N631AA

Part: FRAME — GOUGED (FUSELAGE) · airframe 70,829 hrs · 25,138 cycles

FRAME 231 IS DENTED & GOUGED FROM ACCESS DOOR 113AL LOCKING PIN. INSTALLED A DOUBLER IAW EA B757-53-031426.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,182 hrs · 24,545 cycles

EMERGENCY LIGHT ON SEAT 16C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON SEAT 16C. OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 69,182 hrs · 24,545 cycles

EMERGENCY LIGHT ON SEAT 25D INOPERATIVE. FOUND BROKEN WIRE ON CONNECTOR. REPINNED AND SECURED. OPS CHECK NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 69,182 hrs · 24,545 cycles

SEAT 25D EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING AT CONNECTOR. OPS CHECK NORMAL.

Part: PUMP — LEAKING (LT ENGINE) · airframe 66,834 hrs · 23,683 cycles

LIM - CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED FLIGHT LANDED LIM WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLUID LEAKING FROM LEFT ENGINE DRIVEN PUMP.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT DECK HAS REPAIR DOUBLERS THAT DO NOT GO UNDER THE AFT CHORD ANGLE AND CORROSION ON DOUBLERS. REMOVED AND REPLACED AFT DECK SKIN PER AARD 51-10-05-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,542 hrs · 23,570 cycles

HFEC SURFACE INSPECTION INDICATES CRACK FORWARD LEFT SIDE OF ANTENNA MOUNT AREA, FRAME STATION 1473, STRINGER 30. INSTALLED DOUBLER AT ANTENNA MOUNT AREA, STATION 1473, STRINGER 30 PER EA B757-53-022325.

Part: PANEL — CRACKED (FUSELAGE) · airframe 66,542 hrs · 23,570 cycles

FLOOR SUPPORT PANEL UPPER CHORD AT BODY STATION 418 AND BUTTLINE 0 CRACKED. REMOVED AND REPLACED SUPPORT PANEL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

CORROSION ON TOP OF BEAM AT STATION 365 RIGHT BUTTLINE 10. FLOORBEAM WAS REPAIRED PER SRM 53-00-51-2R 3.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

G-1A GALLEY HAS CORRODED MOUNT ON FLOOR STRUCTURE, AFT OUTBOARD FLOOR FITTING FRAME STATION 320. REPLACED AFT OUTBOARD GALLEY MOUNT AT FRAME STATION 320 PER SRM 51-10-05-0G AND AARD 51-10-05-1 REPAIR 1.

Part: DOOR — CRACKED (L2) · airframe 66,542 hrs · 23,570 cycles

THE LEFT NUMBER 2 DOOR HAS A 1/2 INCH CRACK AT THE INBOARD RADIUS OF THE INNER CORD AT THE UPPER HINGE FRAME CUTOUT. INSTALLED DOUBLER PER SRM 52-10-02-2, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

LEFT NUMBER 4 DOOR AREA, FLOORBOARD SUPPORT IS CORRODED, STATIONS 1661 TO 1681, LEFT BUTTLINE 57. REMOVED CORROSION AS PER SRM 51-10-02-0G. INSTALLED A NEW FLOORBOARD SUPPORT PER SRM 51-10-02-0G, PARAGRAPH 9.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT GALLEY RIGHT AFT MOUNT BLOCK IS CORRODED AT STATION 1714, RIGHT BUTTLINE 52. REPLACED RIGHT AFT MOUNT BLOCK PER AARD 51-10-05-1, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

IN THE CABIN INBOARD OF THE RIGHT NUMBER 4 DOOR THRESHOLD THE FLOORBOARD SUPPORT BETWEEN STATIONS 1640 TO 1661 AT RIGHT BUTTLINE 57 IS CORRODED. REPLACED FLOORBOARD SUPPORT PER AARD 51-10-05-1, REPAIR 1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT GALLEY RIGHT Z ANGLE MOUNT IS CORRODED BETWEEN STATIONS 1715 TO 1721, RIGHT BUTTLINE 50. REMOVED CORROSION AS PER SRM 51-10-02-0G. INSTALLED NEW Z ANGLE MOUNT PER AARD 51-10-05-1, REPAIR 1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT GALLEY LEFT Z-ANGLE MOUNT IS CORRODED AT THE AFT END, STATIONS 1715 TO 1718, LEFT BUTTLINE 52. REPLACED LEFT Z-ANGLE PER AARD 51-10-05-1, REPAIR 1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

