N559AA

Part: SWITCH — FAILED (CABIN PRESSURE) · airframe 67,717 hrs · 35,160 cycles

PRESSURIZATION VALVE WENT TO FULL CLOSED. THE ONLY WAY TO CONTROL CABIN WAS TO USE MANUAL CONTROL WITH PACKS OFF. AN EMERGENCY WAS NOT DECLARED, LANDED UNEVENTFULLY. REPLACED CABIN PRESSURE AUTO/MANUAL SWITCH IAW AMM 21-32-05.

Part: ENGINE — FAILED (NR 1) · airframe 67,138 hrs · 34,791 cycles

AIR INTERRUPT, RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING CLIMBING THRU 25000 HEARD A VIOLENT BANG & ACFT SHOOK, NR 1 ENGINE FAILED. DURING INSPECTION ENGINE WAS FOUND TO HAVE TURBINE BLADE DISTRESS. R & R NR 1 ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,943 hrs · 34,672 cycles

L1 DOOR EMER LIGHT DID NOT ILLUMINATE ON TEST. R & R LIGHT ASSEMBLY. SYS CHECKED NORMAL.

Part: O-RING — SPLIT (SHUT-OFF VAVLE) · airframe 66,519 hrs · 34,402 cycles

RIGHT HYD SYS QTY LOSS. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED SPLIT O RING ON SPOILER SOV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STRUT — MALFUNCTIONED (NLG) · airframe 65,164 hrs · 33,625 cycles

DFW CREW REPORTED RED NOSE GEAR LIGHT ILLUMINATED AFTER TAKEOFF FOLLOWED BY LOSS OF PRESSURIZATION. AUTO SPOILER DO NOT USE & STALL INDICATION FAILURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPACKED NOSE STRUT. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 64,633 hrs · 33,327 cycles

LT HAND WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED INBD FORMER DOUBLER IAW EA MD80-57-032474.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 64,480 hrs · 33,247 cycles

DAMAGE TO FORWARD ENTRY DOOR, EXTERNAL SKIN LOWER EDGE. BLENDED OUT DAMAGE & INSTALLED EXTERNAL DOUBLE IAW AARD 52-10-00-2.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,877 hrs · 32,893 cycles

FORWARD ENTRY EMERGENCY DOME LIGHT WEAK & STAYS ILLUMINATED WHEN AIRCRAFT POWER & EMERGENCY SWITCH ARE BOTH OFF. REPLACED THE FORWARD POWER BATTERY. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,877 hrs · 32,893 cycles

AFT EMERGENCY DOME LIGHT WEAK & ILLUMINATES WHEN POWER IS OFF. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: DUCT — LEAKING (AC BAY) · airframe 62,463 hrs · 32,089 cycles

SFO - INFLIGHT SJC-DFW CREW REPORTED TAIL COMPARTMENT TEMPERAURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. EMERGENCY DECLARED FLIGHT DIVERTED SFO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND TOP DUCT LEAK FROM TUBING ABOVE HEAT EXCHANGER. REPOSITIONED SCAFT HOSE AND CLAMPS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COUPLER — OUT OF POSITION (AC BAY) · airframe 62,444 hrs · 32,078 cycles

PVR - CREW REPORTED TAIL COMPARTMENT OVERHEAT WARNING. EMERGENCY DECLARED FLIGHT RETURNED PVR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED LEFT PRIMARY HEAT EXCHANGER INLET DUCT SLIDING PNEUMATIC COUPLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 60,412 hrs · 30,954 cycles

TUL - INFLIGHT DFW-STL. CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT TUL ON 05/26/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,384 hrs · 30,936 cycles

AFT ACCESSORY, SHEAR TIE CRACKED AT AFT SIDE OF STATION 1451 AFT OF LONGERON 2 RIGHT. REMOVED CRACKED SHEAR TIE AND INSTALLED SERVICEABLE SHEAR TIE PER AARD 51-10-00-5 AND BOEING DRAWING 9911860 CONF 1.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,114 hrs · 30,783 cycles

