N103US
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2016-05-14 – 2016-05-14 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2016-05-14 – 2016-05-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS GROUNDED: SEAT 22ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 22ABC.REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 20ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMING THE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 20ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 12DEF O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 12DEF. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 15ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 15ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 18ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMING THE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 18ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43.PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 14DEF O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 14DEF. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 24ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMING THE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 24ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 19ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. AINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 19ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 25DEF O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 25DEF. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 10DEF O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMING THE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 10DEF. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 25ABC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMINGTHE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 25ABC. REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS GROUNDED: SEAT 2AC O2 MASK COMPARTMENT WILL NOT RELEASE WHILE PERFORMING THE DROP TEST IAW AMM 35-23-00. MAINTENANCE OPENED AND INSPECTED MASK CONTAINER AT 2ABC REPACKED AND STOWED MASKS AS NEEDED, PER AMM 35-21-43 AND PERFORMED SATISFACTORY DROP TEST IAW AMM 35-23-00.
AIRCRAFT WAS NOT GROUNDED: 4R DOOR EMERGENCY CYLINDER ACCUMULATOR SHOWS 1450 PSI AT 50 DEGREES F. REQUIRES SERVICING. MAINTENANCE SERVICED 4R DOOR ACCUMULATOR IAW AMM 52-10-00.
AIRCRAFT IN BASE MAINTENANCE: RH EMERGENCY ESPU FAULTED. MAINTENANCE REPLACED RH EMER ESPU IAW AMM 33-51-38.
AIRCRAFT IN BASE MAINTENANCE: RIGHT EMERGENCY EXIT ESPU FAULTING. MAINTENANCE REPLACED RH EMER ESPU IAW AMM 33-51-38.
AIRCRAFT WAS GROUNDED: HYD Y RSVR LO LVL ECAM. FOLLOWED ECAM AND QRH PROCEDURES. DIVERTED TO STL, LANDED WITHOUT INCIDENT. MAINTENANCE UPON WALKAROUND INSPECTION DISCOVERED LEAKING HYDRAULIC FLUID FROM W/W. CHANGED HYDRAULIC FITTING AND ORING ON YELLOW SYSTEM PTU MANIFOLD LAW AMM 29-13-15.
AIRCRAFT WAS NOT GROUNDED: L3 DOOR PRESSURE ASSIST LOW. SERVICED L3 DOOR PRESSURE ASSIST PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: R3 DOOR PRESSURE ASSIST LOW. SERVICED R3 DOOR PRESSURE.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO A LOUD ELECTRICAL ARCHING SOUND IN FLIGHT. RESET GALLEY AND CABIN SWITCH WITH MOC. SOUND WENT AWAY AFTER RESET AT ABOUT 26,000 FT. NO SMOKE NO FLICKERING NO ECAM MESSAGES NO CIRCUIT BREAKERS POPPED. NOISE CAME BACK LOUDER AT AROUND 4,000FT ON APPROACH THEN WENT AWAY AND EVERYTHING WAS NORMAL. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO A LOUD ELECTRICAL ARCHING SOUND IN FLIGHT. RESET GALLEY AND CABIN SWITCH WITH MOC. SOUND WENT AWAY AFTER RESET AT ABOUT 26,000 FT. NO SMOKE NO FLICKERING NO ECAM MESSAGES NO CIRCUIT BREAKERS POPPED. NOISE CAME BACK LOUDER AT AROUND 4,000FT ON APPROACH THEN WENT AWAY AND EVERYTHING WAS NORMAL. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202312195778: MAINTENANCE FOUND CONTACTOR 27XN WOULD RELAX INTERMITTENTLY WITHOUT COMMAND AND REPLACED IT PER AMM 24-51-55. A SATISFACTORY OPERATIONAL CHECK.** (CLOSED)
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITING CRACKED AT KEEL BEAM RIB W10 AND FR 42. MAINTENANCE REPLACED FITTING PER EA 350064.
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY D DOOR HARD TO OPEN/CLOSE. MAINTENANCE ADJUSTED AFT LAVATORY D DOOR LOWER PIN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: 2L DOOR MADE METALLIC SOUND WHEN CLOSING / ARMING AND WAS DIFFICULT TO ARM. MAINTENANCE ADJUSTED THE GIRT BAR PER AMM 52-11-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS GROUNDED: SMOKE AND ODOR REPORTED BY INFLIGHT CREW AT SEAT ROW 26 AFT INTO THE GALLEY. A BURNING RUBBER ODOR MOST NOTICABLE NEAR SIDEWALLS, STARTING SHORTLY AFTER TAKEOFF. MAINTENANCE ACCOMPLISHED TASK CARD 26L00021001 SMOKE/ ODOR FUMES TROUBLE SHOOTING AND FOUND AFT CARGO COMPARTMENT VENTILATION EXTRACTION FAN AT FAULT. REPLACED AFT CARGO COMPARTMENT VENTILATION EXTRACTION FAN PER AMM 21-28-54. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODOR NOTED IN AIRCRAFT.
AIRCRAFT IN BASE MAINTENANCE: DURING TEST OF PTP PANEL 110RH (NEXT TO FAP PANEL) RECEIVED "EPSU INT LOAD EMER R" MESSAGE. ON EPSU RH (12WL) SIDE "INTERIOR LIGHTS FAULT" IS ILLUMUNATED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202303209220) AND BATTERY (AALA202303204015) PER AMM33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT IN BASE MAINTENANCE: DURING TEST OF PTP PANEL 110RH (NEXT TO FAP PANEL) RECEIVED "EPSU INT LOAD EMER R" MESSAGE. ON EPSU RH (12WL) SIDE "INTERIOR LIGHTS FAULT" IS ILLUMUNATED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202303209220) AND BATTERY (AALA202303204015) PER AMM33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: DURING INSPECTION OF #3 MAIN AXLE PER EA 338915, FOUND STREAK AND SPOTS OF EXPOSED METAL BETWEEN THE THREE AND 8 O'CLOCK POSITION IN THE CHROME PLATING AND ADDITIONAL PITTING ON CHROME. IT WAS DETERMINED THAT THE DAMAGE WAS OUTSIDE THE ON WING REPAIRABLE LIMITS AND THE RIGHT HAND MAIN LANDING GEAR LOWER LEG / SHOCK ABSORBER ASSEMBLY WAS REPLACED PER TASK CARD 26L70032006.
