N192AN

Part: SENSOR — FAULTY (MLG) · airframe 64,382 hrs · 16,839 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING DESCENT BELOW 15,000 CONFIG LIGHT AND GEAR NOT DOWN EICAS MESSAGE ILLUMINATED NUMEROUS TIMES. MAINTENANCE REMOVED AND REPLACED NLG COMPRESSED SENSOR S10067 IAW AMM 32-09-08. OPS CHECK OK.

Part: FMC — FALSE INDICATION (LEFT) · airframe 64,090 hrs · 16,737 cycles

AIRCRAFT NOT GROUNDED: IN CRZ AT FL 390 DUAL FMC FAILURE. LNAV RECOVERED IN 5 MINUTES VNAV REMAINED INOP. QRH CALLED FOR SELECTION OF ALTERNATE NAV SELECTOR, THIS DID NOT CLEAR PROBLEM. ACCOMPLISHED FMC BITE IAW FIM 34-61-00 ALL CKD NORMAL.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 63,833 hrs · 16,657 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND OFF WING SLIDE BOTTLE PRESSURE SWITCH WAS NOT WORKING IN COCKPIT PER JOB CARD 1610. REPLACED SWITCH ASSEMBLY PER AMM 25-65-02.

Part: FMC — MALFUNCTIONED · airframe 63,599 hrs · 16,591 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS BOTH FMCS ON 2 OCCASIONS DELETED ALL WAYPOINTS FROM THE ROUTE AND LEGS PAGE. RESULTING IN A COMPLETE LOSS OF THE FLIGHT PLAN. NO FAILURE MESSAGE. MAINTENANCE UPLOADED FMC SOFTWARE IAW AMM 34-61-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (R4 DOOR SLIDE) · airframe 63,464 hrs · 16,556 cycles

AIRCRAFT WAS NOT GROUNDED: R4 EMERGENCY SLIDE LIGHT INOPERABLE. MAINTENANCE REPLACED SLIDE LIGHT IAW AMM 33-51-06.

Part: LAMP — INOPERATIVE (EXTERNAL LIGHT) · airframe 62,184 hrs · 16,209 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR EXTERNAL SLIDE LIGHT WAS INOPERABLE. MAINTENANCE RELAMPED R1 DOOR EXTERNAL SLIDE LIGHT PER AMM 33-51-06 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,182 hrs · 16,208 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS FROM 9D THROUGH 15DEF WERE VERY DIM. MAINTENANCE REPLACED CHARGER AND BATTERY PACK M10952 PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — FAULTED (CABIN) · airframe 62,108 hrs · 16,187 cycles

L4 DOOR AREA FLASHLIGHT FAULTED. MAINTENANCE REPLACED THE FLASHLIGHT, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 61,875 hrs · 16,114 cycles

L1 JUMP SEAT FLASHLIGHT BATTERY WOULD NOT TEST. MAINTENANCE REPLACED L1 JUMP SEAT FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: HYDRAULIC LINE — LEAKING (CENTER SYSTEM) · airframe 61,731 hrs · 16,063 cycles

HYDRAULIC QUANTITY LOW INDICATION, CENTER HYDRAULIC QUANTITY EICAS MESSAGE DISPLAYED. EMERGENCY DECLARED, DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED HYDRAULIC RIGID LINE FOR THE CENTER HYDRAULIC SYSTEM IAW 29-11-00, NO LEAKS NOTED, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BELLCRANK — SHEARED (R1 DOOR) · airframe 61,671 hrs · 16,044 cycles

THE R1 DOOR SLIDE ARM, BELLCRANK ASSEMBLY, LEVER SHEARED AT THE LOWER GATE ASSEMBLY. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BELLCRANK ASSEMBLY IAW STANDARD PRACTICES. PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 61,623 hrs · 16,032 cycles

L1 DOOR HAD A GUST LOCK SPLINE COLLAR CRACKED. THE AIRCRAFT WAS GROUNDED. REPLACED GUST LOCK COLLAR IAW AMM 52-11-08. OPS CHECKED GOOD.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 59,386 hrs · 15,461 cycles

NR 2 PYLON PRECOOLER LOUVERED PANEL CUT-OUT LANDING SKIN CRACKED AT LOWER EDGE. REPAIRED IAW EA 277444.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 59,386 hrs · 15,461 cycles

CORROSION ON THE UPPER AND LOWER SURFACES OF THE RIGHT OVERWING FUEL PORT SKIN FITTING. REPAIRED THE SKIN IAW AMM 28-11-04 AND EA 277597.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 59,386 hrs · 15,461 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT OVERWING FILL PORT FAILS BONDING RESISTANCE CHECK. UPON REMOVAL OF THE LEFT OVERWING FILL-PORT FITTING CORROSION WAS DISCOVERED ON THE UPPER AND LOWER SURFACES OF THE FILL-PORT LANDING ON THE WING SKIN. REPAIRED SKIN PER EA 277838.

