, COMPLIED WITH EA 293890, PER AMM 33-51-00-710-007.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE SWAPPED POLARITY OF CONNECTORS ON EXIT SIGNS PER AMM 33-51-16 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE: R4 DOOR CYLINDER PRESSURE GAUGE WAS LOW. SERVICED R4 DOOR CYLINDER PER A321 MM 52-10-00-614-001-A.
AIRCRAFT IN BASE MAINTENANCE: L2 DOOR ASSIST BOTTLE CLAMP WOULD NOT ENGAGE. REPLACED AFT CLAMP AT L2 DOOR BOTTLE PER A321 MM 20-21-11, PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE: FLOOR SUPPORT UNDER FLOOR PANEL 231VF IS BROKEN. REPLACED FLOOR SUPPORT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 251AG DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CONNECTING PLATE AT FR 24 BETWEEN FLOOR PANEL 232DF AND 232LF.REPLACED CONNECTING PLATE PER SRM 51-42-11.
L2 AND L3 DOOR DAMPENER BOTTLES HAD LOW PRESSURE. SERVICED THE L3 DOOR DAMPNER BOTTLE IAW AMM 52-22-00-614-002-A, AND JC 26L00005005.
L2 AND L3 DOOR DAMPENER BOTTLES HAD LOW PRESSURE. SERVICED THE L2 DOOR BOTTLES IAW AMM 52-22-00-614-002-A, AND JC 26L00005005.
EMERGENCY LIGHT POWER SUPPLY WAS INOPERATIVE ABOVE ROW 22, NO RESPONSE FROM UNIT TEST. MAINTENANCE REPLACED THE POWER SUPPLYT AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.
L3 DOOR SLIDE BOTTLE DOOR HINGE BROKEN IN FLIGHT, THE DOOR WAS HANGING. REPLACED THE LATCH ON BLUE HYDRAULIC DOOR BELOW THE L3 SLIDE IAW AMM 52-41-24.
L3 DOOR SLIDE BOTTLE DOOR HINGE WAS BROKEN. . REPLACED THE HINGE IAW AMM 52-41-24.
L4 DOOR SLIDE COVER LOOSE UNSECURE. MAINTENANCE SECURED THE SLIDE COVER IAW AMM 25-00-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS GROUNDED: FLOOR PATH LIGHTING ON SEAT 10C LENS FELL OFF. MAINTENANCE REPLACED LENS AT SEAT 10C AS REQUIRED AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
AIRCRAFT WAS GROUNDED: EMERGENCY LIGHTS BATTERY POWER SUPPLY AND ASSOCIATED LIGHTS WERE OUT AT DOOR L AND R3. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT K3 DOOR PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
SEAT MOUNTED EMERGENCY EXIT LIGHT LENS WAS MISSING FROM SEATS 10C AND 22D. REPLACED THE LENSES. OPS CHECKED GOOD, OK FOR SERVICE.
SEAT MOUNTED EMERGENCY EXIT LIGHT LENS WAS MISSING FROM SEAT 22D. REPLACED THE LENS. OPS CHECKED GOOD, OK FOR SERVICE.
DURING APPROACH, RECEIVED A LEFT MAIN GEAR UPLOCK OR DISAGREE, CYCLED GEAR THEN NORMAL LANDING GEAR INDICATION. CHECKED PFR AND PERFORMED TSM 32-31-00. FOUND THE SENSOR 15GA TARGET LOOSE. SECURED THE TARGET IAW AMM 32-31-73. LANDING GEAR CIU BITE TESTED OK, NORMAL
AN OPS TEST OF THE EMERGENCY LIGHTS, THROUGH CIDS, FAULT ON EMERGENCY POWER SUPPLY, EXIT RIGHT 12WL IAW JC 26L00005005. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE POWER SUPPLY IAW AMM 33-51-38, AND PERFORMED A SATISFACTORY OPS CHECK. NO FAULTS NOTED.
FLOOR EMERGENCY LIGHT COVER AT ROW 34 WAS MISSING. INSTALLED THE COVER IAW AMM 33-51-11.
RED LENS MISSING FROM AISLE LIGHT AT 10C. MAINTENANCE REPLACED THE LENS AND PERFORMED SATISFACTORY OPERTIONAL CHECK.
EMERGENCY FLASHLIGHT AT THE L2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-0-00
FUEL CENTER RIGHT TRANSFER FAULT, CENTER TANK RIGHT TRANSFER FUEL PUMP TURNED OFF. MAINTENANCE ACCOMPLISHED TSM 28-26-00-810-805A AND PERFORMED SATISFACTORY OPERATIONAL CHECK. NO FAULTS FOUND.
