N346AN

Part: EEC — UNRELIABLE (NR 1 ENGINE) · airframe 62,256 hrs · 10,288 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON INITIAL POWER APPLICATION FOR TAKE OFF, THE NUMBER ONE ENGINE WAS SUBSTANTALLY SLOWER TO SPOOL UP THAN THE #1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE MAIN ENGINE CONTROL IAW JOB CARD 12L40073001 AND LEAK CHECK WAS GOOD IAW JOBCARD 12L40072003.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,251 hrs · 10,286 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON HORIZONTAL STABILIZER CENTER BOX UPPER SKIN LEADING EDGE AT THE FORWARD SPAR AT RBL 20. REPAIRED SKIN PER EA 297436.

Part: SENSOR — UNRELIABLE (LT ENGINE) · airframe 62,142 hrs · 10,264 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT ENGINE THRUST LEVER BINDING. LAGS RIGHT ENGINE ALL THE TIME. LT ENGINE SLOW TO ACCEL AND SLOW TO DECEL. MAINTENANCE RAN THE ENGINE AND CONFIRMED THAT THE LT ENGINE FAILS THE ACCELERATION CHECK. MAINTENANCE ACCOMPLISHED FIM 73-21-00-815-803. REMOVED AND REPLACED CIT SENSOR IAW AMM 73-21-02. ALL OPS CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (THRUST LEVER) · airframe 62,121 hrs · 10,259 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT ENGINE THRUST LEVER LINKAGE BINDING. NOT AUTO THRUST. AUTO THRUST NORMAL. MAINTENANCE ACCOMPLISHED FIM TASK 76-11-00 FIG 105A. ACCOMPLISHED THRUST LEVER LOAD TEST IAW AMM 76-11-00-501. NO PROBLEMS FOUND AT THIS TIME. NO BINDING NOTED.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 61,558 hrs · 10,143 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE PRESSURE IS LOW. REMOVED AND REPLACED L- 1 DOOR SLIDE IAW AMM 25-66-01.

Part: SEALANT — UNBONDED (FUEL CELL) · airframe 61,102 hrs · 10,043 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS R/H INBOARD WING FUEL TANK HAS RUNNING LEAK OUT OF DRY BAY. ISOLATED 1 LEAK AREA DUE TO FAILED SEALANT AT RIB 9, FROM STRINGER LI6 TO L17, 2 INCHES ABOVE LOWER SKIN VIA BACK BLOW IAW AMM 28-11-00-796-111. REMOVED BAD SEALANT, CLEANED AND APPLIED NEW SEALANT IAW AMM 28-11-00-308-013. LEAK CHECKS GOOD, NO LEAKS NOTED.

Part: LIGHT — BROKEN (SEAT 5A) · airframe 60,401 hrs · 9,889 cycles

DURING AN INSPECTION, FOUND THE SEAT MOUNT EMERGENCY LIGHT TO BE BROKEN AT SEAT 5A. MAINTENANCE CONNECTED THE LIGHT ASSEMBLY. PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: FLASHLIGHT ASSY — MISSING (CABIN) · airframe 59,567 hrs · 9,712 cycles

FLASHLIGHT ASSEMBLY MISSING FROM UNDER AFT FACING MID GALLEY, RIGHT SIDE FLIGHT ATTENDANT SEAT. REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 25-60-00. OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 59,214 hrs · 9,642 cycles

EMERGENCY LIGHTS AT SEATS 39H, 40H, AND 41H WERE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR LOOSE AT ROW 38HJ. CONNECTED THE CONNECTOR AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,040 hrs · 9,604 cycles

JUMP SEAT AT M2 LAVATORY, THE FLASHLIGHT WAS KNOCKED LOOSE, SEAL BROKEN. REPLACED FLASHLIGHT BATTERY AND TAMPER SEAL AT M2 JUMPSEAT POSITION. OPERATIONS CHECK NORMAL. OK FOR SERVICE PER AMM 25-64-01.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 58,159 hrs · 9,439 cycles

MID GALLEY RIGHT FLIGHT ATTENDANT SEAT FLASHLIGHT DOES NOT ILLUMINATE GREEN WITH PRESS TO TEST BUTTON. REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,305 hrs · 9,277 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT OUTBOARD FLAP LOWER SKIN HAS DELAMINATED AREA 28 INCHES FROM TRAILING EDGE AND 16 INCHES FROM INBOARD EDGE. DELAMINATION MEASURES 3 X 4 , IN ADDITION TO 6 INCHES FROM FORWARD EDGE AND 23 INCH FROM INBOARD EDGE. THESE ARE OUT OF LIMITS PER SRM 57-53-01-1A TABLE 1. FLAP REPLACED ON CARD 27-97-11.