Part: SWITCH — DEFECTIVE (NR 1 ENGINE) · airframe 59,374 hrs · 15,457 cycles

THE FLIGHT REJECTED TAKE-OFF DUE TO A COMPRESSOR STALL ON THE NR 1 ENGINE. WITNESSES SAW FLAMES COMING OUT AND A BANGING NOISE ALERTED THE CREW. REJECTED TAKE-OFF INITIATED AT 40KTS. NO FURTHER INCIDENTS OCCURRED. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARD 72-92-12 FOR COMPRESSOR SURGE. REMOVED AND REPLACED THE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07, DEDICATED GENERATOR IAW AMM 73-21-08, TRANSIENT PRESSURE SENSOR UNIT IAW AMM 75-32-15, BLEED VALVE CONTROL UNIT (BVCU) IAW AMM 75-32-01, AND ALTITUDE SWITCH IAW AMM 75-32-07, ACCOMPLISHED AIRLFOW CONTROL TEST 3 IAW AMM 71-00-00, AND ACCELERATION - DECELERATION TEST 11 IAW AMM 71-00-00. NO DEFECTS NOTED AFTER FINAL ENGINE RUN. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: GENERATOR — DEFECTIVE (NR 1) · airframe 59,374 hrs · 15,457 cycles

THE FLIGHT REJECTED TAKE-OFF DUE TO A COMPRESSOR STALL ON NR 1 ENGINE. WITNESSES SAW FLAMES COMING OUT AND A BANGING NOISE ALERTED THE CREW. REJECTED TAKE-OFF INITIATED AT 40KTS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARD 72-92-12 FOR COMPRESSOR SURGE. REMOVED AND REPLACED THE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07, DEDICATED GENERATOR IAW AMM 73-21-08, TRANSIENT PRESSURE SENSOR UNIT IAW AMM 75-32-15, BLEED VALVE CONTROL UNIT IAW AMM 75-32-01, AND ALTITUDE SWITCH IAW AMM 75-32-07, ACCOMPLISHED AIRLFOW CONTROL TEST 3 IAW AMM 71-00-00, AND ACCELERATION, DECELERATION TEST 11 IAW AMM 71-00-00. NO DEFECTS NOTED AFTER FINAL ENGINE RUN. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: LIMITER — MALFUNCTIONED (NR 1 ENGINE) · airframe 59,374 hrs · 15,457 cycles

THE FLIGHT REJECTED TAKE-OFF DUE TO A COMPRESSOR STALL ON NR 1 ENGINE. WITNESSES SAW FLAMES COMING OUT AND A BANGING NOISE ALERTED THE CREW. REJECTED TAKE-OFF INITIATED AT 40KTS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARD 72-92-12 FOR COMPRESSOR SURGE. REMOVED AND REPLACED THE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07, DEDICATED GENERATOR IAW AMM 73-21-08, TRANSIENT PRESSURE SENSOR UNIT IAW AMM 75-32-15, BLEED VALVE CONTROL UNIT IAW AMM 75-32-01, AND ALTITUDE SWITCH IAW AMM 75-32-07, ACCOMPLISHED AIRLFOW CONTROL TEST 3 IAW AMM 71-00-00, AND ACCELERATION, DECELERATION TEST 11 IAW AMM 71-00-00. NO DEFECTS NOTED AFTER FINAL ENGINE RUN. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: SENSOR — DEFECTIVE (NR 1 ENGINE) · airframe 59,374 hrs · 15,457 cycles