AIRCRAFT WAS GROUNDED: DURING INSPECTION OF # 4 MAIN AXLE PER EA 338915, FOUND SPOTS OF EXPOSED METAL BETWEEN FIVE AND 10 O'CLOCK POSITIONS IN THE CHROME PLATING AND ADDITIONAL PITTING ON CHROME. IT WAS DETERMINED THAT THE DAMAGE WAS OUTSIDE THE ON WING REPAIRABLE LIMITS AND THE RIGHT HAND MAIN LANDING GEAR LOWER LEG / SHOCK ABSORBER ASSEMBLY WAS REPLACED PER TASK CARD 26L70032006.
AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EVACUATION COMMAND SWITCH INTERMITTENT. REPLACED EVACUATION PUSH BUTTON SWITCH (3WP) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER ESPM 20-45-11 AND AMM 23-73-00.
AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND AFT MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING BETWEEN FR 42 AND FR 43 AT S42R. REPLACED FITTING PER EA 338751.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND FIXED WINDOW DELAMINATED. REPLACED WINDOW PER AMM 56-11-12.
AIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING SLAT TRACK #6 LOWER AFT BOLT AT WS 6132 AND RIB 11. REPLACED BOLT PER AMM 27-84-64-400-002.
AIRCRAFT IN BASE MAINTENANCE: LEFT WING #4 SPOILER HINGE BOLT HAS WORN THREADS. REPLACED HINGE BOLT PER AMM 27-64-44.
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING PYLON AFT SHACKLES UPPER SLEEVE WAS HARD TO REMOVE FOR INSPECTION. MAINTENANCE FOUND THE PYLON REAR ATTACHMENT BEARING CORRODED AT PYLON STATION 8293 AND RIB 10. REPLACED BEARING PER AMM 57-26-12.
AIRCRAFT IN BASE MAIN_MISSING DOOR DAMPER CYLINDER ACCUMULATOR GAGE SEAL DOOR 842 AT AFT GALLEY AREA (1 EACH). REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA (1 EACH) IN ACCORDANCE WITH AMM 52-13-14-400-001-B. **SUPPLEMENTAL REPORT FOR AALA202209075968: CHANGES MADE TO SECTION 5 AND 5 ADDING SPECIFIC PART INFORMATION AND COMPONENT INFORMATION**
AIRCRAFT IN BASE MAINTENANCE: MISSING DOOR DAMPER CYLINDER ACCUMULATOR GAGE SEAL DOOR 842 AT AFT GALLEY AREA (1 EACH). REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA (1 EACH) IN ACCORDANCE WITH AMM 52-13-14-400-001-B.
AIRCRAFT IN BASE MAINTENACE: CORROSION LEFT WING SLAT TRACK 3 LOWER BOLT (ECCENTRINC). REPLACED BOLT PER AMM 27-84-63-400-002.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING AT FR 43 BETWEEN S41R AND S42R. REPLACED ACTUATOR FITTING PER EA 338751.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R AT THE RIGHT HAND DOOR STOP FITTING #1. REPAIRED FRAME PER SRM 53-41-12-300-011
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 43 BETWEEN S21L AND S22L REPLACED FRAME PER EA 338568
AIRCRAFT WAS NOT GROUNDED: LENS COVER MISSING OFF OF EMERGENCY EXIT LIGHT SEAT 1C. INSTALLED MISSING LENS COVER PER AMM 33-51-19. OPERATIONAL CHECK NORMAL.
AIRCRAFT WAS GROUNDED: ON APPROACH SMELLED OIL/FUMES IN FLIGHT DECK. MAINTENANCE FOUND OIL COMING FROM THE APU LOAD COMPRESSOR DRAIN CAVITY DURING THE INITIAL TROUBLESHOOTING . **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: ON APPROACH SMELLED OIL/FUMES IN FLIGHT DECK. MAINTENANCE FOUND OIL COMING FROM THE APU LOAD COMPRESSOR DRAIN CAVITY DURING THE INITIAL TROUBLESHOOTING . REPLACED APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L31049003.
AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR AFT RIGHT SIDE, HAS COM OFF ITS HINGE. REPLACED DOOR LOCK ASSEMBLY PER AMM 25-45-21.
AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #1 HINGE FITTING FAILS FREE PLAY CHECK DUE TO EXCESSIVE PLAY. REPLACED HINGE FITTING PER EO 5518Y004.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR AFT ACTUATOR FITTING CRACKED AT 2ND FROM TOP FASTENER HOLE. REPLACED FITTING PER EA 328335.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR AFT ACTUATOR FITTING CRACKED AT 2ND FROM TOP FASTENER HOLE. REPLACED FITTING PER EA 328335.**SUPPLEMENTAL REPORT TO ADD CORRECT AIRCRAFT TIMES AND CYCLES TO SECTION 3**
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN FLASHLIGHT ON AFT RIGHT FLIGHT ATTENDANT JUMPSEAT PER AMM 25-56-00.
AIRCRAFT WAS GROUNDED. WHEN SPEED BRAKE WAS USED & FLAPS 2, 180 KNOTS AIRCRAFT WENT INTO A 5-10 DEGREE BANK. HAPPENED AT 9000 FEET AND AGAIN AT 4000 FEET. NO ECAM MESSAGES DISPLAYED DUE TO A UNCOMMANDED ROLL INCIDENT. TROUBLESHOT, REF TSM 27-10-00-810-842-A, NO FAULTS.
AIRCRAFT NOT GROUNDED: 2 TIMES ALL AUTOMATION DISCONNECTS + GOES INTO THRUST LOCK. PERFORMED TSM TASK 22-31-00-810-816-A.
AIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK FUME SMELL IN AIRCRAFT. MAINTENANCE ACCOMPLISHED JOB CARD 26L00021001. FOUND APU OIL COOLER LEAKING. ***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU OIL COOLING FAN IAW AMM 49-57-51. OPS AND LEAK CHECKS GOOD.*** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: FLOOR PATH LIGHTING LENS MISSING AT ROW 13C. MAINTENANCE REPLACED LENS PER MM 33-50-00.
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 2L FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT PER ATA 25-23-00.
AIRCRAFT NOT GROUNDED: MULTIPLE INFORMATION RELATED TO FMGC MISSING ON CA'S SIDE. RESET CIRCUIT BREAKERS FOR BOTH FMGC. PERFORMED OPERATIONAL TEST IAW AMM 22-83-34. OPS CHECK GOOD.