SEAT 32C EMERGENCY LIGHT LENS MISSING. MAINTENANCE REPLACED THE LENS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
RETURNED DEPARTURE, UNABLE TO RETRACT LANDING GEAR. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. RECONFIGURED AIRCRAFT INTO FLIGHT PRIOR TO GEAR SWUNG IAW AMM 32-00-00-860-001-A. RETURNED AIRCRAFT BACK TO GROUND CONFIGURATION IAW AMM 32-00-00-860-002A. AIRCRAFT WAS GROUNDED.
UNABLE TO RETRACT LANDING GEAR. NO EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. REPLACED PRIORITY VALVE 1064GM IAW AMM 29-11-33, LEAK CHECKED GOOD. REPLACED RELAY 62GA IAW 32-31-08.
UNABLE TO RETRACT LANDING GEAR. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. REPLACED PRIORITY VALVE 1064GM IAW AMM 29-11-33, LEAK CHECKED GOOD. RELACED RELAY 62GA IAW 32-31-08.
CORROSION FOUND ON THE RIGHT WING SKIN UPPER SURFACE AT WS 7792, RIB 14. REPAIRED THE WING SKIN IAW EA 281442.
CORROSION FOUND ON THE LEFT WING UPPER SURFACE SKIN AT WS 8744, BETWEEN RIBS 14 AND RIB 15. REPAIRED THE LEFT WING SKIN IAW EA 281165.
CORROSION FOUND ON THE LEFT WING UPPER SURFACE SKIN BETWEEN RIBS 14 AND 15. REPAIRED THE WING SKIN IAW EA 281165.
CORROSION FOUND ON THE RIGHT WING UPPER SKIN AT RIB 14, INBOARD OF THE NR 3 SPOILER INBOARD HINGE FITTING. REPAIRED THE WING SKIN IAW EA 281442.
CRACKED SKIN AT THE TOP OF THE L4 DOOR FORWARD SIDE. REPLACED SKIN IAW SRM 51-72-11 AND SRM 51-21-11.
LEFT WING, NR 6 SLAT TRACK CLOSEOUT PLATE, HAS A WORN AREA INTO THE LOWER SKIN OF THE NR 2 SLAT. REPAIRED SLAT IAW EA 281928 D2.
CORROSION FOUND ON THE RIGHT ELEVATOR OUTBOARD RIB LEADING EDGE. REPLACED RIB IAW SRM 514411, DRAWING D55281545, EA 281099, AND CMM 552115.
CORROSION FOUND ON LEFT OTBD SEAT TRACK LOCATED AT FR 39, STRINGER 23. REPLACED SEAT TRACK IAW SRM 51-42-11.
CORROSION FOUND ON THE SEAT TRACK AT TWO PLACES BETWEEN FRAMES 41 - 47, Y1292. REPLACED THE SEAT TRACK IAW SRM 51-42-11.
CORROSION FOUND ON THE FLOOR SUPPORT, FRAMES 65, 66, AND 67, -Y317.9. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND B/P D53472814.
CORROSION WAS FOUND ON THE FLOORBEAM, -Y1292, FRAME 66. REPLACED THE FLOORBEAM IAW SRM 51-42-11.
CORROSION ON THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 68, Y-765. REPAIRED THE FLOOR SUPPORT AIW SRM 51-42-11 AND DRAWING D53472780.
CORROSION FOUND ON THE FLOOR SUPPORT, FRAMES 12 TO 24, Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.
CORROSION FOUND ONE INCH FORWARD FRAME 68 DOOR SEAL, AT THE R4 DOOR SILL AREA. REMOVED DAMAGED AND INSTALLED A REPAIRED SILL PLATE FRAME IAW SRM 53-41-14-300-01, FIG 20101, REPAIR PRINCIPLE 7.
R4 EXIT LIGHT COVER FELL OFF. REPLACED THE EMERGENCY LIGHT COVER.
AIRCRAT NOT GROUNDED. CLICKING SOUND AT DOOR L3 NEAR THE CABIN PRESSURE WARNING LIGHT. REPLACED EMERGENCY POWER SUPPLY UNIT IIWL IAW AMM.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT SEAT 9 RIGHT HAS A MISSING LENS COVER. REMOVED AND REPLACED LIGHT FITTING. OPERATIONAL CHECK PER AMM 33-51-18-400-001-A GOOD.
SEAT 9-D EMERGENCY LIGHT HOUSING TORN. REPLACED EMERGENCY LIGHT HOUSING.
L3 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY IAW AMM.
