N649AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,138 hrs · 23,461 cycles

EMERGENCY LIGHTS FROM ROWS 26 THRU 30 DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 26 THRU 30. OPERATIONS CHECKED NORMAL.

Part: MODULE — DEFECTIVE (CABIN) · airframe 68,140 hrs · 23,462 cycles

SEAT MOUNTED LIGHT ROW 26-36 TOO DIM. REPLACED BATTERY MODULE M10801. OPERATIONS CHECKED NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 66,905 hrs · 23,037 cycles

CABIN EMERGENCY LIGHT LENS COVER BROKEN. REPLACED LENS COVER FOR CABIN EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,230 hrs · 22,427 cycles

EMERGENCY EXIT LIGHT AT ROW 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT ROW 12D. OPS CHECK NORMAL.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 64,836 hrs · 22,292 cycles

DFW - CREW REPORTED SMOKE ODOR IN COCKPIT. EMERGENCY DECLARED FLIGHT LANDED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PANEL — DENTED (HORIZ STAB) · airframe 64,780 hrs · 22,268 cycles

MULTIPLE HAIL DENTS UPPER SURFACE RIGHT HORIZONTAL STABILIZER INBOARD PANEL. ACCOMPLISHED BONDED REPAIR PER EA B757-55-024145.

Part: BEAM — CRACKED (NLG WW) · airframe 64,780 hrs · 22,268 cycles

VERTICAL BEAM ON FORWARD SIDE OF NOSE LANDING GEAR WHEEL WELL PRESSURE DECK STATION 263, LEFT BUTTLINE 10, SHOWS INDICATION OF CRACK AT UPPER END. INSTALLED NEW VERTICAL BEAM PER AARD 51-00-05-1.

Part: DOOR FRAME — DAMAGED (R2 DOOR) · airframe 64,780 hrs · 22,268 cycles

CRACK IN NUMBER 2 RIGHT PASSENGER DOOR IN UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-10-01-2R.

Part: DUCT — FAILED (CABIN) · airframe 63,173 hrs · 21,667 cycles

MIA - FLIGHT ATTENDANTS REPORTED LOOSE CEILING PANEL AND AIR LEAK IN AFT CABIN. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND OVERHEAD AIR DISTRIBUTION DUCT BETWEEN ROW 27 AND ROW 30 DAMAGED. REPLACED DUCT BETWEEN ROWS 27 AND 30. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — INOPERATIVE (TE FLAP) · airframe 63,134 hrs · 21,653 cycles

MIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAY K10104. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

FUSELAGE SKIN CORRODED STATIONS 1680 TO 1740 BETWEEN STRINGERS 29 LEFT TO 25 RIGHT. REPAIRED IN ACCORDANCE WITH EA B757-53-015792.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CORROSION ON STRINGER 29 RIGHT JUST OUTBOARD LAVATORY SERVICE PANEL STATIONS 1640 TO 1680. INSTALL STRINGER REPAIR PER EA B757-53-015796.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 61,439 hrs · 21,034 cycles

FLOOR STRINGER HAD DEEP GOUGE IN IT AT STATION 1496. REPLACED STRINGER FROM STATIONS 1440 TO 1680 PER AARD 51-10-05-1.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

TEE CAP AT AFT CARGO DOOR HAS CORROSION THROUGHOUT STATIONS 1360 TO 1460. INSTALLED NEW TEE CAP PER SRM 51-10-02-0G.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CORROSION BETWEEN AFT LAVATORY SEVICE PANEL AND SKIN STATIONS 1680 TO 1700. INSTALLED NEW SEVICE PAN AND DOUBLER ON SKIN PER SRM 51-10-02-0G.

Part: BRACKET — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CARGO TIE DOWN BRACKET CORRODED AFT OF STATION 1440 AND STRINGER 27 RIGHT. REPLACED TIE DOWN BRACKET PER SRM 51-10-02-G9.

