N653A

Part: FAN — MALFUNCTIONED (RIGHT) · airframe 70,879 hrs · 24,424 cycles

STRONG ELEC ODOR IN THE COCKPIT & THE CABIN. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT RECIRCULATION FAN. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PRESSURE SWITCH — INOPERATIVE (BRAKE SYSTEM) · airframe 69,990 hrs · 24,092 cycles

MIA CREW REPORTED BRAKE SOURCE & ANTISKID ILLUMINATED ON AMBER EICAS SCREEN. EMER DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED ALTERNATE VLV SELECTOR PRESS SWITCH S415 & NR EIGHT WHEEL ANTISKID TRANSDUCER. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 68,714 hrs · 23,644 cycles

LR NR 2 DOOR HAS A SPOT THAT MAY BE CRACKED ON THE INSIDE DOOR FRAME BY HINGE. INSTALLED DOUBLER REPAIR IAW SRM 52-10-02-2R-1 & EA COMP 52-032962.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 68,714 hrs · 23,644 cycles

RT NR 2 DOOR HAS A SPOT THAT MAY BE A CRACK ON THE INSIDE OF THE DOOR FRAME. INSTALLED DOUBLER IAW SRM 52-10-02-2R-1 & EA COMP-52-032963.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 68,660 hrs · 23,625 cycles

EXTENSIVE DAMAGE TO THE HORIZONTAL STABILIZER INBD PANEL JUST FWD OF THE TORQUE BOX. ACCOMPLISHED BONDED REPAIR EA B757-55-032649.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,660 hrs · 23,625 cycles

FWD KEEL BEAM PANEL SUPPORT STRUCTURE CORRODED AT FRAME STATION 879. R & R SUPPORT IAW SRM 51-40-02.

Part: FRAME — CRACKED (STOWAGE BOX) · airframe 68,660 hrs · 23,625 cycles

AFT LIFE RAFT STOWAGE BOX, AFT LT HAND LATCH FRAME CRACKED & BENT. TRIMMED & REMOVED DAMAGED AREA. INSTALLED DOUBLER IAW SRM 51-7011.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,660 hrs · 23,625 cycles

LT MAIN WW, AFT BULKHEAD HYD TUBES SUPPORT BRACKET CORRODED. REPLACED LT WW AFT BULKHEAD BRACKET IAW SRM 51-40-02 & AARD 20-00-00-1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,660 hrs · 23,625 cycles

WEB DOUBLER IS CORRODED IN TWO PLACES ON THE TOP & ON THE ANGLE AT BODY STATIONS 1040 TO 1040 & BL 66 TO 67 LT. R & R DOUBLER IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,660 hrs · 23,625 cycles

LT NR 4 DOOR UNDER DRAIN PAN CORROSION FROM FRAME STATIONS 1640 TO 1720 LT. DRAIN PAN SUPPORT CORROSION R & R DRAIN PAN SUPPORT IAW SRM 51-40-02.

Part: FLEX LINE — LEAKING (RT MLG) · airframe 67,838 hrs · 23,334 cycles

DFW CREW REPORTED RT GEAR DOOR WOULD NOT RETRACT & LT HYDRAULIC PRESSURE & QUANTITY LOSS. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE RT MLG DOOR RETRACT ACTUATOR FLEX LINE SPLIT & LEAKING. R&R LINE. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED).

Part: PANEL — DAMAGED (TE FLAP) · airframe 64,199 hrs · 22,017 cycles

RIGHT WING FLAPS AFT PANEL ASSEMBLY HAS HAIL DAMAGE. ACCOMPLISHED BONDED REPAIR PER EA COMP-57-023327.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 64,199 hrs · 22,017 cycles

LEFT HORIZONTAL STABILIZER OUTBOARD PANEL FORWARD TORQUE BOX HAIL DAMAGED. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023241.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 64,199 hrs · 22,017 cycles

RIGHT HORIZONTAL STABILIZER OUTBOARD PANEL FORWARD TORQUE BOX HAIL DAMAGED. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023240.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 64,199 hrs · 22,017 cycles

LEFT HORIZONTAL STABILIZER INBOARD PANEL FORWARD TORQUE BOX HAIL DAMAGED. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023242.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 64,199 hrs · 22,017 cycles

RIGHT HORIZONTAL STABILIZER INBOARD PANEL FORWARD TORQUE BOX HAIL DAMAGED. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023243.

