N122US

Part: BYPASS VALVE — ODOR (ZONE 100) · airframe 70,127 hrs · 35,601 cycles

AIRCRAFT WAS GROUNDED: BURNT PLASTIC ODOR IN THE CABIN DURING CLIMB. MAINTENANCE REPLACED THE TURBINE BYPASS VALVE 30HH IAW AMM 21-61-53.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,944 hrs · 35,461 cycles

AIRCRAFT WAS NOT GROUNDED: RH FWD PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED RH FWD PASSENGER/CREW DOOR ACCUMULATOR TO THE CORRECT PRESSURE IAW AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,944 hrs · 35,461 cycles

AIRCRAFT WAS NOT GROUNDED: LH FWD PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED LH FWD PASSENGER/CREW DOOR ACCUMULATOR TO THE CORRECT PRESSURE IAW AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,944 hrs · 35,461 cycles

AIRCRAFT WAS NOT GROUNDED: LH AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED LH AFT PASSENGER/CREW DOOR ACCUMULATOR TO THE CORRECT PRESSURE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 69,843 hrs · 35,390 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR PRESSURE LOW. MAINTENANCE SERVICED L2 DOOR IAW AMM 52-13-00.

Part: SENSOR — WORN (ZONE 700) · airframe 69,826 hrs · 35,378 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF ECAM L/G SHOCK ABSORBER FAULT, FOLLOWED BY NUMEROUS OTHER ECAMS. DECESAION MADE TO RETURN TO CLT LANDED OVERWIGHT WITHOUT INCIDENT. MAINTENANCE FOUND GROUND SENSING MECHANISM WORN AND REPLACED GROUND SENSING MECHANISM IAW AMM 32-21-45.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 69,753 hrs · 35,327 cycles

AIRCRAFT IN BASE MAINTENANCE: LH AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE LOW SERVICED LH AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE IAW AMM 51-10-00.

Part: SHADE — STUCK (ZONE 800) · airframe 68,938 hrs · 34,815 cycles

AIRCRAFT WAS NOT GROUNDED: FA STATED WINDOW SHADE IN THE FORWARD EMERGENCY EXIT ROW AIRCRAFT RIGHT WAS STUCK IN THE CLOSED POSITION SO THEY REMOVED IT TO REMAIN IN COMPLIANCE. MAINTENANCE REPLACED FAIRING ON EMERGENCY EXIT DOOR IAW AMM 25-23-47.

Part: SHADE — STUCK (ZONE 200) · airframe 68,938 hrs · 34,815 cycles

AIRCRAFT WAS NOT GROUNDED: FA STATED WINDOW SHADE IN THE FORWARD EMERGENCY EXIT ROW AIRCRAFT RIGHT WAS STUCK IN THE CLOSED POSITION SO THEY REMOVED IT TO REMAIN IN COMPLIANCE. (OPEN)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 68,708 hrs · 34,681 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT R2 DOOR SEAL BROKEN AND LED NOT BLINKING, LIGHT INOP. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BATTERY AT R2 AND REPLACED SEAL IAW AMM 25-60-00.

Part: TACHOMETER — FAULTED (ZONE 700) · airframe 68,451 hrs · 34,522 cycles

AIRCRAFT WAS GROUNDED: BRAKES AUTO BRAKES FAULT ECAM AFTER TAKE OFF AND PRIOR TO ACCELERATION ALTITUDE/THRUST REDUCTION. PERFORMED TSM TASK 32-42-00-810-815-A. MAINTENANCE REPLACED #4 MLG TACHOMETER-DRIVE, PER AMM 32-42-68.

Part: COMPUTER — FAULTED (ZONE 100) · airframe 68,163 hrs · 34,361 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING WHILE PASSING 2000 FT, AN ANTI-ICE FAULT ECAM MESSAGE FOR THE CAPTAINS AND FIRST OFFICERS STANDBY PROBES DISPLAYED. THE FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND TURNED OFF ADR 2 PB AND SWITCHED AIR DATA FO FO 3. THE FLIGHT CREW REPORTED THAT THEY WERE UNABLE TO STAY OUT OF THE CLOUDS AND RETURNED TO DFW WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE #1 PROBE HEATER COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 30-31-34.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 68,108 hrs · 34,334 cycles

AIRCRAFT WAS NOT GROUNDED: 2R FLASHLIGHT NEEDS NEW BATTERY. MAINTENANCE REPLACED BATTERY ON FLASHLIGHT AFTER CABIN 2R OPS NORMAL AS NEEDED AMM 25-00-00.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: INOP EPSU (13WL) ON AFT GALLEY AREA. MAINTENANCE REPLACED EPSU (13WL) ON AFT GALLEY ARE I.A.W AMM 33-51-38-000-001-A AND AMM33-51-38-400-001-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: INOP EPSU (12WL) ON PASSENGER CABIN. MAINTENANCE REPLACED EPSU (12WL) ON PASSENGER CABIN I.A.W AMM 33-51-38-000-001-A AND AMM33-51-38-400-001-A.

Part: BOTTLE — LOW PRESSURE (ZONE 800 SLIDE) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE SLIDE RAFT ON PASSENGER CREW DOOR 841 AT FWD GALLEY AREA. MAINTENANCE REPLACED SLIDE RAFT ON PASSENGER CREW DOOR 841 AT FWD GALLEY AREA IAW TO JOB CARD 26C84152006.

Part: FITTING — DAMAGED (ZONE 100) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: REPLACE LOWER FITTING LOC ON RACK 80VU LH SIDE FOR ACCOMPLISHMENT EA 360316. MAINTENANCE PERFORMED INTERIM REPAIR ON LOWER FITTING LOCATED ON 80VU RACK AT LEVEL FR 23 TO FR 24, STR 32 LH SIDE IAW EA 360316.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST OF THE DOOR DAMPER EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.

Part: BRACKET — CORRODED (ZONE 500) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT ATTACH FITTING INB FLAP LH WING (DURING INSPECTION WAS FOUND CORROSION) L=0.586 INCH W=0.167 INCH D=0.001 INCH. MAINTENANCE REPLACED BRACKET ASSY LOC INB FLAP BTW RIB 14 AND WX4476.559 LH WING IAW A320 SRM 51-42-11-801 AND A320 SRM 51-72-11-911-001 AND DWG D57570280.

Part: SUPPORT BRACKET — EXCESS PLAY (ZONE 600) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT ATTACHMENT FITTING INB FLAP RH WING (DURING INSPECTION WAS FOUND CORROSION) L=0.694 INCH W=0.266 INCH D=0.002 INCH. MAINTENANCE REPLACED BRACKET ASSY LOC INB FLAP BTW RIB 14 AND WX4476.559 RH WING IAW A320 SRM 51-42-11-801 AND A320 SRM 51-72-11-911-001 AND DWG D57570280.

Part: BRACKET — EXCESS PLAY (ZONE 600) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT ATTACH FITTING INB FLAP RH WING. MAINTENANCE REPLACED BRACKET ASSY LOC. INB FLAP BTW RIB 14 AND WX4476.559 RHWING, I.A.W A320 SRM 51-42-11-801 AND A320 SRM 51-72-11-911-001 AND DWG D57570280. FORM ME-0308 GENERATED SEE SDA ID: 221381.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON L=14.2 INCH W=1.34 INCH D=0.006 INCH. MAINTENANCE REPLACED LOWER SPIGOT FITTING BTW RIB 4 TO RIB 5 LH PYLON IAW A320 SRM 54-51-12-300-001.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON L=13.6 INCH W=1.32 INCH D=0.007 INCH. MAINTENANCE REPLACED LOWER SPIGOT FITTING BTW RIB 4 TO RIB 5 RH PYLON IAW A320 SRM 54-51-12-300-00.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION LOCATED ON TRILING EDGE FALSE REAR SPAR TOP SKIN OVERHANG UPPER SURFACE BETWEEN WX3622 AND WX4013 RH WING L=2.232 INC W=0.625 INCH D=0.007 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON TOP SKIN UPPER SURFACE FALSE REAR SPAR BTW RIB WX3622 TO RIB WX4349 ON RH WING IAW EA 360584.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 3 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 1 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 5 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 5 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 6 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: FITTING — CORRODED (ZONE 200) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD LEFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOORBEAM AT FR 20 AND -Y1292. REPLACED FLOORBEAM PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 68 AND FR 70 AT -Y160.5. REPLACED THE FLOOR SUPPORT PER SRM 51-72-11.

Part: BRACKET — CORRODED (ZONE 100) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BRACKET LOCATED AT WEB -Y1732 AT LEVEL FR20 AT FORWARD GALLEY AREA. REPLACED BRACKET LOCATED ON WEB -Y1732 AT LEVEL FR20 AT FORWARD GALLEY AREA. PER A320 SRM 51-42-11-801 AND SRM 51-72-11-911-001 AND DWG D53114112.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE FALSE REAR SPAR STIFFENER 6 DATUM ON RH WING L=3.212 INCH W=1.413 INCH D=0.050 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON TOP SKIN UPPER SURFACE FALSE REAR SPAR BTW RIB WX3622 TO RIB WX4349 ON RH WING IAW EA 360584.

