N647AM

Part: LENS — MISSING (CABIN) · airframe 67,956 hrs · 23,435 cycles

BULLNOSE EMERGENCY LIGHT AT SEAT 31ABC MISSING LENS. REPLACED LENS FOR BULLNOSE EMERGENCY LIGHT AT SEAT 31ABC. OPERATIONS CHECKED NORMAL.

Part: CONTROL PANEL — FAILED (WEATHER RADAR) · airframe 67,919 hrs · 23,424 cycles

MIA CREW REPORTED WEATHER RADAR FAILED ENROUTE. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SHUTTLE VALVE — LEAKING (ANTI-SKID SYS) · airframe 67,348 hrs · 23,221 cycles

INFLIGHT, CREW REPORTED RT HYD FLUID LOSS. FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND ANTI-SKID SHUTOFF VALVE LEAKING. REPLACED BOTH LT AND RT ANTI-SKID SHUTTLE VALVE. SYS GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: PSEU — FAULTY (COCKPIT) · airframe 66,355 hrs · 22,862 cycles

SJU - INFLIGHT MIA-BGI CREW REPORTED COCKPIT WARNING LIGHTS ILLUMINATED WITH HORN GOING OFF DURING FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FAULTY PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,911 hrs · 22,332 cycles

CORROSION ON PRESSURE DECK STATION 1139 AND LEFT BUTTLINE 14.5. INSTALLED DOUBLER PER EA B757-53-024545.

Part: PRESSURE DECK — CORRODED (LT MLG WW) · corrosion level 2 · airframe 64,911 hrs · 22,332 cycles

CORROSION ON THE LOWER SURFACE OF LEFT WHEEL WELL PRESSURE DECK. INSTALLED DOUBLER FROM STATIONS 1120 AND 1139 PER EA B757-53-024545.

Part: SPAR CAP — CORRODED (TE FLAP) · airframe 64,911 hrs · 22,332 cycles

LEFT MAIN INBOARD FLAP HAS CORROSION ON UPPER FORWARD SPAR CAP APPROXIMATELY 28 INCHES FROM INBOARD END OF FLAP. REMOVED AND REPLACED SECTION OF SPAR CAP AND INSTALLED DOUBLERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,798 hrs · 21,526 cycles

THE 27C SEAT AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 27C SEAT AISLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 62,745 hrs · 21,509 cycles

MIA - CREW REPORTED AFTER TAKEOFF GEAR DISAGREE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT MAIN GEAR UPLOCK SENSOR THAT HAD FAULTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ADC — MALFUNCTIONED (LEFT) · airframe 62,001 hrs · 21,248 cycles

MIA - CREW REPORTED DURING CRUISE MACH WINDOW AIR SPEEED KEPT INCRESING. TURNED OFF AUTO THROTTLE AND REDUCED THRUST BUT AIRSPEED WOULD NOT REDUCE. ABOUT 1 MINUTE LATER AIRSPEED BEGAN TO SLOW. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

RIGHT WING REAR SPAR AT SPAR SHUTOFF ACTUATOR ADAPTER SHAFT/PLATE CORROSION UNDER PLATE. REMOVED CORROSION PER SRM 51-10-02. SPOT FACED, CLEANED HOLES AND FACE OF SPOT FACE. PERFORMED HFEC HOLE PROBE OF FASTENER HOLES. PERFORMED FPI INSPECTION IN REWORKED AREA. FLAPPER PEENED AFFECTED AREA AND INSTALLED ADAPTOR PLATE PER EA B757-57-017021.

Part: SERVICE PANEL — DAMAGED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

OUTBOARD OF LEFT SIDEWALL PANEL LAVATORY SERVICE BOX DAMAGED FORWARD EDGE AT WATER HOSE ATTACH POINT FLANGE SEPARATED ON OUTER SURFACE OF BOX. INSTALLED DOUBLER PER SRM 51-40-02-0G AND EA B757-53-016940 DATED 17-MAY-2011.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

FUSELAGE CROWN SKIN DENTED STRINGER 2 RIGHT FRAME STATION 636. DOUBLER INSTALLED ON FUSELAGE CROWN SKIN PER EA B757-53-016981 DATED 18MAY11.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 61,965 hrs · 21,232 cycles

GOUGE ON LEFT HORIZONTAL STAB LEADING EDGE EXCEEDS SRM LIMITS. INSTALLED PERMANENT BONDED DOUBLER REPAIR AS PER SRM 51-70-10-2R.

