N632AA

Part: WIRE — BURNED (CABIN) · airframe 62,543 hrs · 22,140 cycles

LEFT EMERGENCY CHARGER CIRCUIT BREAKER POPPED AND COULD NOT BE RESET. FOUND BURNT WIRES ADJACENT TO THE P34 PANEL ABOVE FIRST CLASS DRAIN LINE. REPAIRED THE WIRING, OPS CHECK NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,654 hrs · 21,476 cycles

FIRST CLASS AISLE EMERGENCY LIGHTS ARE DIM. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (LE SLAT) · airframe 59,929 hrs · 21,236 cycles

LEFT WING NUMBER 1 SLAT SKIN IS CRACKED OUT FROM FASTENERS 2 FEET FROM OUTBOARD EDGE. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.

Part: SKIN — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON LOWER OUTBOARD SKIN OF NUMBER 1 SLAT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 57-43-01-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

NUMBER 1 SLAT HAS CORROSION 30 INCHES FROM INBOARD END ON SLAT SKIN. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON RIGHT NUMBER 7 SLAT ON UPPER SKIN IN AREA OF OUTBOARD MAIN TRACK. INSTALLED FLUSH DOUBLER REPAIR UNDER AARD 57-43-00-1.

Part: SKIN — CORRODED (NR 7 SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON NUMBER 7 SLAT ON UPPER SKIN IN AREA OF OUTBOARD AUXILIARY TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.

Part: SKIN — CORRODED (NR 7 SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON NUMBER 7 SLAT IN AREA OF CENTER RIB ON UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON NUMBER 7 SLAT SKIN IN AREA OF INBOARD AUXILIARY TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

NUMBER 10 SLAT HAS DEEP BLEND WITH BLIND FASTENER ON UPPER SKIN 29.5 INCHES FROM INBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-34-10.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

NUMBER 10 SLAT HAS DEEP BLEND AND BLIND FASTENER 28 INCHES FROM OUTBOARD END ON UPPER SKIN. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

CORROSION ON NUMBER 10 SLAT LOWER SKIN FORWARD OF OUTBOARD AUXILIARY TRACK. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-43-01.

Part: GATE — CRACKED (R2 DOOR) · airframe 59,929 hrs · 21,236 cycles

RIGHT NUMBER TWO ENTRY DOOR HAS A CRACKED UPPER GATE AT THE ROD END ATTACH POINT. REMOVED AND REPLACED UPPER GATE PER ESO 90282.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 59,929 hrs · 21,236 cycles

RIGHT NUMBER TWO ENTRY DOOR LOWER GATE IS CORRODED ON BOTTOM EDGES. REMOVED AND REPLACED LOWER GATE PER ESO 90282.

Part: TORQUE BOX — CRACKED (R2 DOOR) · airframe 59,929 hrs · 21,236 cycles

RIGHT NUMBER TWO ENTRY DOOR HANDLE TORQUE BOX IS CRACKED. INSTALLED NEW TORQUE BOX PER ESO 90282.

Part: GATE — CRACKED (R1 DOOR) · airframe 59,929 hrs · 21,236 cycles

RIGHT NUMBER ONE DOOR UPPER GATE CRACKED. INSTALLED NEW UPPER GATE PER ESO 90284.

Part: PAN — CRACKED (L2 DOOR) · airframe 59,929 hrs · 21,236 cycles

LEFT NUMBER TWO ENTRY DOOR HANDLE BOX CRACKED. REMOVED AND REPLACED DOOR HANDLE BOX PER ESO90282.

Part: PLACARD — DEFORMED (CABIN)

DFW - LEFT FORWARD OVERWING EXIT ARROW DISFORMED. REPLACED LEFT FORWARD OVERWING EXIT ARROW.

Part: PLACARD — DEFORMED (CABIN)

DFW - RIGHT FORWARD OVERWING EXIT ARROW DISFORMED. REPLACED RIGHT FORWARD OVERWING EXIT ARROW.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT LIGHT AFT OF FLAP INOPERATIVE. REPLACED LAMP AT RIGHT EXIT AFT OF FLAP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT LEFT MID CABIN FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT MID CABIN FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - AFT SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY FOR SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - OVERWING EMERGENCY EXIT SIGN LIGHT AT MID CABIN CEILING IS MISSING LENS. REPLACED LENS FOR THE OVERWING EMERGENCY EXIT SIGN LIGHT AT MID CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. RELAMPED AFT LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 17D FORWARD INOPERATIVE. RELAMPED EMERGENCY LIGHT AND REINSTALLED NEW LENS AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (CABIN)

DFW - TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 9D THROUGH 14D. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHT ABOVE RIGHT AFT EMERGENCY EXIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BALLAST AT SEAT 17ABC SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — OUT OF ADJUST (GIRT BAR)

TUL - FOUND DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - FOUND EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RECONNECTED CONNECTOR AT SIDEWALL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

FOUND SEAT 9D EMERGENCY PATH LIGHTS INOPERATIVE. FOUND BAD CONNECTOR AT MUX COVER UNDERSEAT. REPLACED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D AND 15D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 14D AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 15DEF THROUGH 22DEF INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT PIN CONNECTORS AT SEAT 15DEF AND 22DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD LEFT OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT FORWARD LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT COFFEE BAR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT COFFEE BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND RIGHT AFT SERVICE DOOR EXIT LIGHT MARKER ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT MARKER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM OVERWING EXIT TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP BETWEEN OVERWING EXIT AND FORWARD GALLEY. ALSO, REPLACED FORWARD EPM BATTERY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 1630)

AFW - CORROSION BLENDED OUT ON FLOORBOARD AT STA 1640, RBL 57 AND RBL ZERO, BEYOND SRM LIMITS. REPAIRED PER MRB 757-593. TST, 15,867.21 HRS. CYCLES, 5,989. (X)

Part: SKIN — DAMAGED (BS 416)

AFW - FUSELAGE SKIN HAS TEMPORARY REPAIR INSTALLED WITH BLIND FASTENERS BETWEEN S21 AND S22L. REPAIRED PER MRB 757-604. TST, 15,867.21 HRS. CYCLES, 5,989. (X)

Part: FLOOR BEAM — CORRODED (BS 1661)

AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 1661, LBL 9.5, BEYOND SRM LIMITS. REPAIRED PR MRB 757-594. TST 15,867.21 HRS. CYCLES, 5,989. (X)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 377, LBL 42 AND LBL 48, ALSO, LBL 31 AND LBL 22, BEYOND SRM LIMITS. REPAIRED PER MRB 757-596. TST, 15,687.21 HRS. CYCLES, 5,989. (X)

Part: SKIN — DENTED (BS 1400-1420)

AFW - FUSELAGE SKIN HAS SEVERAL DENTS BEYOND SRM LIMITS AT STA 1400 AND STA 1420 FROM S28L TO S27R. REPAIRED PER MRB 757-603. TST, 15,867.21 HRS. CYCLES, 5,989. (X)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 324, RLB 60, BEYOND SRM LIMITS. REPAIRED PER MRB 757-595. TST, 15,687.21 HRS. CYCLES, 5,989. (X)

Part: DECK PLATE — CORRODED (BS 1680/1720)

AFW - DECK PLATE AT STA 1680 AND STA 1720 HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS BL LOCATIONS. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-602. TST, 15,867.21 HRS. CYCLES, 5,989. (X)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - CORROSION BLEND OUT AT STA 365, RBL 10 AND RBL 59, BEYOND SRM LIMITS. REPAIRED PER MRB 757-597. TST, 15,687.21 HRS, CYCLES 5,989. (X)