Part: SKIN PANEL — SCRATCHED (ZONE 100) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: SCRATCH ON INTERNAL SKIN LOCATED BTW FR56 TO FR57 AND BTW STRG42L TO STRG43L IN AFT CARGO COMPARTMENT ,SCRATCH MEASURES ARE L=2.825 INCH W=0.071 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED ON EXTERNAL SKIN LOCATED BTW FR56 TO FR57 AND BTW STRG42L TO STRG 43L IN AFT CARGO COMPARTMENT IAW EA361747 PART B.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L LOCATED BTW FR56 TO FR57 IN AFT CARGO COMPARTMENT (CPCP 534107-01) L= 1.676 IN, W= 0.751 IN, D= 0.002 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR (SPLICE REPAIR) ON STRINGER SECTION OF STRINGER 43L BTW FR55 TO FR58 IN AFT CARGO COMPARTMENT IAW EA 361747.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 41R AT FR 59 IN CARGO COMPARTMENT CORRODED AREA: L=11.185 IN W=0.750 IN D=0.005 IN. MAINTENANCE FOUND 41RH LOWER FLANGE CORRODED AT FR 59.

Part: DOUBLER — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OB FLAP LOWER EXTERNAL DOUBLER LOCATED BTW RIB 14 AND RIB 15 ON RH WING L=3.387 INCH W= 1.842INCH D= 0.026 INCH. MAINTENANCE REPLACED DOUBLER EXTERNAL LOCATED ON OB FLAP LOWER BTW RIB 14 AND RIB 15 ON RH WING IAW A320 SRM 57-53-21-300-003.

Part: FITTING — BURRED (ZONE 100 -) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: BURRED MATERIAL (OVALIZATION) 80 VU RACK LOWER LATERAL FITTING RH SIDE. MEASURE W: 0.335 INCH. MAINTENANCE PERFORMED INTERIM REPAIR LOCATED ON LOWER LATERAL FITTING 80VU RACK AT LEVEL FR 23 TO FR 24, STGR 32 RH SIDE IAW EA 360316 AND REPAIR DRAWING R53113174.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 68,046 hrs · 34,304 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT ANGLE AT RIB 15, OUTBOARD FIXED LEADING EDGE ON LEFT HAND WING. REPLACED SUPPORT ANGLE PER SRM 51-72-11.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 22C MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 22A MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 21B MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 18B MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 20C MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 15B MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 14B MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 14A MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 65,131 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT SEAT 21D MISSING. INSTALLED LIFE VEST PER TASK CARD 26C00025003.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 64,866 hrs · 32,336 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT CABIN DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE OUT OF LIMITS. SERVICED DAMPER PER AMM 52-10-00.

Part: OVEN — ODOR (ZONE 900 - LAV/G) · airframe 64,609 hrs · 32,168 cycles

AIRCRAFT WAS GROUNDED: PASSENGER AND FLIGHT ATTENDANT SMELT BURNING RUBBER AT ROW 3 THROUGH 12. FLIGHT CREW TURNED PED SWITCH ABOVE FLIGHT ATTENDANT PANEL OFF AND SMELL WENT AWAY. MAINTENANCE REPLACED FORWARD GALLEY RIGHT HAND OVEN PER AMM 25-35-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAULTY (ZONE 200 - FUSE) · airframe 63,679 hrs · 31,555 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHTS FLASHED ON/OFF MULTIPLE TIMES IN FLIGHT. MAINTENANCE FOUND FORWARD LEFT EMERGENCY POWER SUPPLY UNIT 10WL FAULTING AND LOW VOLTAGE ON THE RIGHT EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202303289286) AND BATTERY PER AMM 33-51-38 (AALA202303283376). ALSO REPLACED THE BATTERY FOR THE RIGHT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202303282519). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — FAULTY (ZONE 200 - FUSE) · airframe 63,679 hrs · 31,555 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHTS FLASHED ON/OFF MULTIPLE TIMES IN FLIGHT. MAINTENANCE FOUND FORWARD LEFT EMERGENCY POWER SUPPLY UNIT 10WL FAULTING AND LOW VOLTAGE ON THE RIGHT EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202303289286) AND BATTERY PER AMM 33-51-38 (AALA202303283376). ALSO REPLACED THE BATTERY FOR THE RIGHT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202303282519). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — LOW (ZONE 200 - FUSE) · airframe 63,679 hrs · 31,555 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHTS FLASHED ON/OFF MULTIPLE TIMES IN FLIGHT. MAINTENANCE FOUND FORWARD LEFT EMERGENCY POWER SUPPLY UNIT 10WL FAULTING AND LOW VOLTAGE ON THE RIGHT EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202303289286) AND BATTERY PER AMM 33-51-38 (AALA202303283376). ALSO REPLACED THE BATTERY FOR THE RIGHT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202303282519). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: RELAY — FAULTED (ZONE 100 - FUSE) · airframe 63,595 hrs · 31,510 cycles

AIRCRAFT WAS GROUNDED: DOOR LEFT /RIGHT, FORWARD /AFT CABIN STATUS MESSAGE MULTIPLE TIMES INFLIGHT. MAINTENANCE ACCOMPLISHED TSM 52-11-00-810-803A / 52-13-00-810-805 AND REPLACED RELAY12WN PER ESPM 20-46-50. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: RESERVOIR — LEAKING (ZONE 100 - FUSE) · airframe 63,462 hrs · 31,430 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT BRAKE PEDAL GOES FULLY TO FLOOR WITH NO BRAKE FEEL. MAINTENANCE FOUND THE RIGHT HAND BRAKE CONTROL MASTER CYLINDER (2626GM) LEAKING AND REPLACED IT PER AMM 32-42-12. (AALA202303025439) MAINTENANCE ALSO FOUND THE BRAKE HYDRAULIC RESERVOIR (2624GM) LEAKING AND REPLACED IT PER AMM 32-43-11. (AALA202303029571). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: MASTER CYLINDER — LEAKING (ZONE 100 - FUSE) · airframe 63,462 hrs · 31,430 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT BRAKE PEDAL GOES FULLY TO FLOOR WITH NO BRAKE FEEL. MAINTENANCE FOUND THE RIGHT HAND BRAKE CONTROL MASTER CYLINDER (2626GM) LEAKING AND REPLACED IT PER AMM 32-42-12. (AALA202303025439) MAINTENANCE ALSO FOUND THE BRAKE HYDRAULIC RESERVOIR (2624GM) LEAKING AND REPLACED IT PER AMM 32-43-11. (AALA202303029571). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: GENERATOR — NO TEST (OXYGEN) · airframe 63,089 hrs · 31,191 cycles

AIRCRAFT WAS GROUNDED: DURING C6 CHECK, SEAT ROW 26ABC O2 GENERATOR DID NOT DEPLOY WHEN PERFORMING DROP TEST. MAINTENANCE REPLACED SEAT ROW 26ABC O2 GENERATOR ASSEMBLY PER AMM TASK 35-21-41 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,771 hrs · 30,988 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHTS ILLUMINATED OVER AFT ENTRY DOOR AND REAR OF AIRCRAFT ROW 12 AND BACK. RESET CABIN INTERCOMMUNICATION DATA SYSTEM PER AMM 33-50-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: R2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: SKIN PANEL — CORRODED (ZONE 600 - RH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SKIN PANEL UPEER SURFACE BETWEEN RIBS 9 AND 13 AT STRINGER 16 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 335739.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SKIN PANEL UPEER SURFACE BETWEEN RIBS 9 AND 13 AT STRINGER 16 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 335644.

Part: SKIN PANEL — CORRODED (ZONE 600 - RH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SKIN PANEL UPEER SURFACE BETWEEN RIBS 13 AND 18 AT STRINGER 16 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 335739.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SKIN PANEL UPEER SURFACE BETWEEN RIBS 13 AND 16 AT STRINGER 16 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 335644.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SKIN PANEL UPEER SURFACE BETWEEN RIBS 16 AND 18 AT STRINGER 16 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 335644.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 11WL INOPERATIVE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 12WL INOPERATIVE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: TUBE — CRACKED (ZONE 400 - NAC/P) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: #1 ENGINE FIRE EXTINGUISHING TUBE CRACKED FAILED PRESSURE TEST. MAINTENANCE REPLACED FIRE EXTINGUISHING TUBE PER AMM 26-21-49 AND ACCOMPLISHED A SATISFACTORY LEAK CHECK PER AMM 26-21-00.

Part: NONE — CORRODED (ZONE 600 - RH WI) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE LOWER SIDE OF AFT SPAR FACE HYDRAULIC LINE SUPPORT RIB (RIBLET) AT RIB 15. REPLACED RIBLET PER SRM 51-42-11.

Part: NONE — NONE · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT INITIAL LOAD FORWARD LEFT FAULT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT INITIAL LOAD FORWARD LEFT FAULT. **SUPPLEMENTAL REPORT FOR AALA202206247526: REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. ** (CLOSED)

Part: SKIN — CORRODED (ZONE 100 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BETWEEN FR 63 AND FR 64 AND BETWEEN S41R AND S42R. REPAIRED SKIN PER EA 335693.

Part: BRACE — CRACKED (ZONE 100 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: FLOOR SUPPORT ANGLE BRACE CRACKED BETWEEN FR 64 AND FR 65 FAT BL 0. REPLACED FLOOR SUPPORT ANGLE BRACE AS REQUIRED.