R1 DOOR ASSIST GAUGE VIEWING WINDOW MISSING. AIRCRAFT WAS GROUNDED. REPLACED THE DOOR ASSIST GAUGE VIEWING WINDOW IAW AMM 52-11-00.
L1 DOOR ASSIST HANDLE COVER MISSING. REPLACED THE HANDLE COVER IAW AMM 52-10-00. OK FOR SERVICE.
AIRCRAFT WAS NOT GROUNDED. AFT FLIGHT ATTENDANT DIRECT VIEW FLASHLIGHT OPERATIVE BUT LED DOES NOT FLASH. REPLACED AFT FLIGHT ATTENDANT DIRECT VIEW FLASHLIGHT.
AIRCRAFT WAS GROUNDED. FLIGHT DIVERTED DUE TO A BATTERY ISSUE. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE.
MISSING EMERGENCY LIGHT LENS AT SEAT 4C. INSTALLED NEW THE LENS AT SEAT 4C IAW AMM 33-51-18 AND PERFORMED SUCCESSFUL OPS CHECKS.
F/A REPORTED THAT THE AISLE EMERGENCY LIGHT LENS WAS DAMAGED ON SEAT 4C. REMOVED AND REPLACED EMERGENCY LIGHT LENS. OPS CHECKED GOOD IAW AMM 35-51-18.
L2 DOOR, EMERGENCY BATTERY FAILED TO TEST DURING SLIDE CHANGE, SHOWED FAULT EPSU EXT LOAD AFT LT. REMOVED AND REPLACED LEFT AFT SLIDE. OPS CHECKED GOOD.
DELAMINATION ON THE AFT CARGO BAY FLOORBOARD 151DF. REPLACED FLOORBOARD IAW AMM 53-42-14.
DELAMINATION ON AFT CARGO FLOOR PANEL 151GF. REPLACED THE FLOOR PANEL IAW AMM 53-42-14.
LIGHT LENS DETACHED. INSTALLED THE EMERGENCY LIGHT LENS.
LANDING LIGHT MESSAGE DISAGREES WITH AIRCRAFT CONFIGURATION RIGHT SIDE ONLY, STAYS EXTENDED UNTIL RECYCLED. CLEANED THE CONNECTOR ON RIGHT LANDING LIGHT. OPERATIONAL CHECKED GOOD IAW AMM.
AIRCRAFT WAS NOT GROUNDED. DOOR 2R EMERGENCY EXIT SIGN COVER MISSING. REPLACED EMERGENCY EXIT LIGHT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
L1 DOOR EMERGENCY EXIT LIGHT MISSING THE LENS. INSTALLED THE LENS IAW AMM 33-51-13-400-001-A, LIGHT OPS CHECKED OK.
CORROSION ON RIGHT MAIN GEAR REAR PINTLE PIN. REPLACED PINTLE PIN PER CARD 26T00032001.
CENTER NR 1 PUMP FAULT. OPS CHECK OF THE CENTER FUEL PUMP, CHECKED GOOD IAW AMM 28-21-51.
NR 2 ENGINE STALL ECAM MESSAGE AT INITIAL CLIMB LEVEL OFF AT 32,000 FT. MESSAGE APPEARED THREE TIMES WITH ENGINE BANGS. PAX REPORTED SEEING FLASH. RECOVERED BACK TO NORMAL OPS. REMOVED AND REPLACED THE ENGINE. AIRCRAFT GROUNDED.
EXIT LENS OVER THE RT AFT SERVICE DOOR FOUND BROKEN. INSTALLED A NEW LENS.
R2 DOOR VERY HARD TO ARM AND DISARM. REMOVED OBSTRUCTION FROM GIRT BAR.
AIRCRAFT WAS NOT GROUNDED: L2 DOOR SLIDE BULGING WHICH IS PREVENTING THE SLIDE BUSTLE FROM FITTING PROPERLY OVER THE SLIDE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 26L00025011.
AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOAD TRANSMITTING PROFILE SEGMENT AT EMERGENCY EXIT DOOR 834, AFT POSITION IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE SEGMENT PER EA 264342 AND EO 5210Y228.
AIRCRAFT IN BASE MAINTENANCE. WEAR ON RIGHT HAND MAIN LANDING GEAR, OUTBOARD ACTUATOR RETRACTION PIN. REPLACED PIN PER AMM 32-31-46.
AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON FORWARD GALLEY SLIDE RAFT PASSENGER CREW DOOR 831, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-007-A.
AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON FORWARD GALLEY SLIDE RAFT PASSENGER CREW DOOR 841, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-803-A.
AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON AFT GALLEY SLIDE RAFT PASSENGER CREW DOOR 842, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-803-A.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING SLAT TRACK NR 5 LOWER BOLT BETWEEN RIB 9-10. REPLACED LOWER BOLT PER AMM 27-84-64-400-002-A.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING TRACK NR 4 OUTBOARD FLAP PIVOT BOLT. REPLACED PIVOT BOLT PER AMM 27-54-62.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING TRACK NR 3 OUTBOARD FLAP PIVOT BOLT. REPLACED PIVOT BOLT PER AMM 27-54-62.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY COVER FITTING AT FR 68 AND STRINGER 23L. REPLACED COVER FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RIGHT HAND WING OUTBOARD FLAP. REPLACED OUTBOARD FLAP PER AMM 27-54-62.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY CORNER FITTING AT STRINGER 23R AND FR 68. REPLACED CORNER FITTING PER SRM A320 51-72-11 AND DWG D53480019.
AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON LEFT HAND SIDE CENTER WING BOX (2) HOLES 1'' AND 2'' FORWARD OF FRAME 43. REPLACED PRESSURE PLATE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON RIGHT HAND ELEVATOR UPPER SKIN PANEL AT TWO LOCATIONS 6" FROM FASTENER LEADING EDGE BETWEEN RIB 7-9. REPAIRED UPPER SKIN PANEL PER SRM 55-21-11-300-005.
PASSENGER CREW DOOR FINGER AND STRIKER LEVER DAMPER MECHANISM IS OUT OF ADJUSTMENT. MAINTENANCE PROPERLY ADJUSTED IAW AMM 52-13-14-820-002-A.
AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATIONS ON LEFT HAND SIDE BOX BEAM FLANGE HOLE FITTINGS AT STRINGER 24R AND FR 43. REPAIRED SIDE BOX BEAM PER EO 5315Y066.