Part: PANEL — DAMAGED (TE FLAP) · airframe 64,199 hrs · 22,017 cycles

LEFT OUTBOARD MAIN FLAP AFT PANEL HAS HAIL DAMAGE. ACCOMPLISHED BONDED REPAIR PER COMP-57-023331.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 64,199 hrs · 22,017 cycles

LEFT SIDE FORWARD LOWER VERTICAL STAB PLANK HAS 48 HAIL DENTS. INSTALLED BMS 5-92 TYPE V ADHESIVE TO ALL DENTS IN AREA, ALLOWED CURE, SANDED SMOOTH TO AREA CONTOUR AND APPLIED EXTERNAL PRIMER COAT TO AFFECTED AREA PER SRM 51-70-01 AND EA B757-55-023268.

Part: PROBE — FAILED (ZONE 100) · airframe 60,205 hrs · 20,552 cycles

CREW REPORTED TOTAL AIR TEMPERATURE PROBE MICAS MESSAGE DURING FLIGHT. FLIGHT DIVERTED VIVO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TAT PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORROSION FOUND ON SUPPORT BEAM LOCATED BETWEEN STATIONS 640 TO 660, 21 INCHES OUTBOARD OF CENTERLINE. REMOVED AND REPLACED CORRODED SUPPORT BEAM PER SRM 51-10-02-0G, 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORROSION FOUND BETWEEN STATIONS 660 TO 680 ON FLOORBOARD SUPPORT 21 INCHES OUTBOARD OF CENTERLINE. REMOVED AND REPLACED CORRODED SUPPORT BEAM PER SRM 51-10-02-0G, 9.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORROSION - RIGHT FORWARD LAV "M" TIE-DOWN. REPLACED TIE DOWN PER SRM 51-10-02-0G PARAGRAPH 8.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORRODED CREASE ANGLE AT STATION 780. REPLACED CREASE ANGLE PER SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

T-CAP CORRODED STATION 740 RIGHT BUTTLINE 53. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-51-2R 3.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CREASE ANGLE CORRODED STATIONS 665 TO 740 RIGHT BUTTLINE 62. REPLACED ANGLE PER AARD 51-10-05-1.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 59,806 hrs · 20,411 cycles

FORWARD CARGO DOOR HAS 1 INCH DENT ON FORWARD BOTTOM CORNER. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER PER SRM 52-30-01-2R. INSTALLED DOUBLER AND FILLER PER SRM 52-30-01-2R 2, CAT A REPAIR.

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 59,806 hrs · 20,411 cycles

FORWARD CARGO DOOR SEAL LANDING (EDGE FRAME) DENTED AND WORN. REMOVED AND REPLACED EDGE FRAME PER ESO 90114.

Part: DOOR — DENTED (ZONE 800) · airframe 59,806 hrs · 20,411 cycles

FORWARD CARGO DOOR BOTTOM SEAL LANDING DENTED AND WORN (MKD). FORWARD CARGO DOOR BOTTOM SEAL LANDING REPLACED PER ESO 90114.

Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 59,806 hrs · 20,411 cycles

TWO SMALL DENTS WITH SCRATCH ON FORWARD CARGO DOOR APPROXIMATELY 6 INCHES AFT OF DOOR HANDLE. CUT AND REMOVED DAMAGED AREA (1 INCH HOLE) FABRICATED REPAIR DOUBLER AND FILLER PER SRM 52-30-01-2R 2 AND INSTALLED CAT A REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 59,806 hrs · 20,411 cycles