Part: SKIN — GOUGED (FUSELAGE) · airframe 61,439 hrs · 21,034 cycles

GOUGE AT THE RIGHT FUSELAGE AT STATION 377 STRINGERS 15 TO 16 RIGHT. ACCOMPLISHED EA B757-015574.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

SHEAR TIE CORRODED STATION 1380 AND STRINGER 27 RIGHT. REPLACED SHEAR TIE PER SRM 51-10-02-0G.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CORROSION PRESSURE DECK STATION 1122. ACCOMPLISHED DOUBLER REPAIR PER EA 757-53-015573.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,439 hrs · 21,034 cycles

FRAME DAMAGED AT STATION 310 AND STRINGER 4 LEFT. INSTALLED DOUBLER IAW SRM 51-70-11-0G AND EA B757-53-015755.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

RIGHT FORWARD GALLEY CORRODED. REPLACED GALLEY MOUNT IAW IPC 53-01-51-2, SRM 51-10-01-G8 AND AARD 51-10-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

RIGHT AFT GALLEY MOUNT CORRODED. REPLACED GALLEY MOUNT IAW IPC 53-01-51-2 AARD 51-10-05 AND SRM 51-10-02-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

SEAT TRACK NUMBER 4 CORRODED STATION 680. REPLACED SEAT TRACK AT STATIONS 660 TO 710 IAW SRM 53-00-52-2R AARD 53-00-02-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CREASE ANGLE CORRODED STATION 665 TO 755 RIGHT PASSENGER/SERVICE RIGHT NUMBER 2 DOOR THRESHOLD AREA. REPLACED ANGLE IAW SRM 51-10-02-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CABIN SEAT TRACK NUMBER 3 CORRODED. INSTALLED SEAT TRACK WITH SPLICE AT STATION 680 TRACK NUMBER 3 IAW SRM 53-00-52-2R.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 61,439 hrs · 21,034 cycles

FORWARD CARGO DOOR, LOWER EDGE BEAM LANDING DAMAGE TO BOTTOM SIDE. INSTALLED NEW EDGE BEAM AND FASTENERS PER ESO 90114.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

LEFT CREASE ANGLE CORRODED STATIONS 440 STRINGER 17 LEFT. INSTALLED CREASE ANGLE SLICE REPAIR AT STATIONS 440 TO 444 LEFT PER SRM 51-10-02-G8.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,439 hrs · 21,034 cycles

INTERCOSTAL DAMAGED AFT OF LEFT NUMBER 4 DOOR. REPLACED INTERCOSTAL IAW AARD 51-10-05-01.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CORROSION AROUND FASTENERS ON LEADING EDGE OF NUMBER 10 SLAT. INSTALLED STRAP DOUBLER PER EA 57-015594.

Part: PAN — GOUGED (L4 DOOR) · airframe 61,439 hrs · 21,034 cycles

LEFT NUMBER 4 DOOR HAS A HANDLE PAN WITH A DEEP GOUGE. REPLACED HANDLE PAN PER ESO 90108.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 61,439 hrs · 21,034 cycles

CREASE BEAM WEB STATIONS 860 TO 880 DAMAGED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

INTERCOSTAL CORRODED STATIONS 377 TO 383 RIGHT BUTTLINE 63. REMOVED AND REPLACED INTERCOSTAL IN ACCORDANCE WITH SRM 51-10-02-0G.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

INNER CHORD OF CREASE BEAM CORRODED STATION 760 RIGHT SIDE. REMOVED AND REPLACED CREASE BEAM PER SRM 52-10-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,439 hrs · 21,034 cycles

CORROSION ON INTERCOSTAL STATIONS 1600 TO 1620. REPLACED INTERCOSTAL PER SRM 53-60-04-2R.