Part: FORK — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: R2 DOOR CONTACTING GIRT BAR WHEN CLOSING DOOR WHILE ARMED. ADJUSTED TELESCOPIC FORKS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-13-22 AND TASK CARD 26C84252002.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND STABILIZER HINGE FITTING #4 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: NONE — NONE · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CEILING PANEL SEAT ROW 1AC EMERGENCY LIGHT CONNECTOR AND BACK SHELL DAMAGED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CONNECTOR — BROKEN (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CEILING PANEL SEAT ROW 1AC EMERGENCY LIGHT CONNECTOR AND BACK SHELL DAMAGED. **SUPPLEMENTAL REPORT FOR AALA202204125454: REPLACED CONNECTOR AND BACK SHELL (AALA202204272971) PER ESPM 20-44-10. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-00.** (CLOSED)

Part: NONE — BROKEN (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CEILING PANEL SEAT ROW 1AC EMERGENCY LIGHT CONNECTOR AND BACK SHELL DAMAGED. **ORIGINAL REPORT WAS AALA202204125454** REPLACED CONNECTOR AND BACK SHELL (AALA202204272971) PER ESPM 20-44-10. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-00.

Part: FITTING — CRACKED (ZONE 300 - STABS) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR OUTBOARD ACTUATOR FITTING CRACKED. REPLACED FITTING PER SRM 55-26-47-300-003

Part: LIGHT — MISINSTALLED (ZONE 200 - FUSE) · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT 26 ABC EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202204114913: FOUND EMERGENCY LIGHT NOT SECURED PROPERLY, SECURED LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-19-0401** (CLOSED)

Part: NONE — NONE · airframe 62,653 hrs · 30,907 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT 26 ABC EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: O-RING — LEAKING (ZONE 100 - FUSE) · airframe 62,525 hrs · 30,834 cycles

AIRCRAFT WAS GROUNDED: MUSTY ODOR- DIRTY SOCK SMELL DURING DESCENT WITH HP BLEED VALVES OPEN. ODOR DISSIPATES WHEN POWER IS INCREASED. REPLACED 4 EACH O-RINGS ON APU TRANSFER TUBES TO APU OIL COOLER PER AMM 49-91-44. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS NOTED.

Part: LIFE LINE — MISSING (ZONE 200 - FUSE) · airframe 62,473 hrs · 30,804 cycles

AIRCRAFT WAS NOT GROUNDED: CREW REPORTS (2) MISSING OVER WING EXIT LIFE LINES FOR MID CABIN. INSTALLED MISSING LIFELINES PER AMM 54-50-00.

Part: SAFETY VALVE — OPEN (ZONE 100 - FUSE) · airframe 62,032 hrs · 30,560 cycles

AIRCRAFT WAS GROUNDED AFTER TAKE OFF AIRCRAFT WOULD NOT PRESSURIZE AND HAD AN ECAM MESSAGE FOR THE CABIN PRESSURE SAFETY VALVE OPEN. AIRCRAFT RETURNED TO ORD WHERE IT LANDED SAFELY WITH OUT FURTHER INCIDENT. (NO EMERGENCY WAS DECLARED) **SUPPLEMENTAL REPORT FOR AALA202201065279: REPLACED SAFETY VALVES 6HL AND 7HL (AALA202201079223) PER AMM 21-31-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 21-31-00. ** (CLOSED)

Part: SAFETY VALVE — DEFECTIVE (ZONE 100 - FUSE) · airframe 62,032 hrs · 30,560 cycles

AIRCRAFT WAS GROUNDED AFTER TAKE OFF AIRCRAFT WOULD NOT PRESSURIZE AND HAD AN ECAM MESSAGE FOR THE CABIN PRESSURE SAFETY VALVE OPEN. AIRCRAFT RETURNED TO ORD WHERE IT LANDED SAFELY WITH OUT FURTHER INCIDENT. (NO EMERGENCY WAS DECLARED) **ORIGINAL REPORT WAS AALA202201065279** REPLACED SAFETY VALVES 6HL AND 7HL (AALA202201079223) PER AMM 21-31-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 21-31-00.

Part: NONE — NONE · airframe 62,032 hrs · 30,560 cycles

AIRCRAFT WAS GROUNDED AFTER TAKE OFF AIRCRAFT WOULD NOT PRESSURIZE, AIRCRAFT RETURNED TO ORD WHERE IT LANDED SAFELY WITH OUT FURTHER INCIDENT. (NO EMERGENCY WAS DECLARED) **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ACTUATOR — FAULTED (AIR INLET FLAP) · airframe 61,060 hrs · 30,011 cycles

AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF JUST BELOW 80 KIAS FOR MASTER CAUTION FLICKER LIGHT ON OFF VERY QUICKLY NO ASSOCIATED ECAM. MAINTENANCE RAN POST FLIGHT REPORT WITH NO FAULTS NOTED. MAINTENANCE PERFORMED TESTS ON THE FWC, AFS, & LAND AND NORMAL BRAKING SYSTEM WITH NO FAULTS OF THE MASTER CAUTION SYSTEM NOTED. MASTER CAUTION SYSTEM GROUND CHECKS AND TEST NORMAL. MAINTENANCE DID IDENTIFY FAULT CODE 21-61-51 P1 RAM AIR IN ACTUATOR ON THE PFR WHICH THE GMT TIME OF FAULT CORRESPONDS WITH TIME THE TAKE OF WAS REJECTED. MAINTENANCE REPLACED P1 RAM AIR INLET FLAP ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-61-51 AND AMM 21-61-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,253 hrs · 29,567 cycles

AIRCRAFT WAS NOT GROUNDED: AT CRUISE, FLIGHT ATTENDANT REPORTED AFT OVERHEAD EXIT LIGHT ILLUMINATED ALONG WITH DOOR 2LEFT/RIGHT EXIT LIGHTS. TROUBLESHOOT EPSU PER TSM 33-51-00-810-801-A. FAULT EMERGENCY POWER SUPPLY UNIT BATTERY FOUND. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW AMM 323-51-38.

Part: DISPLAY — MALFUNCTIONED (ZONE 200 - FUSE) · airframe 60,032 hrs · 29,460 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW ABORTED TAKE OFF AT 80 KNOTS DUE TO FLEX IN COLUMMN 1 BLANK. MAINTENANCE RESET BOTH FMGCS AND RELOADED FLIGHT PLAN. FMGCS BITE TESTED OK PER AMM 27-96-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 59,271 hrs · 29,053 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) WILL NOT TEST. REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), PER AMM 33-51-38.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 58,324 hrs · 28,423 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY (10WL) FAILED TEST. REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY (10WL) PER AMM 33-51-38.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 58,324 hrs · 28,423 cycles

AIRCRAFT WAS NOT GROUNDED. AFT LEFT EMERGENCY POWER SUPPLY UNIT BATTERY (13WL) FAILED TEST. REPLACED AFT LEFT EMERGENCY POWER SUPPLY UNIT BATTERY (13WL) PER AMM 33-51-38

Part: CONNECTOR — DAMAGED (CABIN) · airframe 58,202 hrs · 28,332 cycles

AIRCRAFT IN BASE MAINTENANCE: ROW 20ABC EMERGENCY LIGHT DOES NOT TURN ON. REPAIRED EMERGENCY LIGHTING LAMP CONNECTOR 5751VC AND OPS CHECKED PER AMM 33-51-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231LF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 232MF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT STRIP AT FR 32 UNDER FLOOR PANEL 231SF. REPLACED FLOOR SUPPORT STRIP PER AMM 53-00-00-400-801A, DWG D53670099 AND SRM 51-31-00-801.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241JF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 251TF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231KF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 251RF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-000-801-A AND AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 252SF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,199 hrs · 28,331 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231SF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: PRESSURE SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 58,056 hrs · 28,251 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL R TK PUMP 1 LO PRESSURE MESSAGE IN CRUISE. TURNED OFF R #1 PUMP. **SUPPLEMENTAL REPORT: REPLACED RIGHT WING #1 PUMP PRESSURE SWITCH PER AMM 28-21-15** (CLOSED)

Part: CHILLER — ODOR (GALLEY) · airframe 56,619 hrs · 27,363 cycles

AIRCRAFT NOT GROUNDED: ELECTRICAL SMELL FROM FWD GALLEY - CHILLER. REMOVED AND REPLACED FWD GALLEY CHILLER IAW AMM 25-34-51-400-001-A. OPERATIONAL TEST IAW AMM 25-34-51 CHECKS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,526 hrs · 27,318 cycles

AIRCRAFT WAS NOT GROUNDED: LENS ON ESCAPE PATH LIGHT SEAT 4C MISSING. MAINTENANCE REPLACED LENS PER STANDARD PRACTICES.

Part: MASTER SWITCH — FAULTY (COCKPIT) · airframe 56,188 hrs · 27,123 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON SHUTDOWN, ENG #1 KEPT RUNNING WITH ENG #1 MASTER SWITCH IN OFF SHUTDOWN ENG #1 WITH FIRE SWITCH REPEAT. MAINTENANCE REMOVED AND REPLACED ENG 1 MASTER SWITCH IAW ESPM 20-45-21.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 56,181 hrs · 27,118 cycles

AIRCRAFT WAS GROUNDED: PILOT DIVERTED TO FPO ON ACCOUNT OF ODOR IN THE COCKPIT. EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED CABIN ODOR INITIAL TROUBLESHOOTING IAW CARD 26L00021001. FOUND NO EVIDENCE OF CABIN ODORS. OPENED UP BOTH ENGINES INSPECTED AREA FOR LEAKS. NO LEAKS CAUSING ODORS. INSPECTED CABIN & E/E BAYS FOR BURNING EQUIPMENT SMELL, NONE NOTED. ALL CHECKS GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 14,779 hrs · 6,830 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER STANDARD PRACTICES.