BOTH LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: SENSOR — INOPERATIVE (NLG) · airframe 58,290 hrs · 29,741 cycles

DFW - CREW REPORTED UPON GEAR RETRACTION, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. LIGHT REMAINED ON AFTER CYCLING GEAR. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED D1-32 NOSE GEAR LOCK SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,180 hrs · 29,682 cycles

AFT CABIN EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EMERGENCY PATH LIGHTS. OPS CHECK NORMAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

LEFT ALTERNATE STATIC PORT DOUBLER IS CORRODED. INSTALLED DOUBLER PER AARD 53-30-00-07.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

CABIN - CORROSION AROUND HOLES IN PAN UNDER GIRT BAR FITTING BRACKET AT STATION 1142 AT AFT SERVICE DOOR [2EA PLACES]. INSTALLED DOUBLER AT APPROXIMATELY STATION 1142 PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

FUSELAGE AFT LAVATORY SERVICE PANEL PAN SEPARATING FROM SKIN AT LOWER FORWARD CORNER. INSTALLED AFT LAVATORY SERVICE PAN AS PER AARD 53-30-00-7.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

CABIN, STATION 1142, AT AFT SERVICE DOOR, CORROSION AROUND HOLES IN PAN UNDER GIRT BAR FITTING BRACKET. REMOVED CORROSION IN PAN UNDER GIRT BAR FITTING BRACKET. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

RIGHT CUSP HAS 2 INCH CRACK AT STATION 1300. INSTALLED CUSP DOUBLER AT STATION 1300 RIGHT SIDE PER AARD 53-20-0-16.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 56,958 hrs · 29,027 cycles

FORWARD ENTRY DOOR INNER SKIN AT FORWARD CORNER IS DENTED. FOUND CRACKED FASTENER HOLE. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

FUSELAGE SKIN HAS DENT WITH GOUGE STATION 507 AT LONGERON 22 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIGURE 30 SHEET 20 VIEW E.

Part: SKIN — BULGED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

FUSELAGE SKIN BULGED STATION 308 BETWEEN LONGERONS 24 AND 25 RIGHT. DOUBLER INSTALLED PER SRM 53-04-00 FIGURE 12B SHEET 18.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

MID CARGO DOOR BEAM HAS CORROSION STATION 636 TO 693. ACCOMPLISHED DOUBLER REPAIR ON CARGO DOOR BEAM FROM STATIONS 636 TO 693 PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

RIGHT CUSP HAS CORROSION, LOWER SIDE, STATIONS 598 TO 617. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

CUSP AT STATIONS 223 TO 226 RIGHT CORRODED. INSTALLED CUSP SHEET PER EA MD80-51-014350 DATED 12/7/10 AND PER AARD 51-10-00-5.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

AFT CARGO - CORROSION AT LONGERON SPLICE 28 LEFT STATIONS 1196 TO 1208. INSTALLED NEW SPLICE PART 3914677-507 PER AARD 51-10-00-5 AND BOEING DRAWING 5936667.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

AFT CARGO - CORROSION AT LONGERON SPLICE 27 LEFT STATIONS 1196 TO 1208. INSTALLED NEW LONGERON SPLICE 3914677-507 PER AARD 51-10-00-5 AND BOEING DRAWING 5936667.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

CORROSION OUT OF LIMITS IN CUSP LEFT SIDE BETWEEN STATIONS 617 TO 636. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

RIGHT CUSP STATION 370 HAS HOLE. CLEARANCE TO INSTALL DOUBLER REF AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,958 hrs · 29,027 cycles

LEFT STATION 984 LOWER FORWARD WINDOW PAN EAR CRACKED. INSTALLED REPAIR ANGLE, STRAP AND FILLERS PER PRELIMINARY EA AND AARD 53-10-00-25.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

NUMBER 4 SEAT TRACK DAMAGED. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

CORROSION ON GALLEY NUMBER 1 OUTBOARD FLOOR MOUNT AT STATION 160. REMOVED OUT OF LIMITS MOUNT, DRILLED, TREATED AND PRIMED NEW ONE AND INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5 AND BOEING DRAWING 9936534.

