N704US

Part: BOTTLE — OUT OF RIG (ZONE 800) · airframe 70,607 hrs · 41,595 cycles

AIRCRAFT WAS GROUNDED: CATERING IS UNABLE TO GET THE FRONT RIGHT DOOR FULLY OPENED AND LOCKED IN PLACE. MAINTENANCE REPLACED R-1 DOOR DAMPER /EMERGENCY CYLINDER PER AMM 52-11-14-400-001B.

Part: CHECK VALVE — FAILED (HYD SYS)

AIRCRAFT WAS GROUNDED: YELLOW HYDRAULIC FAILURE ON APPROACH. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE YELLOW SYSTEM MANIFOLD CHECK VALVE IAW AMM 29-13-14.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 68,266 hrs · 40,056 cycles

AIRCRAFT WAS NOT GROUNDED: PER EMERGENCY LIGHT TEST, FWD LEFT EPSU BATTERY HAD A FAULT. MAINTENANCE REPLACED FWD LEFT EPSU BATTERY IAW AMM 33-51-38.

Part: FIRE WARNING — ILLUMINATED (NR 2 ENGINE) · airframe 67,936 hrs · 39,832 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF INTERMITTENT ENGINE FIRE INDICATION ENGINE NUMBER2. DURING EXECUTION OF COMPANY PROCEDURE ENGINE FIRE INDICATIONRESOLVED BY SELECTING AFFECTED ENGINE THRUST LEVER TO IDLE.CREW OBSERVED ELEVATED NACELLE TEMPERATURE ON AFFECTED ENGINE ONECAM ENGINE SYNOPTIC PAGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DUCT SEAL — LEAKING (ZONE 400) · airframe 67,936 hrs · 39,832 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF INTERMITTENT ENGINE FIRE INDICATION ENGINE NUMBER2. DURING EXECUTION OF COMPANY PROCEDURE ENGINE FIRE INDICATIONRESOLVED BY SELECTING AFFECTED ENGINE THRUST LEVER TO IDLE.CREW OBSERVED ELEVATED NACELLE TEMPERATURE ON AFFECTED ENGINE ONECAM ENGINE SYNOPTIC PAGE. REPLACED SEALS FOR LOWER HP DUCT AND SECURED DUCT IAW AMM 36-11-49, FDU 2 BITES NORMAL IAW AMM 26-12-00.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 67,783 hrs · 39,702 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EPSU INTERNAL LOAD FWD L/H. REPLACED EMERGENCY POWER SUPPLY FIN: 10WL AND TESTED IN ACCORDANCE WITH AMM 33-51-38-400-001-A.

Part: PIN — NOT SEATED (LIGHT CONNETOR) · airframe 67,138 hrs · 39,255 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 22ABC EMERGENCY AISLE PATH LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202406195888: MAINTENANCE FOUND THE WIRE HARNESS ON SEAT 22ABC HAD A PIN THAT WAS NOT SEATED / PUSHED OUT AND RE-SEATED THE PIN. A SATISFACTORY OPERATIONAL CHECK WAS ACOMPLISHED OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED. ** (CLOSED)

Part: LIGHT — INOPERATIVE (SEAT ROW 22ABC) · airframe 67,138 hrs · 39,255 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 22ABC EMERGENCY AISLE PATH LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,649 hrs · 38,956 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU BATTERIY FAIL TEST ON AFT LEFT (13WL). REMOVED AND REPLACED EPSU BATTERI AT 13 WL POSITION.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,649 hrs · 38,956 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY FAIL TEST ON FWD LEFT (10WL) POS. REMOVED AND REPLACED EPSU BATTERY AT 10WL AND POSITION.

Part: ENGINE — LEAKING (NR 1) · airframe 66,398 hrs · 38,798 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF LOW OIL QUANTITY INDICATION. OIL ON NUMBER 1 ENGINE WENT TO 1.5 QUARTS AND OIL PRESSURE REMAINED SOLID AT 40 PSI. THE FLIGHT CREW REPORTED THAT THE ENGINE WAS NOT SHUT DOWN. THE AIRCRAFT LANDED SAFELY AT ORD AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE NOTED OIL IN THE HPC DURING THE ACCOMPLISHEMENT OF A BORESCOPE INSPECTION OF #1 ENGINE. MAINTENANCE REPLACED THE ENGINE PER TASK CARD 26L40071001.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 66,398 hrs · 38,798 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF LOW OIL QUANTITY INDICATION. OIL ON NUMBER 1 ENGINE WENT TO 1.5 QUARTS AND OIL PRESSURE REMAINED SOLID AT 40 PSI. THE FLIGHT CREW REPORTED THAT THE ENGINE WAS NOT SHUT DOWN. THE AIRCRAFT LANDED SAFELY AT ORD AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LATCH — STICKING (LAVATORY DOOR) · airframe 66,330 hrs · 38,752 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY DOOR STICKS. MAINTENANCE REPLACED LAVATORY DOOR LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 65,923 hrs · 38,517 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 24 AND 25 EMERGENCY WALKWAY LIGHTS INOPERATIVE. MAINTENANCE RE-SPLICED BROKEN WIRE FOR EMERGENCY WALKWAY LIGHTS IAW ESPM 20-43-11.

Part: TORQUE LINK — EXCESS PLAY (ZONE 700 - GEARS) · airframe 65,230 hrs · 38,078 cycles

AIRCRAFT WAS GROUNDED: WHILE TROUBLESHOOTING NOSE GEAR VIBRATION ISSUE MAINTENANCE FOUND THE NOSE LANDING GEAR UPPER AND LOWER TORQUE LINKS TO HAVE EXCESSIVE PLAY. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPPER (AALA202309279035) AND LOWER (AALA202309272304) TORQUE LINKS PER AMM 32-21-27.

Part: TORQUE LINK — EXCESS PLAY (ZONE 700 - GEARS) · airframe 65,230 hrs · 38,078 cycles

AIRCRAFT WAS GROUNDED: WHILE TROUBLESHOOTING NOSE GEAR VIBRATION ISSUE MAINTENANCE FOUND THE NOSE LANDING GEAR UPPER AND LOWER TORQUE LINKS TO HAVE EXCESSIVE PLAY. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPPER (AALA202309279035) AND LOWER (AALA202309272304) TORQUE LINKS PER AMM 32-21-27.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 65,080 hrs · 37,981 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT COMMUNICATION FAULT MESSAGE DURING SYSTEM TEST. MAINTENANCE REPLACED THE BATTERIES FOR THE FORWARD EMERGENCY POWER SUPPLY UNIT (AALA202309053439) AND THE LEFT MID EMERGENCY POWER SUPPLY UNIT (AALA202309058255) PER AMM 33-51-00.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 65,080 hrs · 37,981 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT COMMUNICATION FAULT MESSAGE DURING SYSTEM TEST. MAINTENANCE REPLACED THE BATTERIES FOR THE FORWARD EMERGENCY POWER SUPPLY UNIT (AALA202309053439) AND THE LEFT MID EMERGENCY POWER SUPPLY UNIT (AALA202309058255) PER AMM 33-51-00.

Part: PIN — WORN (ZONE 700 - GEARS) · airframe 65,073 hrs · 37,976 cycles

AIRCRAFT WAS GROUNDED: NOSE LANDING GEAR TORQUE LINK CENTER HINGE APEX PIN WORN. REPLACED CENTER HINGE APEX PIN PER AMM 32-21-27.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 64,129 hrs · 37,385 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 25 ABC SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY PER AMM 33-51-18 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WINDSHIELD — CRACKED (ZONE 200 - FUSE) · airframe 62,006 hrs · 36,041 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK FIRST OFFICERS R1 WINDSHIELD CRACKED. REPLACED WINDSHIELD PER AMM 56-11-11.

