N197AN

Part: LIGHT — INOPERATIVE (SEAT 3E) · airframe 58,050 hrs · 16,463 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERABLE AT SEAT 3E. MAINTENANCE REPLACED SEAT EMERGENCY LIGHT IAW AMM 33-51-10.

Part: LIGHT — INOPERATIVE (SEAT 1E) · airframe 58,050 hrs · 16,463 cycles

AIRCRAFT WAS NOT GROUNDED, EMERGENCY LIGHT INOPERABLE AT SEAT 1E. MAINTENANCE REPLACED SEAT EMERGENCY LIGHT PER AMM 33-51-10.

Part: ACM — DAMAGED (ZONE 100 - FUSE) · airframe 57,502 hrs · 16,281 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT 17,000 TURNED OFF APU IAW PROCEDURE. CLIMED ON SINGLE PACK SINGLE SOURCE ON RIGHT PACK. NOTICED CABIN CLIMBING UNCONTROLABLE @ 30,000. INIATED DECENT TO 10,000 RT PACK WAS INOPERTIVE, INOP PACK OFF LIGHT ILLIMINATED ON GROUND AFTER LANDING. MAINTENANCE FOUND THE R/ACM TURBINE OUTLET DUCT SEPERATED, WITH THE UPPER DUCT SEAL ATTACHING CABLE SHEARED AND THE LOWER CABLE BALL PULLED THRU THE TURBINE MOUNTING CASTING. REMOVED AND REPLACED RIGHT PACK ACM IAW AMM 21-51-03. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 57,492 hrs · 16,276 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT FLIGHT ATTENDANT FLASHLIGHT LED INDICATOR WAS NOT FLASHING. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 57,220 hrs · 16,198 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS L2 PASSENGER DOOR ESCAPE SLIDE CYLINDER PRESSURE GAGE BELOW LIMITS. MAINTENANCE REPLACED L2 PASSENGER SERVICE DOOR SLIDE ASSEMBLY IAW AMM 25-66-01 AND CARD 19L80025002.

Part: CONTROL PANEL — FAULTY (L1 DOOR) · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EVACUATION HORN IN CABIN WAS NOT PULSING. MAINTENANCE REPLACED EVACUATION PANEL PER AMM 25-63-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CONTROL PANEL — FAULTY (EES) · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EVACUATION HORN IN CABIN WAS NOT PULSING. MAINTENANCE REPLACED EVACUATION EES PANEL PER AMM 25-63-01.

Part: RIB — CORRODED (CARGO DOOR) · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR FIRST LOWER RIB. REPAIRED RIB PER EA 295901.

Part: DECK PLATE — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT DECK PLATE BETWEEN BS 1680 AND BS 1720, BETWEEN LBL 56 AND RBL 56. REPLACED AFT DECK PLATE PER 51-00-05.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM TEE CAP AT BS 1680 AND RBL 47. REPAIRED FLOOR BEAM T CAP PER SEM 53-60-51-2R-3 AND EA 296039.

Part: MOUNT — CORRODED (BS 1686) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY MOUNT AT BS 1686 AND LBL 49. REPLACED GALLEY MOUNT PER SRM 51-40-02.

Part: ANGLE — CORRODED (BS 1715) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE AT BS 1715 AND RBL 49. REPLACED Z ANGLE PER SRM 51-40-02.

Part: MOUNT — CORRODED (BS 1686) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY MOUNT AT BS 1686 AND RBL 49. REPLACED GALLEY MOUNT PER SRM 51-40-02.

Part: GUTTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GUTTER BOX AT BS 1647 AND LBL 56. REPLACED GUTTER BOX PER 51-00-05-1.

Part: MOUNT — CORRODED (BS 1712) · corrosion level 2 · airframe 56,654 hrs · 16,028 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY MOUNT AT BS 1712 AND LBL 49. REPLACED GALLEY MOUNT PER SRM 51-40-02.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,964 hrs · 15,840 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE FOUND EMERGENCY LIGHTS VERY DIM AT FISRT CLASS SEATS. REMOVED AND REPLACED FIRST CLASS EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,955 hrs · 15,836 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE FOUND THE EMERGENCY LIGHTS DIM FROM ROW 27 TO 36. REMOVED AND REPLACED ROW 27 TO 36 BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,903 hrs · 15,820 cycles