Part: WINGLET — DENTED (LT WING) · airframe 60,160 hrs · 20,593 cycles

TWO DENTS ON TRAILING EDGE OF LEFT WINGLET. ACCOMPLISHED REPAIR PER SRM 57-31-02-1A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,926 hrs · 20,500 cycles

EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 14D. OPS CHECKED NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,926 hrs · 20,500 cycles

FLIGHT ATTENDANT FLASHLIGHT BY MID LAVATORY IS INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT. OPS CHECKED NORMAL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 59,811 hrs · 20,457 cycles

MIA - CREW REPORTED AFTER TAKEOFF BOTH CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 FAILED AT THE SAME TIME WITH "CABIN AUTO INOP" ANNUNCIATED ON UPPER EICAS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH CABIN PRESSURE CONTROLLERS AND CABIN PRESSURE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON TOP OF AFT GALLEY FLOORBEAM DECK PLATE STA 1681, RIGHT BUTTLINE 23 TO 24. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION IN NUMEROUS PLACES ON AFT GALLEY DECK PLATE EXISTING DOUBLER AT STA 1711 TO 1720, LEFT BUTTLINE 16 TO RIGHT BUTTLINE 11. REMOVED AND REPLACED EXISTING DOUBLER PER SRM 53-60-51.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON TOP OF AFT GALLEY FLOOR PLATE AT STA 1680, LEFT BUTTLINE 23 TO 25. REMOVED CORROSION AND INSTALLED DOUBLER PER. SRM 53-60-51.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON TOP OF AFT GALLEY FLOOR PLATE AT STA 1680, LEFT BUTTLINE 38 TO LEFT BUTTLINE 42. REMOVED AND REPLACED DOUBLER AT STA 1681 PER SRM 53-60-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON TOP OF FLOORBEAM DECK AT STA. 1681. RIGHT BUTTLINE 10 TO 12. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON TOP OF AFT GALLEY FLOOR PLATE AT STA 1680, LEFT BUTTLINE 30 TO LEFT BUTTLINE 33. REMOVED AND REPLACED DOUBLER AT STA 1680 LEFT BUTTLINE 30 TO33, PER SRM 53-60-51.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION AT NUMEROUS PLACES ON EXISTING DOUBLER ON TOP OF FLOOR DECK PLATE STATION 1712 TO STATION 1720 RIGHT BUTTLINE 20 TO RIGHT BUTTLINE 40. REMOVED AND REPLACED DOUBLER PER SRM 53-60-51.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION ON AFT GALLEY FLOOR DECK PLATE SURROUNDING EXISTING DOUBLER FROM STA.1711 TO STA. 1713 RIGHT BUTTLINE 19 TO RIGHT BUTTLINE 22. REMOVED AND REPLACED DOUBLER PER SRM 53-60-51.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,770 hrs · 20,445 cycles

CORROSION IN NUMEROUS PLACES ON AFT GALLEY FLOOR DECK PLATE EXISTING DOUBLER AT STA 1711 TO STA 1720, LEFT BUTTLINE 38 TO 55. REMOVED AND REPLACED EXISTING DOUBLER PER SRM 53-60-51.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 58,269 hrs · 19,922 cycles

EMERGENCY LIGHTS AT SEAT ROW 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT MID CABIN RIGHT SIDE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,147 hrs · 19,869 cycles

EXTERIOR RIGHT NUMBER ONE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR RIGHT NUMBER ONE DOOR EXIT LIGHT.

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 57,918 hrs · 19,789 cycles

MIA - DURING TAKEOFF RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED TWICE WITH SUBSEQUENT EICAS MESSAGE. ABORTED TAKEOFF AND AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER TWO ENGINE REVERSE FLOW SENSOR AND PRESSURE REGULATING SHUT OFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,495 hrs · 19,652 cycles

EMERGENCY SEAT MOUNTED LIGHTS INOP FROM ROW 16 TO 25. REPLACED BATTERY AND CHARGER AT LOCATION M10800. OPS CHECKS NORMAL.