Part: STRINGER — DENTED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

DENT AT FRAME STATION 430 STRINGER 15 RIGHT MEASURES .182 DEEP AND EXCEEDS THE .125 LIMIT SET BY SRM 53-00-01-1A 1 DETAIL III. INSTALLED REPLACEMENT STRINGER SECTION AND SPLICE PER SRM 53-00-01-2R 1. INSTALLED DOUBLER AND SHIM PER SRM 53-00-01-2R 2, AND EA B757- 53-016953.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

CORROSION ON WEB BETWEEN STATION 1360 AND 1380 3 INCHES OUTBOARD OF STRINGER 27 RIGHT. INSTALLED NEW WEB PER SRM 51-10-02-0G.

Part: SKIN — DAMAGED (LE SLAT) · airframe 61,965 hrs · 21,232 cycles

NUMBER 9 SLAT HAS PREVIOUS BLEND OUT IN UPPER SKIN EIGHT INCHES FROM OUTBOARD EDGE. REMOVED PREVIOUS BLEND OUTS AND INSTALLED DOUBLER ON SLAT PER AARD 57-43-00-1. INSTALLED COVE SKIN PER ESO 90249.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

RIGHT NUMBER 2 DOOR ON FORWARD FRAME AT CUTOUT CRACKED. INSTALLED DOUBLER REPAIR PER EA COMP-52-016843.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

T-CORD AT AFT CARGO HAS CORROSION AT NUT PLATES. INSTALLED SERVICEABLE T-CHORD PER SRM 51-10-02-0G, PARAGRAPH 9.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

CORROSION ON GALLEY MOUNT STATION 333. REPLACED GALLEY MOUNT PER SRM 51-10-02G9.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

CORROSION ON FRAME 1360 3 INCHES OUTBOARD OF STRINGER 27 RIGHT. DOUBLER REPAIR COMPLETED PER SRM 53-00-07-2R 5.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 61,965 hrs · 21,232 cycles

AFT CARGO DOOR LOWER FORWARD OUTER SKIN CORNER IS DAMAGED AND HAS CORROSION BETWEEM SKIN AND ATTACH ANGLE. REMOVED CORROSION, CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 52-30-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

STATION 365 RIGHT BUTTLINE 62 CORROSION ON FRAME. INSTALLED UPPER CHORD T-ANGLE PER SRM 53-00-51-2, R 3 AND BOEING DWG LOR5L53005.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

CREASE ANGLE AFT OF LEFT NUMBER 1 DOOR, AT APPROXIMATELY STATION 380 HAS TOOLING MARK. REMOVED AND REPLACED CREASE ANGLE FROM APPROXIMATE STATIONS 298 TO 430 PER SRM 51-10-02-0G.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 61,965 hrs · 21,232 cycles

UPPER AFT LIGHTNING HOLE HAS TOOLING DAMAGE. INSTALLED DOUBLER PER SRM 51-70-13-0G.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 61,965 hrs · 21,232 cycles

FORWARD CARGO DOOR, LOWER DOOR EDGE BEAM DAMAGED. COMPLETED INSTALLATION OF NEW EDGE BEAM PER ESO 90114.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

CREASE ANGLE STATIONS 644 TO 735 CORRODED. REPLACED CREASE ANGLE PER SRM 51-10-02 G9.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,965 hrs · 21,232 cycles

FRAME STATION 700 LATERAL FLOORBEAM CRACKED. PERFORMED REPAIR OF LATERAL FLOORBEAM AT FRAME STATION 700 BY THE COMPLETION OF TASK CARD 53-98-01 AND AARD 53-30-51-2.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

LAVATORY K-AFT OUTBOARD MOUNT HAS LIGHT CORROSION. INSTALLED NEW LAVATORY MOUNT PER SRM 51-10-02-OG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 21,232 cycles

STATIONS 1620 TO 1640 LEFT BUTTLINE 48 INTERCOSTAL AT AFT OUTBOARD LAVATORY K MOUNT HAS HEAVY CORROSION. INSTALLED NEW INTERCOSTAL UNDER AFT OUTBOARD LAVATORY K MOUNT PER SRM 51-10-02-0G 10.

Part: LIGHT — INOPERATIVE (LAVATORY SIGN) · airframe 59,879 hrs · 20,501 cycles

ROW 20 CENTER LAVATORY OCCUPIED SIGN LAMPS INOPERATIVE. REPLACED LAMP FOR ROW 20 CENTER LAVATORY OCCUPIED SIGN. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,528 hrs · 20,376 cycles

RIGHT NUMBER 1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERIOR SLIDE LIGHT. OPS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 59,528 hrs · 20,376 cycles

ROW 34 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPAIRED SIDEWALL CONNECTOR AT 34DEF. OPS CHECKED NORMAL.

