N629AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,589 hrs · 22,649 cycles

EMERGENCY EXIT PATH LIGHTING INOPERATIVE FROM ROWS 16 TO 25. REPLACED DEFECTIVE BATTERY PACK ON EMERGENCY LIGHTS CONTROL MODULE M10800.

Part: HYDRAULIC LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 61,016 hrs · 21,735 cycles

MIA - CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY DECREASE. EMERGENCY DECLARED, RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE AUTO PILOT SERVO HYDRAULIC PRESSURE LINE AND THE UNION AND PACKING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,968 hrs · 21,718 cycles

NUMBER 1 SLAT LEFT OUTBOARD POSITION HAS SEVERAL AREAS OF CORROSION. REPLACED SLAT SKIN WITH NEW SKIN PER ESO 90253.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,853 hrs · 21,674 cycles

FIVE LOCAL DEEP BLENDS ON THE UPPER SKIN OF NUMBER 3 SLAT. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,853 hrs · 21,674 cycles

NUMBER 3 SLAT HAS PITTING IN THE LEADING EDGE SKIN AT PREVIOUS BLEND SITES. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2.

Part: WEDGE — WORN (LE SLAT) · airframe 60,853 hrs · 21,674 cycles

REMOVED AND REPLACED TRAILING EDGE WEDGE PER ESO 90246.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

SLANT PANEL ATTACH BRACKET CRACKED AND CORRODED AT FLOOR LEVEL STATION 1720 56 INCHES RIGHT OF CENTER LINE. REPLACED BRACKET PER SRM 51-10-02-0G.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,834 hrs · 21,664 cycles

AFT FUSELAGE SKIN DENT ON GOUGE AT FUSELAGE STATION 1700 BETWEEN STRINGER 14 RIGHT AND 15 RIGHT. REPAIRED BY INSTALLING EXT DOUBLER PER EA 757-53-008236.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,834 hrs · 21,664 cycles

DENT WITH GOUGE ON EXTERNAL SKIN AT STATION 1421, LOWER FUSELAGE BETWEEN STRINGER 29 RIGHT AND 30 RIGHT. ACCOMPLISHED EXTERNAL DOUBLER REPAIR UNDER SRM 53-00-01-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

CORROSION ON STRINGER 29 RIGHT BETWEEN STATIONS 1400 AND 1420. ACCOMPLISHED SPLICE REPAIR UNDER SRM 53-00-03-2.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

BATHTUB FITTING CORRODED. REPLACED FITTING.

Part: SLAT TRACK — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

LEFT WING NUMBER 2 SLAT AT INBOARD AUXILIARY TRACK HAS CORROSION BLENDED OUT OF LIMITS ON THE LOWER NOSE SKIN. INSTALLED STRAP PER ESO 90309.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

NUMBER 2 LEFT OUTBOARD SLAT HAS CORROSION AT FASTENER 20 INCHES FROM OUTBOARD END ON UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

RIGHT WING IRREGULARITY IN NUMBER 8 SLAT SKIN 24 INCHES INBOARD OF OUTBOARD ACCESS PANEL. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

RIGHT WING IRREGULARITY IN NUMBER 8 SLAT SKIN 3 INCHES OUTBOARD OF INBOARD ACCESS PANEL. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

RIGHT WING IRREGULARITY IN NUMBER 8 SLAT SKIN 24 INCHES OUTBOARD OF INBOARD ACCESS PANEL. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 57-43-00-1.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 60,834 hrs · 21,664 cycles

RIGHT WING NUMBER 8 SLAT COVE SKIN CRACKED AT INBOARD TRACK MOUNT CASTING AREA. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 60,834 hrs · 21,664 cycles

RIGHT WING NUMBER 8 SLAT OUTBOARD COVE SKIN CRACKED AT INBOARD TRACK MOUNT CASTING AREA. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.

Part: TORQUE BOX — CRACKED (SERVICE DOOR) · airframe 60,834 hrs · 21,664 cycles

RIGHT NR 4 DOOR TORQUE BOX CRACKED. REPLACED HANDLE TORQUE BOX PER ESO 90108.

Part: PAN — GOUGED (DOOR HANDLE) · airframe 60,834 hrs · 21,664 cycles

LEFT NR 1 DOOR HANDLE PAN GOUGED. REMOVED AND REPLACED HANDLE PAN PER ESO 90283

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 60,834 hrs · 21,664 cycles

LEFT NR 2 DOOR AT LOWER GATE HAS CORROSION ON BOTTOM. REPLACED LOWER GATE PER ESO 90282.

Part: GATE — DAMAGED (SERVICE DOOR) · airframe 60,834 hrs · 21,664 cycles

RIGHT NUMBER 4 DOOR, LOWER GATE AFT RETAINER WORN. REMOVED WORN RETAINER, EXCESSIVE WEAR UNDER RETAINER. REPLACED LOWER GATE ASSEMBLY AND RETAINER PER ESO 90108.