AIRCRAFT WAS NOT GROUNDED: DURING A CHECK, FOUND SEATS EMERGENCY LIGHTS NOT WORKING FROM ROW 27D TO 36D. MAINTENANCE REPLACED BATTERY PACK ABOVE M LAVATORY PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,905 hrs · 15,821 cycles

AIRCRAFT WAS NOT GROUNDED: DURING A CHECK, FOUND SEATS EMERGENCY LIGHTS NOT WORKING FROM ROW 27D TO 36D. MAINTENANCE REPLACED BATTERY PACK ABOVE M LAVATORY PER AMM 35-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,798 hrs · 15,787 cycles

L4 DOOR EXIT SIGN WAS DIM. MAINTENANCE REPLACED THE BATTERY PACK M10801 IAW AMM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,798 hrs · 15,787 cycles

R4 DOOR EXIT SIGN WAS DIM. MAINTENANCE REPLACED THE BATTERY PACK M10801 IAW AMM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,799 hrs · 15,787 cycles

SEAT MOUNTED EMERGENCY LIGHTS WERE DIM FROM 27D TO 36D. MAINTENANCE REPLACED THE BATTERY PACK M10801 IAW AMM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 55,799 hrs · 15,787 cycles

L4 DOOR EXIT SIGN WAS DIM. MAINTENANCE REPLACED THE BATTERY PACK M10801 IAW AMM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 55,799 hrs · 15,787 cycles

THE R4 DOOR EXIT SIGN WAS DIM. MAINTENANCE REPLACED BATTERY PACK M10801 IAW AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 55,571 hrs · 15,722 cycles

FIRST OFFICER`S R2 SLIDING WINDOW WAS DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDOW IAW AMM 56-11-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,239 hrs · 15,633 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEATS 27G THROUGH 36G. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,239 hrs · 15,633 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEATS 27G THROUGH 36G. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-07, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 54,698 hrs · 15,459 cycles

ROW 26D-36D EMERGENCY LIGHTS WILL NOT TURN OFF. AIRCRAFT IS POWERED DOWN. REPLACED THE POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-07. EMERGENCY LIGHTS ROW 26D-36D OPS TESTED OK.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 54,698 hrs · 15,459 cycles

AIRCRAFT WAS NOT GROUNDED. ROW 26D-36D EMERGENCY LIGHTS WILL NOT TURNOFF. A/C IS POWERED DOWN. (BAT OFF). REPLACED BATTERY PACK EQ M10801 AS PER AMM 33-51-07. EMERGENCY AISLE LIGHTS ROW 26D-36D. OPERATIONS TESTS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,698 hrs · 15,459 cycles

AIRCRAFT WAS NOT GROUNDED. ROW 26D-36D EMERGENCY LIGHTS WILL NOT TURNOFF. A/C IS POWERED DOWN. (BAT OFF). REPLACED POWER SUPPLY PER AMM 33-51-07. EMERGENCY AISLE LIGHTS ROW 26D-36D. OPERATIONS TESTS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,563 hrs · 15,431 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHTING INOPERABLE AT AISLE SEAT 27 TO 36. MAINTENANCE REPLACED POWERPACK MODULE (SEE AALA201810189016) AND BATTERY EQ M10801 AS PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: MODULE — FAULTY (CABIN) · airframe 54,563 hrs · 15,431 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHTING INOPERABLE AT AISLE SEAT 27 TO 36. MAINTENANCE REPLACED POWERPACK MODULE AND BATTERY (SEE AALA201810189021) EQ M10801 AS PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,437 hrs · 15,400 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTS WERE DIM AT SEATS 9 TO 16 AND 2R DOOR. MAINTENANCE REPLACED BATTERY PACK PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: ENGINE — ODOR (RIGHT) · airframe 52,413 hrs · 14,873 cycles

DIRTY SOCK ODOR NOTED IN AFT CABIN AT TOP OF DESCENT. AIRCRAFT WAS GROUNDED. COMPLETED DUCT CLEANING. CHANGED THE RIGHT ENGINE IAW 71-94-01.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 52,271 hrs · 14,824 cycles

EMERGENCY LIGHT AT SEAT 32 INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW MM 33-51-00.