AIRCRAFT IN BAE MAINTENANCE. CRACK INDICATIONS ON LEFT HAND SIDE BOX BEAM FLANGE 2 HOLE FITTINGS. REPAIRED SIDE BOX BEAM PER EO 5315Y066.
LEFT ELEVATOR NR 2 HINGE ARM FITTING BETWEEN RIB 6-7 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.
RIGHT ELEVATOR NR 6 HINGE ARM FITTING AT RIB 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.
LEFT ELEVATOR NR 1 HINGE ARM FITTING AT RIB 5 HAS EXCESSIVE PLAY. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.
LT ELEVATOR NR 3 HINGE ARM FITTING BETWEEN RIB 7-8 HAS EXCESSIVE PLAY. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.
LEFT ELEVATOR NR 6 HINGE ARM FITTING AT RIB 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE AT FR 34 BETWEEN STRINGERS 41L AND 42L. REPLACED SHEAR TIE PER SRM 51-72-11 AND DRAWING D532 31712.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 33 BETWEEN STRINGER 42L AND STRINGER 43L. REPLACED CLEAT PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOAD TRANSMITTING PROFILE SEGMENT AT EMERGENCY EXIT DOOR 833 FORWARD POSITION IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE SEGMENT PER EA 264342 AND EO 5210Y228.
LEFT ELEVATOR NR 5 HINGE ARM FITTING AT RIB 10 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SILL BEAM, INTERNAL STRUCTURE AT STRINGER 38R BETWEEN FR 60 AND FR62. REPLACED SILL BEAM PER SRM 51-72-11 AND 53-41-49-300-02.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261DF. REPLACED FLOOR PANEL PER SRM 53-02-00, IRM 9701 REV G AND EA 264132.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y765 BETWEEN FR 21 AND FR24. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53110900.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON AFT GALLEY LOWER SILL AT STRINGER 23R BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY LOWER SILL BETWEEN FR 16 AND FR 20 AT STRINGER 23L. REPLACED LOWER SILL PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FORWARD GALLEY FLOOR PANEL 222CF. REPLACED FLOOR PANEL PER SRM 53-12-00.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 262BG. REPLACED FLOOR PANEL PER EA 264130 AND SRM 53-02-00.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261PF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222EF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY COUPLING AT STRINGER 23R AND FR 66. REPLACED COUPLING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23R BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11 AND EA 264153.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221PF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY LOWER SILL FITTING AT STRINGER 23R BETWEEN FR 16 AND FR 20. REPLACED FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON LEFT HAND ELEVATOR UPPER SKIN PANEL AT 3 PLACES LOCATED 6" TO 13" FROM LEADING EDGE BETWEEN RIB 1-7; AND 2 PLACES LOCATED 6.5' TO 12' FROM TRAILING EDGE BETWEEN RIB 2-7. REPAIRED UPPER SKIN PANEL PER SRM 55-21-11-300-005.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221EF. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261BG. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261AG. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221DF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT FR 66 AND -Y318. REPLACED FLOORBEAM PER SRM A320 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY WEB AT FR 20 AND STRINGER 23R. REPLACED WEB PER SRM 51-72-11 AND DRAWING NR D53114392.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY SEAT TRACK AT -Y1292 BETWEEN FR 12 AND FR 24. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53112812.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251DF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE AT AFT GALLEY UPPER OUTBOARD SPLICE COUPLING AT STRINGER 23L AND FR 66. REPLACED COUPLING PER SRM 51-72-11 AND DWG D53474250.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY UPPER INBOARD SPLICE COUPLING AT STRINGER 23L AND FR 66. REPLACED COUPLING PER SRM 51-72-11 AND DWG D53474250.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y765 BETWEEN FR 12 AND FR24. REPLACED SEAT TRACK PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR BEAM AT -Y464.8 AND STRINGER 23L, BETWEEN FR 66 AND FR 70. REPLACED FLOOR BEAM PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23L BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11.
CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 AND 70, +Y160.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472800.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR FORWARD HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR FORWARD HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.
AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON FORWARD CARGO COMPARTMENT PRESSURE DECK AT FR 36 BETWEEN Y1292 AND Y1523. REPAIRED PRESSURE DECK PER EA 263899.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 151EF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM FITTING NR 1 BEARING. REPLACED HINGE ARM FITTING NR 1 PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM FITTING NR 3 BEARING. REPLACED HINGE ARM FITTING NR 3 PER AMM 55-36-41-0401 AND SRM 51-72-11-401.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151RF. REPLACED FLOOR PANEL PER SRM 53-02-00 / IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151QF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131FF BETWEEN FR 28 AND FR 31, AND BETWEEN -Y765 AND -Y1353. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152CF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151LF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON NR 4 RUDDER HINGE ARM FITTING. REPLACED HINGE ARM FITTING PER SRM 51-72-11 AND AMM 55-36-41-400-001-A.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152FF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND FORWARD CARGO COMPARTMENT PRESSURE DECK AT FR 36 BETWEEN -Y1292 AND -Y1523. REPAIRED PRESSURE DECK PER EA 263900.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 7 BEARING. REPLACED HINGE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 5 BEARING. REPLACED HINGE FITTING PER AMM 55-36-41 AND SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151CF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.
AIRCRAFT WAS NOT GNDED. FLASHLIGHT AT FWD ENTRANCE NEEDS TO BE REPLACED. R & R FLASHLIGHT BATTERY IAW AMM 25-60-10.
AIRCRAFT WAS NOT GNDED. LT CTR EMER POWER SUPPLY IS INOPERATIVE. R & R EMER POWER SUPPLY IAW AMM 33-51-38 PB 0401. OPERATIONAL CHECKED NORMAL.
AIRCRAFT WAS GNDED. NR 1 ENG PYLON HAT CHANNEL CRACKED ON INBD SIDE, UNDER PANEL 413CL, FWD UPPER CORNER OF PANEL. NR 1 ENG PYLON WEB, CHANNEL, R & R IAW SRM 51-42-11 & DWG 52, D54630485.
EMERGENCY LIGHTING OPERATIONAL TEST IAW AMM 33-51-00-710-001-A, PRODUCES EPSU BATTERY FWD LT FAILURE MSG. REPLACED POWER SUPPLY UNIT 10WL BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-810-802-A & 53-51-38.
BUSHING IN FWD LUG OF ACTUATOR ATTACH FITTING ON DOOR IS LOOSE IN FITTING. REPLACED LT MLG DOOR IAW AMM 52-81-00. REFER TO MX NON-ROUTINE 26-0553-8-0722 005, SN 18 FOR INFORMATION OF WORK ACCOMPLISHED.