THE FLIGHT REJECTED TAKE-OFF DUE TO A COMPRESSOR STALL ON NR 1 ENGINE. WITNESSES SAW FLAMES COMING OUT AND A BANGING NOISE ALERTED THE CREW. REJECTED TAKE-OFF INITIATED AT 40KTS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARD 72-92-12 FOR COMPRESSOR SURGE. REMOVED AND REPLACED THE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07, DEDICATED GENERATOR IAW AMM 73-21-08, TRANSIENT PRESSURE SENSOR UNIT IAW AMM 75-32-15, BLEED VALVE CONTROL UNIT IAW AMM 75-32-01, AND ALTITUDE SWITCH IAW AMM 75-32-07, ACCOMPLISHED AIRLFOW CONTROL TEST 3 IAW AMM 71-00-00, AND ACCELERATION, DECELERATION TEST 11 IAW AMM 71-00-00. NO DEFECTS NOTED AFTER FINAL ENGINE RUN. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: BLEED VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 59,374 hrs · 15,457 cycles

THE FLIGHT REJECTED TAKE-OFF DUE TO A COMPRESSOR STALL ON NR 1 ENGINE. WITNESSES SAW FLAMES COMING OUT AND A BANGING NOISE ALERTED THE CREW. REJECTED TAKE-OFF INITIATED AT 40KTS. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARD 72-92-12 FOR COMPRESSOR SURGE. REMOVED AND REPLACED THE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07, DEDICATED GENERATOR IAW AMM 73-21-08, TRANSIENT PRESSURE SENSOR UNIT IAW AMM 75-32-15, BLEED VALVE CONTROL UNIT IAW AMM 75-32-01, AND ALTITUDE SWITCH IAW AMM 75-32-07, ACCOMPLISHED AIRLFOW CONTROL TEST 3 IAW AMM 71-00-00, AND ACCELERATION, DECELERATION TEST 11 IAW AMM 71-00-00. NO DEFECTS NOTED AFTER FINAL ENGINE RUN. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 59,287 hrs · 15,431 cycles

AIRCRAFT IN BASE MAINTENANCE. R4 FLIGHT ATTENDANT INBOARD FLASHLIGHT INOPERABLE. REPLACED R4 FLIGHT ATTENDANT INBOARD FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,288 hrs · 15,431 cycles

EXIT SIGNS AT THE L1 DOOR INOPERATIVE. REPLACED THE BATTERY PACK M10798 IAW AMM 33-51-07. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,288 hrs · 15,431 cycles

EXIT SIGNS AT THE R1 DOOR INOPERATIVE. REPLACED THE BATTERY PACK M10798 IAW AMM 33-51-07. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,288 hrs · 15,431 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM 1E TO 4E INOPERATIVE. REPLACED THE BATTERY PACK M10798 IAW AMM 33-51-07. LIGHTS CHECKED GOOD.

Part: BOTTLE — DEFECTIVE (EVAC SLIDE) · airframe 59,102 hrs · 15,380 cycles

AIRCRAFT WAS GROUNDED. CREW REPORTS RIGHT HAND OVER WING SLIDE SQUID NR 2 WON'T TEST. REPLACED RIGHT HAND OVER WING SLIDE BOTTLER PER WORK CARD 25-96-03 AND AMM 25-65-02. OPERATIONS CHECK NORMAL, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 59,098 hrs · 15,378 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR LIGHT INDICATION INOPERATIVE. REPLACED THE LIGHT. OPS CHECKED OK IAW AMM 33-50-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,024 hrs · 15,362 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 3E MISSING LENS FOR EMERGENCY ESCAPE PATH LIGHTING. INSTALLED LENS EMERGENCY ESCAPE PATH PER AMM 33-51-11.

Part: SIGN — INOPERATIVE (CABIN) · airframe 58,861 hrs · 15,316 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN ABOVE THE L4 DOOR IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 58,848 hrs · 15,310 cycles

THE AIRCRAFT WAS NOT GROUNDED. ROW 29 EDF EMERGENCY LIGHT OVERHEAD MISSING LENS. INSTALLED NEW LIGHT LENS IAW AMM 33-51-00.

Part: LENS — MISSING (CABIN) · airframe 58,443 hrs · 15,207 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OVERHEAD AT SEAT 13ABC BULLNOSE HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 58,061 hrs · 15,109 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE FORWARD RIGHT OVERWING EXIT IS BROKEN. REPLACED LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — UNSECURE (EXTERIOR) · airframe 57,990 hrs · 15,091 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. SECURED THE LIGHT IAW SRM 33-51-00 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — BROKEN (EXIT SIGN) · airframe 57,528 hrs · 14,974 cycles

EMERGENCY EXIT SIGN BY THE L2 DOOR HAS A BROKEN LENS. REPLACED THE LENS IAW AMM 33-24-00. OPS CHECKED GOOD.