Part: FILTER — CLOGGED (CABIN) · airframe 51,904 hrs · 14,698 cycles

THE AIRCRAFT WAS GROUNDED. FLIGHT ATTENDANTS REPORTED ACRID SMELL DURING FLIGHT. PASSENGERS ALSO COMPLAINED OF SMELL. ACCOMPLISHED AIR QUANTITY CARD 05-96-70 FOUND RECIRCULATION FAN AIR FILTERS CLOGGED. REPLACED HIGH EFFICIENCY HEPA FILTERS IAW MM 21-25-02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,694 hrs · 14,650 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE FORWARD GALLEY FORWARD JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: COMPUTER — FAULTY (ALERTING SYS) · airframe 51,098 hrs · 14,524 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. AFTER TAKEOFF ON GEAR RETRACTION, THE LEFT ENGINE EGT INDICATED AN OVERHEAT AND MULTIPLE RED EICAS MESSAGES. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL MODULE AND FUEL CUTOFF SWITCH IAW AMM 76-11-02, AND LEFT ENGINE INDICATION AND CREW ALERTING SYSTEM COMPUTER IAW AMM 31-41-02. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: FUEL CONTROL — FAULTY (LT ENGINE) · airframe 51,098 hrs · 14,524 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE, AFTER TAKEOFF ON GEAR RETRACTION THE LEFT ENGINE EGT INDICATED AN OVERHEAT AND MULTIPLE RED EICAS MESSAGES. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL MODULE AND FUEL CUTOFF SWITCH IAW AMM 76-11-02, AND LEFT ENGINE INDICATION AND CREW ALERTING SYSTEM COMPUTER IAW AMM 31-41-02. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SWITCH — FAULTY (LT ENGINE) · airframe 51,098 hrs · 14,524 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. ACCOUNT AFTER TAKEOFF UPON GEAR RETRACTION THE LEFT ENGINE EGT INDICATED AN OVERHEAT AND MULTIPLE RED EICAS MESSAGES. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL MODULE AND FUEL CUTOFF SWITCH IAW AMM 76-11-02, AND LEFT ENGINE INDICATION AND CREW ALERTING SYSTEM COMPUTER IAW AMM 31-41-02. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,969 hrs · 14,491 cycles

L4 DOOR EXIT LIGHT COVER IS MISSING. FABRICATED TEMPORARY REPLACEMENT AND INSTALLED IAW EA 272249. REMOVED AND REPLACED LENS IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 50,257 hrs · 14,297 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT R2 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 49,912 hrs · 14,192 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: CHANNEL — LACK OF LUBE (SLIDING WINDOW) · airframe 49,905 hrs · 14,189 cycles

AIRCRAFT WAS NOT GROUNDED. CAPTAINS SLIDING WINDOW IS EXTREMELY DIFFICULT TO OPEN AND CLOSE. LUBRICATED GUIDE CHANNEL AND TRACKS IAW AMM 56-10-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,147 hrs · 13,732 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS AT L1 DOOR AND IN FWD SECTION OF FIRST CLASS ARE INOPERATIVE. R & R THE CHARGER AND BATTERY ASSEMBLIES AT FS 366 IAW AMM 33-51-07. OPS CHECK NORMAL.

Part: CHARGER — FAULTY (CABIN) · airframe 48,147 hrs · 13,732 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS AT L1 DOOR AND IN FORWARD SECTION OF FIRST CLASS ARE INOPERATIVE. R & R THE CHARGER AND BATTERY ASSEMBLIES AT FS 366 IAW AMM 33-51-07. OPS CHECK NORMAL.

Part: DECK PLATE — CORRODED (BS 1720) · corrosion level 2 · airframe 47,791 hrs · 13,641 cycles

AFT DECK PLATE IS CORRODED AT BS 1720 AND LBL 36. REPAIRED DECK PLATE IAW 53-60-51-3.

Part: DECK PLATE — CORRODED (BS 1720) · corrosion level 2 · airframe 47,791 hrs · 13,641 cycles

AFT DECK PLATE IS CORRODED AT FUSELAGE STATION 1720 AND LBL 2. REPAIRED DECK PLATE IAW 53-60-51-3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,431 hrs · 13,308 cycles

EMERGENCY LIGHTS INOPERATIVE AT L3 & R3 DOORS. R & R BATTERY PACKS IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL. THE ACFT WAS GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,431 hrs · 13,308 cycles

EMERGENCY LIGHTS INOPERATIVE FIRST CLASS SEAT L1 & L2 DOORS. R & R BATTERY PACK IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL. THE ACFT WAS GNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,128 hrs · 13,013 cycles

LAST TWO SEGMENTS OF OVERHEAD LT SIDE OF EMER LIGHTS ARE INOPERATIVE, BAG BINS. R & R POWER SUPPLY CHARGER & BATTERY M737 IAW AMM 33-51-07. EMER OVERHEAD AISLE LIGHTS & GALLEY, AFT EXIT LIGHT. OPERATIONAL TESTED OK. SEE ALSO AALA20151014004.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,128 hrs · 13,013 cycles

LAST TWO SEGMENTS OF OVERHEAD LT SIDE OF EMER LIGHTS ARE INOPERATIVE, BAG BINS. R & R POWER SUPPLY CHARGER & BATTERY M737 IAW AMM 33-51-07. EMER OVERHEAD AISLE LIGHTS & GALLEY, AFT EXIT LIGHT OPERATIONAL TESTED OK. SEE ALSO AALA20151014005.

