N662AA

Part: STRAP — MIGRATED (L4 DOOR) · airframe 69,542 hrs · 24,037 cycles

INFLIGHT NOISE AT LT NR 4 DOOR. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND GIRT BAR STRAP MIGRATED INTO AIRSTREAM. SECURED STRAP & ACCOMPLISHED PRESSURIZATION OF ACFT WITH NO FAULTS NOTED. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,320 hrs · 23,952 cycles

FUSELAGE SKIN DAMAGED AT STATION 420 & STRINGER 20 LT. INSTALLED DOUBLER REPAIR IAW EA B757-53-035827.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,320 hrs · 23,952 cycles

TWO SCRIBE LINES ON FUSELAGE SKIN FROM STATIONS 600 TO 661 BETWEEN STRINGERS 6 & 10 LT. THE SCRIBE LINES WERE DETERMINED TO BE A MAX DEPTH OF .0025 INCHES BY LASER MEASUREMENT. ACCOMPLISHED REPAIR IAW EAB757-53-035905.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,320 hrs · 23,952 cycles

SCRIBE LINES FOUND IN ZONE NR 3 FROM STATIONS 600 TO 661 BETWEEN STRINGERS 6 TO 10 RT IAW ECO F1541BN. THE SCRIBE LINES WERE DETERMINED TO BE A MAX DEPTH OF .0025 INCHES BY LASER MEASUREMENT. ACCOMPLISHED REPAIR IAW EA B757-53-035905.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,320 hrs · 23,952 cycles

CORROSION WAS FOUND AROUND THE NUTPLATE HOLES ON FLOORBOARD SUPPORT. R & R FLOORBOARD SUPPORT IAW AARD 51-00-05-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,622 hrs · 22,594 cycles

ESCAPE PATH LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 36D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,622 hrs · 22,594 cycles

ESCAPE PATH LIGHT AT SEAT 31D INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 31D. OPS CHECK NORMAL.

Part: ATTACH FITTING — DAMAGED (FUSELAGE) · airframe 65,622 hrs · 22,594 cycles

UPPER T-CAP SPLICE, FLOORBEAM ATTACHMENT DAMAGED. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B757-53-028441.

Part: SPLICE PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,622 hrs · 22,594 cycles

CORROSION ON THE LOWER RIGHT HORIZONTAL HINGE SPLICE PLATE AT AFT ATTACH FITTING AT STATION 1844. REMOVED CORROSION AND REPAIRED PER EA B757-55-028434.

Part: SPLICE PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,622 hrs · 22,594 cycles

CORROSION ON LOWER LEFT HORIZONTAL HINGE SPLICE PLATE AT AFT ATTACH FITTING STATION 1844. REMOVED CORROSION AND REPAIRED PER EA B757-55-028416.

Part: SPLICE PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,622 hrs · 22,594 cycles

CORROSION ON RIGHT LOWER OUTER HORIZONTAL STABILIZER HINGE SPLICE PLATE AT STATION 1844. REMOVED CORROSION AND REPAIRED PER EA B757-55-028434.

Part: SPLICE PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,622 hrs · 22,594 cycles

CORROSION ON THE RIGHT OUTER HORIZONTAL HINGE SPLICE PLATE AT AFT ATTACH FITTING AT STATION 1844. REMOVED CORROSION PER EA B757-55-028435.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,623 hrs · 22,223 cycles

FORWARD EMERGENCY LIGHT ABOVE RIGHT WING INOPERATIVE. REPLACED LAMP FOR FORWARD EMERGENCY LIGHT ABOVE RIGHT WING. OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 64,353 hrs · 22,128 cycles

SEATS 21DEF EMERGENCY LIGHT IS INOPERATIVE. REPAIRED BROKEN WIRE IN HARNESS.