FLIGHT 1870 EN-ROUTE, AFTER ROTATION, THE FLIGHT CREW HEARD A UN-NORMAL CLUNK. THE GEAR HANDLE WAS PLACED UP. THE GEAR INDICATORS SHOWED GREEN SOLID ALL 3 & FLASHING RED ON NOSE & RT MAIN GEAR. ALSO, A GEAR UNSAFE ECAM MSG CAME ON. THE CREW TRIED CYCLING THE GEAR, BUT WAS UNSUCCESSFUL. THE FLIGHT DECLARED AN EMER, RETURNED & DID A FLYBY OF THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED NLG EXTENSION PROXIMITY SENSOR 25GA. PERFORMED A GEAR SWING & FUNCTIONAL CHECKS WITH NO ABNORMAL INDICATIONS OR NOISE NOTED.
2L DOOR SLIDE PACK FELL OFF DOOR EN ROUTE. REINSTALLED ASSEMBLY AS REQUIRED.
FLIGHT ATTENDANT & TWO PAXS NOTICED AN ODOR, BOTH GOT LIGHT HEADED AS WELL. ACCOMPLISHED JOB CARD 26L00021005 CABIN ODOR TROUBLESHOOT. REPLACED RT ENG LPT SHAFT PLUG O RINGS IAW AMM TASK 72-55-00-960-002A. ACCOMPLISHED JOB CARD 26L00021004 DECONTAMINATION OF THE ECS ENGS & APU.
AT TOUCHDOWN RUDDER PEDALS JAMMED. TRAVELLING APPROX 1/2 MILE, FORCIBLY PUSHING ON PEDALS PRODUCED A MECHANICAL CRUNCH SOUND FOLLOWED BY NORMAL PEDAL OPERATION. FOUND PLASTIC COVER FOR FIRST OFFICERS PEDAL POSITION ADJUSTER BROKEN & INTERFERING WITH PEDAL TRAVEL. REPLACED SAME IAW AMM 27-21-43-400-002-A.
FLIGHT DIVERTED TO MIA DUE TO CREW O2 LEAKING DOWN TO 640 PSI INFLIGHT. REPLACED O2 BOTTLE IAW AMM 35-11-41 PB 0401. NO LEAKS NOTED.
C11 CHECK, LT SIDE CABIN EMERGENCY LIGHTS WILL NOT TEST IAW WEEKLY CHECK. REPLACED LT SIDE CABIN EMERGENCY POWER SUPPLY UNIT.
RIGHT OVERWING SLIDE HAS LOOSE SCREW. RE-TORQUED RT OVERWING SLIDE SCREW IAW A320 SRM 5149-00.
DOOR 2L HARD TO ARM & DISARM. LUBED LOWER GIRT BAR ATTACHMENT.
FLIGHT CONTROL SLAT LOCKED WING TIP BRAKE ON. REPLACED LT SLAT WING TIP BRAKE, 35CV, IAW A320 AMM 27-81-51. OPERATIONS CHECKED GOOD, NO LEAKS NOTED.
CARGO FLOOR PANEL 151MF CRACKED. R & R FLOOR PANEL IAW AMM 53-42-14-400-001A.
CARGO FLOOR PANEL 151QF CRACKED. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.
CARGO FLOOR PANEL 152RF CRACKED. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.
CARGO FLOOR PANEL 131FF HAS ONE CRACK. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.
CARGO FLOOR PANEL 151GF DELAMINATED. R & R FLOOR PANEL IAW AMM 53-42-14-400-001A.
ROW 3 EMERGENCY FLOOR PATH LIGHTING LENS MISSING. REPLACED ROW 3 EMERGENCY FLOOR PATH LIGHTING LENS AS REQUIRED.
AFT RIGHT DOOR EXIT LIGHT LENS MISSING. REPLACED LENS AS REQUIRED AT AFT RIGHT DOOR.
ROW 13 EMERGENCY FLOOR PATH LIGHTING LENS MISSING. REPLACED ROW 13 EMERGENCY FLOOR PATH LIGHTING LENS AS REQUIRED.
CREW REPORTED THE SLATS BECAME STUCK IN THE FIRST POSITION AFTER REQUESTING FLAPS 1. FLAPS RESPONDED AND WORKED NORMALLY WITH THE SLATS STUCK. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SUP WILL BE PROVIDED AFTER COMPLETION OF CORRECTIVE ACTION.
EMERGENCY LIGHT SYSTEM TEST FAILED DUE TO EXTERNAL POWER SUPPLY UNIT (EPSU) INTERNAL LOAD FAULT TASK 33-51-00-710-001A. RELAMPED CABIN EXIT MARKING AND LOCATION SIGNS AS REQUIRED RESTORING EPSU MEMORIZED INTERNAL LOADS. CABIN EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECKS SATISFACTORY REFERENCE AIRBUS A/M/M 33-51-00-710-009-A AND 33-51-00-710-001-A.
THERE IS AN ODOR ON THE AIRCRAFT WITH APU ON OR OFF AND BOTH ENGINES ON. ODOR REMAINED WITH BLEEDS OFF DURING DE-ICE. ALSO HAD STATUS MESSAGE ON ECAM "ONE PACK ONLY IF WAI ON". BLEED PAGE NORMAL. MAINTENANCE REMOVED AND REPLACED THE APU. LOAD COMPRESSOR SEAL DETERMINED TO BE ROOT CAUSE OF FAILURE.
FORWARD FLIGHT ATTENDANTS REPORTED MODERATE ELECTRICAL SMELL IN FORWARD GALLEY. DIVERTED BACK TO CLT AFTER REPORTS OF BREATHING ISSUES. FOUND OVEN IN FORWARD GALLEY CAUSING ODOR. REMOVED AND REPLACED THE OVEN.
FORWARD FLIGHT ATTENDANT REPORTED A MODERATE ELECTRICAL SMELL IN THE FORWARD GALLEY SHORTLY AFTER TAKEOFF. FLIGHT DECK CREW NOTICED A SLIGHT SMELL AFTER TAKEOFF THAT QUICKLY DISSIPATED. ALL THREE F/A'S REPORTED BREATHING DIFFICULTIES SO THE FLIGHT RETURNED TO CLT. THERE WERE NO PASSENGER COMPLAINTS. MAINTENANCE FOUND THE OVEN IN THE FORWARD GALLEY TO BE THE CAUSE OF THE SMELL. OVEN WAS REMOVED AND REPLACED IAW AIRBUS MAINTENANCE MANUAL 25-35-19-400-003-A.