SEATS 32C,27C,20C,16C,12C EMERGENCY EXIT LIGHT ARE OUT. REPLACED LIGHT BULBS AND BITE TEST EMERGENCY POWER SUPPLY PER AMM.
NR 1 L1 DOOR FWD EXIT SIN LIGHT PANEL LOOSE. RE-SECURED PANEL PER AMM.
R4 DOOR ASSIST BOTTLE PRESSURE LOW. ACCOMPLISHED SERVICING OF R4 DOOR ASSIST BOTTLE IAW AMM.
MISSING LENS ON EMERGENCY EXIT LIGHT AT 1C. REPLACED THE LENS AT 1C AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
THE L3 DOOR EMERGENCY FLASHLIGHT SEAL LOOSE. REPLACED MISSING HARDWARE ON THE FLASHLIGHT.
L1 GIRT BAR LATCH, NOT LOCKING IN PLACE. LUBRICATED GIRT BAR LATCH, OPS CHECKED GOOD IAW AMM.
MISSING EMERGENCY LIGHT LENS OVER THE L4 DOOR. INSTALLED A NEW LENS.
SMOKE, SDCU UPPER ECAM. TROUBLESHOT IAW TSM 26-17-00-810-802-A. FOUND DETECTOR INOPERATIVE. REPLACED SDCU CHANNEL 2 SMOKE DETECTOR 3WH IAW AMM 26-16-15-000-001-A, AND 26-16-15-400-001.
L4 DOOR SLIDE BUSTLE LOOSE. SECURED BUSTLE.
L1 DOOR EMERGENCY EXIT LIGHT LENS NOT SECURE. REPLACED THE LENS.
INBOUND FLIGHT CREW REPORTED THE L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE ASSIST BOTTLE IAW AMM 52-10-00.
MIGRATED, AND LOOSE LEFT MAIN LANDING GEAR DOOR FORWARD HINGE BEARING. REPLACED FORWARD HINGE IAW SRM 51-42-11-001.
L4 DOOR EMERGENCY LIGHT COVER MISSING. REPLACED THE LIGHT COVER.
SEAT ROW 5ABC EMERGENCY LIGHT LENS COVER MISSING. REMOVED AND REPLACED SEAT ROW 5ABC EMERGENCY LIGHT LENS.
AIRCRAFT WAS NOT GROUNDED. MISSING MID LAVATORY EMERGENCY LIGHT LENS. INSTALLED NEW LENS AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS MISSING SEAT 30C. INSTALLED LENS AT SEAT 30C PER AMM 33-51-18.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS MISSING SEAT 25C. INSTALLED LENS AT SEAT 25C PER AMM 33-51-18.
RIGHT WING MAIN LANDING GEAR SUPPORT FITTING FORWARD LUG CRACKED AT RIB 5. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RT WING MLG SUPPORT FITTING IAW TASK CARD 26L70057002 AND EA 261982. UPDATED SECTIONS 4, 5 AND 7. MAINTENANCE REPLACED THE RT WING MLG SUPPORT FITTING IAW TASK CARD 26L70057002 AND EA 261982.
AIRCRAFT IN BASE MANINTENANCE: RIGHT SIDE BOX BEAM UPPER FLANGE AFT 2 HOLES HAVE CRACK INDICATIONS AT FRAME 43 AND -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.
AIRCRAFT IN BASE MANINTENANCE: LT SIDE BOX BEAM UPPER FLANGE AFT 2 HOLES HAVE CRACK INDICATIONS AT FRAME 43 AND +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.
AIRCRAFT WAS NOT GNDED. OPERATIONAL TEST OF ESCAPE FACILITY FAILED. PERFORM BITE TEST IAW TASK 33-51-00-810-806, FOUND EMER POWER SUPPLY UNITS 11WL & 12WL FAULTING. REPLACED BATTERIES IAW AMM 33-51-38-000-01. SATISFACTORY OPERATIONAL CHECK ACCOMPLISHED IAW 33-51-38. SEE AALA 201603149005 FOR 11WL PART INFORMATION.
AIRCRAFT WAS NOT GNDED. OPERATIONAL TEST OF ESCAPE FACILITY FAILED. PERFORM BITE TEST IAW TASK 33-51-00-810-806, FOUND EMER POWER SUPPLY UNITS 11WL & 12WL FAULTING. REPLACED BATTERIES IAW AMM 33-51-38-000-01. SATISFACTORY OPERATIONAL CHECK ACCOMPLISHED IAW 33-51-38. SEE AALA 201603169005 FOR 12WL PART INFORMATION.