Part: SENSOR — DEFECTIVE (ZONE 500 - LH WI) · airframe 62,006 hrs · 36,041 cycles

AIRCRAFT WAS GROUNDED: 1 HOUR +20 MINUTES INTO FLIGHT-GREEN "FUEL OT XFRD" ECAM-CHECKED FUEL OUTER TANK AT 0-LEFT TANK ABOUT 2000# RIGHT TANK 8000# RIGHT TANK QUANTITY WAS FLASHING. AIRCRAFT DIVERTED TO STL DUE TO A FUEL IMBALANCE WHERE IT LANDED WITHOUT FURTHER INCIDENT. NOTE: NO EMERGENCY WAS DECLARED. REPLACED LEFT MAIN HIGH LEVEL SENSOR 17 QJ1 PER AMM 28-46-15.

Part: CONNECTOR — LOOSE (ZONE 200 - FUSE) · airframe 61,868 hrs · 35,946 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ON TAXI OUT AIRCRAFT LEFT EMERGENCY EXIT OVER WING SIGN ILLUMINATED RIGHT SIDE OUT. MAINTENANCE ADJUSTED CONNECTION ON EMERGENCY LIGHT ON THE RIGHT SIDE EMERGENCY EXIT LIGHT PER AMM 33-51-15.

Part: CONTROL SERVO — FAULTY (ZONE 700 - GEARS) · airframe 61,845 hrs · 35,935 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI IN, NOSE WHEEL STEERING FAULT WITH LOSS OF STEERING AUTHORITY. MAINTENANCE REPLACED NOSE WHEEL STEERING SERVO CONTROL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-51-51.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 61,607 hrs · 35,786 cycles

AIRCRAFT WAS NOT GROUNDED: DURING DESCENT DOOR RIGHT EMERGENCY EXIT WARNING ON ECAM. FLIGHT ATTENDANTS CHECKED CHECKED DOOR EXIT LIGHT ILLUMINATED. ADJUSTED PROXIMITY SWITCH TO TARGET GAP PER AMM 52-21-00.

Part: FLAP — UNSECURE (ZONE 800 - DOORS) · airframe 61,592 hrs · 35,779 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT EMERGENCY EXIT DOOR ECAM FAULT MESSAGE. RE-SECURED FLAP ON RIGHT EMERGENCY EXIT DOOR PER TSM 52-21-00. ECAM FAULT CLEARED WITH NO ADDITIONAL FAULTS.

Part: SLIDE RAFT — UNSERVICEABLE (ZONE 800 - DOORS) · airframe 61,586 hrs · 35,777 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 SLIDE PRESSURE HARD TO READ. REPLACED ESCAPE SLIDE RAFT AT PASSENGER CREW DOOR L1 PER AMM 25-62-44-400-007-A.

Part: SLIDE — DEFECTIVE (ZONE 800 - DOORS) · airframe 61,585 hrs · 3,577 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE PRESSURE HARD TO READ. REPLACED SLIDE PER AMM 25-62-44-400-007-A.

Part: LIGHT — LOOSE (ZONE 200 - FUSE) · airframe 61,587 hrs · 35,778 cycles

AIRCRAFT IN BASE MAINTENANCE: DOOR R2 EXIT LIGHT COVER LOOSE. INSTALLED CORRECTLY DOOR R2 EXIT LIGHT COVER PER AMM 33-51-13-400-001-A

Part: ELEVATOR — CORRODED (ZONE 300 - STABS) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND ELEVATOR INBOARD ACTUATOR FITTING ATTACHMENT LUGS. REPLACED ELEVATOR PER EO 5518Y004-001,

Part: HINGE FITTING — WORN (ZONE 700 - GEARS) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR HINGE FITTING BEARING LOOSE AND BORE WORN. REPLACED HINGE FITTING PER CMM 52-81-18-000-810-A01..

Part: NUT — STUCK (ZONE 500 - LH WI) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INTERCONNECTING STRUT NUT SPANNER STUCK. REPLACED INTERCONNECTING STRUT PER TASK CARD 26C57057001.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING #2 SLAT TRACK BOLT. REPLACED BOLT PER AMM 27-84-63-400-001-A.

Part: FITTING — WORN (ZONE 600 - RH WI) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING INTERCONNECTING STRUT INBOARD FLAP ON RIGHT WING AND FOUND BORE OUT OF TOLERANCE. ON FITTING ON THE REAR SPAR AT WX4476.559 AND RIB 14. REPLACED FITTING PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL CENTER FITTING AT FR 66 AND S23L. REPLACED CENTER FITTING PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 64 AND FR 66 AT +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 61,585 hrs · 35,776 cycles

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.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 PRINCIPLE 5.

Part: FITTING — WORN (ZONE 500 - LH WI) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT FITTING BEARING HAS EXCESSIVE PLAY, FOUND BORE OUT OF TOLERANCE. REPLACED FITTING PER SRM 51-42-11.

Part: HINGE FITTING — CRACKED (ZONE 700 - GEARS) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING CRACKED. REPLACED HINGE FITTING PER SRM 51-72-11.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING, TRAILING EDGE OF TOP SKIN PANEL #2, LOCATED AT BETWEEN WING RIB 7 TO RIB 8. REPAIRED SKIN PANEL PER EA 334135.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 61,585 hrs · 35,776 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING, TRAILING EDGE OF TOP SKIN PANEL #2, LOCATED AT BETWEEN WING RIB 7 TO RIB 8. REPAIRED SKIN PANEL PER EA 334135. **SUPPLEMENTAL REPORT TO CORRECT SECTION 7 CORROSION LEVEL TO REFLECT LEVEL 2**

Part: BATTERY — DISCHARGED (FWD FLASHLIGHT) · airframe 60,519 hrs · 35,140 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASH LIGHT LOW BATTERY. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 59,813 hrs · 34,769 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY SMOKE WARNING CAME ON IN FLIGHT FOR A FEW SECONDS, THEN DISAPPEARED. ACCOMPLISHED TEST PER AMM 26-17-00-710-001-A, NO FAULTS NOTED.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 59,145 hrs · 34,404 cycles

AIRCRAFT WAS NOT GROUNDED: L1 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED L1 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY PACK. FLASHLIGHT OPERATIONS CHECKS GOOD PER AMM 25-65-00.

Part: PRESSURE SWITCH — LOW PRESSURE (LT WG FUEL PUMP) · airframe 59,049 hrs · 34,351 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL LEFT TANK PUMP #2 LOW PRESSURE FAULT. REPLACED LEFT WING FUEL PUMP #2 PRESSURE SWITCH, ACCOMPLISHED A SATISFACTORY LEAK AND OPERATIONAL CHECK PER AMM 28-21-15.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 58,591 hrs · 34,090 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD FLASHLIGHT FLIGHT ATTENDANT JUMPSEAT CAN NOT VERIFY CHARGE. REPLACED BATTERY AS REQUIRED.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 58,560 hrs · 34,072 cycles

AIRCRAFT WAS NOT GROUNDED. FLASHLIGHT AT 1L DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT BATTERY.

Part: WIRE HARNESS — DEFECTIVE (EMERGENCY LIGHTS) · airframe 58,189 hrs · 33,811 cycles

AIRCRAFT NOT GROUNDED - SEAT MOUNTED EMERGENCY LIGHTS INOP, ROWS 24ABC AND 25ABC. REMOVED AND REPLACED EMERGENCY HARNESS PER AMM 33-51-00, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 58,171 hrs · 33,795 cycles

AIRCRAFT NOT GROUNDED - EMERGENCY LIGHTS, SEAT MOUNTED ROW 24ABC AND 25ABC, INOPERATIVE. RESEATED LOOSE ELECTRICAL CONNECTOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: FITTING — CRACKED (RT MLG WW) · airframe 57,476 hrs · 33,348 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR FITTING UPPER JOINT STRAP WAS FOUND TO BE FULLY SEVERED ACROSS THE INBOARD ATTACH FASTENER ROW COMMON TO THE ACTUATOR FITTINGS. THE FAILURE OF THE STRAP CAUSED AN OVERLOADING CONDITION THAT RESULTED IN DAMAGE TO THE ACTUATOR FORWARD AND AFT FITTINGS. REPLACED UPPER JOINT STRAP (AALA202002249037), FORWARD ACTUATOR FITTING (AALA202002249040) AND AFT ACTUATOR FITTING (AALA202002249039) PER EA 303390 AND EA 303467.