Part: MODULE — INOPERATIVE (ANTI SKID SYS) · airframe 56,981 hrs · 56,981 cycles

MIA INFLIGHT T1944/29JUN SJU TO IAD. CREW REPORTED RT HYDRAULIC SYSTEM LOSS. SHUT DOWN RT HYDRAULIC SYSTEM. LANDED MIA WITHOUT INCIDENT. REPLACED RT HAND ANTISKID CONTROL MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: HYDRAULIC LINE — LEAKING (MLG)

CCS INFLIGHT T2133/03MAY - CREW REPORTED LEFT HYDRAULIC SYSTEM FAILED AFTER LOWERING LANDING GEAR. LANDED WITHOUT INCIDENT AND AIRCRAFT WAS TOWED TO GATE. FOUND A HOSE ASSEMBLY AT MAIN LANDING GEAR DOWNLOCK AT LEFT MAIL LANDING GEAR LEAKING. REPLACED HOSE FOR LEFT MAIN LANDING GEAR DOWNLOCK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,868 hrs

DFW EMERGENCY SPOT LIGHT AT SEAT 18F INOPERATIVE. REPLACED LAMP FOR EMERGENCY SPOT LIGHT AT SEAT 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: ACTUATOR — LEAKING (RIGHT REVERSER)

JFK INFLIGHT - LOSS OF RIGHT HYDRAULIC DURING LANDING. LANDED JFK WITHOUT INCIDENT. AIRCRAFT TAXIED TO GATE NORMALLY. REPLACED ACTUATOR FOR RIGHT REVERSER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LAX - EMERGENCY LIGHT AT FORWARD LEFT HAND OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT STATION 310 AT FORWARD LEFT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS ON SEAT ROWS 16 TO 26 INOPERATIVE. REPLACED BATTERY PACKS AND CHARGER FOR EMERGENCY LIGTHS ON SEAT ROWS 16 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT ALL SEATS INOPERATIVE. REPLACED ALL BATTERY PACKS AND MODULES FOR EMERGENCY LIGHTS AT ALL SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

STL - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 16 TO 24D INOPERATIVE. REPLACED BATTERY PACKS AT MID AND FORWARD CABIN AND BATTERY AND MODULE AT MID AND AFT CABIN FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - EMERGENCY EXIT LIGHT AT DOOR RIGHT ONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT DOOR RIGHT ONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DEFECTIVE (CABIN)

MIA EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY LIGHT WIRE BUNDLE CONNECTOR AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (HYD SYSTEM)

EN ROUTE, LOST CENTER SYSTEM HYDRAULIC QUANTITY. LANDED WITHOUT INCIDENT. REPLACED 2 CENTER HYDRAULIC MODULE FLEX LINES AND SERVICED CENTER HYDRAULIC OIL QUANTITY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE)

DEN - FLT 432 - EN ROUTE DEN-DFW, AFTER TAKEOFF, THE LEFT ENGINE HAD WHAT APPEARED TO BE A PRESSURE STALL. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. PERFORMED ENGINE BORESCOPE PER MM. REPLACED THE LEFT AND RIGHT HP3 SOLENOIDS, HP2 SOLENOID, LEFT AND RIGHT HP3 BLEED VALVES AND HP2 BLEED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERWING EMERGENCY EXIT LIGHT DAMAGED. REPLACED AFT OVERWING EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (ROW 16-25)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM 16D TO 25D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, MID FUSELAGE AISLE EXIT SIGN INOPERATIVE. REPAIRED GROUND AT LIGHT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY OVERWING EXIT SIGN INOPERATIVE. REPAIRED GROUND AT LIGHT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HANDLE PAN — GOUGED (R4 DOOR)

AFW - FOUND R-4 DOOR HANDLE PAN HAD SMALL GOUGE BLENEDD BEYOND SRM LIMITS. PER MRB 757-959, BLEND OUT AND REFINISHED PER SRM. (M)

Part: SKIN — DAMAGED (HORIZ STAB)

AFW - LEFT AND RIGHT NR 3 STABILIZER UPPER SKIN PANELS HAVE SEVERAL DENTS, HAIL DAMAGE. PER MRG 757-957. REINSPECT EVER C-CHECK. (M)

Part: CONNECTOR — BROKEN (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROWS 6E AND 28D INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS BY PASSENGER SEAT ROWS 6E AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (NLG)

LAX - FLT NR 201 - DURING APPROACH TO SNA WIHT LANDING GEAR HANDLE IN DOWN POSITION, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR DOORS AND GEAR AMBER LIGHTS REMAINED OUT. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR GREEN LIGHT ASSEMBLY. ACCOMPLISHED BITE CHECK AT GROUND PROXIMITY UNIT WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)