C11 CHECK, EMER LIGHT SYS BITE TEST GIVES FAULT EXTERNAL LOAD MID LT. TROUBLESHOOTING SHOWS EXTERNAL FAULT ON ESPU AT L2 DOOR. REPLACED L2 DOOR SLIDE ASSEMBLY IAW 26C13053004 & 26C13053010. REPLACED THE SLIDE LAMP HARNESS, LED. ACCOMPLISHED A SATISFACTORY LIGHT SYS TEST.
C11 CHECK, RT ELEVATOR UPPER SURFACE HAS DELAMINATION 69" OTBD OF RIB 1. REPAIRED IAW SRM-55-21-11-201 PARAGRAPH.5E 205.
EMERGENCY POWER SUPPLY UNIT 12WL WOULD NOT TEST. R & R EPSU 12WL. CHECKED OK IAW AMM 31-51-38.
FLIGHT 1930 EN-ROUTE, FWD OVEN HAS PLASTIC RESIDUE ON BURNER ELEMENT, SMOKES BADLY NEEDS CHANGE OUT. CATERING REPLACED OVEN CONTAINER. OPERATIONS CHECKED GOOD.
APU AUTO SHUTDOWN AT GATE RAMP REPORTS SMOKE & SPARKS & NO APU FIRE INDICATION. REPLACED THE APU & ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK IAW 26L31049003.
2L DOOR ARMING LEVER BROKEN OFF. REPLACED 2L DOOR ARMING LEVER IAW AMM 52-22-22-000-001.
AFT RT PAX & CREW DOOR ASSIST BOTTLE PRESS READING 1400 PSI AT +20C. SERVICED RT AFT PAX & CREW DOOR ASSIST BOTTLE TO SERVICEABLE PRESS IAW AMM 52-10-00-614-001. OK FOR SERVICE.
EMERGENCY EXIT ARM & DISARM LEVER BROKEN AT LOCATION 2L. R & R EMER EXIT ARM & DISARM LEVER AT LOCATION 2L DOOR IAW AMM 52-22-22.
SLIDE ARMED INDICATOR LIGHT PANEL DAMAGED ON L2 EMER EXIT IAW AMM 52-73-21. REPLACED L2 DOOR SLIDE ARMED INDICATION LIGHT ASSEMBLY IAW AMM 52-73-21. OPERATIONS CHECKED NORMAL.
2L ARM & DISARM HANDLE BROKEN OFF. R & R EMER EXIT ARM & DISARM LEVER AT LOCATION 2L DOOR IAW AMM 52-22-22.
EMERGENCY LIGHT LENS COVER MISSING AT SEAT 5 LT. REPLACED LENS.
ROW 1 LT MISSING EMER LIGHT LENS. INSTALLED NEW LENS ON EMER LIGHT AT ROW 1 LT.
L3 DOOR ACTUATOR NEEDS SERVICE. SERVICED L3 DOOR ACTUATOR.
THE DOOR ARMING PADDLES AT 2L, 2R & 3R DOORS ARE FLOPPY & LOOSE. SECURED YELLOW DOOR ARM PADDLES.
THE L1 DOOR EMER EXIT MARKER LENS MISSING. INSTALLED MISSING L1 DOOR EMER EXIT MARKER LIGHT LENS AS REQUIRED.
THE AFT RT FLASHLIGHT INOPERATIVE. R & R BATTERY AT AFT JUMP SEAT FLASHLIGHT, ACFT RT. OPERATIONS CHECKED GOOD.
LENS COVERS MISSING AT ROW 8 FOR EMER EXIT FLOOR LIGHTING. REPLACED LENS COVER AT ROW 8 ACFT RT EMER EXIT LIGHT IAW AMM 33-51-00.
THE L2 DOOR EMER EXIT LENS MOUNTING TABS BROKEN. REPLACED & SECURED L2 DOOR EMER EXIT LENS IAW 33-51-00.
THE AFT RT EXIT DOOR EMER ASSIST BOTTLE LOW IN NITROGEN PRESS. SERVICED AFT RT EXIT DOOR EMER ASSIST BOTTLE WITH NITROGEN IAW AMM 52-10-00-614-001.
EN ROUTE FROM MCO TO PHL, CREW REPORTED A CABIN ODOR & DIRTY SOCK SMELL. CREW MEMBERS COMPLAINED OF HEADACHE, NAUSEA & SCRATCHY THROAT. SMELL WAS OVERWHELMING, TAKEOFF TO LANDING, CRUISE SEEMED OK. ACCOMPLISHED JOB CARD 26L00021001. FOUND APU OIL OVER SERVICED. ACCOMPLISHED JOB CARD 26L00021002, APU BURNOUT. RAN APU & BOTH PACKS. NO ODOR NOTED AT THIS DATE & TIME.