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 63,871 hrs · 21,964 cycles

ORD - CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE CAME WHEN FLAPS SELECTED TO 20 DEGREES. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER SIX AND SEVEN TRANSMISSIONS THAT HAD TRIPPED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 63,867 hrs · 21,960 cycles

MIA (REPEAT ITEM) CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE AND THE TRAILING EDGE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT INBOARD FLAP OUTBOARD TRANSMISSION AND RIGHT OUTBOARD FLAP OUTBOARD TRANSMISSION OVERLOAD INDICATORS TRIPPED. RESET INDICATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (TE FLAP) · airframe 63,861 hrs · 21,957 cycles

MIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED FLAP PDU POSITION TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 63,231 hrs · 21,727 cycles

ROW 21D EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR FOR ROW 21D EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 63,231 hrs · 21,727 cycles

LEFT FORWARD OVERWING UPPER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FORWARD OVERWING UPPER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,231 hrs · 21,727 cycles

R4 DOOR AFT EXIT SIDEWALL EMERGENCY LIGHT LENS BROKEN. REPLACED LENS FOR R4 DOOR AFT EXIT SIDEWALL EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 63,231 hrs · 21,727 cycles

R4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR R4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 63,231 hrs · 21,727 cycles

AFT CARGO DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT CARGO DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,747 hrs · 21,547 cycles

RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 62,747 hrs · 21,547 cycles

ROW 9DEF SEAT MOUNTED AFT EMERGENCY LIGHT INOPERATIVE. REPLACED PLUG ON SEAT HARNESS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,747 hrs · 21,547 cycles

RIGHT AFT LAVATORY SIDEWALL EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR AFT LAVATORY SIDEWALL EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 62,747 hrs · 21,547 cycles

RIGHT NUMBER 4 DOOR FORWARD LOWER SIDEWALL EMERGENCY LIGHT INOPERATIVE. REPLACED CONNECTOR FOR RIGHT NUMBER 4 DOOR FORWARD LOWER SIDEWALL EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

AFT CARGO INTERCOSTAL BODY STATION 1620 AT LEFT BUTTLINE 3 CORRODED. REMOVED CORROSION AND REPLACED INTERCOSTAL PER B757 53-00-53 AND DWG 146N5451.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,325 hrs · 21,388 cycles

OVERHEAD EMERGENCY LIGHT AT STATION 880 INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPS CHECK NORMAL.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

FORWARD CARGO DOOR INTERNAL WEB ANGLE CORRODED NEAR CENTER LOWER EDGE. REMOVED AND REPLACED WEB ANGLE IAW SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

FORWARD CARGO DOOR INTERNAL WEB ANGLE CORRODED NEAR FORWARD LOWER CORNER. REMOVED AND REPLACED WEB ANGLE PER SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

FORWARD CARGO DOOR INTERNAL WEB ANGLE CORRODED NEAR CENTER LOWER EDGE. REMOVED AND REPLACED WEB ANGLE IAW SRM 51-40-02.

Part: SKIN — CHAFED (LE SLAT) · airframe 62,325 hrs · 21,388 cycles

LEFT WING FIXED LEADING EDGE SLAT NUMBER 3 HAS UPPER TRAILING EDGE BOTTOM SURFACE CHAFED (ABOUT 12 SQUARE INCHES-LOCALIZED). REPAIRED NR 3 SLAT T/E WEDGE AS REQUIRED BY REMOVING DAMAGE 2 AREAS. FABRICATED BY REMOVING DAMAGE 2 AREAS, FABRICATING AND BONDING, FILLER, INTERNAL DOUBLER HONEYCOMB CORE PLUG AND EXTERNAL (UPPER) REPAIR DOUBLER IAW B757-200 SRM 51-70-10 AND 57-43-02.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

FORWARD CARGO DOOR INTERNAL WEB ANGLE CORRODED NEAR FORWARD LOWER CORNER. REMOVED AND REPLACED WEB ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

AFT CARGO FLOOR SUPPORT (Z) ANGLE CHAFED THROUGH BODY STATION 1460, LEFT BUTTLINE 11. REMOVED DAMAGED AREA IAW B757 AARD 53-60-53-7. FABRICATED ANGLE AND FILLER IAW B757 AARD 53-60-53-7. LOCATED DRILLED AND DEBURRED IAW B757 AARD 53-60-53-7. TREATED WITH ALODINE AND PRIMED IAW B757 AARD 83-60-53-7 AND INSTALLED IAW B757 AARD 53-60-53-7.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN FLOOR SUPPORT ANGLE BODY STATIONS 1661 TO 1681.8 RIGHT BUTTLINE 54 CORRODED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN FLOOR SUPPORT ANGLE BODY STATIONS 1675 TO 1680 CORRODED AT RIGHT BUTTLINE 52 (ABOUT 6 SQUARE INCHES). REMOVED FLOOR SUPPORT ANGLE IAW B757 SRM 51-40-02. LOCATED AND DRILLED NEW ANGLE PN 146N5246U62. INSTALLED ANGLE ON NEW FLOOR SUPPORT PER SRM 51-40-02.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 62,325 hrs · 21,388 cycles

LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE HAS PUNCTURE AND DENT. REPAIRED PER SRM 51-70-10 AND 57-53-01.