Part: INDICATOR — LEAKING (HYD FILTER) · airframe 57,298 hrs · 9,276 cycles

THE AIRCRAFT LOST LEFT HYDRAULIC PRESSURE, WITH LEFT HYDRAULIC SYSTEM PRESSURE. EICAS MESSAGE AND HYDRAULIC QTY 0.01 RF. HYD PRESS 120 INDICATIONS. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED DPI ON HYD FILTER MODULE IAW AMM 29-11-17.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 57,207 hrs · 9,259 cycles

CAPTAIN`S SLIDING WINDOW VERY DIFFICULT TO LATCH AND UNLATCH. ADJUSTED THE WINDOW IAW WORK CARD 56-95-21. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,207 hrs · 9,259 cycles

LEFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER IAW AMM 33-51-07.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,207 hrs · 9,259 cycles

LEFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER, BATTERY PACK, IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,207 hrs · 9,259 cycles

LEFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LIGHT BATTERY CHARGER AND BATTERY PACK IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,207 hrs · 9,259 cycles

LEFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (ANTI-SKID SYS) · airframe 57,106 hrs · 9,240 cycles

FOLLOWING GEAR EXTENSION, ANTI-SKID MESSAGE ON EICAS, WENT AROUND. NO MESSAGE ON NEXT GEAR EXTENSION UNTILL 1000 AFL DISSAPPEARED BY 500 FEET AFL. FOUND THE ANTI-SKID CONTROL BOX WITH TWO FAULTS. BOX 3-7 AND NR 3 TRANSDUCER. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IAW AMM 32-42-01. REMOVED AND REPLACED THE NR 3 TRANSDUCER IAW AMM 32-42-06. OPS CHECKED GOOD.

Part: TRANSDUCER — FAULTY (ANTI-SKID SYS) · airframe 57,106 hrs · 9,240 cycles

FOLLOWING GEAR EXTENSION, AN ANTI-SKID MESSAGE ILLUMINATED. WENT AROUND. NO MESSAGE ON NEXT GEAR EXTENSION UNTILL 1000 AGL DISAPPEARED BY 500 FEET AGL. FOUND ANTI-SKID CONTROL BOX WITH TWO FAULTS, BOX 3-7 AND NR 3 TRANSDUCER. REMOVED AND REPLACED THE ANTI-SKID CONTROL UNIT IAW AMM 32-42-01. AND REMOVED AND REPLACED THE NR 3 TRANSDUCER IAW AMM 32-42-06. OPERATIONS CHECKED GOOD.

Part: CHARGER — NO TEST (ZONE 200) · airframe 56,508 hrs · 9,122 cycles

AIRCRAFT WAS GROUNDED. OFF-WING RIGHT SQUIB TEST 1 INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY (AALA201710239001) AT M962 PER AMM 25-65-17. ACCOMPLISHED SQUIB TEST PER AMM 26-21-04. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCOLORED (ZONE 200) · airframe 56,508 hrs · 9,122 cycles

AIRCRAFT WAS GROUNDED. OFF-WING RIGHT SQUIB TEST 1 INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY (AALA20171021003) AND BATTERY ASSEMBLY AT M962 PER AMM 25-65-17. ACCOMPLISHED SQUIB TEST PER AMM 26-21-04. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 55,483 hrs · 8,939 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT FORWARD GALLEY MID PARTITION RIGHT JUMPSEAT IS MISSING. REPLACED FLASHLIGHT. OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 55,483 hrs · 8,939 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT FORWARD GALLEY MID PARTITION LEFT JUMPSEAT IS MISSING. REPLACED THE FLASHLIGHT. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 55,291 hrs · 8,898 cycles

EMERGENCY EXIT LIGHTS AT ROWS 35HJ THROUGH 41HJ ARE INOPERATIVE. CONNECTED A LOOSE CONNECTOR AT ROW 35HJ IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 54,924 hrs · 8,839 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 7A HAS BROKEN WIRES. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 54,924 hrs · 8,839 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN ON THE RIGHT BEHIND FIRST CLASS IS LOOSE. RESECURED SIGN IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — MISSING (SEAT 7A) · airframe 54,598 hrs · 8,780 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7A IS MISSING. REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FALSE INDICATION · airframe 53,812 hrs · 8,621 cycles

ON APPROACH, A TRAILING EDGE FLAP DISAGREE MESSAGE WAS DISPLAYED WHEN FLAP 5 WAS SELECTED AND FLAP DID NOT PASS 1. EMERGENCY DECLARED. EXTENDED FLAPS ELECTRICALLY TO 20 AND LANDED UNEVENTFUL. ACCOMPLISHED FSEU BITE CHECK IAW TASK CARD 27-51/809 AND FSPM M839 CHECK. INSPECTED FLAPS SYSTEM WITH NO DISCREPANCIES NOTED. OPERATED FLAP FULL TRAVEL AND STEP BY STEP SEVERAL TIMES IAW AMM 27-51-00/201. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 52,165 hrs · 8,341 cycles

FLIGHT DECK EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECKED NORMAL.