Part: DUCT — CRACKED (LT PYLON) · airframe 59,492 hrs · 20,361 cycles

AUA - CREW REPORTED LEFT ENGINE OVERHEAT INDICATION DURING CLIMB. ACCOMPLISHED QRH PROCEDURE AND LIGHT EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNED AUA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED LEFT ENGINE PYLON FOUND HP2 DUCT CRACKED. REMOVED AND REPLACED HP2 ELBOW DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 59,178 hrs · 20,253 cycles

RIGHT NUMBER 1 AFT EXIT LENS ASSEMBLY DAMAGED. REPLACED LIGHT ASSEMBLY FOR RIGHT NUMBER 1 AFT EXIT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,178 hrs · 20,253 cycles

RIGHT EXTERIOR DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR DOOR EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 59,178 hrs · 20,253 cycles

RIGHT NUMBER ONE FORWARD DOOR EXIT MARKER MISSING LENS. REPLACED LENS AT RIGHT NUMBER ONE FORWARD DOOR EMERGENCY PATH LIGHTING EXIT MARKER. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 58,891 hrs · 20,134 cycles

EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR AFT EXIT MARKER STICKER PEELING. REPLACED PLACARD.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 58,446 hrs · 19,976 cycles

LEFT MAIN FLAP FRETTING DAMAGE IN 5 PLACES ON UPPER INTERSPAR SKIN PANEL APPROX 10 INCHES FROM INBOARD END. CUT OUT DAMAGED AREA AND REPAIRED USING FLUSH FILLER AND DOUBLER PER SRM 51-70-2R4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,223 hrs · 19,907 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT TOO DIM FROM SEAT ROW 9 TO 15. REPLACED BATTERY PACK AT SEAT ROW 9, OPS CHECKED NORMAL.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 58,214 hrs · 19,904 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROWS 16 TO 15 DIM. REPLACED BATTERY PACK AT SEAT ROW 19.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 58,214 hrs · 19,904 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 DIM. REPLACED BATTERY PACK AT SEAT ROW 33.

Part: SEQUENCE VALVE — FAILED (MLG DOOR) · airframe 55,719 hrs

DFW INFLIGHT - GEAR WARNING INDICATION AFTER GEAR RETRACTION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT DOOR SEQUENCE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN) · airframe 55,703 hrs

LGA - EMERGENCY LIGHT LENS MISSING AT AFT RIGHT GALLEY. REPLACED LIGHT ASSEMBLY AT AFT RIGHT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PROXIMITY SENSOR — MALFUNCTIONED (LANDING GEAR)

MIA - DURING LANDING GEAR RETRACTION GEAR INDICATION ILLUMINATED. AIRCRAFT FLEW THROUGH WAKE OF AIRBUS WITH VIBRATION AND INDICATIONS EXTINGUISHED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED INSPECTION OF LANDING GEAR AND LEFT PROXIMITY SYSTEM. FOUND NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,652 hrs

JFK - EMERGENCY LIGHT AT OVERHEAD SEAT 16C INOPERATIVE. REPLACED FUSE AT M10770 FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,652 hrs

JFK - EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,652 hrs

JFK - EMERGENCY LIGHTS AT SEAT ROW 27 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 27 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: THRUST REVERSER — DAMAGED (RT ENGINE)

SJU INFLIGHT T1937/04OCT - CREW HEARD LOUD BOOM FROM RT ENGINE CLIMBING THROUGH FLIGHT LEVEL 320. ENGINE GAS TEMPERATURE WENT TO AMBER AT 615 DEGREES. N1 WAS AMBER. THROTTLE REDUCED TO IDLE AND ALL PARAMETERS NORMAL AT IDLE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. FOUND RIGHT ENGINE THRUST REVERSER DAMAGE. FLIGHT FERRIED TO DFW FOR ENGINE CHANGE. AIRCRAFT OUT OF SERVICE FOR EVALUATION AND REPAIR. 10-16-07 REPLACED NR 2 ENGINE ON 06 OCT 2007 AT SJU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSDUCER — INOPERATIVE (RT ENGINE)

PHX INFLIGHT T2289/01OCT - CAPTAIN REPORTED HEARING LOUD BANG FROM THE NUMBER TWO ENGINE AT FLIGHT LEVEL 400. ENGINE GAS TEMPERATURE AND OTHER ENGINE INDICATIONS DECREASED. CAPTAIN SHUTDOWN NR 2 ENGINE & LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 22 MINUTES. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE COMPRESSOR. REPLACED NR 2 ENGINE POWER LEVEL ANGLE TRANSDUCER AND RT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — LOW PRESSURE (R4 DOOR)

DFW - RIGHT NUMBER FOUR SLIDE PRESSURE LOW. REPLACED SLIDE TO RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — UNKNOWN (CABIN)

MIA - AFTER LANDING, CREW RECEIVED A LEFT WING SLIDE EICAS MESSAGE MOMENTARILY. REPLACED LEFT OVERWING SLIDE PACK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LOOSE (LEFT ENGINE)