Part: STIFFENER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

AFT PIT DOOR LOWER FORWARD VERTICAL STIFFENER IS CORRODED. REMOVED AND REPLACED AFT PIT DOOR LOWER FWD VERTICAL STIFFENER PER SRM 51-40-02 AND BOEING DRAWING 146N6603.

Part: STIFFENER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

AFT CARGO DOOR LOWER AFT VERTICAL STIFFENER IS CORRODED. REMOVED AND REPLACED STIFFENER IAW BAC DWG 146N6603 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN FLOOR SUPPORT ANGLE BODY STATIONS 1661 TO 1640 AT RIGHT BUTTLINE 54 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

LEFT WING NUMBER 4 LEADING EDGE SLAT HAS INDICATIONS OF LIGHT CORROSION ON UPPER SURFACE. REPAIRED IAW AARD 57-43-00-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

LEFT WING NUMBER 3 LEADING EDGE SLAT HAS INDICATIONS OF LIGHT CORROSION ON UPPER SURFACE. REPAIRED IAW AARD 57-43-00-01.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,325 hrs · 21,388 cycles

LEFT WING OUTBOARD SLAT NUMBER 1 UPPER SKIN CRACKED AND DENTED OVERWING STATION 711. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED PERMANENT REPAIR PER SRM 57-43-01-2R.

Part: TERMINAL — OVERHEATED (CIRCUIT BREAKER) · airframe 62,325 hrs · 21,388 cycles

P37 CIRCUIT BREAKER TERMINAL LUG OVERHEATED. REMOVED AND REPLACED TERMINAL LUG PER BSWPM20-30-00.

Part: CIRCUIT BREAKER — BURNED (NLG WW) · airframe 62,325 hrs · 21,388 cycles

NOSE WHEEL WELL LIGHT CIRCUIT BREAKER C1205 IN THE P34 IS BURNT. REMOVED AND REPLACED CIRCUIT BREAKER C1205 PER B757 SWPM20-30-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

EXTERIOR FUSELAGE SKIN, LIGHTNING STRIKE AT STATION 580 STRINGER 27 LEFT. AIRCRAFT CURRENTLY UNDER GOING MAINTENANCE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

EXTERIOR FUSELAGE SKIN AT STATION 1862 BETWEEN STRINGERS 1 AND 2 HAS A SMALL HOLE IN IT. INSTALLED REPAIR DOUBLER PER SRM 53-00-01-2R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

FLOORBEAM CORRODED STATION 1681. ACCOMPLISHED FLOORBEAM REPAIR.

Part: TEAR STRAP — DEBONDED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

EXTERNAL FUSELAGE STATION 1600 BETWEEN STRINGERS 8 AND 10 LEFT TEAR STRAP HAD AREAS DISBONDED. CURRENTLY UNDERGOING REPAIRS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

FUSELAGE INTERNAL STRINGER ANGLE STATION 685 TO 677 CRACKED (2 PLACES). CURRENTLY UNDERGOING REPAIRS.

Part: BRACKET — DAMAGED (NLG WW) · airframe 62,325 hrs · 21,388 cycles

CAMLOCK BRACKET IN P34 PANEL BESIDE NOSE WHEEL WELL LIGHT CIRCUIT BREAKER HAS ELECTRICAL ARCH DAMAGE. REMOVED DAMAGE PER SRM 51-20-02-0G AND ALODINED PER SRM 51-20-01-01. NO MATERIAL LOSS. (SUPPLEMENTAL CLOSED)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN WEB CORRODED AT STATION 1720 RIGHT BUTTLINE 65. REMOVED AND REPLACED WEB PER SRM 51-40-02 AND BAC 146N8722.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN UNDER FLOOR, OVERWING PRESSURE DECK CORRODED AT BODY STATION 1000 TO 1020, LEFT BUTTLINE 65. REMOVED AND REPLACED SHEAR WEB WEB IAW AAL B757 SRM 51-40-02 AND BAC DWG 144N5140. (SUPPLEMENTAL CLOSED)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