Part: FITTING — CRACKED (RT MLG WW) · airframe 57,476 hrs · 33,348 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR FITTING UPPER JOINT STRAP WAS FOUND TO BE FULLY SEVERED ACROSS THE INBOARD ATTACH FASTENER ROW COMMON TO THE ACTUATOR FITTINGS. THE FAILURE OF THE STRAP CAUSED AN OVERLOADING CONDITION THAT RESULTED IN DAMAGE TO THE ACTUATOR FORWARD AND AFT FITTINGS. REPLACED UPPER JOINT STRAP (AALA202002249037), FORWARD ACTUATOR FITTING (AALA202002249040) AND AFT ACTUATOR FITTING (AALA202002249039) PER EA 303390 AND EA 303467.

Part: STRAP — SEVERED (FRAME 43) · airframe 57,476 hrs · 33,348 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR FITTING UPPER JOINT STRAP WAS FOUND TO BE FULLY SEVERED ACROSS THE INBOARD ATTACH FASTENER ROW COMMON TO THE ACTUATOR FITTINGS. THE FAILURE OF THE STRAP CAUSED AN OVERLOADING CONDITION THAT RESULTED IN DAMAGE TO THE ACTUATOR FORWARD AND AFT FITTINGS. REPLACED UPPER JOINT STRAP (AALA202002249037), FORWARD ACTUATOR FITTING (AALA202002249040) AND AFT ACTUATOR FITTING (AALA202002249039) PER EA 303390 AND EA 303467.

Part: PROXIMITY SENSOR — CONTAMINATED (MLG DOOR) · airframe 57,155 hrs · 33,149 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS LANDING GEAR DOOR INDICATING NOT CLOSED (ACAM) LEFT SIDE. MAINTENANCE FOUND PROX SENSORS 27GA AND 29GA TO BE COATED WITH GREASE, CLEANED SENSORS AND CLEANED CONNECTOR PLUGS, CYCLED GEAR DOOR SERVERAL TIMES IAW AMM 32-31-00, COULD NOT DUPLICATE.

Part: LIGHT — BROKEN (CABIN) · airframe 57,034 hrs · 33,059 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT LIGHT FORWARD OF MAIN CABIN DOOR BROKEN. MAINTENANCE REPLACED EXIT LIGHT COVER PER AMM 33-51-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 56,610 hrs · 32,759 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON DESCENT WE GOT AN INDICATION AFT SMOKE LAV, IT WENT ON FOR A FEW SECONDS THEN WENT OUT, THE FA'S GOT A WARNING ALSO, THEY DIDN'T SEE OR SMELL ANY SMOKE. MAINTENANCE ACCOMPLISHED BITE AND OPS CHECK OF LAV SMOKE DETECTOR SYSTEM IAW AMM 26-17-00-810-801A AND AMM 26-17-00-710-001A AND NO DEFECTS NOTED.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1R PATH LIGHT ABOVE DOOR LENS DAMAGED. MAINTENANCE REPLACED DOOR PATH LIGHT PER AMM 33-51-16-400-001-A PROCEDURE 4.B STEP (5).

Part: STRUT — CORRODED (LT WING TE FLAP) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING INBOARD FLAP INTERCONNECTING STRUT. REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.

Part: FITTING — CRACKED (FRAME 2) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 295813.

Part: FITTING — CRACKED (FRAME 2) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 295813.

Part: HINGE FITTING — EXCESS PLAY (LT HORIZ STAB) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR #4 HINGE HAS EXCESSIVE PLAY ON THE HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA(1 EA). CHARGED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT 842 PASSENGER CREW DOOR IAW AMM 52-10-00-614-001-A.

Part: SLIDE RAFT — DEFORMED (PAX DOOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS DEFORMATION OF SLIDE RAFT AT PASSENGER CREW DOOR R2 AT AFT GALLEY AREA (1 E/A). REMOVED AND REPLACED ESCAPE SLIDE RAFT ON 842 PASS CREW DOOR IAW AMM 25-62-44-400-803-A. DOCUMENTED IAW CARD 26C84252002.

Part: FITTING — CORRODED (RT WING) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INTERCONNECTING STRUT ATTACHMENT FITTING ON THE OUTBOARD FLAP. REPLACED FITTING PER SRM 51-72-11.

Part: WINDOW FRAME — CRACKED (FRAME 2) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND WINDSHIELD FRAME AT FR 2 AND Y0. REPLACED WINDSHIELD FRAME PER EA 295811.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 SEGEMENT CRACKED. REPLACED SEGMENT PER SRM 51-72-11.

Part: FRAME — CRACKED (FRM 16) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 16 BETWEEN S10R AND S11R. REPLACED FRAME PER EA 2953839.

Part: FRAME — CRACKED (FRM 16) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 16 BETWEEN S10R AND S11R. REPLACED FRAME PER EA 2953839.

Part: WINDOW FRAME — CRACKED (FRAME 2) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND WINDSHIELD FRAME AT FR 2 AND Y0. REPLACED WINDSHIELD FRAME PER EA 295811.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND LATERAL WINDOW FRAME AT FR 4 AND Y625. REPLACED WINDOW FRAME PER EA 295816.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND WINDSHIELD FRAME AT FR 2 AND Y0. REPLACED WINDSHIELD FRAME PER EA 295811.

Part: WINDOW FRAME — CRACKED (FRAME 4) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND LATERAL WINDOW FRAME AT FR 4 AND Y625. REPLACED WINDOW FRAME PER EA 295817.

Part: FRAME — CRACKED (FRM 68) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R. REPAIRED FRAME PER SRM 53-41-12-300-011.

Part: HINGE FITTING — WORN (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE FITTING PER SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY AT VERTICAL STABILIZER RIB 5. REPLACED HINGE FITTING PER AMM 55-36-41-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY AT VERTICAL STABILIZER RIB 4. REPLACED HINGE FITTING PER AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER SRM 51-72-11.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR #5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HINGE #2 HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY AT VERTICAL STABILIZER RIB 2. REPLACED HINGE FITTING PER AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #4 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #6 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR HINGE #6 HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 56,165 hrs · 32,452 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: STRUCTURE — DAMAGED (LT AILERON) · airframe 56,158 hrs · 32,449 cycles

AIRCRAFT WAS GROUNDED: LEFT AILERON INBOARD TRAILING EDGE CORNER SHOWS APPROX. 1 IN. PIECEOF ALUMINUM STRIP BROKEN OFF AND DISBONDED.REPLACED AILERON PER AMM 27-14-41-400-001-A.

Part: ELEVATOR — VIBRATION · airframe 54,901 hrs · 31,659 cycles

DURING CLIMB, AT 310 KTS, FELT AN AIRFRAME VIBRATION. FLIGHT ATTENDANT IN REAR GALLEY CALLED AND SAID BACK OF PLANE WAS VIBRATING BADLY. LEVELED OFF AT FL 320 AND SLOWED THE ACFT TO 74 AND VIBRATION WENT AWAY, SLOWLY INCREASED SPEED TO .8 WITH NO FURTHER PROBLEMS. ACCOMPLSUHED TSM PROCEDURE 27-30-00-810-850-A. REPLACED INBOARD GREEN SYSTEM SERVO CONTROL ELEVATOR IAW AMM 27-34-51-0901. ADJUSTEDMENT AND TESTED OK.