Part: LENS — BROKEN (ZONE 200) · airframe 43,827 hrs · 12,739 cycles

EMERGENCY EXIT LIGHT LENS COVER BROKEN AT L1 DOOR. INSTALLED LENS COVER. OPERATIONS CHECKED GOOD IAW MM 33-51-00-501.

Part: PROBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 43,719 hrs · 12,710 cycles

DURING TAKEOFF FIRST OFFICERS AIRSPEED REMAINED STUCK AT 47 KNOTS. TAKEOFF ABORTED AT APPROX 90 KNOTS. FOUND FIRST OFFICER`S PITOT TUBE BLOCKED BY DEBRIS. R & R PITOT IAW AMM 34-11-01. PERFORMED OPERATIONAL & LEAK CHECK. SYS CHECKED NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 42,480 hrs · 12,397 cycles

FOUND SEAT 4D EMER PATH LIGHTING INOPERATIVE. REPLACED PINS IN THE SEAT CONNECTOR.

Part: PUMP — FAILED (FUEL TANK) · airframe 42,385 hrs · 12,374 cycles

RIGHT CTR FUEL PUMP EICAS MESSAGE WITH PRESSURE LIGHT & OVER 30,000 LBS OF FUEL IN THE TANK. RETURNED TO DEPARTURE, EMERGENCY DECLARED, AND LANDED UNEVENTFULLY. REMOVED AND REPLACED N3 TACH GENERATOR AND CONNECTOR PER AMM 77-12-02 AND SWPM 20-61-00. RAN ENGINES, OPS CHECK OF FUEL PUMPS AND ENGINES OK.

Part: ACTUATOR — LEAKING (NR 2 SPOILER) · airframe 41,192 hrs · 12,094 cycles

RT HYD QTY SYS LOSS FOLLOWED BY RT HYD QTY EICAS MSG & RESERVOIR LIGHT ON OVERHEAD ILLUMINATED. EMER DECLARED FLIGHT DIVERTED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND HYD FLUID LEAKING FROM NR 2 SPOILER ACTUATOR. REPLACED NR 2 SPOILER POWER CONTROL ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: ENGINE — FAILED (LEFT) · airframe 38,288 hrs · 11,424 cycles

JFK CREW REPORTED LOSS OF LT ENGINE OIL PRESSURE. ASSOCIATED EICAS "OIL PRESSURE" MESSAGE. CREW SHUTDOWN ENGINE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE AT JFK ON 09/29/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — BURNED OUT (CABIN) · airframe 37,391 hrs · 11,199 cycles

CREW REPORTED ELECTRICAL BURNING ODOR DURING THE FLIGHT. NO OTHER ABNORMAL INDICATIONS OR SMOKE. FLIGHT LANDED MIA WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED BURNED OUT CEILING LIGHT IN FIRST CLASS AT SEAT 1AB. SYS GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: CONTROL PANEL — FAILED (FIRE WARNING) · airframe 37,321 hrs · 11,179 cycles

REPEAT: CREW REPORTED NO INFLIGHT RESTART OF LT ENGINE. LT ENGINE VALVE DISCRETE REMAINED ILLUMINATED AFTER MOVING FUEL CONTROL SWITCH TO RUN WITH NO FUEL FLOW OBSERVED. SINGLE ENGINE TIME 32 MINUTES. FLIGHT LANDED WITHOUT INCIDENT. REPLACED FIRE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GOVERNOR — FAILED (LT ENGINE) · airframe 37,319 hrs · 11,178 cycles

CREW REPORTED NO INFLIGHT RESTART ON LT ENGINE. LEFT ENGINE VALVE ILLUMINATED WITH EICAS MESSAGE WHEN FUEL SWITCH PLACED IN EITHER ON OR OFF POSITION. FLIGHT LANDED WITHOUT INCIDENT. REPLACED LT FUEL FLOW GOVERNOR. SYS GROUND CHECK NORMAL OPS.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 37,319 hrs · 11,178 cycles

RIGHT NR 4 DOOR LOWER GATE CORRODED AT FWD AND AFT EDGE. ACCOMPLISHED REPAIR IAW REO-G16250, REV B AND EA COMP 52-029979.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,319 hrs · 11,178 cycles

NUMEROUS BLENDOUTS ON FUSELAGE EXTERIOR SKIN ARE OUT OF LIMITS BETWEEN STATIONS 199 TO 231 AND BUTTLINE 0 AND LEFT BUTTLINE 14. ACCOMPLISHED REPAIR IAW EA B757-53-029961.