LEFT NUMBER 4 DOOR THRESHOLD SILL SUPPORT DRAIN FLOORBOARD SUPPORT L-ANGLE IS CORRODED FROM STATIONS 1675 TO 1680, LEFT BUTTLINE 54. REPLACED L-ANGLE PER AARD 51-10-5.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT GALLEY FORWARD CENTER MOUNT BLOCK IS CORRODED AT FRAME STATION 1687, BUTTLINE 0. REPLACED G-4 GALLEY FORWARD CENTER FLOOR FITTING PER AARD 51-10-05-1, REPAIR 1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

RIGHT NUMBER 4 DOOR THRESHOLD AREA SILL DRAIN SUPPORT FLOOR L-ANGLE IS CORRODED FROM STATIONS 1661 TO 1681, RIGHT BUTTLINE 57. REPLACED L ANGLE PER AARD 51-10-05-1, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

IN THE CABIN INBOARD OF THE RIGHT NUMBER 4 DOOR THRESHOLD THE FLOORBOARD SUPPORT BETWEEN STATIONS 1661 TO 1681 AT RIGHT BUTTLINE IS CORRODED. REPLACED FLOORBOARD SUPPORT PER AARD 51-10-05-1, REPAIR 1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

AFT GALLEYS RIGHT FORWARD MOUNT BLOCK IS CORRODED AT STATION 1687, RIGHT BUTTLINE 52. REPLACED GALLEY RIGHT FORWARD FLOOR FITTING PER AARD 51-10-05-1, REPAIR 1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

CORROSION ON Z ANGLE FROM STATIONS 1715 TO 1721. REPLACED Z ANGLE PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,542 hrs · 23,570 cycles

IN THE AFT CARGO, BELOW THE CABIN FLOOR THE INTERCOSTAL AT BUTTLINE 0, STATIONS 1580 TO 1600 IS CRACKED AT THE NUTPLATE. REMOVED AND REPLACED INTERCOSTAL BETWEEN STATIONS 1580 AND 1600 BUTTLINE 0 PER SRM 51-10-02-0G, PARAGRAPH 9.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

N/R 1838571. CORROSION ON HAT CHANNEL FROM FRAME STATIONS 1683 TO 1715. INSTALLED AFT CENTER HAT CHANNEL PER SRM 51-10-02-OG.

Part: SPAR — CRACKED (R2 DOOR) · airframe 66,542 hrs · 23,570 cycles

THE RIGHT NUMBER 2 DOOR HAS A CRACK AT THE OUTBOARD RADIUS OF THE INNER SPAR CHORD AT THE UPPER HINGE FRAME CUTOUT. INSTALLED UPPER HINGE CUTOUT DOUBLER PER SRM 52-10-02-2R 1 FIGURE 201 SHEETS 1 THROUGH 5 AND ESO 90282.

Part: FASTENER — CORRODED (LE SLAT) · corrosion level 2 · airframe 66,542 hrs · 23,570 cycles

NUMBER 1 SLAT INBOARD END, REAR SPAR-BLIND FASTENERS AND BLEND AREA HAVE CORROSION. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SLIDE — OUT OF POSITION (L4 DOOR) · airframe 66,297 hrs · 23,468 cycles

LEFT NUMBER 4 DOOR SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED. SLIDE FELL OUT OF HOUSING AND ASSIST BOTTLE DISCHARGED. AIRCRAFT FERRIED TO MIA FOR REPAIRS. REPLACED LEFT NUMBER 4 DOOR SLIDE AND ASSIST BOTTLE ON 01/24/2012 AT MIA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FUSE PIN — WORN (TE FLAP) · airframe 63,699 hrs · 22,497 cycles

ONT - INFLIGHT MIA-LAX. CREW REPORTED ON APPROACH AIRCRAFT EXPERIENCED A WINDSHEAR EVENT, POSSIBLE FLAP OVERSPEED WAS REPORTED. EMERGENCY DECLARED FLIGHT DIVERTED ONT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT FERRIED TO LAX. FOUND ONE LEFT OUTBOARD AND TWO RIGHT OUTBOARD FLAP FUSE PINS WORN. REPLACED PINS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TUBE — BLOCKED (NR 2 ENGINE) · airframe 62,271 hrs · 21,984 cycles

TUL - CREW REPORTED NUMBER 2 ENGINE INDICATION PROBLEM. FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BLOCKAGE IN P1 TUBE. REPLACED P1 TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,271 hrs · 21,983 cycles

ORIGINAL DOUBLER TO BE CHANGED AT NEXT C-CHECK PER BOEING. REMOVED DOUBLER AND INSTALLED NEW DOUBLER PER EA B757-53-013141.