Part: MECHANISM — DEFECTIVE (R1 DOOR) · airframe 54,532 hrs · 31,413 cycles

THE AIRCRAFT WAS NOT GROUNDED. ON DESCENT, CIDS PANEL SLIDE ARMED WARNING LIGHT STARTED FLASHING. LOWER DU IND 1R DISARMED ACCOMPANIED BY DOOR 1R CABIN PRESSURE WARNING LIGHT AT DOOR. SLIDE ARMED HANDLE FLUSH. CLEAN DEBRIS AND LUBE ESCAPE SLIDE RELEASE MECHANISM R1 DOOR PER AMM 52-10-00. CHECKED RELEASE MECHANISM SEVERAL TIMES. OPERATIONS CHECK NORMAL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 53,785 hrs · 30,914 cycles

EMERGENCY EXIT LIGHT COVER MISSING JUST BELOW LEFT OVERWING EXIT. INSTALLED THE COVER. OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 53,303 hrs · 30,619 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REPLACED THE LENS IAW AMM 33-51-15.

Part: BOTTLE — LOW PRESSURE (DOOR SLIDE) · airframe 53,296 hrs · 30,614 cycles

SLIDE BOTTLE LEFT ON CIDS TEST, LOW PRESSURE. MAINTENANCE REPLACED LEFT RESERVOIR BOTTLE IAW AMM 25-62-46, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 52,604 hrs · 30,183 cycles

FORWARD EMERGENCY CABIN POWER SUPPLY FAULTING. REPLACED FORWARD EMERGENCY LIGHT UNIT PER AMM 33-51-38-401.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 52,296 hrs · 30,001 cycles

AIRCRAFT WAS NOT GROUNDED. 2 LEFT DOOR SLIDE PACK COVER LOOSE. REATTACHED SLIDE COVER PER AMM 25-62-50-400-801C1.

Part: FAN — ODOR (EXTRACT) · airframe 52,273 hrs · 29,985 cycles

AIRCRAFT WAS NOT GROUNDED. VENT EXTRACT FAULT BURNING SMELL FROM EXTRACT FAN. REPLACED EXTRACT FAN PER AMM REF 21-26-51 P/B 0401. OPERATIONS CHECK NORMAL

Part: COVER — LOOSE (L2 DOOR) · airframe 52,260 hrs · 29,977 cycles

AIRCRAFT WAS NOT GROUNDED. SLIDE COVER ON L2 DOOR LOOSE. RESECURED SLIDE COVER (DECORATIVE) ON 2L DOOR PER 25-62-50.

Part: COVER — UNSECURE (L2 DOOR) · airframe 52,246 hrs · 29,967 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE COVER 2L WOULD NOT STAY ON. RESECURED SLIDE COVER AT 2L AND PERFORMED SUCCESSFUL OPERATIONS CHECK.

Part: FLASHLIGHT — INOPERATIVE (L2 JUMPSEAT) · airframe 51,878 hrs · 29,687 cycles

FLASHLIGHT AT FLIGHT ATTENDANT L2 JUMPSEAT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,423 hrs · 29,379 cycles

EMERGENCY.EXIT BATTERY AFT LEFT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTTERY .AFT L REF IAW AMM 33-51-38.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 51,407 hrs · 29,370 cycles

WHILE ATTEMPTING SLIDE CHANGE AT THE L2 DOOR, REPLACEMENT SLIDE WAS FOUND TO BE DEFECTIVE FROM STOCK. REINSTALLED L2 DOOR SLIDE IAW JC 26L00025011. SLIDE WAS SENT OUT FOR REPAIR DUE TO BEING UNPACKED, DEPLOYED. VENDOR TESTED AND REPAIRED IAW CMM 25-61-20.

Part: LATCH — OBSTRUCTED (EMER EQUIP DOOR) · airframe 51,067 hrs · 29,180 cycles

EMERGENCY EQUIPMENT DOOR JAMMED. REMOVED DEBRIS FROM DOOR LATCH. OPS CHECKED GOOD.

Part: NUT — CORRODED (RT MLG) · airframe 51,049 hrs · 29,170 cycles

RIGHT MAIN LANDING GEAR AFT PINTLE PIN, NUT, AND WASHER HAVE PITTING. REMOVED AND REPLACED PIN, NUT AND WASHER.

Part: PIN — CORRODED (RT MLG) · airframe 51,049 hrs · 29,170 cycles

RIGHT MAIN LANDING GEAR AFT PINTLE PIN, NUT, AND WASHER HAVE PITTING. REMOVED AND REPLACED PIN, NUT AND WASHER.

Part: FITTING — CRACKED (FRAME 42) · airframe 51,049 hrs · 29,170 cycles

WHILE ACCOMPLISHING WORK CARD 26T14753005 TO INSPECT MLG DOOR KEEL BEAM HINGE AND ACTUATOR FITTINGS, CRACK DETECTED AT LEFT ACTUATOR, AFT FLANGE.KEEL BEAM ATTACH POINT, STRINGER 41L AND FR 42. REPAIRED DOOR ACTUATOR FITTING PER EA # 270779 REVISION A.

Part: FITTING — CRACKED (FRAME 42) · airframe 51,049 hrs · 29,170 cycles

WHILE ACCOMPLISHING WORK CARD 26T14753005 TO INSPECT MLG DOOR KEEL BEAM HINGE AND ACTUATOR FITTINGS, A CRACK WAS DETECTED AT THE LEFT ACTUATOR, AFT FLANGE.KEEL BEAM ATTACH POINT, STRINGER 41L AND FRAME 42. REPAIRED DOOR ACTUATOR FITTING IAW EA 270779 REVISION A.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 50,945 hrs · 29,114 cycles

EMERGENCY LIGHTS ON WILL NOT TURN OFF, WHEN SELECTED OFF. EMERGENCY LIGHT SYSTEM CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,570 hrs · 28,872 cycles

EMERGENCY LIGHT LENS MISSING AT THE L1 DOOR. REPLACED THE LENS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,455 hrs · 28,117 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT AND AFT CABIN LEFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,455 hrs · 28,117 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT AND AFT CENTER CABIN LEFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 49,272 hrs · 27,981 cycles

FLIGHT CREW REPORTED THAT AN ACID, BURNING RUBBER & MUSTY ODOR CAME ON VERY STRONG RESULTING IN A SLIGHT BURNING IN EYES. DIVERTED WITH NO EMERGENCY WAS DECLARED AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE APU OIL SYSTEM OVERSERVICED AND SERVICED IT TO THE PROPER LEVEL.

Part: LENS — MISSING (CABIN) · airframe 48,167 hrs · 27,319 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT ABOVE R2 DOOR IS MISSING LENS. INSTALLED NEW LENS IAW AMM 33-51-11-401.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR NR 6, HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR NR 5 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: FITTING — WORN (LT MLG DOOR) · airframe 47,826 hrs · 27,102 cycles

EXCESSIVE PLAY ON BEARING OF FWD FITTING ON LT MLG MAIN DOOR. R & R FWD FITTING ON LT MLG MAIN DOOR IAW CMM 52-81-18.

Part: STRIKER — OUT OF ADJUST (ZONE 800) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. OUT OF ADJUSTMENT DIMENSION A PAX CREW DOOR 842, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT DIMENSION A J2 SENGER CREW DOOR 842, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IAW MM 52-13-14-820-002-A.

Part: BOLT — CORRODED (FLAP TRACK) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. RT WING OTBD FLAP NR 4 TRACK PIVOT BOLT IS CORRODED. REPLACED PIVOT BOLT IAW SRM 51-42-11 & 51-72-11.