Part: SWITCH — BROKEN (EMERGENCY LIGHTS) · airframe 37,319 hrs · 11,178 cycles

LEFT NR 4 DOOR EMERGENCY LIGHTS TEST SWITCH ON DOOR LINER BROKEN. REPLACED LT NR 4 DOOR EMERGENCY LIGHTS TEST SWITCH . OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (ZONE 100) · airframe 37,319 hrs · 11,178 cycles

FUSELAGE SKIN, LT SIDE INSIDE RVSM AREA UPPER AFT CORNER THREE REPAIR FASTENERS ARE NOT FLUSH AND OUT OF WAVINESS. ACCOMPLISHED REPAIR IAW EA B757-53-029879 AND REO-G16229, REV A.

Part: PROBE — FAILED (TAT SYSTEM) · airframe 36,671 hrs · 11,026 cycles

MIA - CREW REPORTED EICAS MESSAGE FOR "TAT PROBE". EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED TOTAL AIR TEMPERATURE PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 36,671 hrs · 11,026 cycles

SEAT 4E EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 4E. OPS CHECKED NORMAL.

Part: FRAME — DENTED (FUSELAGE) · airframe 36,671 hrs · 11,026 cycles

DENT ON TOP OF FRAME AT STATION 580 BETWEEN STRINGERS 24 AND 25 LEFT. ACCOMPLISHED FRAME REPAIR SPLICE PER SRM 53-00-07-2R 5 DETAIL 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,218 hrs · 10,917 cycles

EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32D. OPS CHECK NORMAL.

Part: GENERATOR — INOPERATIVE (RT ENGINE) · airframe 33,487 hrs · 10,337 cycles

INFLIGHT, CREW REPORTED RIGHT ENGINE INTEGRATED DRIVE GENERATOR TRIPPED OFF LINE. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PANEL — UNSECURE (CABIN) · airframe 32,691 hrs · 10,162 cycles

FLIGHT ATTENDANTS REPORTED SOME OF THE EMERGENCY LIGHTS CAME ON IN THE BACK OF THE AIRCRAFT DURING FLIGHT. FOUND THE PANEL OVER LEFT NUMBER 3 DOOR THAT HOLDS EMERGENCY LIGHT AND ZONE TEST SWITCH NOT SECURED. INSTALLED HARDWARE. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,379 hrs · 9,281 cycles

EMERGENCY LIGHT ON SEAT ROWS 16 TO 26 INOPEATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 16. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 28,379 hrs · 9,281 cycles

EMERGENCY LIGHT ON SEAT ROWS 16 TO 26 INOPEATIVE. REMOVED AND REPLACED EMERGENCY LIGHT MODULE AT ROW 16. OPS CHECK NORMAL.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 27,834 hrs · 9,173 cycles

LARGE DENT AND DELAMINATION ON NUMBER 10 SLAT TRAILING EDGE WEDGE. REMOVED TRAILING EDGE WEDGE AND INSTALLED NEW WEDGE PER ESO 90253.

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 26,254 hrs · 8,840 cycles

ORD - CREW REPORTED A BURNING SMELL IN THE CABIN. IN-FLIGHT ENTERTAINMENT SYSTEM WAS DEACTIVATED AND NO CHANGE NOTED. AUXILIARY POWER UNIT WAS TURNED OFF AND NO CHANGE NOTED. EMERGENCY DECLARED, RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PLASTIC MELTED ON HOT PLATE OF COFFEEMAKER ON LEFT SIDE OF AFT CABIN. ALL OTHER PARAMETERS CHECKED AND NO FURTHER ODORS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,536 hrs · 8,635 cycles

EMERGENCY PATH LIGHTS AT CENTER SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK FOR COACH CENTER SECTION.