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,271 hrs · 21,983 cycles

SHEAR WEB CORRODED AT APPROXIMATE STATION 960 AND RIGHT BUTTLINE 69. REMOVED AND REPLACED SHEAR WEB PER SRM 51-70-12-0G.

Part: ROTARY ACTUATOR — FAULTY (LE SLAT) · airframe 61,746 hrs · 21,783 cycles

ORD - CREW REPORTED ON APPROACH LEADING EDGE LIGHT ILLUMINATED WHEN FLAPS SELECTED. EMERGENCY DECLARED LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 14 AND 15 SLAT ROTARY ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 61,692 hrs · 21,764 cycles

AFT EMERGENCY PATHWAY LIGHTS IN COACH INOPERATIVE. REPLACED MODULE FOR EMERGENCY PATHWAY LIGHTS IN COACH. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,692 hrs · 21,764 cycles

AFT EMERGENCY PATHWAY LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATHWAY LIGHTS IN COACH. OPS CHECKED NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 61,692 hrs · 21,764 cycles

FORWARD EMERGENCY PATHWAY LIGHTS IN COACH INOPERATIVE. REPLACED MODULE FOR FORWARD EMERGENCY PATHWAY LIGHTS. OPS CHECKED NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,692 hrs · 21,764 cycles

FORWARD EMERGENCY PATHWAY LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY PATHWAY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,931 hrs · 21,481 cycles

LEFT NUMBER 1 AND RIGHT NUMBER 1 MARKING EMERGENCY FLOOD LIGHTS AND SEAT-MOUNTED EGRESS LIGHTS IN FIRST CLASS CABIN ARE VERY DIM AND WOULDN’T CHARGE. REMOVED AND REPLACED BATTERY MODULE AND PACK M10798 FOR FORWARD CABIN FLOOD AND FIRST CLASS SEAT-MOUNTED EGRESS LIGHTS. OPS CHECKED NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 60,931 hrs · 21,481 cycles

LEFT NUMBER 1 AND RIGHT NUMBER 1 MARKING EMERGENCY FLOOD LIGHTS AND SEAT-MOUNTED EGRESS LIGHTS IN FIRST CLASS CABIN ARE VERY DIM AND WOULDN’T CHARGE. REMOVED AND REPLACED BATTERY MODULE AND PACK M10798 FOR FORWARD CABIN FLOOD AND FIRST CLASS SEAT-MOUNTED EGRESS LIGHTS. OPS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 59,934 hrs · 21,116 cycles

EMERGENCY LIGHT AT RIGHT NUMBER FOUR R4 DOOR INOPERATIVE. RESET LAMP AT RIGHT NUMBER FOUR DOOR.

Part: BALLAST — OVERHEATED (CABIN) · airframe 59,833 hrs · 21,080 cycles

FLIGHT ATTENDANT REPORTED SMOKE AND ELECTRICAL SMELL IN AFT GALLEY AREA. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED OVERHEATED LIGHT BALLAST IN AFT GALLEY AREA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 59,116 hrs · 20,833 cycles

KIN - INFLIGHT MIA-MAR. CREW REPORTED ELECTRICAL SMELL IN THE CABIN. EMERGENCY DECLARED LANDED KIN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE WAS ACCOMPLISHED AT MIA. FOUND TRIM AIR PRESSURE REGULATING VALVE CONNECTOR LOOSE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,805 hrs · 20,719 cycles

FUSELAGE SKIN CORRODED AT DRAIN MAST. REPAIRED IAW EA B757-53-005790.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,805 hrs · 20,719 cycles

DOUBLER CORRODED AT DRAIN MAST. REPAIRED IAW SRM 51-40-02 AND EA B757-53-00-5790.

Part: TRANS PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,785 hrs · 20,713 cycles

AFT CARGO TRANSITION PANEL CORRODED. REPAIRED IAW SRM 51-70-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - RIGHT NUMBER ONE DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR FLOOD LIGHT AT RIGHT NUMBER ONE DOOR.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 57,651 hrs

SJU - EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. REPLACED SEAT 20D SEAT TO WALL HARNESS PLUG.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 57,651 hrs

SJU - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REINSTALLED SEAT 20D SEAT TO WALL HARNESS PLUG.