THE 2L DOOR EXIT SIGN DOES NOT ILLUMINATE. ACCOMPLISHED RESET OF CIDS DIRECTORS IAW TSM 24-00-00-810-818-A. NO FAULT NOTED AT THIS TIME, ACFT OK FOR SERVICE.
EMERGENCY LIGHT LENS IS MISSING AT SEAT 5C. REPLACED SEAT 5C EMERGENCY LIGHT LENS.
MAINTENANCE REPORTED THE EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 9R. INSTALLED EMERGENCY AISLE LIGHT LENS AT ROW 9R AS REQUIRED.
THE RT SIDE AIR PRESS FOR SLIDES DEPLETED. TROUBLE SHOT IAW TSM 25-62-00-810-810-A, SWITCH ON BOTTLE AT FAULT. R & R INFLATION RESERVOIR FOR ESCAPE SLIDE R3 DOOR IAW AMM 25-62-49-400-001-A.
FORWARD MEGAPHONE INOPERATIVE. REPLACED FORWARD MEGAPHONE.
MEGAPHONE LOCATED IN THE FWD OVERHEAD BIN ABOVE SEAT 1AC ACTIVATION HANDLE HAS DISLOCATED FROM THE BODY MAKING IT UNUSEABLE AND UNABLE TO TRANSMIT. SECURED MEGAPHONE HANDLE AND OPS CHECKED GOOD.
R4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R4 DOOR EMERGENCY CYLINDER TO PROPER PRESSURE IAW AMM 52-10-00-614-001A.
AFT FLIGHT ATTENDANT SEAT FIRE EXTINGUISHER GAUGE IN THE RED. REMOVED AND REPLACED AFT FLIGHT ATTENDANT SEAT FIRE EXTINGUISHER.
EMERGENCY EXIT LIGHT ROW 9 A/C RIGHT INOPERATIVE. RE-SECURED EMERGENCY LIGHT ASSEMBLY AND LENS AT ROW 9ABC. OPERATIONAL CHECK NORMAL.
EMERGENCY LIGHT LENS AT ROW 9 AIRCRAFT RIGHT NEEDS RE-ATTACHING. MAINTENANCE RE-ATTACHED LENS FOR EMERGENCY LIGHT AT ROW 9 RIGHT.
LENS MISSING ON EMERGENCY LIGHT ROW 9 RIGHT. INSTALLED LENS ON EMERGENCY LIGHT ROW 9 RIGHT.
2S CHECK AFT CARGO FLOOR PANEL BETWEEN FR 50 AND FR 53, S38L TO S38R AT Z-500 IS DELAMINATED (24 IN X 31 IN AREA). REMOVED AND REPLACED PANEL IAW A321 AMM 53-42-17-400-001-A.
2S CHECK - AFT CARGO FLOOR PANEL AT FR 42, Y-765 AND Z-500 IS DELAMINATED (6 IN X 4 IN AREA). REMOVED AND REPLACED FLOOR PANEL MCGILL IRM 9701 REV G.
S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER 41R BETWEEN FR34 TO FR35.8. SPLICED IN NEW SECTION OF STRINGER 41R BETWEEN FR34 TO FR35.8 IAW A321 SRM 51-42-11, 51-72-11 & AIRBUS DRAWING D53372500.
S2 CHECK - DELAMINATION ON FLOORBOARD 221DF BETWEEN FR16 TO FR 21, Z-500 & BETWEEN Y254 TO -Y254. REPLACED FLOORBOARD 221DF IAW MCGILL IRM 9701 REV G.
S2 CHECK - WATER INGRESSION INDICATION ON LEFT ELEVATOR APPROX 6 INCHES FROM TRAILING EDGE & 118 INCHES FROM OUTBOARD TIP. REPAIRED LEFT ELEVATOR IAW A321 SRM 55-21-11 PARA 5K FIG 211.
S2 CHECK - WATER INGRESSION INDICATION ON LEFT ELEVATOR APPROX 5.25 INCHES FROM TRAILING EDGE & 36 INCHES FROM OUTBOARD TIP. REPAIRED LEFT ELEVATOR IAW A321 SRM 55-21-11 PARA 5E FIG 205.
S2 CHECK - WATER INGRESSION INDICATION ON LEFT ELEVATOR APPROX 12 INCHES FROM TRAILING EDGE & 129.5 INCHES FROM OUTBOARD TIP. REPAIRED LEFT ELEVATOR IAW A321 SRM 55-21-11 PARA 5G FIG 207.