DENT IN FORWARD CARGO DOOR THAT IS OUT OF LIMITS PER SRM 52-30-01-1A. LOCATED INCHES FROM THE AFT EDGE AND 28 INCHES FROM THE LOWER EDGE. CUT AND REMOVED DAMAGED AREA OF SKIN, FABRICATED DOUBLER AND INSTALLED PER SRM 52-30-01-2R 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CABIN, STATIONS 1620 TO 1640, FLOORBOARD SUPPORT, LEFT BUTTLINE 28 TOP AND BOTTOM CORRODED. REPLACED FLOORBOARD SUPPORT (146N5281-6) AND SUPPORT FITTING (146N5283-5) PER AARD 51-10-05-1 REPAIR 1. USED BOEING DRAWING NUMBER 146N5271 FOR PART VERIFICATION.

Part: SKIN — GOUGED (FUSELAGE) · airframe 59,806 hrs · 20,411 cycles

FUSELAGE SKIN GOUGED AT STATION 340 NEAR CENTERLINE NUMBER 3 FORWARD OF LEFT NUMBER 1 DOOR. DAMAGE WAS REMOVED PER ESO 26-531001-5765. FABRICATED AND INSTALLED REPLACEMENT FOR DOUBLER MPN 141N8316-26 PER AARD 51-10-05-1.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 59,806 hrs · 20,411 cycles

CABIN, STATIONS 324 TO 345, LEFT BUTTLINE 32, FLOORBOARD SUPPORT HAS HOLE IN IT. REMOVED AND REPLACED FLOORBOARD SUPPORT PER AARD 51-10-05-1 REPAIR 1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

LEFT WING NUMBER 4 SLAT HAS CORROSION 40 INCHES OUTBOARD FROM INBOARD END, 9 INCHES FORWARD OF UPPER TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 4 SLAT REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

FLOOR SUPPORT IS CORRODED BEYOND LIMITS. FRAME STATIONS 1637 TO 1639, RIGHT BUTTLINE 24, WATER LINE 208. LOCATED BELOW THE AFT INBOARD MOUNT FOR LAVATORY MODULE M. REMOVED AND REPLACED FLOOR SUPPORT STATIONS 1620 TO 1640 RIGHT BUTTLINE 24 PER AARD 51-10-05-1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

SCUFF PLATE SUPPORT ANGLE CORRODED AT FRAME STATION 1680, WATERLINE 208, LEFT BUTTLINES 61 TO 66.5, STRINGER 17 LEFT. INSTALLED NEW SCUFFPLATE SUPPORT ANGLE PER SRM 51-10-02-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORROSION INSIDE NUMBER 3 SEAT TRACK OF CABIN FLOOR, FRAME STATIONS 679 TO 683 RIGHT BUTTLINE 25, WATER LINE 208, UNDER G-2 MID GALLEY. INSTALLED NUMBER 3 SEAT TRACK STATIONS 640 TO 780 SRM 51-10-02-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

CORROSION INSIDE NUMBER 4 SEAT TRACK OF CABIN FLOOR, FRAME STATIONS 679 TO 685, RIGHT BUTTLINE 46, WATER LINE 208, UNDER G-2 MID GALLEY. INSTALLED NEW NUMBER 4 SEAT TRACK FROM STATIONS 640 TO 780 PER SRM 51-10-02-0G.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

LEFT WING NUMBER 1 SLAT HAS CORROSION LEADING EDGE 29.5 INCHES OUTBOARD END 7.5 INCHES FORWARD FROM UPPER AFT TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 1 SLAT REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

NUMBER 2 SLAT HAS CORROSION 29 INCHES INBOARD FROM OUTBOARD END, 8 TO 9 INCHES FORWARD OF UPPER TRAILING EDGE OF NOSE SKIN. REMOVED CORRODED AREA AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,806 hrs · 20,411 cycles

LEFT WING NUMBER 1 SLAT HAS CORROSION ON LEADING EDGE 41.5 INCHES INBOARD FROM OUTBOARD END, 5 INCHES FORWARD FROM UPPER AFT TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 1 SLAT REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 58,388 hrs · 19,917 cycles