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: DEFORMATION ON SLIDE RAFT, PASSENGER CREW DOOR 842, AT AFT GALLEY AREA. REPLACED SLIDE RAFT PASSENGER CREW DOOR 842 AT AFT GALLEY AREA PER JOB CARD 26C84252006 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 54,944 hrs · 26,434 cycles

DEFORMATION ON THE PASSENGER DOOR SLIDE. REPLACED THE DOOR SLIDE IAW AMM 26-62-44.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON SIDE BOX BEAM RIGHT HAND FORWARD HOLE OF THE PRESSURE PLATE BRACKET. REPLACED BRACKET PER SRM 51-42-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON SIDE BOX BEAM LEFT HAND FORWARD HOLE OF THE PRESSURE PLATE BRACKET. REPLACED BRACKET PER SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: CYLINDER — NO TEST (PAX DOOR DAMPER) · airframe 54,944 hrs · 26,434 cycles

DURING AN OPERATIONAL TEST OF THE PASSENGER DOOR, SPEED DECREASED AT THE END WHEN THE DOOR OPENED. MAINTENANCE REPLACED THE DOOR DAMPER IAW AMM 52-11-14-400-001-B, STEP 4. ADJUSTMENT AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SUPPORT ANGLE — CRACKED (BULKHEAD) · airframe 54,944 hrs · 26,434 cycles

CRACKED SUPPORT ANGLE ON THE AFT FACE OF THE FORWARD BULKHEAD AT FRAME 46, STRINGER 38L IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 221PF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-06, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 232EF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-06, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

THE FORWARD GALLEY FLOOR PANEL 231FF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-06, AND IRM 9701, REV I.

Part: PLATE — CRACKED (EMERGENCY EXIT) · airframe 54,944 hrs · 26,434 cycles

PLATE FOUND CRACKED ON THE EMERGENCY EXIT DOOR. REPLACED THE PLATE IAW AMM 52-21-11-400-002.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 54,944 hrs · 26,434 cycles

THE AFT GALLEY FLOOR PANEL 216AG DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 231CF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-06, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 231BF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-12-00, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 221EF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-12-00, AND IRM 9701, REV I.

Part: WINDOW — GLAZED (PAX DOOR) · airframe 54,944 hrs · 26,434 cycles

PASSENGER DOOR OUTER WINDOW PANE WAS GLAZED. REPLACED THE WINDOW PANE IAW AMM 56-31-11-400-002-A.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 221DF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-12-00, AND IRM 9701, REV I.

Part: STOP FITTING — GOUGED (FRAME 54) · airframe 54,944 hrs · 26,434 cycles

AFT CARGO DOOR FRAME STOP FITTING WAS GOUGED AT FRAME 54. REPLACED THE STOP FITTING IAW SRM 51-42-11, AND 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 221LF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-12-00, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 54,944 hrs · 26,434 cycles

FORWARD GALLEY FLOOR PANEL 222EF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-12-00, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 232DF IS DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-12-12.

Part: WINDOW — CRAZED (R1 DOOR) · airframe 54,944 hrs · 26,434 cycles

R1 DOOR OUTER WINDOW PANE CRAZED. REPLACED THE WINDOW PANE IAW AMM 56-31-11-400-002-A.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING NR 3 LEADING EDGE SLAT TRACK FORWARD BOLT. REPLACED BOLT PER AMM 27-84-63-400-002-A.

Part: STRUT — CORRODED (LT WING TE FLAP) · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-400-001-A.

Part: STRUT — CORRODED (RT WING TE FLAP) · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE RIGHT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-400-001-A.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE BOX BEAM BRACKET CRACKED AT FR 43 AND -Y1650. REPLACED BRACKET PER EO 5315Y066-001.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BRACKET ON LEFT HAND SIDE BOX BEAM AT FR 43 AND +Y1650. REPLACED BRACKET PER EA 5315Y066-001.

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 AT THE RIGHT HAND SIDE DOOR STOP NR 7 AREA. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: SKIN — SATURATED (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER RIGHT HAND SIDE SURFACE HAS INDICATION OF TRAPPED WATER BETWEEN BEARINGS 6 AND 7 AROUND THE HOIST POINT. REPAIRED RUDDER LEFT HAND SIDE SKIN PER SRM 55-41-13-300-029.

Part: SKIN — SATURATED (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER LEFT HAND SIDE SURFACE HAS INDICATION OF TRAPPED WATER BETWEEN BEARINGS 6 AND 7 AROUND THE HOIST POINT. REPAIRED RUDDER LEFT HAND SIDE SKIN PER SRM 55-41-13-300-029.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 66 AND 68, -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE ARM NR 7 ON THE VERTICAL STABILIZER HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE ARM PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-67) · corrosion level 2 · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 64 AND 67, -Y464.8. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 66) · corrosion level 2 · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 66, -Y1162.5. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE RIGHT AFT DOOR FRAME LOWER SILL BETWEEN FRAMES 66 AND 68. REPAIRED THE DOOR SILL IAW SRM 53-41-14-300-001, FIGURE 20101.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 54,944 hrs · 26,434 cycles

CORROSION FOUND ON THE LEFT AFT LOWER DOOR SILL, FRAME 68 AND STRINGER 23L. REPAIRED THE LOWER DOOR SILL IAW SRM 53-41-14-300-001.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 54,944 hrs · 26,434 cycles

RIGHT ELEVATOR UPPER AND LOWER SKINS HAD INDICATIONS OF TRAPPED WATER IN SEVERAL LOCATIONS. REPLACED THE ELEVATOR IAW SRM 55-21-11-283-004.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

RUDDER NR 3 HINGE ARM, RIB 5 WAS WORN. REPLACED HINGE ARM IAW SRM 51-72-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 288333.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

RUDDER HINGE ARM NR 4 HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE ARM IAW SRM 51-72-11.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE ARM NR 5 ON THE VERTICAL STABILIZER HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE ARM PER SRM 51-72-11.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE ARM #2 ON THE VERTICAL STABILIZER HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE ARM PER SRM 51-72-11.

Part: HINGE ARM — WORN (RUDDER) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE ARM NR 1 ON THE VERTICAL STABILIZER HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE ARM PER SRM 51-72-11.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 54,944 hrs · 26,434 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE PANEL AT FR 36 AND Y1292. REPAIRED PRESSURE PANEL PER EO 5316Y209-001.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 54,732 hrs · 26,303 cycles

SEAT EMERGENCY LIGHT AT THE L3 WAS INOPERATIVE. MAINTENANCE SEATED THE ELECTRICAL CONNECTOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 54,215 hrs · 25,961 cycles

EMERGENCY FLASHLIGHT DAMAGED AT THE R2 DOOR AREA. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: PLUG — LEAKING (APU) · airframe 53,577 hrs · 25,565 cycles

FLIGHT ATTENDANT REPORTED AN ODOR IN THE CABIN. ACCOMPLISHED SMOKE ODOR FUMES TROUBLESHOOTING IAW J/C 26L00021001, AND SMOKE ODOR FUMES TROUBLESHOOTING IAW J/C 26L00021002. FOUND FACTORY LOCKED PLUG LEAKING. THE AIRCRAFT WAS GROUNDED. REPLACED THE APU IAW J/C 26L31049003.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 53,032 hrs · 25,246 cycles

L2 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE CYLINDER IAW AMM 52-13-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 53,032 hrs · 25,246 cycles

R2 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-13-00.

Part: HINGE PIN — LOOSE (JUMP SEAT) · airframe 52,685 hrs · 25,041 cycles

AFT FLIGHT ATTENDANT JUMPSEAT, AT THE L2 DOOR CONTINUES TO FALL OPEN EXPOSING EMERGENCY EQUIPMENT AND BLOCKS THE L2 EMERGENCY EXIT. REINSTALLED THE HINGE PIN ON THE JUMPSEAT DOOR. OPERATES NORMAL. OK FOR SERVICE.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 52,246 hrs · 24,799 cycles

AIRCRAFT NOT GROUNDED. AIRCRAFT RIGHT SIDE OVER WING EMERGENCY EXIT COVER FELL OFF. REINSTALLED SLIDE ARM COVER PER AMM 52-73-21.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 52,246 hrs · 24,799 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT AFT EXIT DOOR (2R) SLIDE COVER LOOSE. SECURED R2 DOOR SLIDE COVER.

Part: COVER — UNSECURE (R2 DOOR) · airframe 52,236 hrs · 24,793 cycles

AIRCRAFT NOT GROUNDED. 2R SLIDE PACK COVER IS LOOSE AND FALLS OFF DOOR. RESECURED 2R SLIDE PACK COVER.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 51,991 hrs · 24,652 cycles

L4 DOOR ASSIST BOTTLE PRESSURE 1100 PSI. SERVICED THE DOOR ASSIST BOTTLE IAW AMM .

Part: DOOR — UNSECURE (ESCAPE ROPE) · airframe 51,340 hrs · 24,269 cycles

ESCAPE ROPE DOOR OVER CAPTAIN WILL NOT STAY SECURE. INSTALLED ESCAPE ROPE DOOR. OK FOR SERVICE.