S2 CHECK - WATER INGRESSION INDICATION ON LEFT ELEVATOR APPROX 6 INCHES FROM TRAILING EDGE & 76 INCHES FROM OUTBOARD TIP. REPAIRED LEFT ELEVATOR IAW A321 SRM 55-21-11 PARA 5E FIG 205.
2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK 5 INCHES FORWARD OF FR55, Z-500, Y-1292. REPLACED SEAT TRACK 5 INCHES FORWARD OF FR55, Z-500, Y-1292 IAW A321 SRM 51-72-11.
S2 CHECK - LEVEL 2 GALVANIC CORROSION ON L4 DOORWAY SILL PLATE AT FR64, Z-500. REPAIRED L4 DOORWAY SILL PLATE AT FR64, Z-500 IAW A321 SRM 53-41-14 FIG 201.
S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, Y1589. REPLACED L4 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, Y1589 IAW AIRBUS DRAWING 18D53480505.
S2 CHECK - LEVEL 2 FRETTING CORROSION ON LEFT WING LOWER FUEL ACCESS PANEL 540MB BETWEEN S8L TO S11L & BETWEEN RIB 17 & RIB 18. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540MB IAW A321 SRM 57-27-11.
S2 CHECK - LEVEL 2 FRETTING CORROSION ON LEFT WING LOWER FUEL ACCESS PANEL 540HB BETWEEN S8L TO S11L & BETWEEN RIB 13 & RIB 14. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540HB IAW A321 SRM 57-27-11.
MEGAPHONE IN AFT CABIN INOPERATIVE. MAINTENANCE INSTALLED SERVICEABLE MEGAPHONE.
RED LENS COVER FOR EMERGENCY FLOOR LIGHT AT DOOR 2L MISSING. REPLACED MISSING LENS.
C11 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR35 TO FR35.5, BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL BETWEEN FR35 TO FR35.5, BETWEEN Y254 TO -Y254 IAW MCGILL IRM 9701 REV G.
C11 CHECK - DELAMINATION ON FLOOR PANEL 251FF AT FR60, BL 0. REPLACED FLOOR PANEL 251FF IAW MCGILL IRM 9701 REV G.
C11 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR20 TO FR24, BETWEEN Y-765 TO Y-1292. REPLACED FLOOR PANEL BETWEEN FR20 TO FR24, BETWEEN Y-765 TO Y-1292 IAW MCGILL IRM 9701 REV G.
C11 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR20 TO FR24, S23L, BETWEEN Y765 TO 7254. REPLACED FLOOR PANEL BETWEEN FR20 TO FR24, S23L, BETWEEN Y765 TO 7254 IAW MCGILL IRM 9701 REV G.
2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16, BETWEEN Y505 TO Y1380. REPLACED FLOOR PANEL 221PF IAW MCGILL IRM 9701 REV G.
2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68, BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW MCGILL IRM 9701 REV G.
C11 CHECK - LEVEL 2 CORROSION ON FLOOR BEAM BETWEEN FR16 TO FR20, Y-254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y-254 IAW A321SRM 51-42-11 AND AIRBUS DRAWING D53115054.
C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Y254 IAW A321 SRM 51-72-11.
2S CHECK - LEVEL 2 CORROSION ON DUMMY RAIL AT FR16, Y503. REPLACED DUMMY RAIL AT FR16, Y503 IAW A321 SRM 51-72-11AND TYPICAL REPAIR 320-2528-10-0011C.
C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK AT FR24 +2 INCHES, -Y1292. REPLACED SEAT TRACK AT FR24 +2 INCHES, -Y1292 IAW A321 SRM 53-21-15 FIG 1 & EA 201021.
C11 CHECK - LEVEL 2 SURFACE CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A321 SRM 51-72-11.
C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR20 TO FR24, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR24, -Y189 IAW A321 SRM 51-72-11.
C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A321 SRM 51-72-11.
C11 CHECK - LEVEL 2 CORROSION ON WEB ANGLE BETWEEN FR20 TO FR24, BETWEEN -Y1584 TO -Y1732. REPLACED WEB ANGLE BETWEEN FR20 TO FR24, BETWEEN -Y1584 TO -Y1732 IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53112783.
MX - LAX - EEL - SEAT ROW 16 LT EMERGENCY LIGHT INOP. MAINTENANCE FOUND PLUG REMOVED. RE-INSTALLED PLUG.