Part: SLIDE RAFT — DEFORMED (ZONE 800) · airframe 47,826 hrs · 27,102 cycles

DEFORMATION ON SLIDE RAFT PACK ASSEMBLY AT DOOR 841 AT FWD GALLEY AREA. WHEN DOOR IS FULL OPEN, SLIDE & RAFT TOUCH THE FUSELAGE. REPLACED SLIDE.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT WING OTBD FLAP HAS DELAMINATION ON THE UPPER SURFACE TE. REPLACED FLAP IAW TASK CARD 26L00027009.

Part: STRIKER — OUT OF ADJUST (ZONE PAX DOOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. OUT OF ADJUSTMENT DIMENSION A PAX CREW DOOR 841, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT DIMENSION A J2 PAX CREW DOOR 841 IAW AMM 52-11-14-820-002-A.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT WING ACCESS PANEL 540HB, HAS AN ELONGATED FASTENER HOLE. REPLACED ACCESS PANEL IAW AMM 57-27-400-002-A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN DOOR SILL AT STRINGER 23R IS CORRODED, BETWEEN FRAME 16 & 20. R & R SILL IAW EA 114968.

Part: HINGE FITTING — WORN (LT SPOILER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT WING SPOILER NR 2 CTR HINGE FITTING STOP BOLT WORN. REPAIRED HINGE FITTING IAW SRM 57-70-00 TABLE 202 PARAGRAPH 5 C FIGURE 201.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE FASTENER HOLE HAS CRACK INDICATION, AT FRAME 43 & STRINGER 15 RT. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & STRINGER 15 LT. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. NLG RT AFT DOOR, AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: HINGE PIN — CORRODED (NLG) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. NLG TORQUE LINK CTR HINGE PIN IS CORRODED. R & R PIN IAW SRM 51-72-11 & 51-42-11.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. NLG LT AFT DOOR, FWD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. NLG RT AFT DOOR, FWD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. NLG LT AFT DOOR, AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261AG HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR UPPER SURFACE HAS 5 AREAS WHERE THERE WAS AN INDICATION OF TRAPPED WATER, BETWEEN ELEVATOR STATIONS 131 & 527, & BETWEEN RIB 2 & 9. REPAIRED ELEVATOR IAW SRM 55-21-11-2011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261BG HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FLOOR PANEL 212EF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261PF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR LOWER SURFACE HAS 1 AREA WHERE TRAPPED WATER WAS INDICATED, BETWEEN ELEVATOR STATIONS 131 - 181 & BETWEEN RIB 1 & 2. REPAIRED ELEVATOR IAW SRM 55-21-11-201-1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261DF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00-201& IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 222EF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE FRAME WEB IS CORRODED AT FRAME 20 & STRINGER 23L. R & R WEB IAW SRM 51-72-11 & DWG D53114392.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. SEAT RAIL BEAM COUPLING HAS ELONGATED HOLE AT FRAME 66 +Y765. REPLACED COUPLING IAW SRM A319 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 221EF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR PANEL 261FF IS CORRODED. R & R FLOOR PANEL IAW SRM 51-72-11-001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. LONGITUDINAL FLOORBEAM AT Y 765 IS CORRODED, BETWEEN FRAME 66 & 70. R & R BEAM IAW SRM A319 51-72-11 & DWG D53472000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN SEAT TRACK AT Y -765 IS CORRODED, BETWEEN FRAME 64 & 66. R & R SEAT TRACK IAW SRM 51-72-11 & DWG D53472090.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN SEAT RAIL AT Y -1379.5 IS CORRODED, BETWEEN FRAME 12 & 16. R & R SEAT RAIL IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. CORROSION ON R2 DOOR SILL, BETWEEN FRAME 66 & 68, AT STRINGER 23 RT. REPLACED DOOR SILL IAW EA 258087 & DWG D53480009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 262BG HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. MAIN CABIN FLOOR PANEL 242MF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 231CF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. LONGITUDINAL FLOORBEAM AT Y -1292 IS CORRODED, BETWEEN FRAME 12 & 24. R & R FLOORBEAM IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. CORROSION ON RAIL SEAT BEAM, BETWEEN FRAME 64 & 66 AT +Y765. REPLACED BEAM IAW SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CORNER FITTING AT FRAME 68 & STRINGER 23L IS CORRODED. R & R FITTING IAW SRM 51-72-11 & DWG D53480009.

Part: SKIN — SATURATED (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RUDDER RT SURFACE SKIN HAS 2 AREAS WHERE THERE WAS INDICATION OF TRAPPED WATER, BETWEEN 14.7" & 15.25" FROM THE TE & BETWEEN 17" & 19.5", FROM THE LOWER EDGE & 1 AREA OF DELAMINATION, 14.7" FROM THE TE & 26.47" FROM THE LOWER EDGE. RUDDER REPAIRED IAW EA 258240.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. LONGITUDINAL FLOORBEAM AT Y -765 IS CORRODED, BETWEEN FRAME 66 & 77. R & R FLOORBEAM IAW SRM 51-72-11 & DWG D53472800.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN DOOR SILL AT STRINGER 23L IS CORRODED, BETWEEN FRAME 66 & 68. R & R SILL IAW SRM 2-11 & DWG D53480009.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. COUPLING AT FRAME 66 & STRINGER 23 RT HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE FRAME WEB IS CORRODED AT FRAME 20 & STRINGER 23R. R & R FRAME WEB IAW SRM 51-72-11 & DWG D531143331.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR UPPER SURFACE HAS 3 AREAS WHERE THERE WAS INDICATION OF TRAPPED WATER, BETWEEN ELEVATOR STATION 131 - 466, & BETWEEN RIB 2 - 9. REPAIRED ELEVATOR IAW SRM 55-21-11-2011.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR PANEL 262FF IS CORRODED. R & R FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 221DF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. COUPLING AT FRAME 66 & STRINGER 23 RT HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. EXCESSIVE PLAY ON RUDDER NR 2 HINGE. REPLACED HINGE IAW AMM 55-36-400-001-A.

Part: HINGE — EXCESS PLAY (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. EXCESSIVE PLAY ON RUDDER NR 4 HINGE. REPLACED HINGE IAW AMM 55-36-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RUDDER HINGE FITTING NR 1 HAS EXCESSIVE PLAY. REPLACED RUDDER HINGE FITTING IAW AMM 55-36-41-000-001-A & SRM 51-72-11.

Part: HINGE — EXCESS PLAY (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. EXCESSIVE PLAY ON RUDDER NR 7 HINGE. REPLACED HINGE IAW AMM 55-36-400-001-A.

Part: HINGE — EXCESS PLAY (RUDDER) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. EXCESSIVE PLAY ON RUDDER 3 HINGE. REPLACED HINGE IAW AMM 55-36-400-001-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,826 hrs · 27,102 cycles

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

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 1 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR NR 1 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR NR 3 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 6 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 5 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. FASTENER HOLE HAS CRACK INDICATION ON LOWER FUSELAGE SKIN, AT FRAME 35 & STRINGER 30 LT. REPAIRED SKIN IAW EA 257956.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 2 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 3 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. RT ELEVATOR NR 2 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 47,826 hrs · 27,102 cycles

AIRCRAFT IN BASE MX. LT ELEVATOR NR 2 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42-400-001-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,252 hrs · 26,738 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE, PAX ROW 9. REPLACED POWER SUPPLY UNIT. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,154 hrs · 26,680 cycles

ROWS 8 - 10, EMER EXIT MARKERS WILL NOT ILLUMINATE. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-61-38-000-001-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,030 hrs · 26,591 cycles

EMERGENCY EVACUATION LIGHTS AT EMER EXIT ROW BOTH LT & RT SIDE INOPERATIVE. REPLACED POWER SUPPLY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 46,770 hrs · 26,408 cycles

IN DESCENT, HYD Y LOW LEVEL FOLLOWED ECAM, LANDED WITHOUT INCIDENT. FOUND AN O RING CUT & LEAKING ON THE PTU COUPLING HALF. THE COUPLING HALF & O RING WERE REPLACED & NO DEFECTS WERE NOTED DURING THE OPERATIONAL CHECK.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 46,626 hrs · 26,310 cycles

FLIGHT 823 WAS ABOUT 30 MINUTES FROM LANDING WHEN THEY HAD A GREEN SYS HYD LOW PRESSURE. DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. FOUND A HYDRAULIC LINE IN THE LT PYLON LEAKING. REPLACED THE LINE IAW AMM 29-11-49. ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,614 hrs · 26,303 cycles

OVERWING EMER EXIT HATCH LIGHTS ON PAX SEATS WILL NOT ILLUMINATE. REPLACED EMER EXIT POWER SUPPLY UNIT 12WL. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38 PB401.

Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 46,300 hrs · 26,126 cycles

AFT MEGA PHONE UNSERVICEABLE. R & R AFT MEGA PHONE IAW AMM 25-65-51. OPERATIONS CHECKED OK.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 45,695 hrs · 25,773 cycles

CLIMBING OUT OF 10,000 FT, FLIGHT ATTENDANT ADVISED 1L LOW PRESSURE FLASHING & 1L SLIDE SHOWS UNARMED ON ECAM. ADJUSTED PROXIMITY SWITCH HANDLE 4WN1 IAW AMM 52-71-00-820-002-A. ALL INDICATIONS OPERATE NORMAL IAW AMM 52-73-00-710-001-A.

Part: CONNECTOR — OUT OF ALIGNMENT (EMERGENCY LIGHTS) · airframe 45,695 hrs · 25,773 cycles

EMERGENCY EXIT LIGHT SYS FAILS AFT LT SLIDE. REMOVED R2 DOOR ESCAPE SLIDE & SECURED ELECTRICAL CONNECTOR ON SLIDE. REINSTALLED SAME SLIDE & OPS CHECKED THE EMERGENCY LIGHT SYS. THE EMERGENCY EXIT LIGHT SYS OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 45,689 hrs · 25,769 cycles

EMERGENCY EXIT LIGHT SYS FAILS ON L1 DOOR SLIDE. REPLACED L1 DOOR SLIDE IAW 26L00025011 & OPS CHECKED GOOD.

Part: PUMP — SHUTDOWN (HYDRAULIC SYS)

AIRCRAFT DIVERTED AFTER LOSING GREEN HYD SYS. REPLACED LT ENG GREEN SYS HYD PUMP IAW A319 AMM 29-11-51. AFTER INSPECTION PUMP WAS FOUND WITH NO FAULTS.

Part: SLIDE RAFT — DEFECTIVE (L2 DOOR) · airframe 43,847 hrs · 24,669 cycles

WITH L2 SLIDE COVER IN PLACE, WHEN YOU OPEN THE L2 DOOR, IT HITS THE SIDE OF FUSELAGE & FALLS OFF. R & R L2 DOOR ESCAPE SLIDE IAW JOB CARD 26L00025011. OPERATIONS CHECKED OK. SLIDE COVER CLEARS FUSELAGE.

Part: SLIDE RAFT — UNSERVICEABLE (L1 DOOR) · airframe 43,504 hrs · 24,467 cycles

THE FUSELAGE SKIN PAINT DETERIORATED AT L1 DOOR SLIDE RAFT DECORATIVE COVER CONTACT POINT IAW EO 2514Y110. NO BARE METAL & NO DAMAGE TO FUSELAGE SKIN. R & R L1 DOOR EMER SLIDE ASSEMBLY.

Part: FLAP — OUT OF ADJUST (EMERGENCY EXIT) · airframe 43,033 hrs · 24,158 cycles

THE RT FWD WING EMERGENCY EXIT INDICATES NOT ARMED AFTER TAKEOFF. SLIDE LIGHT ARM IS ILLUMINATED. NEGATIVE UNUSUAL AIR NOISE. ACFT PRESSURIZED. ADJUSTED FWD RT OVERWING EMERGENCY EXIT DOOR FLAP, OK FOR SERVICE. DOOR ARMED & ANNUNCIATOR NORMAL.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 41,785 hrs · 23,241 cycles

EMERGENCY FLASHLIGHT INOPERATIVE AT L1 DOOR DOES NOT BLINK. REPLACED FLASHLIGHT.

Part: SLIDE — DISLODGED (L2 DOOR) · airframe 41,778 hrs · 23,234 cycles

STRAP HANGING OUT OF 2L DOOR. R & R 2L DOOR SLIDE.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 41,652 hrs · 23,134 cycles

MX REPORTED THE FWD MEGAPHONE INOPERATIVE. MX R & R THE FWD MEGAPHONE IAW AMM 25-60-00.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 41,430 hrs · 22,957 cycles

CREW REPORTED THE AFT RT SERVICE DOOR EXIT LIGHT COVER NOT ATTACHED. MX REPLACED AND SECURED EXIT LIGHT COVER AT AFT RT SERVICE DOOR. OPS NORMAL. REF MPPM 541-01-10.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,058 hrs · 22,684 cycles

C11 CHECK - TWENTY THREE AREAS OF WATER ENGRESSION ON LT ELEVATOR UPPER SURFACE AT APPROX 4.5" FWD OF T/E & 11" THRU 201" FROM INBD EDGE. REPAIRED LT ELEVATOR UPPER SURFACE IAW AMM 27-34-41-400-001.

Part: COVER — MISSING (CABIN) · airframe 39,905 hrs · 21,914 cycles

CREW REPORTED THE EXIT LIGHT MISSING NEXT TO 2L DOOR SLIDE RAFT COVER. MAINTENANCE INSTALLED NEW EXIT LIGHT COVER AT 2L DOOR AS NEEDED.

Part: LENS — MISSING (CABIN) · airframe 37,465 hrs · 20,377 cycles

ROW 10 AIRCRAFT RIGHT EMERGENCY EXIT RED COVER MISSING. REPLACED EMERGENCY EXIT RED LENS AT ROW 10.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,979 hrs · 20,073 cycles

EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. REMOVED & REPLACED AFT EMERGENCY POWER SUPPLY UNIT. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 33,306 hrs · 17,702 cycles

FLT 1897 - ATL - EEL - EMERGENCY LIGHT LENS MISSING AT R-1 DOOR. MAINTENANCE REPLACED EMERGENCY LIGHT LENS AT R-1 DOOR.