Part: DRIVE SHAFT — LEAKING (NR 1 ENGINE) · airframe 55,288 hrs

MIA INFLIGHT - NR 1 ENGINE OIL PRESSURE ND QUANTITY LOSS DURING CRUISE. CREW SHUT DOWN NR 1 ENGINE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 50 MINUTES. REPLACED NR 1 ENGINE ON 28 OCT AT MIA DUE TO LEAK FROM RADIAL DRIVE SHAFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,963 hrs

DFW EMERGENCY LIGHT AT AFT SEAT 17D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,963 hrs

DFW EMERGENCY LIGHTS AT LT HAND OVERHEAD SEAT ROW 23 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT HAND OVERHEAD SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,259 hrs

DFW - EMERGENCY LIGHT AT BULL NOSE OVERHEAD SEATS 1AB AND 2EF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BULL NOSE OVERHEAD SEATS 1AB AND 2EF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22, 23, 25 AND LEFT EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK M735 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22, 23, 25, AND LEFT EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY GROUND FLOOD LIGHT AT LEFT CABIN INOPERATIVE. RELAMPED EMERGENCY GROUND FLOOD LIGHT AT LEFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

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

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

DFW - FOUND EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA OVERHEAD EMERGENCY LIGHT AT 18C INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 18C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT ON AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - AFT AISLE EMERGENCY LIGHTS ARE MORE BRIGHT FROM THE EXIT ROWS BACK THAN FROM THE EXIT ROWS FORWARD. REMOVED AND REPLACED FORWARD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — MALFUNCTIONED (COCKPIT)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT WHEN UNARMED AT COCKPIT REMAIN ILLUMINATED. REPLACED EMERGENCY EXIT LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOSE — DEFECTIVE (MLG)

DFW - FLT 868 - EN ROUTE DFW-BOS, DURING CLIMB-OUT, LEFT SIDE HYDRAULIC SYSTEM FAILED. DECLARED EMERGENCY, ACCOMPLISHED ALTERNATE GEAR EXTENSION, RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE MLG DOWN LOCK ACTUATOR PRESSURE HOSE ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 18D INOPERATIVE. CONNECTOR DISCONNECTED AT SEAT 18D. RECONNECTED CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SWITCH — FAILED (CABIN)

ORD - FLT 1470 - BEFORE FLIGHT AT GATE, R3 AND L3 AFT SLIDE EMERGENCY LIGHTS FAILS TEST FROM EXTERIOR EMERGENCY LIGHT TEST SWITCH. LEFT MIDWING EMERGENCY LIGHT AND RIGHT MIDWING AFT EMERGENCY LIGHT FAIL TEST FROM EXTERIOR EMERGENCY TEST SWITCH. ALL TEST GOOD FROM INTERIOR EMERGENCY LIGHT TEST SWITCH. REPLACED EXTERIOR EMERGENCY LIGHT SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: POWER SUPPLY — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FORWARD EMERGENCY FLOOR LIGHTS REMAINED ON WHEN TURNED OFF. RECONNECTED FORWARD EMERGENCY FLOOR LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 18F INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHTS AT DOOR 2R AND SECOND RIGHT OVERWING DOOR INOPERATIVE. RESECURED LOOSE EMERGENCY LIGHT CONNECTORS AT DOOR 2R AND AT SECOND RIGHT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — GOUGED (BS 1600)

AFW - FOUND FLOOR BEAM AT STATION 1600 LBL 13 HAD A GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-857. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-860. (M)

Part: SILL — CORRODED (BS 1410)

AFW - FOUND UPPER CHORD ON LOWER MAIN SILL, NR 2 CARGO DOOR CUTOUT HAS CORROSION REMOVED BEYOND LIMITS. PER MRB 757-862. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-861. (M)

Part: DECK PLATE — CORRODED (BS 1720)

AFW - FOUND DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATIONS, CORROSION REMOVED IS BEYOND SRM LIMITS. PER MRB 757-855. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FOUND FLOOR BEAM AT STATION 365 RBL 61 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-856. (M)

Part: FLOOR BEAM — SHORT ED (BS 1640)

AFW - FLOOR BEAM AT STA 164 HAS SEVERAL FASTENER LOCATIONS THAT DO NOT MEET FASTENER SPACING REQUIREMENTS OF SRM 53-00-51, FIGURE 203. TST: 14,011.16 HRS. CYCLES: 5,028. (X)