Part: CUSP WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

CUSP AT STATIONS 716 TO 718 RIGHT IS OUT OF LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

CORROSION ON GALLEY NUMBER 1 CENTER FLOOR MOUNT AT STATION 160. REMOVED OUT OF LIMITS MOUNT, DRILLED, TREATED AND PRIMED NEW ONE AND INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5 AND BOEING DRAWING 9936534.

Part: PAN — CRACKED (WINDOW) · airframe 56,958 hrs · 29,027 cycles

LEFT STATION 1022 UPPER AFT WINDOW PAN EAR CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,958 hrs · 29,027 cycles

WINDOW PAN CRACKED, UPPER FORWARD CORNER BETWEEN OVERWING EXIT DOORS LEFT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 29,027 cycles

FOUND CORROSION UNDER G-1 GALLEY DRAIN PAN ON SUBFLOR. INTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,958 hrs · 29,027 cycles

GEAR RIGHT WHEEL WELL LONGERON 20 RIGHT CRACKED STATION 996. INSTALLED REPAIR DOUBLER AND FILLER ON RIGHT LONGERON 20 AT STATION 996 PER AARD 53-10-00-18.

Part: PAN — CRACKED (WINDOW) · airframe 56,958 hrs · 29,027 cycles

RIGHT STATION 946 UPPER FORWARD WINDOW PAN EAR CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,958 hrs · 29,027 cycles

RIGHT STATION 1136 LOWER FORWARD WINDOW PAN EAR CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,954 hrs · 28,478 cycles

ESCAPE PATH LIGHTS FROM 3 TO 19 INOPERATIVE. REPLACED BATTERY PACK FOR ESCAPE PATH LIGHTS FROM 3 TO 19. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,954 hrs · 28,478 cycles

ROW 3 TO 6 EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD CABIN BATTERY PACK FOR ROW 3 TO 6 EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,954 hrs · 28,478 cycles

FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT FORWARD CABIN EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: DOOR — OPEN (NLG) · airframe 55,891 hrs · 28,442 cycles

AUS - CREW REPORTED VIBRATIONS FROM NOSE GEAR AREA. EMERGENCY DECLARED FLIGHT RETURNED AUS LANDED WITHOUT INCIDENT. FOUND LEFT FORWARD NOSE GEAR DOOR PARTIALLY OPEN ON ARRIVAL. INSPECTED NOSE GEAR DOOR RELEASE MECHANISM AND LINKAGE-NO DEFECTS/DAMAGE NOTED. VERIFIED DOORS SECURED CLOSED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,097 hrs · 26,944 cycles

OVERWING EMERGENCY LIGHTS COME ON WHEN ELECTRICAL POWER TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER MM 33-53-00-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 26,944 cycles

THE 1510 CANT FRAME CRACKED AT LOWER LT ALIGNMENT PIN. INSTALLED REPAIR DOUBLER IAW EA NR MD 80-53-006585.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,041 hrs · 26,916 cycles

FORWARD CABIN OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER AMM 33-53-00-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,041 hrs · 26,916 cycles

BATTERY PACK AB5-4 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK S/N OFF 19032 S/N ON 20770 PER AMM 33-60-98-4, OPERATIONALLY CHECKED GOOD PER MCM CARD 4289.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,041 hrs · 26,916 cycles

BATTERY PACK AB5-3 INOPERATIVE. REMOVED AND REPLACED BAT5016 S/N OFF 18667 S/N ON 14940 IN ACCORDANCE WITH AMM 33-60-98-4, OPERATIONALLY CHECKED PER MCM CARD 4289.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,041 hrs · 26,916 cycles

CRACKS IN FORWARD SIDE OF BULKHEAD AT STATION 37 AT UPPER LEFT RADOME ALIGNMENT PIN. INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: STOP FITTING — CRACKED (DOOR) · airframe 53,041 hrs · 26,916 cycles

STOP FITTING CRACKED AT AFT END OF DOOR, AT THE END OF NUMBER 3 BEAM.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,041 hrs · 26,916 cycles

MID CARGO DOOR STOP CRACKED. REPLACED WITH NEW DOOR STOP --CDK 2345-3 ON DOO2492 PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,041 hrs · 26,916 cycles

DOOR STOP FITTING CRACKED, LOWER AFT EDGE OF AFT CX DOOR. REPLACED FITTING PER ESO 80174.