CIDS CAUTION LIGHT FOR LEFT WING SLIDE RESERVOIR PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED LEFT WING SLIDE RESERVOIR BOTTLE IAW AIRBUS MAINTENANCE MANUAL 25-62-46-400-001-A.
MULTIPLE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED MID-CABIN POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.
SEAT MOUNTED EMERGENCY EXIT LIGHTS ROWS 3, 7, 15, 20-24 AND 26 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.
AFT JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY IN AFT JUMPSEAT EMERGENCY FLASHLIGHT.
THE 2L EMERGENCY EXIT DOOR DIFFICULT TO ARM. CLEANED AND LUBED 2L DOOR GIRT BAR.
TWO FLOOR LEVEL EMERGENCY LIGHT COVERS IN FIRST CLASS MISSING. REPLACED LIGHT COVERS.
FAA SAFETY INSPECTOR FOUND THE FOLLOWING UPON PREFLIGHT, 'ESCAPE SLIDE BALL LOCKS PAINTED OVER'. MAINTENANCE REMOVED PAINT AS REQUIRED PER ENGINERING ORDER EO2508Y025, REV 'A'.
AFT RIGHT SERVICE DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REPLACED AFT RIGHT DOOR SLIDE (R2).
LAX - EES - ELECTRICAL HARNESS MISROUTED ON R-2 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON R-2 DOOR ESCAPE SLIDE RAFT PACK.IAW AMM 25-62-44-400-007-0.
LAX - EES - ELECTRICAL HARNESS MISROUTED ON R-1 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON R-1 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.
LAX - EES - ELECTRICAL HARNESS NOT CONNECTED ON L-2 DOOR ESCAPE SLIDE RAFT. RECONNECTED ELECTRICAL HARNESS ON L-2 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.
LAX - EES - ELECTRICAL HARNESS MISROUTED ON L-1 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON L-1 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.
PHL-DEN - EMERGENCY LANDING - WHILE EN ROUTE PHL-DEN, CREW RECEIVED YELLOW HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY CAUSED BY PTU RUNNING CONTINUOUSLY. YELLOW QUANTITY DROPPED TO ZERO, CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC POWER TRANSFER UNIT IAW AIRBUS MAINTENANCE MANUAL 29-23-41.
FLT 1809 - CLT - EES - IN FLIGHT, THE 2-L DOOR SLIDE RED CABIN PRESSURE LIGHT AND THE SLIDE ARMED LIGHT ON THE FORWARD F/A PANEL WERE FLASHNG. THE FLIGHT ATTENDANT NUDGED THE 2-L DOOR ARMING HANDLE SEVERAL TIMES AND BOTH LIGHTS EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED RELAY 3EN1 IAW AIRBUS MAINTENANCE MANUAL 52-71-00-820-002.
FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 2-L SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.
LOG PAGE 7184362 - FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 2-R SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.
FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 1-L SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.
FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 1-R SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.
SAL - S5 - EEL - L-2 DOOR SLIDE RAFT DIRECTIONAL GUIDANCE LIGHTS FAILED TO ILLUMINATE DURING SLIDE RAFT DEPLOYMENT. REPLACED SLIDE RAFT ASSEMBLY IAW JOB CARD 26L00025007.
SAL - S5 - MAJOR REPAIR - CORROSION ON UPPER SURFACE OF LOWER SILL AT FR19 + 6 INCHES, S23R AT R-1 DOOR. REPLACED LOWER SILL BETWEEN FR16 TO FR20, S23R AT R-1 DOOR IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110339.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 5 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 12 RIGHT WING. REPLACED NR 5 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 12 RIGHT WING IAW A320 AMM 27-84-67.
SAL - S5 - MAJOR REPAIR - CORROSION ON 2 EACH NR 4 SLAT ATTACHMENT BOLTS ON SLAT TRACK NR 10 RIGHT WING. REPLACED 2 EACH NR 4 SLAT ATTACHMENT BOLTS ON SLAT TRACK NR 10 RIGHT WING IAW A320 AMM 27-84-66.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING. REPLACED NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING IAW A320 AMM 27-84-64.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - GALVANIC CORROSION ON COUNTER SINK HOLES OF RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14 TO RIB 15 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBS 9 TO RIB 10. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBS 9 TO RIB 10 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBS 8 TO RIB 9. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBS 8 TO RIB 9 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 700 TO WS 1406 & BETWEEN RIBS 2 TO RIB 3. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 4862 TO WS 5512 & BETWEEN WS 700 TO WS 1406 & BETWEEN RIBS 2 TO RIB 3 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBS 12 TO RIB 13. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBS 12 TO RIB 13 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 TO RIB 7. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 TO RIB 7 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK RAIL BETWEEN FR56 TO FR64, -Y1292. REPAIRED SEAT TRACK RAIL BETWEEN FR56 TO FR64, -Y1292 IAW A320 SRM 53-41-15.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 3 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 7 RIGHT WING. REPLACED NR 3 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 7 RIGHT WING IAW A320 AMM 27-84-65.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 4 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 9 RIGHT WING. REPLACED NR 4 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 9 RIGHT WING IAW A320 AMM 27-84-66.
SAL - S5 - MAJOR REPAIR - CORROSION ON SLAT ATTACHMENT BOLT ON TRACK NR 1 ON RIGHT WING. REPLACED SLAT ATTACHMENT BOLT ON TRACK NR 1 ON RIGHT WING IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - CORROSION ON LOWER SILL AT FR62, S38R. REPAIRED LOWER SILL AT FR62, S38R IAW A320 SRM 51-41-49.
SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLTS 2 EACH ON SLAT TRACK NR 4 RIGHT WING. REPLACED ATTACHMENT BOLTS 2 EACH ON SLAT TRACK NR 4 RIGHT WING IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLT ON SLAT TRACK NR 3 RIGHT WING. REPLACED ATTACHMENT BOLT ON SLAT TRACK NR 3 RIGHT WING IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER FORWARD CORNER FITTING AT FR66, S23L AT L-2 DOOR CUTOUT AREA. REPLACED LOWER FORWARD CORNER FITTING AT FR66, S23L AT L-2 DOOR CUTOUT AREA IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480009.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 1 SLAT TRACK TO SLAT ECCENTRIC ATTACHMENT BOLT ON RIGHT WING. REPLACED NR 1 SLAT TRACK TO SLAT ECCENTRIC ATTACHMENT BOLT IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR49 TO FR50, -Y1292. REPAIRED SEAT TRACK BETWEEN FR49 TO FR50, -Y1292 IAW A320 SRM 53-00-15.