Part: SHROUD — MISSING (EMERGENCY LIGHT) · airframe 56,282 hrs

ORD EMERGENCY LIGHT SHROUD AT SEAT 17D MISSING. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 56,282 hrs

ORD, EMERGENCY LIGHT SOCKET AT SEAT 17D AFT DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D AFT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: SHROUD — DAMAGED (CABIN) · airframe 56,282 hrs

ORD EMERGENCY LIGHT SHROUD AT SEAT 5E DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,102 hrs · 56,102 cycles

JFK - EMERGENCY LIGHTS AT SEAT 26D TO LAST ROW INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 26D TO LAST ROW. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,102 hrs · 56,102 cycles

JFK - EMERGENCY LIGHT SIGN AT RT OVERWING DOOR INOPERATIVE. REPLACED SIGN FOR EMERGENCY LIGHT AT RT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,102 hrs · 56,102 cycles

JFK - EMERGENCY LIGHT ARROWS AT LT AND RT NR 4 DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ARROWS AT LT AND RT NR 4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LAMP — MISSING (EMERGENCY LIGHTS) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (SEAT 17D) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (SEAT 17D) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D MISSING LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — MISSING (EMERGENCY LIGHTS) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 54,348 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D MISSING RED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY SEAT MOUNTED LIGHTS AT FORWARD SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT FORWARD SECTION OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT SEATS 3E, 26D, AND 35D HAVE BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEATS 3E, 26D, AND 35D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT SEAT 35D INOPERATIVE. REPLACED SEAT 35D CONNECTOR FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY PATH LIGHT AT 17D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT SOCKET AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROW 9 INOPERATIVE. FOUND LOOSE CONNECTION. RECONNECTED LOOSE PLUG FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - BOTH EMERGENCY LIGHTS AT SEAT 17 BROKEN. REPLACED LIGHT ASSEMBLY FOR BOTH EMERGENCY LIGHTS AT SEAT 17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (FUSELAGE)

DFW - EMERGENCY LIGHTS AT L4 INOPERATIVE. REPLACED COLLAR ON LIGHT ASSEMBLY AND REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (FUSELAGE)

DFW - EMERGENCY EXIT LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MIA SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN AT SEAT 17D. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA EMERGENCY LIGHTS AT SEATS 1E TO 14D INOPERATIVE. REPLACED FIRST CLASS AND MID SECTION EMERGENCY LIGHT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA EMERGENCY LIGHT OVER SEAT 10D INOPERATIVE. REPLACED MID SECTION BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA THE 1L AND 1R SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED 1L AND 1R SIDEWALL EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA) FIRST CLASS LOWER AISLE WALL EMERGENCY LIGHT INOPERATIVE. REPLACED FIRST CLASS LOWER AISLE WALL EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA SEAT 3B EMERGENCY LIGHT INOPERATIVE. REPLACED FIRST CLASS EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — INOPERATIVE (EMERGENCY LIGHT)

MIA - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT ROW 18. REPAIRED ELECTRICAL PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — LEAKING (LEFT)

EN ROUTE LIM-DFW AT CRUISE, SMOKE DEVELOPED IN THE AIRCRAFT. RECEIVED EICAS LOW OIL PRESSURE FOR LT ENGINE. OIL QUANTITY DECREASED RAPIDLY. EMERGENCY DECLARED AND RETURNED TO LIM WITHOUT FURTHER INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - ROW 27 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 27D SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 15D INOPERATIVE. REPLACED SOCKET ASSEMBLY AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DRAIN LINE — LEAKING (HYDRAULIC SYS)

DEN - FLT 2329 - EN ROUTE DFW-DEN, LOST LEFT SIDE HYDRAULIC PRESSURE. LANDED DEN WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC DRAIN TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 29DEF)

TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 29DEF WOULD NOT TEST. RECONNECTED SEAT TO WALL CONNECTOR FOR SEAT 29DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — DEFECTIVE (CABIN)

DFW - FLT T0600 - EN ROUTE SNA/DFW DURING CRUISE, EMERGENCY EXIT LIGHTS ILLUMINATED SEVERAL TIMES AND THEN EXTINGUISHED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AFT CABIN EMERGENCY LIGHT TEST SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)