Part: BLEED AIR SYS — FUMES (APU) · airframe 51,047 hrs · 24,138 cycles

AIRCRAFT WAS GROUNDED. FUMES REPORTED IN CABIN AND COCKPIT. ITEM DEFERRED FOR FERRY TO CLT. MAINTENANCE FOUND SOURCE TO BE APU BLEED. ACCOMPLISHED JOB CARDS; CABIN AIR QUALITY, APU SMELL IN CABIN AND ECS DECONTAMINATION

Part: GIRT BAR — OBSTRUCTED (L2 DOOR SLIDE) · airframe 50,973 hrs · 24,101 cycles

L2 DOOR WILL NOT SHOW THE SLIDE IS ARMED. REMOVED DEBRIS FROM GIRT BAR FLOOR FITTING.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 50,927 hrs · 24,070 cycles

R2 SLIDE COVER LOOSE. SECURED THE SLIDE COVER. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (AFT PAX DOOR) · airframe 50,889 hrs · 24,049 cycles

AFT LT PASSENGER DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED ASSIST BOTTLE TO NORMAL PRESSURE IAW AMM 52-11-14.

Part: LENS — MISSING (CABIN) · airframe 50,662 hrs · 23,923 cycles

AIRCRAFT NOT GROUNDED. SEAT 3C EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT LENS SEAT 3C IAW AMM 33-50-00.

Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT) · airframe 50,132 hrs · 23,620 cycles

CAPTAIN`S SLIDING WINDOW DIFFICULT TO OPEN, DOES NOT SLIDE SMOOTHLY. LUBE THE SLIDING WINDOW. SLIDING WINDOW OPEN AND CLOSES GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 50,132 hrs · 23,620 cycles

EXIT COVER BY THE L1 DOOR IS OFF. REPLACED EXIT COVER BY 1L DOOR.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 49,518 hrs · 23,277 cycles

LIGHT BY BOTTOM OF 1R DOOR IS MISSING A LENS COVER. REPLACED LENS IAW AMM 33-51-00. AIRCRAFT WAS GROUNDED.

Part: AILERON — DAMAGED (LT WING) · airframe 49,373 hrs · 23,179 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT WING AILERON, PREVIOUS REPAIR ON LOWER SURFACE DAMAGED. CAME APART 2 INCHES FROM LEADING EDGE AND 16 INCHES FROM INBOARD END. REPAIRED AILERON PER EA 254027A.

Part: O-RING — LEAKING (APU OIL SYS) · airframe 49,238 hrs · 23,085 cycles

DIRTY SOCKS ODOR THROUGH OUT CABIN RECORDED BY CREW WITH APU ON PACKS ON. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND OIL LEAK AT APU FUEL CONTROL UNIT. REMOVED AND REPLACED O-RING IAW AMM 49-32-11.

Part: CONTROL VALVE — LEAKING (NR 2 ENGINE) · airframe 49,050 hrs · 22,977 cycles

AIRCRAFT WAS GROUNDED, DURING TAXIOUT A TRAILING ACFT REPORTED FUEL LEAKING FROM NR 2 ENGINE COWL. MAINTENANCE LOOKED AT LEAK AND CONFIRMED SIGNIFICANT FUEL LEAK. MAINTENANCE R & R E2 HP TURBINE CLEARANCE CONTROL VALVE IAW AMM 75-21-10.

Part: APU — LEAKING (ZONE 100) · airframe 48,873 hrs · 22,865 cycles

FLIGHT CREW REPORTED THAT AT THE GATE, ON ENTERING THE ACFT A STRONG CRAYON ODOR WAS NOTED, ALONG WITH A MILD BURNING OF THE EYES . THE CABIN CREW SHOWED UP 10 MINUTES LATER AND EXPERIENCE SAME ODOR IN CABIN. AIRCRAFT WAS GROUNDED. MAINTENANCE SUSPECTED THE APU IS LEAKING OIL FROM THE TURBINE SHAFT BUT ADDITIONAL TROUBLESHOOTING IS REQUIRED. MAINTENANCE REPLACED APU IAW TASK CARD.

Part: OIL COOLER — LEAKING (APU) · airframe 48,643 hrs · 22,758 cycles

ON ENTERING AIRCRAFT DURING THE BOARDING PROCESS A FLIGHT ATTENDANT AND THE FIRST OFFICER REPORTED DIRTY SOCK ODOR. AIRCRAFT GROUNDED. MAINTENANCE DETERMINED THAT THE CABIN ODOR WAS FROM THE APU BLEED AIR SYSTEM AND SUSPECT THE APU OIL COOLER IS THE SOURCE. CLEANED APU PLENUM AND COMPARTMENT PER JOB CARD 26L00021002, RAN APU NO LEAKS NOTED. PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM PER JOB CARD 26L00021004.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,142 hrs · 22,520 cycles

AIRCRAFT IN BASE MX. EMER POWER SUPPLY 11WL INOPERATIVE. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-001-A.

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · airframe 48,142 hrs · 22,520 cycles

AIRCRAFT IN BASE MX. CORROSION ON LT MLG DOOR FWD HINGE FITTING. REPLACED HINGE FITTING IAW EA 260323 & SRM 51-72-11, SRM 51-42-11 & DWG D53370600.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 48,142 hrs · 22,520 cycles

AIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151GF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 & IRM 9701 REV G.

Part: PUMP — FAULTED (FUEL SYSTEM) · airframe 48,057 hrs · 22,477 cycles

AIRCRAFT WAS NOT GNDED. CTR PUMP NR 1 FAULT. ACCOMPLISHED TSM 28-21-00-810-813-A. OPERATIONAL CHECKED NORMAL. REPLACED CONTACTOR & RELAY 35QA AS A PRECAUTIONARY IAW ESPM 20-46-50. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 48,050 hrs · 22,472 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR HARD TO ARM. FOUND DEBRIS IN FLOOR GIRT BAR CONNECTION. REMOVED DEBRIS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SEAL — LEAKING (APU) · airframe 47,088 hrs · 21,978 cycles

AIRCRAFT WAS NOT GNDED. MUSTY ODOR EMANATES FROM AC SYS, DURING ALL FLIGHT PHASES. USED APU BLEED FOR TAKEOFF. FOUND OIL LEAK IN APU AREA. REPLACED LUBE & SCAVENGE SEALS IAW AMM 49-91-41.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 46,555 hrs · 21,666 cycles

FLIGHT 827 MULTIPLE BIRD STRIKES DURING TAKEOFF AT APPROX V1. SMELL FILLED ACFT & FELT SEVERAL THUMPS FROM BIRD STRIKES. RETURNED & FOUND EVIDENCE OF BIRD STRIKE TO NR 1 ENG. PERFORMED BORESCOPE IAW CARD 26L40072006, WITH NO DEFECTS NOTED.

Part: CONTAINER — DIRTY (GALLEY) · airframe 46,407 hrs · 21,572 cycles

EN-ROUTE, FLIGHT 1832 REPORTED A CABIN ODOR RESEMBLING ROTTEN EGG SMELL. THE ODOR WAS IN THE VICINITY OF 1R DOOR. THE SMELL WAS SO STRONG THAT THE A FLIGHT ATTENDANT WAS PUT ON O2 & THE COCKPIT CREW REQUESTED PARAMEDICS MEET THE ACFT UPON LANDING. ACCOMPLISHED JC 26L00021001, TROUBLE SHOT CABIN AIR QUALITY. RAN ENGS & APU, BOTH PACKS, CHECKED GALLEY, GALLEY EQUIPMENT & LAVATORY, NO FAULTS OR ODORS NOTED. GALLEY TRASH REMOVED & CLEANED BY CONTRACT UTILITY, NO 30 DAY HISTORY. OK FOR CONTINUED SERVICE.

Part: HINGE FITTING — WORN (THRUST REVERSER) · airframe 46,193 hrs · 21,455 cycles

NUMBER 1 ENG INBD THRUST REVERSER AFT HINGE BEARING LOOSE & ROTATES IN THE HINGE FITTING. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.

Part: HINGE FITTING — WORN (THRUST REVERSER) · airframe 46,193 hrs · 21,455 cycles

NUMBER 1 ENG INBD THRUST REVERSER MIDDLE HINGE BEARING LOOSE & ROTATES IN THE HINGE FITTING. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 45,514 hrs · 21,103 cycles

AFT MEGA PHONE INOPERATIVE. REPLACED THE AFT MEGA PHONE.

Part: SLIDE — NO TEST · airframe 45,428 hrs · 21,057 cycles

CIDS PANEL GIVES FAULT EPSU EXTERNAL LOAD AFT L. R & R THE RT AFT SLIDE & RAFT ASSEMBLY.

Part: WIRE HARNESS — BURNED (ZONE 700) · airframe 44,791 hrs · 20,711 cycles

AFTER TAKEOFF GOT AUTO BRAKE FAULT, ACCOMPANIED BY BRAKE RELEASE MSG. FOUND BRAKE FAN WIRING BURNED THROUGH THE CONDUIT OF 2M HARNESS & NR 1 WHEEL TACH WIRING ALSO BURNED. REPLACED DAMAGED WIRING IAW AMM SUPPLEMENTAL INFO 32-11-43-000-001-A.