Part: STRUT — OUT OF ADJUST (TE FLAP) · airframe 32,864 hrs · 17,439 cycles

FLT 1420 - PHL-CLT - EMERGENCY LANDING - FLAPS LOCKED - ALIGNMENT FAULT. ACCOMPLISHED A MCDU WING TIP BRAKE (WTB) RESET. ACCOMPLISHED A LEFT AND RIGHT WING INTERCONNECTING STRUT ADJUSTMENTS IAW AMM 27-51-44-05. OPERATIONAL CHECKS WAS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, -Y254 IAW EA 115064 & AIRBUS DRAWING D53110900.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL PANEL 540JB. REPLACED LEFT WING FUEL PANEL 540JB IAW B757 SRM 57-21-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 232YG BETWEEN FR28 TO FR35, Y1028. FABRICATED & REPLACED CABIN FLOOR PANEL 232YG BETWEEN FR28 TO FR35, Y1028 IAW IRM 970 REV G & JOB CARD 26C24053002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, -Y765. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, -Y765 IAW A319 SRM 51-40-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 262EF BETWEEN FR66 TO FR68, -Y1162. FABRICATED & REPLACED CABIN FLOOR PANEL 262EF BETWEEN FR66 TO FR68, -Y1162 IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 261EF BETWEEN FR66 TO FR68, Y1162, S23L. FABRICATED & REPLACED CABIN FLOOR PANEL 261EF BETWEEN FR66 TO FR68, Y1162, S23L IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 231LF BETWEEN FR24 TO FR28, Y254. FABRICATED & REPLACED CABIN FLOOR PANEL 231LF BETWEEN FR24 TO FR28, Y254 IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 262HG BETWEEN FR64 TO FR66, -Y795. FABRICATED & REPLACED CABIN FLOOR PANEL 262HG BETWEEN FR64 TO FR66, -Y795 IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 261PF BETWEEN FR68 TO FR70. FABRICATED & REPLACED CABIN FLOOR PANEL 261PF BETWEEN FR68 TO FR70, IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - AREA OF DELAMINATION ON CABIN FLOOR PANEL 261DF BETWEEN FR66 TO FR68, C/L. FABRICATED & REPLACED CABIN FLOOR PANEL 261DF BETWEEN FR66 TO FR68, C/L IAW IRM 970 REV G & JOB CARD 26C26053004.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR16 TO FR24, -Y1292. REPLACED FLOOR SUPPORT BEAM BETWEEN FR16 TO FR24, -Y1292 IAW A319 SRM 51-42-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - NR # 26C26053005/006-2 - LEVEL 2 GALVANIC CORROSION ON TOP OF FLOOR BEAM BETWEEN FR66 TO FR69, Y1292. REPLACED FLOOR BEAM BETWEEN FR66 TO FR69, Y1292 IAW A319 SRM 51-42-00 & AIRBUS DRAWING # 18D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON TOP OF FLOORBEAM BETWEEN FR66 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Y1292 IAW A319 SRM 51-42-00& AIRBUS DRAWING 18D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON TOP OF FLOORBEAM BETWEEN FR66 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Y1292 IAW A319 SRM 51-42-00 & AIRBUS DRAWING 18D53472816.

Part: PANEL — SATURATED (RT WING) · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - RIGHT WING LOWER FUEL PANEL 640FB WEIGHT IS EXCEEDING ITS LIMIT. ACTUAL WEIGHT IS 1.29KG. MAX ALLOWABLE WEIGHT IS 1.10 KG +/- 0.1KG. REPLACED RIGHT WING LOWER FUEL PANEL 640FB IAW JOB CARD 26C60057091.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 51-74-00 & 51-73-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 32,556 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - CRACK ON LEFT SHEAR PLATE BETWEEN FR68 TO FR69. REPLACED LEFT SHEAR PLATE BETWEEN FR68 TO FR69 IAW A319 SRM 53-41-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SHEAR TIE BETWEEN FR69 TO FR70, -Y1160. REPLACED SHEAR TIE BETWEEN FR69 TO FR70, -Y1160 IAW EO 5307Y284.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A319 SRM 51-71-11.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL PANEL 540NB. REPLACED LEFT WING FUEL PANEL 540NB IAW B757 SRM 57-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A319 SRM 51-71-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON TOP OF FLOORBEAM AT FR66 TO FR70, Y765. REPLACED FLOORBEAM AT FR66 TO FR70, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 THRU FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 THRU FR70, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON TOP OF FLOORBEAM AT FR66 TO FR70, Y765. REPLACED FLOORBEAM AT FR66 TO FR70, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR24, FR25 & FR30, -Y1292. REPLACED FLOORBEAM AT FR24, FR25 & FR30, -Y1292 IAW A319 SRM 51-42-00, 51-44-11, & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON TOP OF FLOORBEAM BETWEEN FR16 TO FR20, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y1292 IAW A319 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y254. REPLACED FLOORBEAM AT FR66, Y254 IAW AIRBUS DRAWING 18D53472800 & D53472750.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y254. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y254 IAW AIRBUS DRAWING 18D53472800 & 10D53472750.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,776 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT FR66, S20R, -Y300. REPLACED FLOORBEAM AT FR66, S20R, -Y300 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR66, -Y464.8. REPLACED FLOORBEAM AT FR66, -Y464.8 IAW A319 SRM 51-72-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - WATER ENTRAPMENT IN LEFT ELEVATOR UPPER SKIN BETWEEN RIB 1 THRU 10. REPLACED LEFT ELEVATOR IAW A319 AMM 27-34-41-04.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE AT FR70, S23L. REPLACED SHEAR PLATE AT FR70, S23L IAW A319 SRM 51-72-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - WATER ENTRAPMENT IN RIGHT ELEVATOR UPPER SKIN BETWEEN RIB 1 THRU 10. REPLACED RIGHT ELEVATOR IAW A319 AMM 27-34-41-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON TOP OF FLOOR SUPPORT BEAM AT FR66, Y460. REPLACED FLOOR SUPPORT BEAM AT FR66, Y460 IAW A319 SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Y81 IAW A319 SRM 51-42-00 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOORBEAM AT FR16, FR18, FR20, FR21, & FR23, Y254. REPLACED CABIN FLOORBEAM AT FR16 THRU FR23, Y254 IAW A319 SRM 51-42-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 17,385 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR14 TO FR16, Y495. REPLACED FLOORBEAM BETWEEN FR14 TO FR16, Y495 IAW A319 SRM 51-42-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,856 hrs · 17,434 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOOR ANGLE ON AFT SIDE OF CIRCUIT BREAKER BULKHEAD & RIGHT SIDE OF COCKPIT DOOR CUTOUT. REPLACED FLOOR ANGLE ON AFT SIDE OF CIRCUIT BREAKER BULKHEAD & RIGHT SIDE OF COCKPIT DOOR CUTOUT IAW A319 SRM 51-72-11.

Part: LENS — MISSING (CABIN) · airframe 32,054 hrs · 16,970 cycles

FLT 1252 - JAX-DCA - EMERGENCY LIGHTS - SEAT 10C EMERGENCY EXIT LIGHT COVER MISSING. REPLACED MISSING EMERGENCY LIGHT LENS AT SEAT 10C. OPERATIONAL CHECK WAS GOOD.

Part: GIRT BAR — DAMAGED (R2 DOOR SLIDE) · airframe 31,176 hrs · 16,459 cycles

FLT 1651 - AFTER TAKEOFF 2R SLIDE ARMING HANDLE MOVES OUT OF ARMED POSITION, DISARMS SLIDE AND WILL NOT GO BACK INTO THE ARMED POSITION. MAINTENANCE REMOVED METAL SHAVING FROM GIRT BAR FITTING & CLEANED DEBRIS FROM SLIDE ASSEMBLY.

Part: SLIDE — TORN (L1 DOOR)

IAD - A STRAP FROM THE L-1 DOOR ESCAPE SLIDE/RAFT TO THE SLIDE COVER WAS FOUND TORN OFF. MAINTENANCE REPLACED THE L-1 DOOR ESCAPE SLIDE/RAFT. OK FOR SERVICE.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 23,128 hrs · 23,128 cycles

FOUND SKIN DELAMINATION BOTTOM OF LEFT BLEV-18" FROM I/B END. REMOVED DAMAGE AND REPOTTED AREA PER SRM 55-21-11, DEFECT SIZE: 6" X 1.5".

Part: STRAP — MISROUTED (ESCAPE SLIDE)

THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE LT FORWARD ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.