AFT PIT AREA UNDER AFT GALLEY, STRINGER 29 LEFT AT INTERSECTION OF FRAME 1700 HAS EXFOLIATED CORROSION. CURRENTLY UNDERGOING REPAIRS.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

MAIN CABIN UNDER FLOOR, WEB REPAIR DOUBLER BODY STATIONS 1711 TO 1720 HAS CORROSION, RIGHT BUTTLINES 32 TO 42 (ABOUT 2 SQUARE INCHES). CURRENTLY UNDERGOING REPAIRS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,325 hrs · 21,388 cycles

AFT CARGO FRAME UPPER CHORD CORRODED BODY STATION 1440, RIGHT BUTTLINE 2. CURRENTLY UNDERGOING REPAIRS.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

WEB AT STRINGER 13 LEFT STATION 680 IS CRACKED. CURRENTLY UNDERGOING REPAIRS.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

WEB AT STRINGER 12 RIGHT STATION 680 IS CRACKED. CURRENTLY UNDERGOING REPAIRS.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,325 hrs · 21,388 cycles

WEB AT STRINGER 13 RIGHT STATION 680 IS CRACKED. CURRENTLY UNDERGOING REPAIRS.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 61,732 hrs · 21,172 cycles

SJU INFLIGHT STT-JFK. CREW REPORTED ON CLIMBOUT RIGHT ENGINE COMPRESSOR STALLS. RETARDING RIGHT THROTTLE AND COMPRESSOR STALL CEASED. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT SJU ON 07/12/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,324 hrs · 20,304 cycles

RIGHT AFT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK FOR RIGHT AFT EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 58,321 hrs · 19,940 cycles

CORROSION REAR SPAR UPPER T-CAP INBOARD OF MAIN LANDING GEAR FORWARD TRUNNION. REPAIRED PER EA B757-57-009791 DATED 3/26/2010.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 58,321 hrs · 19,940 cycles

CORROSION ON SPAR T-CAP BETWEEN WING STATIONS 190 AND 210. REPAIRED PER EA B757-57-009791 DATED 3/26/2010.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,321 hrs · 19,940 cycles

VERTICAL STIFFENERS CRACKED STATION 700 AT LEFT BUTTLINE 24 AND LEFT BUTTLINE 48. REMOVED AND REPLACED VERTICAL STIFFENERS WITH SERVICEABLE STIFFENERS PER SRM 51-10-02-0G.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 58,321 hrs · 19,940 cycles

NUMBER 2 SLAT OUTBOARD UPPER TRAILING EDGE CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,934 hrs · 19,461 cycles

EMERGENCY LIGHT INOPERATIVE ON TRACK OF SEAT 35D. RELAMPED, OPS CHECK NORMAL.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHTS)

LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 26DEF AND 27DEF BROKEN. REPLACED POWER SUPPLY M10801 FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 26DEF AND 27DEF.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 26DEF AND 27DEF BROKEN. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 26DEF AND 27DEF.

Part: MODULE — DEFECTIVE (CABIN) · airframe 55,197 hrs

DFW SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 16 TO ROW 25 DIM. REPLACED M10800 MODULE.

Part: MODULE — DEFECTIVE (CABIN) · airframe 55,197 hrs

DFW SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 26 TO 36 INOPERATIVE. REPLACED EMERGENCY LIGHT MODULE M10801.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW EMERGENCY LIGHTS AT AFT SEAT ROW 3 BULLNOSE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHTS AT OVERHEAD BULLNOSE SEAT 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT OVERHEAD BULLNOSE SEAT 2E. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — DAMAGED (TE FLAPS) · airframe 52,112 hrs

AMA INFLIGHT T2466/14MAR SFO TO DFW - CREW REPORTED LEADING EDGE FLAP ASYMMETRY MESSAGE. LANDED AMA WITHOUT INCIDENT. FOUND LEFT WING CONNECTOR DAMAGED. REPLACED LEFT WING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — SMOKE (WINDOW HEAT)