Part: BLADE — OUT OF BALANCE (ENGINE) · airframe 44,110 hrs · 20,331 cycles

STRONG VIBRATION FELT THROUGHOUT ACFT, BUT STRONGEST IN AFT SECTION. ENG 1 & 2 VIBRATION NO MORE THAN 1.2 TO 1.4 INCHES CRUISE & 2.8 INCHES DECENT. ACCOMPLISHED JOB CARD 26T00027006 ELEVATOR SERVO CONTROLS & HINGE BEARINGS FOR PLAY. SPICED SEAL IN PANEL 197GB LT SIDE IAW AMM 53-35-13. ACCCOMPLISHED FAN TRIM BALANCE, IAW A320 AMM 77-32-34-860-043-A AND 77-32-34-750-001-A. PRIOR TO BALANCE THE RUMBLE AND VIBRATION WAS DUPLICATED. AFTER BALANCE NO RUMBLE OR VIB. NOTED, REF LP 8745028.

Part: LENS — MISSING (CABIN) · airframe 43,734 hrs · 20,116 cycles

DOOR 2R EMER LIGHT LENS COVER MISSING AT TOP OF DOOR. REPLACED DOOR 2R EMER LIGHT LENS COVER ABOVE DOOR IAW AMM 33-51-01.

Part: COVER — MISSING (CABIN) · airframe 43,650 hrs · 20,073 cycles

CREW REPORTED ROW 24 EMER FLOOR LIGHTING COVER BROKEN & MISSING. REPLACED COVER, OK FOR SERVICE.

Part: BYPASS VALVE — LEAKING (NLG DOOR) · airframe 43,611 hrs · 20,048 cycles

AIRCRAFT RETURNED AFTER IT LOST HYD GREEN SYS AT APPROX ALT OF 8000'. FOUND NLG DOOR GND OPENING BYPASS VLV WAS LEAKING. REPLACED BYPASS VLV IAW AMM 32-31-15-000-001-A. AS PRECAUTIONARY, REPLACED NR 1 ENG GREEN SYS HYD PUMP IAW AMM 29-11-51-00-041-A & REPLACED ASSOCIATED FILTERS.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 42,750 hrs · 19,683 cycles

THE RT AFT PAX DOOR ASSIST BOTTLE LOW PRESS. SERVICED RT AFT PAX DOOR ASSIST BOTTLE IAW AMM 52-10-00-614.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 42,546 hrs · 19,572 cycles

DOOR 2L SLIDE STICKING OUT BLOCKING TRASH BIN FROM REMOVAL. REPLACED DOOR 2L DOOR SLIDE IAW JOB CARD 26L00025011.

Part: LENS — MISSING (CABIN) · airframe 41,659 hrs · 19,123 cycles

EMERGENCY LIGHT LENS MISSING IN AFT RT GALLEY. INSTALLED EMERGENCY LIGHT LENS IN AFT RT GALLEY.

Part: FAN — FAILED (CABIN AIR) · airframe 41,067 hrs · 18,786 cycles

INFLIGHT VIBRATION FELT IN COCKPIT PLUS ELECTRICIAL ODOR. THOUGH AIR CONDITIONING SYS ALSO REPORTED BY F/A IN CABIN. DESCENDED AND VIBRATION, ODOR GONE, 10 MIN LATER SAME CONDITION, DIVERTED. DURING DESCENT GOT ECAM TO SECURE BLOWER FAN, DID SO, NO VIBRATION OR ODOR. R & R AVIONICS VENT BLOWER FAN. FAN SENT TO ENGINEERING FOR INVESTIGATION. SUP: WILL BE FILED UPON DETERMINATION OF FAILURE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 40,506 hrs · 18,441 cycles

F/A REPORTS ACFT LEFT FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: LENS — MISSING (CABIN) · airframe 40,252 hrs · 18,292 cycles

FLOOR LEVEL EMERGENCY LIGHT AT L1 DOOR MISSING LENS. INSTALLED NEW LENS AT L1 DOOR FLOOR LEVEL EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 40,198 hrs · 18,261 cycles

1R DOOR FLOOR LEVEL EXIT PATH EMERGENCY LIGHT COVER MISSING. REPLACED MISSING COVER AT 1R DOOR.

Part: CHILLER — FAULTY (GALLEY) · airframe 38,832 hrs · 17,579 cycles

FLIGHT ATTENDANT REPORTED FORWARD GALLEY CHILLER NOT COOLING AND HAS METALLIC ODOR. REMOVED AND REPLACED CHILLER.

Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK IN ANGLE BRACKET AT OVERWING EMERGENCY EXIT DOOR 834 INTERNAL AREA BETWEEN FR39 TO FR41, (BEAM 1). REPLACED ANGLE BRACKET AT OVERWING EMERGENCY EXIT DOOR 834 INTERNAL AREA IAW A320 SRM 51-72-11.

Part: STRIKER — OUT OF ADJUST (R1 DOOR) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - R1 DOOR (842) DAMPER/EMERGENCY ASSIST DIMENSION "A" BETWEEN FINGER AND STRIKER LEVER IS OUT OF ADJUSTMENT. ADJUSTED DIMENSION IAW AMM 52-13-14-820-002-A PROCEDURE 3.D STEP 4.A.

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AT FR42. REPLACED LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AT FR42 IAW A320 CMM 52-81-18-400-809-A01.

Part: SLIDE — MISRIGGED (CABIN) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - BALL LOCK PINS ARE NOT FLUSH WITH THE OUTER SURFACE OF THE BALL LOCK MECHNISM ON THE RIGHT OFFWING ESCAPE SLIDE. REPACKED RIGHT OFFWING SLIDE IAW A320 CMM 25-60-58 REV 19 & FOLDING PROCEDURES P-11907 REV R & CHECKED THAT BALL PINS ARE FLUSH WITH THE OUTER SURFACE OF THE BALL LOCK MECHNISM.

Part: SLIDE — MISRIGGED (CABIN) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - BALL LOCK PINS ARE NOT FLUSH WITH THE OUTER SURFACE OF THE BALL LOCK MECHNISM ON THE LEFT OFFWING ESCAPE SLIDE. REPACKED LEFT OFFWING SLIDE IAW A320 CMM 25-60-58 REV 19 & FOLDING PROCEDURES P-11907 REV R & CHECKED THAT BALL PINS ARE FLUSH WITH THE OUTER SURFACE OF THE BALL LOCK MECHNISM.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR 640LB BETWEEN WS 70 TO WS 141 & BETWEEN RIB 8 TO RIB 11. REPLACED RIGHT WING FUEL DOOR 640LB IAW A320 AMM 57-27-11-400-002-A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF LOWER RIGHT WING FUEL DOOR PANEL 640NB BETWEEN WS 970 TO WS 1020 & BETWEEN S8R TO S11R. REPLACED LOWER RIGHT WING FUEL DOOR PANEL 640NB IAW A320 AMM 57-27-11-400-002-A.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER LEFT WING FUEL ACCESS DOOR 540JB BETWEEN WS 779 TO WS 827, BETWEEN S8L & S11L & BETWEEN RIB 14 TO RIB 15. REPLACED LOWER LEFT WING FUEL ACCESS DOOR 540JB IAW A320 AMM 57-27-11-400-002-A.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR 640JB BETWEEN WS 779 TO WS 827 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640JB IAW A320 AMM 57-27-11-400-002-A.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR 640AB BETWEEN WS 70 TO WS 141 & BETWEEN RIB 2 TO RIB 3. REPLACED RIGHT WING FUEL DOOR 640AB IAW A320 AMM 57-27-11-400-001-A.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER LEFT WING FUEL ACCESS DOOR 540LB BETWEEN WS 874 TO WS 924 & BETWEEN RIB 16 TO RIB 17. REPLACED LOWER LEFT WING FUEL ACCESS DOOR 540LB IAW A320 AMM 57-27-11-400-002-A.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR 640HB BETWEEN WS 732 TO WS 779 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640HB IAW A320 AMM 57-27-11-400-002-A.

Part: FUEL DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL DOOR 640QB BETWEEN WS 1073 TO WS 1120 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640QB IAW A320 AMM 57-27-11-400-002-A.

Part: FUEL DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL DOOR 540HB BETWEEN WS 670 TO WS 732 & BETWEEN RIB 12 TO RIB 13 .REPLACED LEFT WING FUEL DOOR 540HB IAW A320 AMM 57-27-11-400-002-A.

Part: STRIKER — OUT OF ADJUST (L2 DOOR) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - L2 DOOR (832) DAMPER/EMERGENCY ASSIST DIMENSION "A" BETWEEN FINGER AND STRIKER LEVER IS OUT OF ADJUSTMENT. ADJUSTED DIMENSION IAW AMM 52-13-14-820-002-A STEP 4.A.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 252EF BETWEEN FR47 TO FR51 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 252EF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.

Part: STRUT — CORRODED (TE FLAP) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9 IAW A320 AMM 27-51-44-400-001-A.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232PF BETWEEN FR24 TO FR28 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232PF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK ON SEGMENT ANGLE AT OVERWING EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 ALSO BETWEEN BEAM NR 1 TO BEAM NR 3. REPLACED SEGMENT ANGLE AT OVERWING EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.