Part: GUARD — DAMAGED (EMERGENCY LIGHTS) · airframe 52,419 hrs

DFW - EMERGENCY LIGHT GUARD AT SEAT 27D DAMAGED. REPLACED EMERGENCY LIGHT GUARD AT SEAT 27D.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 52,419 hrs

DFW - RIGHT AFT OVERWING EXIT MARKER DECAL DAMAGED. REPLACED RIGHT AFT OVERWING EXIT DECAL.

Part: BRAKE ASSY — OVERHEATED (MLG) · airframe 51,571 hrs

DFW - DURING TAKEOFF ROLL BRAKE TEMPERATURE LIGHT FLASHED AT 100 KNOTS FOLLOWED BY A STEADY LIGHT AND TEMPERATURE HIGH INDICATION. ABORTED TAKEOFF AT 110 KNOTS. AIRCRAFT TOWED TO HANGAR FOR EVALUATION. REPLACED NUMBER ONE MAIN LANDING GEAR BRAKE ASSEMBLY AND TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 50,493 hrs

LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. SECURED LOOSE BATTERY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,635 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 14, 18, 21, AND 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 14, 18, 21 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS FROM SEAT ROWS 20 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 20 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY ESCAPE PATH LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT FLIGHT DECK OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FLIGHT DECK OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — INOPERATIVE (SERVICE DOOR)

LAS - RAMP SERVICE FOUND SLIDE PACK AT LEFT SERVICE DOOR BROKEN AND ON GROUND. CATERING DROPPED SLIDE WHEN SERVICING AIRCRAFT. SLIDE DID NOT DEPLOY. REPLACED SLIDE FOR LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHUTOFF VALVE — INOPERATIVE (A/C PACK)

ORD - INFLIGHT FLIGHT ATTENDANTS AND PILOTS REPORTED HOT SMELL AND SMALL AMOUNT OF SMOKE IN MID CABIN. RETURNED TO ORD AND LANDED OVERWEIGHT WITHOUT INCIDENT. SMOKE CLEARED ON FINAL. ACCOMPLISHED OVERWEIGHT INSPECTION AND LEAK CHECK. AS PRECAUTION REPLACED BOTH PACK PRESSURE SHUT OFF VALVES AND EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FORWARD OVERWING EMERGENCY EXIT SIGN ON BOTH SIDES INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD OVERWING EMERGENCY EXIT SIGN ON BOTH SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ATL - EMERGENCY EXIT SIGNS OVER ROW 20AB AND 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS OVER ROWS 20AB AND 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING OVERNIGHT MAINTENANCE FOUND AFT UPPER CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT UPPER CABIN EMERGENCY LIGHT BATTERY PACK B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — MALFUNCTIONED (NR 2 ENGINE)

AIRCRAFT EN ROUTE FROM ORD-MIA, LOSS ENGINE OIL PRESSURE ON CLIMB-OUT. EMERGENCY DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED. REMOVED AND REPLACED THE NR 2 ENGINE. LEAK AND SYSTEM GROUND CHECKED NORMAL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK, FS 1295-1309. REPLACED SEAT TRACK PER 53-05-00. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO HORIZONTAL AND VERTICAL LEG OF DOOR BEAM. INSTALLED DOUBLER REPAIR AT STATION 1172.1 TO STATION 1195.1. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM FIRST CLASS TO MID CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (L1 DOOR)

MIA - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)