Part: LIGHT — NOT SEATED (CABIN) · airframe 57,500 hrs · 14,969 cycles

EXTERNAL EMERGENCY EXIT SLIDE LIGHT AT THE L4 DOOR IS INOPERATIVE. RESEATED THE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECK GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 57,307 hrs · 14,920 cycles

MERGENCY EXIT SIGN NEAR THE L2 DOOR IS DETACHED. INSTALLED THE SIGN. OPERATIONAL CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,213 hrs · 14,894 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L2 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,677 hrs · 14,769 cycles

EMERGENCY LIGHT HAS A MISSING LENS COVER. INSTALLED THE LENS. OPERATIONAL CHECK GOOD.

Part: STRAP — FRAYED (EVAC SLIDE) · airframe 56,527 hrs · 14,730 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR MOUNTED SLIDE D-RING VELCRO STRAP FRAYED. REMOVED AND REPLACED STRAP IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: SIGN — LOOSE (CABIN) · airframe 56,486 hrs · 14,720 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT L3 DOOR IS LOOSE. RE-ATTACHED EXIT SIGN IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: COVER — OUT OF ADJUST (L2 DOOR) · airframe 56,149 hrs · 14,636 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE COVER IS OUT OF ADJUSTMENT. REPOSITIONED COVER IAW AMM 52-11-02. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,123 hrs · 14,630 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN ROWS 26 THROUGH 36 ARE DIM. REMOVED AND REPLACED AFT BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: HEATER — ODOR (ZONE 200) · airframe 56,123 hrs · 14,630 cycles

AIRCRAFT WAS GROUNDED. SIDEWALL PANEL AT SEAT 17F REPORTED TO BE HOT TO TOUCH ACCOMPANIED BY A BURNING PLASTIC ODOR. REMOVED AND REPLACED THE FORWARD HATCH CENTER PANEL HEATER STRIP IAW AMM 21-45-05. SYSTEM CHECKS NORMAL.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 56,114 hrs · 14,625 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN IS DETACHED. SECURED EXIT SIGN. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — FAILED (GIRT BAR) · airframe 55,888 hrs · 14,569 cycles

GIRT BAR CIRCUIT BREAKER TRIPPED AFTER ALL CABIN DOORS WERE ARMED FOR DEPARTURE. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED L2 GIRT BAR PROXIMITY SWITCH IAW AMM 25-66-11. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,689 hrs · 14,488 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY EGRESS LIGHTING IS DIM BETWEEN ROWS 9 AND 15. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,497 hrs · 13,141 cycles

CABIN AFT DECK IS CORRODED BETWEEN FUSELAGE STATIONS 1680 AND 1740 FROM LEFT BUTTLINE 58 TO RIGHT BUTTLINE 58. REMOVED AND REPLACED AFT DECK PER SRM 51-10-02-0G.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,969 hrs · 13,010 cycles

L3 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R L3 DOOR EXTERIOR EMER LIGHT LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: ECU — FAULTY (RT ENGINE) · airframe 50,688 hrs · 12,937 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING CLIMB THROUGH 10,900 FEET A LOUD BANG ASSOCIATED WITH YAW WAS FELT. EEC OFF & RT ENG LIMITER LIGHTS ILLUMINATED. A THROTTLE SPLIT OF 3/4 KNOB WAS NOTED. R & R DECU A IAW AMM 73-21-10-004-0001-R04-4 & 73-21-10-404-010-R04-4. R & R DECU BLOWER IAW AMM 73-21-10-404-032-R04 & 73-21-10-004-022-R04. PERFORMED CHECKS IAW MCM 72-92-12. SYSTEM CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,575 hrs · 12,445 cycles

AFT FUSELAGE SKIN HAS PUNCTURE HOLE AT STATION 1668 & BETWEEN STRINGERS 29 & 28 RT. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-1R3 & FEA 17065.