MIA INFLIGHT T447/13JAN - LEFT ENGINE BLEED LIGHT ILLUMINATED ON TAKEOFF ROLL. WOULD NOT RESET. ENGINE BLEED RESET ON DESCENT. LANDED MIA WITHOUT INCIDENT. FOUND LOOSE LINE AT HIGH STAGE VALVE. SECURED LINE AND RESEATED CONNECTORS AT HIGH STAGE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — FAULTY (CABIN)

MIA - SEAT MOUNTED EMERGENCY LIGHTS AT 34D INOPERATIVE. REPAIRED FAULTY WIRING FOR SEAT MOUNTED EMERGENCY LIGHTS AT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - FIRST CLASS EMERGENCY LIGHTS AT RIGHT 1 AND LEFT 1 DOOR EXIT SIGNS INOPERATIVE. REPLACED FRONT EMERGENCY LIGHT MODULE BATTERY PACK FOR THE FIRST CLASS EMERGENCY LIGHTS AT RIGHT 1 AND LEFT 1 DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (CABIN DOOR)

MIA - CABIN SERVICES CONTRACTOR INADVERTANTLY DEPLOYED SLIDE WHILE OPENING L4 DOOR. SLIDE DROPPED OUT AND DOOR ASSIST BOTTLE DISCHARGED BUT SLIDE FAILED TO INFLATE. REPLACED SLIDE AND RESERVOIR FOR EMERGENCY SLIDE AT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AISLE EMERGENCY LIGHTS AT STATIONS 635L AND 830L INOPERATIVE. REPLACED BATTERY PACK M10567 FOR AISLE EMERGENCY LIGHTS AT STATIONS 635L AND 830L. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 16 THROUGH 24. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — LEAKING (LT ENGINE)

DFW - FLT 2478 - EN ROUTE LAS-MIA, 1 HR AND 8 MIN INTO FLT LT HYD PUMP PRESSURE EICAS MESSAGE DISPLAYED. FOLLOWED QRH PROCEDURE AND SECURED LT ENGINE HYD PUMP. 40 MIN LATER, A BUZZING SCOURING SENSATION AND SOUND APPEARED. A MIN LATER RECEIVED A CALL FROM NR 1 FLT ATTENDANT ABOUT A SIMILAR SOUND FROM THE WING AREA. RAISED GEAR HANDLE TO CHK FOR POSSIBLE GEAR DOOR MISRIG,NO HELP. GEAR HANDLE PLACED TO OFF, 2 MINUTES LATER LT HYD FLUID STARTED TO DECREASE. WENT TO BELOW RF LEVEL AT .50 AND SECURED THE LT ELEC PUMP. FLUID LOSS CONTINUED TO 0.00 AND FLUCTUATED BETWEEN THERE AND .09. DIVERTED TO DFW, LANDED WITHOUT INCIDENT. REPLACED LT ENG DRIVE PUMP, LEAK AND OPS CHK GOOD. SYS GRND CHKED NORMAL. (M)

Part: FITTING — CRACKED (FUSELAGE)

TUL - FOUND AFT INBOARD FITTING CRACKED AT STATION 205.65 BEYOND LIMITS. FABRICATED AND INSTALLED BUSHING PER ESO 90309. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — INOPERATIVE (GALLEY DOOR)

LGA - FLT 1132 - GALLEY SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15 THROUGH 23 DIM. ACCOMPLISHED OPS CHECK PER THE MM. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 5 DIM. ACCOMPLISHED EMERGENCY LIGHT OPERATIONAL CHECKS PER THE MM. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT IN MOST AFT OF AIRCRAFT INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIP AT MOST AFT OF AIRCRAFT. SYSTEM GROUND CHECKED, NOMRAL OPERATION. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT LAST 3 SEAT ROWS OF FIRST CLASS CABIN INOPERATIVE. REPLACED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT DIVIDER BETWEEN FIRST CLASS AND COACH SECTION OF CABIN. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X0

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: PAN — GOUGED (L-4 DOOR)

AFW - FOUND L-4 DOOR PAN HAS GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-844. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FOUND FLOOR BEAM, AT STATION 365, HAS CORROSION REMOVED ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. PER MRB 757-845. (M)

Part: DECK PLATE — CORRODED (BS 1680)

AFW - FOUND DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATION AREAS ARE BEYOND SRM LIMITS. PER MRB 757-849. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FOUND ON UPPER SURFACE OF FLOOR BEAM, AT STATION 377, HAD CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-846. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FOUND FLOOR BEAM AT STATION 1640 HAD CORROSION REMOVED BEYOND SRM LIMITS AT LBL 37, 39, 40, 50 AND 55. PER MRB 757-848. (M)