Part: LENS — BROKEN (CABIN) · airframe 25,110 hrs · 8,499 cycles

CREW REPORTED RIGHT NUMBER ONE DOOR FORWARD EMERGENCY EXIT LIGHT LENS IS BROKEN AND DETACHED FROM BASE. REPLACED RIGHT NUMBER ONE DOOR FORWARD EMERGENCY LIGHT ASSEMBLY. OPS CHECK IS OK.

Part: CONTROL PANEL — FAILED (ELECTRICAL SYS) · airframe 25,029 hrs · 8,473 cycles

CREW REPORTED VARIOUS ELECTRICAL FAILURES DURING T/O AND CLIMBOUT. LEFT AND CENTER FLIGHT DIRECTOR VNAV WOULD NOT ENGAGE, AUTOTHROTTLE WOULD NOT ENGAGE, AND LEFT ELECTRICAL HYDRAULIC PUMP FAILED. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED MODE CONTROL PANEL AND LEFT HYDRAULIC PUMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,177 hrs

DFW - SEAT MOUNTED EMERGENCY AISLE LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY AISLE LIGHTS.

Part: LENS — MISSING (CABIN)

DFW - RIGHT OVERWING EXIT SIGN LENS MISSING. INSTALLED SERVICEABLE EXIT SIGN LENS.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - LEFT NUMBER ONE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER ONE DOOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY LIGHT.

Part: CONTACT — OPEN (RELAY)

ORD INFLIGHT T268/22SEP SEA TO JFK. CREW REPORTED AIR GROUND SYSTEM EICAS MSG WITH SEVERAL COMPONENT FAILURES OF INERTIAL REFERENCE SYSTEM AND MAIN BATTERY CHARGER FOLLOWED BY FAILURE OF ALL CAPTAINS INSTRUMENTS. LANDED ORD. ON LANDING ACFT WENT OFF END OF RUNWAY. NO INJURIES REPORTED. ACFT HAD BLOWN TIRES. FOUND B1 AND B2 CONTACTS OPEN ON K106 RELAY. REPLACED B1 AND B2 CONTACTS FOR RELAY K106. EICAS COMPUTERS REPLACED. REPLACED MAIN AND APU BATTERIES AND CAPTAINS WIPER MOTOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT RT NR 4 DOOR INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT RT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INCORRECT (CABIN)

DFW EMERGENCY LIGHT AT SEAT 25D HAS WRONG LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CARGO BAY)

DFW EMERGENCY LIGHT AT AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 3B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 29D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — MALFUNCTIONED (LT ENGINE)

LAX - DURING CLIMB AT 6000 FEET, LEFT ENGINE COMPRESSOR STALLED. ENGINE GAS TEMPERATURE AT 914 DEGREES. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. LANDED WITH ENGINE AT IDLE. REPLACED NUMBER ONE ENGINE ON 05 APR AT LAX DUE TO BLEED VALVE CONTROL UNIT FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK AT FRONT OF FIRST CLASS FOR EMERGENCY LIGHTS AT FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHTS FROM ROW 26 AFT TO LEFT AND RIGHT NUMBER 4 DOOR INOPERATIVE. FOUND LEFT NUMBER 4 DOOR FORWARD EXIT LIGHT L759 SHORTED. REPLACED LEFT NUMBER 4 EXIT LIGHT ASSEMBLY FOR EMERGENCY LIGHTS FROM ROW 26 AFT TO LEFT AND RIGHT NUMBER 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY LIGHT ASSEMBLY AT 17D BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

UNCOMMANDED ILLUMINATION OF EMERGENCY LIGHTS FOR ROWS 16 THROUGH 24. REPLACED EMERGENCY LIGHTS CHARGER AND BATTERY FOR ROW 16 THROUGH 24. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: ENGINE — SURGES (LEFT)

ON TAKEOFF ROLL AT ORD, LEFT ENGINE AT STD POWER SETTING STARTED SURING BETWEEN 1.5 AND 1.6 EPR SEVERAL TIMES ABORTED TAKEOFF. (M)

Part: SLIDE — MALFUNCTIONED (PAX DOOR)

MIA - FLT 68 - UPON ARRIVAL AT MIA, FORWARD ENTRY DOOR SLIDE PARTIALLY DEPLOYED AFTER DOOR OPENED. SLIDE WAS REMOVED FROM COMPARTMENT AND GIRT BAR BEFORE INFLATION OCCURRED. DOOR WAS DISARMED. INSPECTED SLIDE ARMING MECHANISM. OPERATION CHECKS GOOD. REPLACED L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)