JFK INFLIGHT T160/09OCT - SMOKE REPORTED FROM ELECTRICAL CONNECTOR AT LOWER LEFT CORNER OF CAPTAINS FORWARD WINDOW. WINDOW HEAT SWITCHED TURNED OFF AND SMOKE DISSIPATED. LANDED JFK WITHOUT INCIDENT. REPLACED FORWARD WINDOW AND WINDOW HEAT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 6E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — MISSING (CABIN)

MIA - EMERGENCY EXIT SIGN ABOVE LEFT NUMBER FOUR DOOR MISSING. REPLACED EMERGENCY EXIT SIGN ABOVE LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY EXIT LIGHT LENS MISSING AT FIRST CLASS AFT OF COAT CLOSET. REPLACED MISSING LENS FOR MISSING EMERGENCY EXIT LIGHT LENS AT FIRST CLASS AFT OF COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LATCH HANDLE — BROKEN (RAFT COMPARTMENT)

CLO - RIGHT HAND AFT RAFT OVERHEAD COMPARTMENT LATCH HANDLE IS BROKEN. RAFT COMPARTMENT WILL NOT OPEN DURING NORMAL OR EMERGENCY PROCEDURES AND COULD NOT BE OPEN FOR SECURITY CHECKS. PARTS NOT IN STOCK AT CLO. FERRIED AIRCRAFT TO MIA FOR REPAIR PER SPOTTING MESSAGE 03-098 DATED 3/23/04. REPLACED RIGHT HAND LATCH HANDLE ASSEMBLY FOR RIGHT HAND AFT RAFT OVERHEAD COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA LEFT AFT DOOR EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR LEFT AFT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA RIGHT AFT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA EMERGENCY LIGHTS AT ROW SEAT 25B TO 34D DIM. REPLACED AFT CABIN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE IN FIRST CLASS CABIN. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (ROW 9D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 9D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — WORN (BS 1862.7)

AFW - FOUND STATION 1862.7 HAS SMALL AREA OF WEAR, BEYOND SRM LIMITS. REPAIR PER MRB 757-1038. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

AFW - AFT CARGO DOOR LOWER SILL INNER CHORD HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-1037. (M)

Part: FLOOR SUPPORT — CORRODED (BS 408)

AFW - FLOOR STRUCTURE AT STATION 408 RBL 57 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1030. (M)

Part: FLOORBEAM — CORRODED (BS 310)

AFW - FLOORBEAM AT STATION 310 RBL 3 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1032. (M)

Part: FLOOR SUPPORT — CORRODED (BS 403)

AFW - FLOOR STRUCTURE AT STATION 403 RBL 59 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1034. (M)

Part: FLOOR SUPPORT — CORRODED (BS 357)

AFW - FOUND FLOOR STRUCTURE AT STATION 357 RBL 62 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1029. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM AT STATION 377 RBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1035. (M)

Part: DOOR PAN — GOUGED (L4 DOOR)

AFW - L-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS. REPAIR PER MRB 757-1040. (M)

Part: FLOORBEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-1036. (M)

Part: FLOOR SUPPORT — CORRODED (BS 331)

AFW - FLOOR STRUCTURE AT STATION 331 RBL 3 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1031. (M)

Part: FLOORBEAM — CORRODED (BS 365)

AFW - FOUND FLOORBEAM AT STATION 365 RBL 61 HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIRED PER MRB 757-1028. (M)

Part: FLOOR SUPPORT — CORRODED (BS 372)

AFW - FLOOR STRUCTURE AT STATION 372 RBL 62 HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-1027. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT, MAINTENANCE FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN THE FORWARD CABIN INTERMITTENT. REPLACED CONNECTOR AT RIGHT SIDE FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RIB — DRILL MARKS (VERT STAB)

AFW - FOUND VERTICAL STABILIZER RIB AT STATION 206 HAS DRILL MARKS. (M)

Part: SKIN — SCRATCHED (BS 1580)

AFW - FOUND SCRATCH IN SKIN AFT FUSELAGE APPROX STATION 1580, STRINGER 27R. (M)

Part: STRIP — DEFECTIVE (CABIN EEL)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)