FLT 1515 - LAS - EEL - EMERGENCY LIGHT LENS COVER MISSING AT ROW 2 LEFT. REPLACED EMERGENCY LIGHT LENS COVER.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66, Y1732. REPLACED FLOORBEAM AT FR66, Y1732 IAW AIRBUS DRAWING D53480019.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOOR PANEL 261EF INSERTS. REPLACED FLOOR PANEL 261EF IAW MCGILL IRM 9701 REV G.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOOR PANEL 262GF INSERTS. REPLACED FLOOR PANEL 262GF IAW MCGILL IRM 9701 REV G.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOOR PANEL 261HG INSERTS. REPLACED FLOOR PANEL 261HG IAW MCGILL IRM 9701 REV G.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOOR PANEL 261CG INSERTS. REPLACED FLOOR PANEL 261CG IAW MCGILL IRM 9701 REV G.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOOR PANEL 262HG INSERTS. REPAIRED FLOOR PANEL 262HG DAMAGED SKIN IAW A321 SRM 53-02-00.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW AIRBUS DRAWING D53472816.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Y1292 IAW AIRBUS DRAWING 53472169 & 18D53472816.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67, Y1292. REPLACED FLOORBEAM AT FR67, Y1292 IAW AIRBUS DRAWING 53472169 & 18D53472816.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, Y765. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, Y765 IAW AIRBUS DRAWING 18D53472815.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW AIRBUS DRAWING 18D53472815.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66, Y254. REPLACED FLOORBEAM AT FR66, Y254 IAW A321 SRM 51-44-12.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW AIRBUS DRAWING D53472817.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1292 IAW AIRBUS DRAWING D53472780.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR68, -Y765. REPLACED FLOORBEAM AT FR68, -Y765 IAW AIRBUS DRAWING 18D53472816.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR69, Y1292. REPLACED FLOORBEAM AT FR69, Y1292 IAW AIRBUS DRAWING 53472780 & 18D53472816.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66, -Y1732. REPLACED FLOORBEAM AT FR66, -Y1732 IAW AIRBUS DRAWING D5347207500100.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON RIGHT AFT ENTRY DOOR SILL AT FR66 + 1 INCH, -Y254. REPAIRED RIGHT AFT ENTRY DOOR SILL AT FR66 + 1 INCH, -Y254 IAW EA 102370.
CLT - DROP-IN - MAJOR REPAIR - LOG # 4666808 - CORROSION ON AFT END OF SEAT TRACK AT FR64, -Y765. REPLACED SEAT TRACK AT FR64, -Y765 IAW AIRBUS DRAWING # 18D53472832.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON SHEAR WEB BETWEEN FR69 TO FR70 OUTBOARD & AFT OF -Y1292. REPLACED SHEAR WEB BETWEEN FR69 TO FR70 OUTBOARD & AFT OF -Y1292 IAW AIRBUS DRAWING 53474180.
CLT - DROP-IN - MAJOR REPAIR - CRACK ON SHEAR WEB BETWEEN FR68 TO FR69 OUTBOARD OF Y1292. REPLACED SHEAR WEB BETWEEN FR68 TO FR69 OUTBOARD OF Y1292 IAW AIRBUS DRAWING D53480019.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON SHEAR WEB STRUCTURE BETWEEN FR69 TO FR70 & OUTBOARD OF Y1292. REPLACED SHEAR WEB STRUCTURE BETWEEN FR69 TO FR70 & OUTBOARD OF Y1292 IAW TYPICAL REPAIR 25-28-01B & AIRBUS DRAWING 18D53474180.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON WEB BETWEEN FR69 TO FR70 OUTBOARD & AFT OF -Y1292. REPLACED WEB BETWEEN FR69 TO FR70 OUTBOARD & AFT OF -Y1292 IAW AIRBUS DRAWING D53474180.
CLT - DROP-IN - MAJOR REPAIR - CORROSION ON SHEAR WEB BETWEEN FR67 TO FR70 OUTBOARD OF Y1292. REPLACED SHEAR WEB BETWEEN FR67 TO FR70 OUTBOARD OF Y1292 IAW TYPICAL REPAIR 25-28-01B & AIRBUS DRAWING 18D53474180.
INSP SEA - EEL - EMERGENCY EXIT LIGHT LENS FOR SEAT 29 MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS.
FLT 1624 - CLT-ORD - EMERGENCY LIGHTS - ROW 29 FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT CONTACT (7260VC10 PLUG) AT WALL DISCONNECT. OPERATIONAL CHECK WAS GOOD.
FLT 1547 - SEA - EEL - EMERGENCY LIGHT LENS AT SEAT 5L IS MISSING. MAINTENANCE REPLACED EMERGENCY LIGHT LENS.
FLT 965 - SFO - EMERGENCY EGRESS SYSTEM - AFT RIGHT EXIT DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED AFT RIGHT DOOR ASSIST BOTTLE PRESSURE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-03.