LEFT NUMBER 1 DOOR EMERGENCY FLASHLIGHT HOLDER BROKEN. REPLACED HOLDER FOR EMERGENCY FLASHLIGHT. OPS CHECK NORMAL.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 58,388 hrs · 19,917 cycles

EMERGENCY FLASHLIGHT SECURE STRAP ON RIGHT SIDE OF MID GALLEY MISSING. INSTALLED EMERGENCY SECURE STRAP ON FOR EMERGENCY FLASHLIGHT. OPS CHECK NORMAL.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,794 hrs · 19,707 cycles

CORROSION ON HAT CHANNEL AT STATION 1716 BUTT LINE 0. REMOVED AND REPLACED CENTER HAT CHANNEL PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,794 hrs · 19,707 cycles

CORROSION ON FLOORBEAM. REMOVED CORROSION AND REPAIRED PER SRM 53-00-51.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,794 hrs · 19,707 cycles

CORROSION ON WEB STATION 1701-1719 LEFT BUTT LINE 64-70. REMOVED AND REPLACED WEB PER SRM 51-10-2.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,794 hrs · 19,707 cycles

CORROSION ON TEE ANGLE LEFT BUTT LINE 56. REMOVED AND REPLACED TEE ANGLE PER SRM 51-10-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,794 hrs · 19,707 cycles

CORROSION ON AFT GALLEY FLOOR STATION 1680 TO 1720 LEFT BUTT LINE 52 TO RIGHT BUTT LINE 52. REMOVED AND REPLACED AFT DECK PLATE PER SRM 51-10-02.

Part: SHROUD — BROKEN (CABIN) · airframe 57,448 hrs · 19,598 cycles

EMERGENCY LIGHT AT SEAT 1D AFT PROXIMITY LIGHT HAS SHROUD BROKEN. REPLACED SHROUD.

Part: MODULE — INOPERATIVE (CABIN) · airframe 57,448 hrs · 19,598 cycles

EMERGENCY LIGHT AT SEAT ROW 9 TO 16 INOPERATIVE. REPLACED MODULE AND BATTERY PACK M10799.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 57,174 hrs · 19,491 cycles

EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT 13D, OPS CHECK NORMAL.

Part: ACCELEROMETER — MALFUNCTIONED (VIBRATION DETECT) · airframe 56,782 hrs · 19,359 cycles

DFW - CREW REPORTED RIGHT ENGINE HIGH VIBRATION INDICATION, INDICATED 4.3. COMPLETED QRH CHECKLIST AND THE INDICATOR WENT TO 5.0. CREW SHUTDOWN RIGHT ENGINE. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED VIBRATION ACCELEROMETER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,407 hrs · 19,223 cycles

SLAT NUMBER 9 LEADING EDGE SKIN CRACKED AT OUTBOARD DRIVE TRACK. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4 .

Part: APU — MALFUNCTIONED (APU BAY) · airframe 55,739 hrs · 18,964 cycles

MIA - AIRCRAFT REPORTED AUXILIARY POWER UNIT OIL QUANTITY LOSS. RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT AND LEFT ENGINE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 55,072 hrs

MIA - EMERGENCY LIGHT AT R4 DOOR INOPERATIVE. REPLACED LAMP AT R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: UNKNOWN — SMOKE (CABIN)

RNO - ORD TO SFO AT FLIGHT LEVEL 380, VISIBLE SMOKE WAS REPORTED AROUND SEAT ROWS 12 TO 13. MOMENTS LATER THE SMOKE ALARMS IN THE MID AND AFT LAVATORIES ACTIVATED. BEGAN THE SMOKE REMOVAL PROCESS BY ACTIVATING THE RECIRCULATION FANS. THE SMOKE DISSIPATED QUICKLY AND THE SMOKE ALARMS QUIT. LANDED RNO WITHOUT INCIDENT WITH NO VISIBLE SIGNS OF SMOKE IN CABIN. INSPECTED ALL LAVATORIES, ALL SIDEWALLS AND OVERHEAD. INSPECTED OVERHEAD PANELS IN AREA WHERE SMOKE WAS THOUGHT TO ORIGINATE. INSPECTED CARGO COMPARTMENTS, AIRCRAFT BAYS, SEAT POWERPORTS AND SEATS. NO DEFECTS NOTED. PLACARDED RIGHT HAND RECIRCULATION FAN AS PRECAUTION. INSPECTED RIGHT HAND RECIRCULATION FAN AT SFO. SYSTEM GROUND CHECKED NORMAL OPE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT LEFT 737 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FLOORBOARD SUPPORT IS CORRODED TOP INSIDE RIGHT OF LEFT NUMBER ONE DOOR AFT CORNERS IN AN AREA OF ONE BY THREE INCHES. REPAIRED SUPPORT PER ESO 90309 DATED 2/21/05.