Part: IDG — FAILED (LT ENGINE) · airframe 48,538 hrs · 12,437 cycles

LAX CREW REPORTED LT ENG GENERATOR ANNUNCIATOR ILLUMINATED. LT ENG GENERATOR WAS DISCONNECTED IAW THE QRH. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG INTEGRATED DRIVE GENERATOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: PLACARD — DAMAGED (CABIN) · airframe 41,385 hrs · 10,687 cycles

RIGHT AFT OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECAL FOR RIGHT AFT OVERWING EXIT MARKER. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 41,385 hrs · 10,687 cycles

AFT RIGHT GALLEY DOOR EXIT DECAL MARKER DAMAGED. REPLACED DECAL FOR AFT RIGHT GALLEY DOOR EXIT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,385 hrs · 10,687 cycles

LEFT AFT OVERWING EXIT FORWARD LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT OVERWING EXIT FORWARD LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,385 hrs · 10,687 cycles

RIGHT AFT OVERWING EXIT FORWARD FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT OVERWING EXIT FORWARD FLOOD LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,385 hrs · 10,687 cycles

LEFT FORWARD OVERWING EXIT FORWARD FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FORWARD OVERWING EXIT FORWARD FLOOD LIGHT. OPS CHECK NORMAL.

Part: PLACARD — MISSING (EXIT SIGN) · airframe 41,303 hrs · 10,655 cycles

FORWARD RIGHT EMERGENCY EXIT SIGN ARROW MISSING DECAL. REPLACED EXIT SGIN DECAL. OPS CHECK NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 41,113 hrs · 10,602 cycles

SEAT 20D SEAT-MOUNTED EMERGENCY EVACUATION LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 20D WALL-TO-SEAT CONNECTOR FOR EMERGENCY EVACUATION LIGHT. OPS CHECK NORMAL.

Part: IDG — FAILED (RT ENGINE) · airframe 40,413 hrs · 10,397 cycles

INFLIGHT, CREW REPORTED RIGHT GENERATOR FAILED, RESET PER QRH AND LOST A SECOND TIME AFTER 15 MINUTES. FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. PLACARD RIGHT ENGINE GENERATOR (IDG) INOPERATIVE PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED RIGHT INTEGRATED DRIVE GENERATOR ON 03/03/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 40,400 hrs · 10,390 cycles

CABIN RIGHT 2 DOOR INNER CHORD AT UPPER HINGE CUTOUT HAS NICK IN RADIUS. INSTALLED DOUBLER AT UPPER HINGE CUTOUT PER SRM 52-10-02-2R.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,400 hrs · 10,390 cycles

CORROSION ON DECK PLATE AT STATION 1682 AND LEFT BUTTLINE 4. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-60-51-2R 2.

Part: STRAP — CRACKED (FUSELAGE) · airframe 34,943 hrs · 9,089 cycles

STRAP CRACKED CABIN FLOOR STATION 365 LEFT BUTTLINE 24. INSTALLED DOUBLER PER SRM 53-10-51-211 AND AARD 53-30-51-1

Part: TRANSMITTER — FAULTY (HYDRAULIC SYS) · airframe 34,667 hrs · 9,022 cycles

HNL - CREW REPORTED LEFT HYDRAULIC QUANTITY EICAS MESSAGE. HYDRAULIC QUANTITY INDICATED ZERO. EMERGENCY DECLARED RETURNED HNL LANDED WITHOUT INCIDENT. REPLACED LEFT HYDRAULIC QUANTITY TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PROBE — BLOCKED (AIR TEMPERATURE) · airframe 34,637 hrs · 9,015 cycles

HNL - CREW REPORTED FLIGHT MANAGEMENT COMPUTER FAULTS AND TOTAL AIR TEMPERATURE ERROR. EMERGENCY DECLARED, RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND INSECT DEBRIS PLUGGING TOTAL AIR TEMPERATURE PROBE. REPLACED PROBE AND AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,437 hrs · 8,514 cycles

EMERGENCY LIGHTS FAILED TO FULLY ILLUMINATE FROM ROW 18 TO AFT EXIT IDENTIFIERS. REPLACED BATTERY M10801. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,437 hrs · 8,514 cycles

EMERGENCY LIGHTS FAILED TO FULLY ILLUMINATE FROM ROW 18 TO AFT EXIT IDENTIFIERS. REPLACED BATTERY PACK M10800. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,126 hrs · 8,218 cycles

MID-COACH SEAT EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR MID COACH SEAT EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 30,088 hrs · 7,947 cycles