Part: SLIDE — INOPERATIVE (PAX CABIN)

CLT - THE MAIN CABIN ENTRY DOOR WOULD NOT ARM. THE SLIDE ARMED LIGHT WOULD FLASH ON AND OFF ON ECAM DOOR DISPLAY. ALSO, THE HANDLE WAS SPONGY. MAINTENANCE REPLACED THE MAIN CABIN ENTRY DOOR SLIDE/RAFT. OK FOR SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

BFM - FOUND DOOR SILL BEAM CORRODED 1.2 INCHES LONG BY .080 INCH WIDE BY .052 INCH DEEP, BETWEEN FRAME 66-68, Y1970, -Z240. REMOVED AND REPLACED PART PER SRM 51-74-00, 53-41-14, 53-42-11, 51-77-11, 51-42-11. (M)

Part: SILL — CORRODED (FUSELAGE)

BFM - FOUND SILL PLATE ASSEMBLY CORRODED 5 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP, L2 DOOR SILL PLATE ASSEMBLY, Y1732 FORWARD OF FRAME 66. REMOVED AND REPLACED PER SRM 53-41-14, 53-41-11. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

BFM - FOUND FLOOR PANEL CORRODED 2 INCHES BY 38.5 INCHES BY 13 INCHES AND .5 INCH BY 10 INCH AREA, PANEL NR 222FF, FRAME 16-20, Y=-1732, Z=-240. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-02-00. CORROSION LEVEL 2, TASK NR JA-220-53300. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 36 INCHES, 1 INCH BY 12 INCHES, 1 INCH BY 10 INCHES, PANEL NR 221FF, FRAME 16-20, Y=1732, Z=-240. REMOVED AND INSTALLED NEW PANEL. CORROSION LEVEL 2, TASK NR JA-220-53300-001. (M)

Part: BEAM — CORRODED (FUSELAGE)

FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .023 INCHE DEEP, FRAME 66, -Y1292, -Z240. REMOVED AND REPLACED BEAM PE SRM 53-41-15, 51-74-00, 51-42-11. (M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM CORRODED 1 INCH BY .20 INCH BY .27 INCH DEEP AREA, FRAME 67, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15 51-42-11, 53-00-14, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

BFM - FOUND FLOORBOARD CORRODED 1.3 INCHES BY 1.125 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, -Y1732, -Z240. REMOVED AND REPLACED FLOORBOARD PER SRM 51-42-11, 51-74-00. (M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM CORRODED 2 INCHES BY 1.6 INCHES BY .058 INCH DEEP AREA, FRAME 68, -Y1732, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M)

Part: PLATE — CORRODED (FUSELAGE)

BFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH BY 1.4 INCH BY .025 INCH, FRAME 69, -Y1732, -Z240. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-02-00, 51-77-10, 51-11-00, 51-72-11. CORROSION LEVEL 2, TASK NR JA-260-53500.(M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM CORRODED 1.2 INCH BY 1 INCH BY .047 INCH DEEP AREA, BETWEEN FRAME 68 AND 69, Y1292,-Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

BFM - FOUND SEAT TRACK CORRODED 1.5 INCHES BY 2.4 INCHES BY .067 INCHES DEEP AREA, BETWEEN FRAME 67 AND 68, -Y1732, -Z24. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED SEAT RACK PER SRM 53-00-15, 51-74-00, 51-42-00, 53-00-14. (M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM ASSEMBLY CORRODED 1 INCH BY 1.2 INCH BY .035 INCH DEEP AREA, BETWEEN FRAME 64/65, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

BFM - FOUND FLOOR PANEL CORRODED 1.5 INCH BY 2.5 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, Y1732, -Z240. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-42-11, 51-74-00. (M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM CORRODED 1 INCH BY .65 INCH BY .045 INCH DEEP AREA, FRAME 20, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-11-14, 51-23-11. CORROSION LEVEL 2. TASK NR JA-220-53500. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

BFM - FOUND CORSSBEAM CORRODED, 1 INCH BY .7 INCH BY .55 INCH DEEP, FRAME -Y254, CROSSBEAM C68 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M)

Part: SHEAR PLATE — CORRODED (FUSELAGE)

BFM - FOUND SHEAR PLATE CORRODED 1.2 INCH BY 1.3 INCH BY .012 INCH AREA, BETWEEN C69-C70, Y-1292. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11, 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2

BFM - FOUND BEAM CORRODED 2.8 IN BY 1.2 INCH BY .050 INCH DEEP AREA, FRAME 16, -Y1292, -Z240. CORROSION LEVEL 2, TASK NR JA-220-53500. FABRICATED AND INSTALLED ANGLE, DOUBLER, FILLER PER SRM 53-11-14, 53-1-14, 51-42-11. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

BFM - FOUND CROSSBEAM CORRODED 1.3 INCHES BY 1.9 INCH BY .033 INCH AREA, C68, Y-765, AND -Z240. REMOVED AND REPLACED CROSSBEAM PER SRM 51-74-00, 53-00-15, 53-00-14. (M)

Part: BEAM — CORRODED (FUSELAGE)

BFM - FOUND BEAM CORRODED 1 INCH BY .75 INCH BY .024 INCH DEEP, FRAME 68, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 53-00-14. CORRODED LEVEL 2, TASK NR JA-260-53500. (M)

Part: PSU — INOPERATIVE (EMERGENCY LIGHT)

PHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT POSITION FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHL - THE EMERGENCY POWER SUPPLY UNIT, FORWARD BATTERY PACK, WAS INOPERATIVE IN THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK. OPERATIONALLY CHECKS OK. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TPA - FOUND FLOORBEAM WITH 1 INCH SQUARE CORRODED AREA, UPPER SURFACE FLOOR SUPPORT BEAM Y765 AT FRAME 66. REMOVED AND REPLACED FLOORBEAM PER SRM 53-41-04. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND BEAM CORRODED .5 INCH AREA AROUND ATTACH HOLE, UPPER SURFACE FLOOR SUPPORT BEAM Y1292 AT FRAME 66. BLENDED CORRODED AREA AND RESTORED FINISH PER EA 94374. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT BEAM Y1732 FRAME 66. CLEANED CORRODED AREA, INSTALLED REPAIR ANGLES PER SRM 53-41-14 FIG 201. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PIT - FOUND BEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT 71292 AT FRAME 68. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR TRIPLER AT EXISTING SPLICE PER EA 94375. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOORBEAM Y1292 AT FRAME 16. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-11-15. (M)

Part: PROXIMITY SENSOR — FAULTY (NLG)

PIT - FLT 1686 - EN ROUTE DFW-PIT, ON APPROACH TO PIT, WHEN THE LANDING GEAR WAS EXTENDED, RECEIVED 'L/G DOORS NOT CLOSED' AND 'L/G SYSTEM DISAGREE' MESSAGES. THE NOSE GEAR DID NOT INDICATE GREEN. THE LANDING GEAR WAS RECYCLED AND THE GEAR EXTENDED ON THE SECOND ATTEMPT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOWNLOCK SYSTEM NR 1 PROXIMITY SENSOR (FIN 18GA). SYSTEM FUNCTIONALLY CHECKED OK. (M)

Part: LANDING GEAR — MALFUNCTIONED (NLG)

PIT - FLT 2153 - EN ROUTE PIT-MSP, THE NOSE LANDING GEAR FAILED TO EXTEND ON APPROACH TO MSP. THE LANDING GEAR WAS CYCLED AND WAS EXTENDED ONCE MORE. THE LANDING GEAR EXTENDED OK ON THE SECOND ATTEMPT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TESTED SYSTEM. CLEANED AND CHECKED CLEARANCES OF PROXIMITY SENSORS. SYSTEM BITE CHECK ON THE LANDING GEAR CONTROL AND INTERFACE UNIT WAS PERFORMED. NO FAULTS WERE FOUND. OK FOR SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

SFO - ROWS SIX AND THIRTEEN SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE WITH BROKEN WIRES AT THE SEAT CONNECTORS. MAINTENANCE REPLACED THE WIRES. OPERATIONALLY CHECKED OK. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

TPA - THE RIGHT OVERWING EXIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRES FOUND UNDER THE SEAT AND REPLACED THE POWER SUPPLY. OPS CHECKED OK. (M)