SAL - S5 - MAJOR REPAIR - CORROSION ON CORNER FITTING AT FR68, S23R AT R-2 DOOR AREA. REPLACED CORNER FITTING AT FR68, S23R AT R-2 DOOR AREA IAW A320 SRM 51-72-11 & AIRBUS DRAWING 6279150.
SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLTS 3 EACH ON SLAT TRACK NR 2 RIGHT WING. REPLACED ATTACHMENT BOLTS 3 EACH ON SLAT TRACK NR 2 RIGHT WING IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - CORROSION ON NR 1 SLAT TRACK ATTACHMENT BOLTS 3 EACH AT AFT UPPER, FORWARD UPPER, & FORWARD LOWER POSITIONS OF NR 1 SLAT LEFT WING. REPLACED NR 1 SLAT TRACK ATTACHMENT BOLTS 3 EACH AT AFT UPPER, FORWARD UPPER, & FORWARD LOWER POSITIONS OF NR 1 SLAT LEFT WING IAW A320 AMM 27-84-63.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR18, Y503.2. REPLACED DUMMY RAIL BETWEEN FR12 TO FR18, Y503.2 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - NR 6282214 - CORROSION ON INBOARD COUPLING OF FLOORBEAM AT FR67 + 16 INCHES, -Y1162. REPLACED INBOARD COUPLING OF FLOORBEAM AT FR67 + 16 INCHES, -Y1162 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON HARDWARE OF CENTER HINGE FITTING ATTACHMENT ON LEFT WING NR 2 SPOILER. REPLACED HARDWARE OF CENTER HINGE FITTING ATTACHMENT ON LEFT WING NR 2 SPOILER IAW A320 CMM 57-72-21.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK FLANGE BETWEEN FR24 TO FR25 + 8 INCHES, -Y765. REPAIRED SEAT TRACK FLANGE BETWEEN FR24 TO FR25 + 8 INCHES, -Y765 IAW A320 SRM 53-21-15.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT FLOORBEAM BETWEEN FR64 TO FR66 + 4 INCHES, -Y1292. REPLACED SEAT FLOORBEAM BETWEEN FR64 TO FR66 + 4 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RAIL SEAL BEAM BETWEEN FR64 TO FR66 + 5 INCHES, Y765. REPLACED RAIL SEAL BEAM BETWEEN FR64 TO FR66 + 5 INCHES, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 10 INCHES TO FR65 + 20 INCHES, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 + 10 INCHES TO FR65 + 20 INCHES, -Y1732 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162.5. REPLACED FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162.5 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 11 INCHES TO FR67 + 15 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 11 INCHES TO FR67 + 15 INCHES, Y1292 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 4 INCHES TO FR67 + 17 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 4 INCHES TO FR67 + 17 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 10.5 INCHES TO FR66 + 4 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR65 + 10.5 INCHES TO FR66 + 4 INCHES, Y1292 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y1292 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON INBOARD COUPLING OF FLOORBEAM AT FR67 + 5 INCHES, Y1162. REPLACED INBOARD COUPLING OF FLOORBEAM AT FR67 + 5 INCHES, Y1162 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y254. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y254 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, Y512.5. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y512.5 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5347219020300.
SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM Z-PROFILE ASSEMBLY BETWEEN FR64 TO FR65, -Y1732. REPLACED FLOORBEAM Z-PROFILE ASSEMBLY BETWEEN FR64 TO FR65, -Y1732 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON LOWER SHAPE SILL OF R-2 DOOR WAY BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SHAPE SILL OF R-2 DOOR WAY BETWEEN FR66 TO FR68, S23R.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - NR 6282202 - CORROSION ON CENTER SHAPE SILL AT L-2 DOOR BETWEEN FR66 TO FR68, S23L. REPLACED CENTER SHAPE SILL AT L-2 DOOR BETWEEN FR66 TO FR68, S23L IAW A320 SRM 51-72-11.
SAL - S-5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT STRUCTURE BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R. REPLACED STAMPING SUPPORT BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53230861.
SAL - S5 - MAJOR REPAIR - WEAR ON SUPPORT FITTING ASSEMBLY AT R-2 DOOR. REPLACED SUPPORT FITTING ASSEMBLY AT R-2 DOOR IAW A320 CMM 52-13-15.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR37 TO FR39, -Y765. REPLACED SEAT TRACK BETWEEN FR37 TO FR39, -Y765 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.
SAL - S5 - MAJOR REPAIR - NR 6284552 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.
SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 42 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 42 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 5 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA131 TO STAB STA 227, 23 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 23 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 6 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 466 TO STAB STA 589, 69 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 466 TO STAB STA 589, 69 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 6 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 527 TO STAB STA 601, 37 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 7 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 527 TO STAB STA 601, 37 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 7 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 13 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 9 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 13 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 9 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - NR 6284654 - TRAPPED WATER FOUND IN RIGHT HAND ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA181 TO STAB STA271, 32 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT HAND ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA181 TO STAB STA271, 32 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 5 INCHES FROM TRAILING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 446 TO STAB STA 601, 32 INCHES INBOARD FROM HORIZ STAB RIB 9 TO RIB 10 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 446 TO STAB STA 601, 32 INCHES INBOARD FROM HORIZ STAB RIB 9 TO RIB 10 & 5 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.
SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 56 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 10 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 56 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 10 INCHES FROM LEADING EDGE IAW A320 SRM 55-21-00.
FLT 727 - DEN - EEL - R2 DOOR EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.
LOG PAGE 8599434 - FLT 1781-OKC - BURNING ODOR AROUND ROW 20 RT - NO VISIBLE SMOKE. MAINTENANCE FOUND NO OBVIOUS DEFECTS TO CAUSE BURNING ODOR. MAINTENANCE RELAMPED THE READING LIGHT AT 20D. NO SUBSEQUENT EVENTS.
FLT 1195 - PHL - EEL - FORWARD CEILING EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE RESET THE POWER SUPPLY UNIT - OPERATIONAL CHECK GOOD.