EMERGENCY EXIT LIGHT AT OVERHEAD BIN 16ABC INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT OVERHEAD BIN 16ABC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 19C INOPERATIVE. REPLACED LAMP AT SEAT ROW 19C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT LEFT OVERWING INOPERATIVE. REPLACED LAMPS AT LEFT OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 16C INOPERATIVE. REPLACED LAMP AT SEAT ROW 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 17C INOPERATIVE. REPLACED LAMP AT SEAT ROW 17C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — DAMAGED (ZONE 200)

DFW - EMERGENCY LIGHT LEFT FORWARD OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GUARD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 18D GUARD DAMAGED. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 20C INOPERATIVE. REPLACED LAMP AT SEAT ROW 20C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 18C INOPERATIVE. REPLACED LAMP AT SEAT ROW 18C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: UNKNOWN — SMOKE (CABIN)

LAX INFLIGHT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. DEPLOYED SIX SLIDES FOR EMERGENCY EVACUATION. FLIGHT ATTENDANTS REPORTED RT NR FOUR DOOR WOULD NOT COMPLETELY OPEN. FERRIED AIRCRAFT TO TUL FOR EVALUATION AND REPAIR OF RT NR FOUR DOOR. INSPECTED DOOR RIG AND POWER ASSIST SYSTEM. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: WIRE — SHORTED (PSU)

LAX INFLIGHT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. FLIGHT ATTENDANTS REPORTED RT HAND SIDE OXYGEN MASKS DID NOT DROP. FLIGHT ATTENDANTS MANUALLY DROPPED MASKS AND OXYGEN DID NOT FLOW. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. DEPLOYED SIX SLIDES FOR EMERGENCY EVACUATION. FERRIED AIRCRAFT TO TUL FOR EVALUATION AND REPAIRS OF PASSENGER SERVICE UNITS (PSU). FOUND SHORED WIRE AFT OF MID GALLEY AND REPAIRED. AL PSUS SENT TO SHOP FOR INSPECTION AND REINSTALLED. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: ENGINE — FAILED (NR 1)

LAX INFLT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. DEPLOYED 6 SLIDES FOR EMERGENCY EVACUATION. FOUND EVIDENCE OF OIL ON NR 1 ENGINE INTERMEDIATE PRESSURE BLADES STAGE 5 AND 6 AND HIGH PRESSURE BLADE STAGE 1. ALSO FOUND OIL LEAKING ON COMPRESSOR CASE AT 6 OCLOCK POSITION. REPLACED NR 1 ENGINE ON 07AUG AT LAX. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

BOS - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — INOPERATIVE (GALLEY)

MAN T95/10MAY - AFT GALLEY NUMBER ONE OVEN CIRCUIT BREAKER POPPED PRECEDED BY ELECTRICAL FUMES AND SMOKE ALARM. CIRCUIT BREAKER TRIPPED AND COLLARED. AIRCRAFT DISPATCHED TO BOS IN ACCORDANCE WITH PDL 25 99M. REPLACED AFT GALLEY NUMBER ONE OVEN IN BOS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - LEFT NUMBER FOUR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER FOUR EXTERIOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - AFT OVERWING EMERGENCY LIGHT AT RIGHT WING INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR AFT OVERWING EMERGENCY LIGHT AT RIGHT WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

MIA - DURING OVERNIGHT MANTENANCE, FOUND SEAT 18D EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTION. RECONNECTED SEAT 18D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 24 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT PINS OF GRILL TO SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHT AT SEAT 24D INOPERATIVE. TIGHTENED AISLE EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSDUCER — FAILED (ELEVATOR)

AFTER TAKEOFF AT ALTITUDE WHEN THE AUTOPILOT WAS TURNED ON THE TRIM WOULD RUN NOSE UP IMMEDIATELY. EACH AUTOPILOT WAS TRIED WITH SAME RESULTS, RETURN TO DFW. REPLACED RIGHT ELEVATOR NEUTRAL SHIFT TRANSDUCER, OPS CHECK GOOD. PERFORMED ALL REQUIRED CHECKS. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - EMERGENCY LIGHT AT ROW 24 AND L4 DOOR INOPERATIVE. SECURED LOOSE CONNECTION AT ROW 24. RELAMPED L4 DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - FOUND EMERGENCY LIGHT AT ROW 18D INOPERATIVE. RECONNECTED CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)