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - CORROSION AT FLOORBEAM AT RIGHTHAND BUTTLINE 0 INCH TO 24 INCH. INSTALLED REPAIR IN ACCORDANCE WITH SRM 53 00 51 2.

Part: SUPPORT — CORRODED (THRESHOLD)

TUL - LEFT NR 4 DOOR THRESHOLD FORWARD DRAIN PAN SUPPORT AT STATION 1680 CORRODED THROUGH IN AREA OF 1 INCH BY 3 INCHES. REPLACED SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FLOOR CHANNEL SUPPORT CORRODED AT RT RIB LINE NUMBER 38 AT STATION 316 TO 324 IN AN AREA OF 1 INCH BY 3 INCHES. DRILLED UP NEW INTERCOSTAL, DEBURRED, TREATED, PRIMED AND PAINTED AND INSTALLED.

Part: LIGHT — BROKEN (L1 DOOR)

DFW - L1 DOOR FORWARD EXIT SIGN ASSEMBLY IS BROKEN. REPLACED L1 DOOR FORWARD EXIT SIGN LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SEAT MOUNT EMERGENCY LIGHT INOPERATIVE AT 6E. BATTERY PACK FAILED DUAL FEED CHECK. SECURED LOOSE SEAT CONNECTOR AT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — DAMAGED (GIRT BAR)

DFW - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DIRTY (CABIN)

MIA - FOUND FORWARD EMERGENCY LIGHT ON SEAT 6E INOPERATIVE. CLEANED CONNECTOR ON LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (NLG)

SJU - FLT 1470 - EN ROUTE ORD-SJU - DURING LANDING, NOSE GEAR INDICATION FAILED TO INDICATE DOWN AND LOCKED UPON EXTENSION. AIRCRAFT LANDED AT SJU WITHOUT INCIDENT. INSPECTION FOUND DAMAGED NOSE LANDING LIGHT ASSEMBLY. BROKEN GLASS FROM LANDING LIGHT FOUND EMBEDDED IN NOSE GEAR TARGETS. ALSO, FOUND BROKEN DOWNLOCK SENSOR AND GLASS INSIDE GEAR PIN HOLE AT BRACE. REPLACED LIGHT ASSEMBLY AND DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT 16F INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT 16F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ABOVE PAX SEAT 14C INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR ABOVE PAX SEAT 14C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SILL — CORRODED (CARGO DOOR)

AFW - INNER CHORD HAS CORROSION REMOVED, MATERIAL REMAINING IS BEYOND SRM LIMITS PER MRB 757-887. TST: 15,185 HOURS. CYCLES: 5,323. (X)

Part: STUB FRAME — GOUGED (PASSENGER DOOR)

AFW - STUB FRAME INSTALLATION, LT FORWARD NR 1 DOOR, HAD GOUGE BLENDED BEYOND 10 PERCENT OF THICKNESS PER MRB 883. TST: 15,185 HOURS. CYCLES: 5,323. (X)

Part: DECK PLATE — CORRODED (BS 1720)

AFW - DECK PLATE HAS CORROSION BLENDED BEYOND SRM LIMITS IN VARIOUS LOCATIONS PER MRB 757-880. TST: 15,185 HOURS. CYCLES: 5,323. (X)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STA 1640, RBL 55 AND RBL 58 HAS CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-718. TST, 13,759 HOURS. CYCLES, 4,865. (X)