FLT 1075 - PHL - EMERGENCY EQUIPMENT - FORWARD CABIN FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT'S FLASHLIGHT.
FLT 752 SEA-PHL - EMERGENCY EQUIPMENT - R-2 DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE TO PROPER PRESSURE.
FLT NR 1521 - CLT-DEN - EMERGENCY EQUIPMENT, SMOKE LAV + CRG DET FAULT DURING PREFLIGHT. MAINTENANCE REPLACED FORWARD LAV SMOKE DETECTOR. BITE CHECK SMOKE DETECTOR CONTROL UNIT. SYSTEM OPS NORMAL. MESSAGE CLEARED.
PHL - THE FORWARD RIGHT SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILS THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD RIGHT SERVICE DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.
MCO FLT 656 EN ROUTE DCA TO MCO, FLIGHT WAS INBOUND TO MCO, AT 3,000 FT, WHEN THE CABIN CREW REPORTED SMOKE IN THE CABIN. THE FLT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL AT THE GATE, A STRONG SULFUR ODOR WAS NOTED, ALONG WITH A POPPED RIGHT HAND, CABIN RECIRCULATION FAN CIRCUIT BREAKER. OPERATIONS ALSO NOTED THAT THERE WERE MULTIPLE BRUSH FIRES IN THE AREAS SURROUNDING THE NORTH AND EAST OF THE AIRPORT. MAINTENANCE PLACED THE RIGHT HAND, CABIN RECIRCULATION FAN ON MEL.
AT 41 INCHES FROM END, 64 INCHES FROM OPP END, 4 INCHES FROM EDGE, 15 INCHES FROM OPP EDGE CRACKED. FILLED AND INSTALLED PRECURED DOUBLER IAW SRM 53-02-00 FIG 203. DEFECT SIZE: 5 INCHES.
BEAM Y254 FWD CABIN, DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-72-11; CORROSION LEVEL 2; TASK JA-220-53500. DEFECT SIZE: .5 INCH X .5 INCH.
RIGHT AFT DOOR SILL FR 66; CORROSION LEVEL 2; TASK JA-260-53500. SPLICE ANGLE REPAIR IAW SRM 53-41-14. DEFECT SIZE: 10 INCHES X .846 INCH.
BEAM - Y1292 FROM FRAME 66 THRU FRAME 68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 6 INCHES.
BEAM Y1292 FROM FRAME 66-68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 4 INCHES.
BEAM - Y1292 AT FRAME 16; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 1 INCH.
CIDS PANEL CAUTION LIGHT ILLUMINATED IN FLIGHT AND ON LANDING. MAINTENANCE FOUND L-2 DOOR SLIDE INFLATION BOTTLE PRESSURE LOW. MAINTENANCE REPLACED L-2 DOOR SLIDE INFLATION BOTTLE. OK FOR SERVICE.
DURING THE EMERGENCY LIGHTS TEST, A MESSAGE DISPLAYED INDICATING THAT THE LEFT EXIT EMERGENCY POWER SUPPLY UNIT BATTERY HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN THE LEFT EXIT POSITION. OPERATIONALLY CHECKS OK. (M)
ONT - FLT 46 - LAX-PHL, AFTER TAKEOFF, A FUEL IMBALANCE DEVELOPED, ACCOMPANIED BY A 'FUEL AUTO TRANSFER FAULT' MESSAGE. BY ABOUT FL180, THE IMBALANCE HAD REACHED 3,000 LBS, WITH THE LEFT WING LOSING FUEL. MANUAL FEED WAS SELECTED, BUT DID NTO HAVE ANY AFFECT. BY FL230, FLIGHT DECLARED AN EMERGENCY AND BEGAN TO RETURN TO FIELD AT LAX. THE FUEL IMBALANCE CONTINUED TO WORSEN, SO CREW OPTED TO LAND AT A CLOSER ALTERNATE AIRPORT. FLIGHT DIVERTED TO ONT. DURING APPROACH, RECEIVED A 'RIGHT WING TANK OVER FULL' OVER FULL MESSAGE. BY THE TIME THE AIRCRAFT REACHED THE GATE, THERE WAS A 9,000 POUND IMBALANCE AND FUEL WAS SPILLING OUT OF THE RIGHT WING VENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO LAX, WHERE THE CE
PVD - THE LEFT AND RIGHT BATTERY PACKS WOULD NOT TEST. MAINTENANCE REPLACED THE BATTERY PACKS. OPERATIONALLY CHECKED OK. (M)
LAX - THE EMERGENCY LIGHTS DO NOT TEST PROPERLY. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNITS. TESTED OK. (M)