Part: STRUT — CORRODED (TE FLAP) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON LEFT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED LEFT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9 IAW A320 AMM 27-51-44-400-001-A.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK ON SEGMENT ANGLE OF OVERWING EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM NR 1 TO BEAM NR 3. REPLACED SEGMENT ANGLE OF OVERWING EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 251GF BETWEEN FR51 TO FR54 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251GF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232XF BETWEEN FR32 TO FR35 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 232XF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L & S42L. REPAIRED FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L & S42L IAW EA 504554.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK ON SEGMENT ANGLE OF OVERWING EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM NR 1 TO BEAM NR 3. REPLACED SEGMENT ANGLE OF OVERWING EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK ON SEGMENT ANGLE AT OVERWING EMERGENCY EXIT DOOR 843 BETWEEN FR 38 TP FR 39 & BETWEEN BEAM NR 1 TO BEAM NR 3. REPLACED SEGMENT ANGLE AT OVERWING EMERGENCY EXIT DOOR 843 IAW EO 5210Y228.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL (CENTER FITTING) AT AFT PASSENGER/CREW DOORWAY BETWEEN FR66 TO FR68, S23R. REPLACED SHAPE SILL AT AFT PASSENGER/CREW DOORWAY BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: FLAP — CORRODED (LT WING) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION AT 2 POINTS ON INTERNAL AREA BETWEEN INNER RIB & OUTBOARD RIB 14 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.

Part: SKIN — WORN (SLAT TRACK) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - WORN AREA INTERNAL LOWER SKIN OF SLAT TRACK NR 5 AT SLAT NR 2 BETWEEN WS 486 TO WS 670 OF RIGHT WING. REPAIRED RIGHT WING LOWER SKIN OF SLAT TRACK NR 5 AT SLAT NR 2 BETWEEN WS 486 TO WS 670 IAW A320 EA 503633.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT AFT PASSENGER/CREW DOORWAY AT FR68, S23R. REPLACED CORNER FITTING AT AFT PASSENGER/CREW DOORWAY AT FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK IN WEB OF FLIGHT COMPARTMENT FLOOR STRUCTURE BETWEEN FR8 TO FR11, S23R, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, S23R, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53113322.

Part: RIB — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION AT 6 POINTS ON INTERNAL AREA OF OUTBOARD FACE OF RIB 15 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CRACK ON WEB AT FLIGHT COMPARTMENT FLOOR STRUCTURE AREA BETWEEN FR8 TO FR11, Y765. REPLACED FLIGHT COMPARTMENT FLOOR STRUCTURE WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110285.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1732 TO Y1292. REPLACED FLOOR PANEL 231FF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16 & BETWEEN Y254 TO Y1732. REPLACED FLOOR PANEL 221PF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR21 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 221DF IAW A320 SRM 53-12-00 FIG 206 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 242LF BETWEEN FR42 TO FR47 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 242LF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701 REV G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON L1 DOOR CENTER FITTING BETWEEN FR16 TO FR20, S23R. REPLACED L1 DOOR CENTER FITTING BETWEEN FR16 TO FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO Y1732. REPLACED FLOOR PANEL 261BG IAW A320 SRM 53-02-00 FIG 209, EA 503641 & IRM 9701, REV G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT FORWARD PASSENGER/CREW DOORWAY BETWEEN FR16 TO FR20, S23L. REPLACED CENTER FITTING AT FORWARD PASSENGER/CREW DOORWAY BETWEEN FR16 TO FR20, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y254 TO -Y1732. REPLACED FLOOR PANEL 262BG IAW A320 SRM 53-02-00 F209, EA 503642/504555A & MCGILL IRM 9701 REV G.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, -Y1292. REPLACED COUPLING AT FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, -Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, Y1292 IAW A320 SRM 51-72-11, 53-41-15, AIRBUS DRAWING D53472176 & D53472831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A320 SRM 51-42-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47 TO FR64, Y765. REPLACED SEAT RAIL BETWEEN FR47 TO FR64, Y765 IAW A320 SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR26 BETWEEN S41L TO S42L. REPLACED CLEAT AT FR26 BETWEEN S41L TO S42L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53230829.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47 TO FR64, -Y765. REPLACED SEAT RAIL BETWEEN FR47 TO FR64, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION CORNER FITTING AT FORWARD CARGO DOORWAY AT FR28, S38R. REPLACED CORNER FITTING AT FORWARD CARGO DOORWAY AT FR28, S38R IAW A320 SRM 51-72-11 & EA 503689.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - 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 & AIRBUS DRAWING D53231730.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC 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 & D53110920.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, -Y1292. REPLACED COUPLING AT FR64, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472831.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR52 TO FR56 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW A320 SRM 53-02-00 FIG 209, IRM 9701, REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 53-72-11 & AIRBUS DRAWING D53110920 & D53112812.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151DF BETWEEN FR49 TO FR53 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151DF IAW A320 SRM 53-02-00 FIG 209 & IRM 9701, REV G.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,782 hrs · 17,553 cycles

2S CHECK - LEVEL 2 FILFORM CORROSION ON FLOOR STRUCTURE WEB BETWEEN FR12 TO FR16, Y1732. REPLACED FLOOR STRUCTURE WEB BETWEEN FR12 TO FR16, Y1732 IAW A320 SRM 51-72-11 EA 503659 & AIRBUS DRAWING D53114392.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE ARM END FITTING NR 7 AT FORK END AT VERTICAL STABILIZER STA 561, RIB 11. REPLACED RUDDER HINGE ARM END FITTING NR 7 IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON R1 DOOR LOWER SILL FITTING BETWEEN FR16 TO FR20, -Y1732. REPLACED R1 DOOR LOWER SILL FITTING BETWEEN FR16 TO FR20, -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110339.

Part: SILL — CORRODED (FUSELAGE) · airframe 38,782 hrs · 17,553 cycles

2S CHECK - CORROSION ON R2 DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732. REPAIRED R2 DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53480505, D53480076 & EA 503612.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 37,780 hrs · 16,964 cycles

L2 DOOR ASSIST BOTTLE PRESSURE BELOW 1300 PSI. SERVICED L2 DOOR ASSIST BOTTLE TO 1850 PSI.

Part: LENS — MISSING (CABIN) · airframe 37,525 hrs · 16,839 cycles

R2 DOOR LOWER EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT LENS ON R-2 DOOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,752 hrs · 16,419 cycles

EMERGENCY FLASHLIGHT BATTERY DEAD ON REAR RT FLIGHT ATTENDANT SEAT AND REAR SWING F/A SEAT. REMOVED AND REPLACED BATTERIES IN EMERGENCY FLASHLIGHTS.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL # 232DF BETWEEN FR12 TO FR16, Z-500, -Y510. REPLACED FLOOR PANEL # 232DF IAW JOB CARD # 26C22053014 & IRM 9701.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Z-500, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Z-500, -Y765 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69.6, Z-500, -Y1292. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69.6, Z-500, -Y1292 IAW A320 SRM 51-72-11 & TYPICAL REPAIR # TR320-2528-10-0011C.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - SHEAR PLATE CRACKED BETWEEN FR68 TO FR69, Z-500, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, Z-500, -Y1162.5 IAW A320 SRM 53-41-14, 51-21-11, 51-23-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y254 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A320 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL # 221DF BETWEEN FR16 TO FR20, Z-500, Y=0. REPLACED FLOOR PANEL # 221DF IAW IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK FLOORBEAM AT FR64, Z-500, -Y765. REPLACED SEAT TRACK FLOORBEAM AT FR64, Z-500, -Y765 IAW A320 SRM 51-72-11 & EA # 201988.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, Z-500 & BETWEEN -Y1162.5 TO -Y1292. REPLACED SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, Z-500 & BETWEEN -Y1162.5 TO -Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, Z-500, -Y765. REPLACED FLOORBEAM AT FR20, Z-500, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING # D53112807.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, -Y254 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y765 IAW A320 SRM 53-41-15 FIG 102 & # EA 201988.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+4 INCHES TO FR68-4 INCHES. REPLACED SHAPE SILL BETWEEN FR66+4 INCHES TO FR68-4 INCHES IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68-6 INCHES TO FR69+4 INCHES, Z-500, Y1162.5. REPLACED FLOORBEAM BETWEEN FR68-6 INCHES TO FR69+4 INCHES, Z-500, Y1162.5 IAW A320 SRM 51-42-11, 51-72-11 & EA # 201988.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON DOOR SILL AT FR66, Z-500, Y1589. REPLACED DOOR SILL AT FR66, Z-500, Y1589 IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Z-500, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Z-500, Y765 IAW A320 SRM 53-41-15 FIG 102 & # EA 201988.