FLT 873 LAS-SAN - FUMES - PASSENGERS SEATED AFT OF THE WING COMPLAINED OF FUMES IN THE CABIN, EYE IRRITATION AND SNEEZING. MAINTENANCE INSPECTED THE APU FOR LEAKS - NONE NOTED. RAN THE APU AND BOTH ENGINES INDEPENDENTLY WITH NO ODORS NOTED. AIRCRAFT IS OK FOR SERVICE.
FLT NR 1910 CLT-LGA - DIV - CREW REPORTED GREEN HYDRAULIC LOW LEVEL LIGHT DURING CRUISE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. AIRCRAFT WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE REPLACED RUPTURED HYDRAULIC SENSE LINE, AND DUE TO FILTER DEBRIS, REPLACED HYDRAULIC PUMP AND ASSOCIATED FILTERS.
CLT - RECEIVED -EMER L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.
RDU - FLT 873 ON TAKEOFF, RDU TO PHL, DURING TAKEOFF ROLL, THE AIRCRAFT RIGHT BRAKE LOCKED UP. THE FLIGHT REJECTED TAKEOFF AT ABOUT 50-60 KNOTS. AFTERWARDS, THE TOWER REPORTED TO THE CREW THAT THE NR 3 MAIN GEAR WHEEL ASSEMBLY APPEARED TO HAVE SMOKE COMING FROM IT. THE CREW REQUESTED EMERGENCY EQUIPMENT FOLLOW THE FLIGHT BACK TO THE GATE. THE FLIGHT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 BRAKE ASSEMBLY FOR WEAR, ALL FOUR MAIN GEAR WHEEL ASSEMBLIES FOR FLAT SPOTTING, AND THE BRAKE STEERING CONTROL UNIT. OK FOR SERVICE.
PIT - S1 - SILL, 1 INCH X 1 INCH X .07 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-006; CABIN FLOOR, R-2 DOOR SEAL ASSY ON CROSSBEAM C66 AND AFT ENDI OF FRAME - Y1732. REPLACED DOOR SEAL IAW SRM 51-74-00, 53-41-14, 51-42-11.
BFM - S1 - FLOOR SUPPORT, 2 INCH X 3 INCH X 0.075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR - Y254 BET FR 16 AND 20. FABRICATED PARTS IAW SRM 53-00-14 FIG 206 PR SRM 53-11-14, 51-74-00, 53-14-00, 51-42-11.
BFM - S1 - FLOOR WEB, 1.5 INCH X 2 INCHES X 0.50 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR; Y1584, BET FR14 AND 16. REMOVED AND REPLACED IAW SRM.
BFM - S1 - TRACK ASSEMBLY, 2 INCH X 2 INCH X 0.50 INCH AREA, CORROSION LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR- Y254 BET FR16 AND 23. REMOVED AND REPLACED IAW SRM.
BFM - S1 - SUPPORT, 2 INCH X 5 INCHES X .025 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FL -Y189, FR 20. REMOVED AND REPLACED IAW SRM.
BFM - S1 - DUMMY RAIL, 2 INCHES X 1 INCH X .050 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500. MAIN CABIN FLOOR @ FR 16, LB -Y81. REPLACED DUMMY RAIL IAW SRM.
BFM - S1 - FLOOR SUPPORT, 2 INCHES X 12 INCHES X 0.020 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR BET FR 16, 20, BL-Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.
BFM - S1- SEAL SUPPORT, .5 INCH X .5 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500-015, MAIN CABIN FLOORBOARD SEAL SUPPORT AT Y1584 BETWEEN 14 AND 16. REMOVED AND REPLACED FLOORBOARD SEAL SUPPORT IAW SRM 51-74-00, SRM 53-11-14, SRM 51-42-11.
BFM - S1 - FLOOR SUPPORT, 1.5 INCH X 2 INCHES X .040 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-200-53500, BTW FR 16 AND 20, Y1292, FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.
BFM - S1 - FLOORBEAM- 2 INCHES X 1.5 INCHES X .04 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500-012, Y1292, BTW C68 AND C69 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11.
PIT - S1 - DUMMY RAIL, 2.5 INCHES X 2 INCHES X .075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR FR 16, Y503.2. REPLACED DUMMY RAIL (BEAM) ALT PN INSTALLED IAW SRM 51-74-00, 53-11-14, 51-42-11.
BFM - S1 - BEAM, 18 INCHES X 2 INCHES X .03 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 260-53500-004, MAINT CABIN FLOOR Y1292 BET C66 AND C68. REMOVED AND REPLACED FLOORBEAM IAW SRM.
BFM - S2 - SHEAR PLATE, 1 INCH X 1 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW 69 AND 70, BL - Y1292. REMOVED AND REPLACED SHEAR PLATE (WEB) IAW SRM.
BFM - S1 - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN DECK FLOOR RAIL, FRAME 68, -Y765. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, 51-42-11.
THE SLIDE SHOP FOUND THAT THE BRIDGING ON UPPER TUBE AT RUNWAY END HAD A SEAM SEPARATION. THE REPAIR SHOP SENT THE SLIDE BACK TO THE VENDOR FOR REPAIR.
DURING EMERGENCY LIGHTS TEST, RECEIVED 'EPSU INT LOAD EMER R' FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK AT THE RIGHT EMERGENCY EXIT. OPERATIONALLY CHECKS OK. (M)
LGA - THE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN PED SWITCH IS TURNED ON. MAINTENANCE REPLACED RELAY. OPERATIONALLY CHECKS OK. (M)
BOS - L1 DOOR ARMING CAM BROKE. MAINTENANCE REPLACED THE CAM. SMELL PIECE FELL FROM MAIN ENTRY DOOR. REPLACED DOOR HOOK. OPS OK. (M)
DCA-LGA - FLT 6360 - PASSENGER REPORTED ELECTRICAL FUMES AT ROW 20. MAINTENANCE REPLACED SEB AT ROW 20. SYSTEM TEST OK. (M)
BOS - FOUND FORWARD LEFT ESCAPE SLIDE FAILED EMERGENCY LIGHT CHECK. CIDS DISPLAYED EPSU EXT LOAD FWD LT. MAINTENANCE REPLACED THE FORWARD LEFT ESCAPE SLIDE. OPERATIONAL CHECK OK. (M)
DURING A-2 CHECK VISUAL INSPECTION, FOUND A 12 INCH BY 36 INCH DISBONDED AREA AT SLIDE DOOR COVERING OUTER SKIN AND LEFT A/C RT OFF WING SLIDE DOOR. REMOVED AND REPLACED SLIDE. (X)