Part: COVER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11/SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON JOINT COVER BETWEEN FR12 TO FR14, -Y81, -Z500. REPLACED JOINT COVER BETWEEN FR12 TO FR14, -Y81, -Z500 IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67.5, Z-500, Y512.5. REPLACED FLOORBEAM BETWEEN FR64 TO FR67.5, Z-500, Y512.5 IAW A320 SRM 51-42-11, 51-43-11 & EA # 201988.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-BEAM BETWEEN FR66.6 TO FR68.6, Z-500 & BETWEEN Y1162.5 TO Y1292. REPLACED Z-BEAM BETWEEN FR66.6 TO FR68.6, Z-500 & BETWEEN Y1162.5 TO Y1292 IAW A320 SRM 53-41, 51-42-11, 51-72-11 & EA # 201988.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM APPROX 1 INCH FORWARD OF FR16, Z-500, Y503.2. REPLACED FLOORBEAM AT FR16, Z-500, Y503.2 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y1292 IAW A320 SRM 51-42-11 & 51-21-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, -Y1162.5 IAW A320 SRM 53-41-14 FIG 2 ITEM 15A & TYPICAL REPAIR # TR320-2528-10-0011C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, Z-500, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, Z-500, -Y189 IAW A320 SRM 51-72-11 & 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL PLATE AT FR68, Z-500, -Y1292. REPAIRED R2 DOOR SILL PLATE AT FR68, Z-500, -Y1292 IAW A320 EA 201968.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, Z-500, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Z-500, -Y81 IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y464.8. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y464.8 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66, -Y765 IAW A320 SRM 53-00-14 FIG 102, 51-72-11 & EA # 201988.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Z-500, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Z-500, -Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, Z-500, Y1292 IAW A320 SRM 51-42-11 & 51-44-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Z-500, -Y1292.5. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Z-500, -Y1292 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 16,406 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL AT FR66, Z-500, -Y1589. REPLACED DOOR SILL AT FR66, Z-500, -Y1589 IAW A320 EA 201968 & A320 SRM 53-41-14.

Part: BALL LOCK — OBSTRUCTED (EVAC SLIDE) · airframe 36,339 hrs · 16,203 cycles

NEW OVERHAULED SLIDE ARRIVED FROM VENDOR WITH ENCLOSURE BALL LOCKS PAINTED OVER RENDERING SLIDE UNSERVICEABLE. MAINTENANCE ACCOMPLISHED E/O #2508Y025 PAINT REMOVAL FROM THE OVERWING SLIDE ENCLOSURE BALL LOCKS MAKING SLIDE SERVICEABLE AGAIN.

Part: MECHANISM — OBSTRUCTED (GIRT BAR) · airframe 35,669 hrs · 15,832 cycles

CREW REPORTED FORWARD SERVICE DOOR ARMING HANDLE BINDS IN THE ARMING PROCESS. MAINTENANCE CLEARED DEBRIS FROM GIRT BAR ATTATCH MECHANISM.

Part: UPLOCK — STUCK (NLG DOOR) · airframe 34,923 hrs · 15,460 cycles

LOUDER THAN USUAL WIND NOISE THAT APPEARED TO BE COMING FROM NOSE GEAR OR RADOME AREA AT ALL ALTITUDES AND AIRSPEEDS OVER 220 KTS. DURING LATTER STAGE OF FLIGHT, NOTICED AMBER X'S AT NOSE GEAR DOOR POSITION INDICATOR. FOUND NLG DOOR UPLOCK STUCK IN CLOSED POSITION NOT ALLOWING DOORS TO FULLY CLOSE. REMOVED AND REPLACED NLG DOOR UPLOCK ASSEMBLY PER AIRBUS MAINTENANCE MANUAL 32-31-14.

Part: LENS — MISSING (CABIN) · airframe 31,554 hrs · 13,835 cycles

LOG PAGE 4662621 - FLT 894-ATL - EEL - EMERGENCY LIGHT LENS MISSING RT FORWARD OVERWING EXIT. MAINTENANCE INSTALLED EMERGENCY LIGHT LENS RT FORWARD OVERWING EXIT.

Part: LENS — MISSING (CABIN) · airframe 29,089 hrs · 12,652 cycles

FLT 958 - ORD - EEL - LENS FOR R2 DOOR LOWER EMERGENCY EXIT LIGHT MISSING. REPLACED MISSING LENS IAW AIRBUS MAINTENANCE MANUAL 33-51-13-04-400-001.

Part: O-RING — LEAKING (BRAKE SYSTEM) · airframe 28,792 hrs · 12,536 cycles

FLT 977 CLT-PDX - RETURN TO FIELD - CREW REPORTED LOSS OF YELLOW HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED O-RING ON BRAKE AUTOMATIC SELECTOR 2576GM. SERVICED SYSTEM AND OPERATED WITH NO LEAKS NOTED.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 27,814 hrs · 12,112 cycles

LOG PAGE 4260655 FLT NR 1723 CLT-FLL EMERGENCY EQUIPMENT L2 DOOR ASSIST LOW PRESSURE. MX SERVICED THE L2 DOOR ASSIST BOTTLE PER AIRBUS MM 52-10-00-614-001.

Part: DIAPHRAGM — DEFECTIVE (R2 DOOR) · airframe 24,723 hrs · 10,890 cycles

FLT 9225 - MBJ-CLT - R2 DOOR WOULD NOT MOVE WITH NORMAL PRESSURE. MAINTENANCE REPLACED THE DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE RIGHT AFT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. DOOR OPERATION NORMAL.

Part: NONE — ODOR (CABIN)

FLIGHT 103, CLT-MSY, RUBBER ODOR FROM ROW 6 AFTER, NEVER DISSIPATED FOR ENTIRE FLIGHT. MAINTENANCE CREW RAN SYSTEM ON APU AND ENGINES, ISOLATED PROBLEM TO RIGHT PACK. RELEASED PER MEL. RAN BOTH PACKS, AND COULDN'T DUPLICATE BURNING ODOR. CABIN DOES HAVE A NEW INTERIOR ODOR. REMOVED MEL 21-5201A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND FLOORBEAM CORRODED Y1292 STA 66 - 68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15, DWG D53474180; CORROSION TASK JA-260-53500, DEFECT SIZE: 2" BY 60" BY .100".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND CORROSION FLOORBEAM AT Y1292 LEFT FRAME 66-68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 AREAS - 1" DIA AND 1" BY 2".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND FLOORBEAM CORRODED -Y1292 STA 66 - 68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15, DWG 53474180, DEFECT SIZE: 2" BY 60" BY .100".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND CORROSION ON BEAM AT -Y254 C18 AND C16. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1-1/2" BY 1-1/2" BY .040".

Part: SEAT TRACK — CORRODED (BS 254) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND TRACK CORRODED Y254 AT 16 TRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; CORRODED TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2" BY 2" BY .100".

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND RT SHEAR TIE PLATE AT STA 69 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; TASK NR JA-260-53500, DEFECT SIZE: 1/4" BY 1/4" BY 1/4".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND FLOORBEAM CORRODED 2 AREAS, AT Y 1292 LEFT FRAME 66 - 68. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 2; TASK JA-260-53500, DEFECT SIZE: 1" DIAMETER AND 1" AND 2".

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND CORROSION RT AFT DOOR SILL STA 66. CUT OUT AND INSTALLED ANGLES PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1/4" BY 1/4" BY .090".

Part: SILL — CORRODED (BS 66) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND CORROSION STA 66 LT AFT DOOR SILL. CUT OUT, PUT IN FILLER PER SRM 53-41-00 REP. 06; CORROSION LEVEL 1, TASK JA-260-53500, DEFECT SIZE: 1" BY 4".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,169 hrs · 18,169 cycles

FOUND FLOORBEAM CORRODED, TOP SIDE. REPLACED FLOORBEAM PER SRM 51-72-11L, CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1" BY 1".

Part: EPSU — FAULTY (EMERGENCY LIGHT)

PHL - THE EMERGENCY LIGHTS FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE MIDDLE, RIGHT EMERGENCY POWER SUPPLY UNIT (FIN 12WL). OPERATIONALLY CHECKS OK.

Part: SLIDE — UNSECURE (L1 DOOR)

THE L1 DOOR SLIDE BECAME PARTIALLY UNSTOWED DURING THE CLOSING OF THE DOOR. MAINTENANCE REMOVED AND THEN INSTALLED THE SAME GIRT BAR. OPERATIONAL CHECKS NORMAL.

Part: EPSU — FAULTY (EMERGENCY LIGHT)

PIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: EPSU — FAULTY (EMERGENCY LIGHT)

PIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT AND BATTERIES. OPERATIONALLY CHECKS OK.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT)

PHL - THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT WAS FAULTING DURING TEST. MAINTENANCE REPLACED THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. (M)

Part: SLIDE — DESTROYED (PAX DOOR)

THE RT FORWARD SLIDE FELL APART WHEN COVER WAS REMOVED. MAINTENANCE REPLACED THE ESCAPE SLIDE. OK FOR SERVICE. (M)

Part: DOOR — STUCK (COCKPIT)

CLT - FLT 654 - EN ROUTE AUA-PHL, WHILE IN FLIGHT, THE COCKPIT DOOR WOULD NOT OPEN. THE CIRCUIT BREAKER CONTROLLING THE COCKPIT DOOR LOCKS WAS PULLED, HOWEVER, THE DOOR STILL REMAINED STUCK CLOSED. A CREW MEMBER THEN TRIED TO EXIT THE COCKPIT THROUGH THE EMERGENCY EGRESS PANEL. THE QUICK RELEASE PINS FOR THE PANEL WERE REMOVED, BUT THE PANEL WOULD NOT RELEASE. THE CREW DECIDED TO DIVERT TO CLT WHERE REPAIRS COULD BE MADE. MAINTENANCE TRIMMED .125 INCH OF MATERIAL FROM ALONG THE LOWER EDGE OF ALL THREE COVER PLATE SLOTS FOR THE LATCH TENONS OF THE COCKPIT DOOR. SYSTEM OPERATIONALLY CHECKS OK. THE EMERGENCY EGRESS PANEL WAS FOUND TO TAKE SOME EFFORT TO GET IT TO RELEASE, HOWEVER, THE PANEL DID RELEASE DURI