Part: DUCT — BURST (RT ENGINE) · airframe 51,999 hrs · 8,315 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACFT OVERWEIGHT. DURING CLIMB, CREW OBSERVED THE RT ENGINE OVERHEAT LIGHT ILLUMINATED. QRH FOLLOWED AND LIGHT EXTINGUISHED AT APPROXIMATELY 25 PERCENT N2. MAINTENANCE FOUND RT ENGINE HIGH PRESSURE TURBINE COOLING DUCT BURST. R & R DUCT IAW AMM 70-00-00. ACCOMPLISHED ENGINE RUN WITH NO LEAKS NOTED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,613 hrs · 7,893 cycles

EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROW 23H - 28H. R & R M732 BATTERY CHARGER IAW MM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,641 hrs · 7,735 cycles

SEAT 33H TO 41H, SEAT & CEILING EMER LIGHTS INOPERATIVE. R & R CHARGER M734 IAW 33-51-07. ALL CHECKED NORMAL. SEE AALA20150722010 FOR ADDITIONAL PART INFORMATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,641 hrs · 7,735 cycles

SEAT 33H TO 41H, SEAT & CEILING EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW 33-51-07. ALL CHECKED NORMAL. SEE AALA20150722002 FOR ADDITIONAL PART INFORMATION.

Part: SHIM — MIGRATED (RT WING) · airframe 47,648 hrs · 7,589 cycles

RIGHT WING AFT PITCH LOAD FITTING HAS PROTRUDING SHIM. R & R SHIM UNDER RT WING AFT PITCH LOAD FITTING IAW EA 57-039334.

Part: TRUNNION — GOUGED (LT MLG) · airframe 47,648 hrs · 7,589 cycles

LEFT MLG SIDE STRUT TRUNNION FITTING GOUGED AT LOWER WING WW AREA. COMPLIED WITH EA 767-5754-39-A2171.

Part: TRUNNION — GOUGED (RT MLG) · airframe 47,648 hrs · 7,589 cycles

RIGHT MLG SIDE STRUT TRUNNION FITTING GOUGED AT LOWER WING WW AREA. COMPLIED WITH EA 767-5754-39-A2170.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

NUMBER 8 SEAT TRACK AT BS 353 CORRODED UNDER & AROUND GALLEY TIE DOWN FITTING. R & R SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

SEAT TRACK 6 CROWN IS CORRODED AT STATION 347 & BL 20R. REPLACED SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1230-1432) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

CABIN SEAT TRACK AT RBL 88.5 BETWEEN FS 1230 & 1432 IS CORRODED. R & R SEAT TRACK IAW SRM 51-40-02.

Part: MOUNT — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

NUMBER 2 ENG, AFT ENGINE MOUNT, OTBD FLANGE HAS RUST BUILD UP. R & R AFT MOUNT IAW AMM 71-21-02-024.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

149AL PANEL FWD TEE IS CORRODED. R & R TEE ON PANEL 149AL IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

UPPER SURFACE OF FLOORBEAM AT FS 325 IS CORRODED AT RBL 54. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,648 hrs · 7,589 cycles

UPPER SURFACE OF FLOORBEAM AT FS 325 IS CORRODED AT LBL 24. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-4 FIG 201.

Part: CIRCUIT CARD — FAILED (OVERHEAT WARNING) · airframe 47,478 hrs · 7,561 cycles

AIR INTERRUPT, DIVERTED & AN EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE CREW REPORTED LEFT BLEED DUCT LEAK MSG RECEIVED & LIGHT ILLUMINATED. ACCOMPLISHED FIM 26-18-00-815-804 DURING WHICH M691 CARD FAILED TEST. R & R CARD. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,229 hrs · 7,522 cycles

RIGHT WING EXTERNAL EMER LIGHT INOPERATIVE. R & R LAMPED IN LIGHT. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 47,229 hrs · 7,522 cycles

RIGHT WING LIGHT AFT OF FIRST FUSELAGE LIGHT INOPERATIVE. R & R LAMPED IN LIGHT. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,229 hrs · 7,522 cycles

LEFT WING EXTERNAL EMER LIGHT INOPERATIVE. R & R LAMPED IN LIGHT. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,229 hrs · 7,522 cycles

L1 EXTERNAL EMER LIGHT INOPERATIVE. R & R LAMPED IN LIGHT. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,229 hrs · 7,522 cycles

R4 DOOR EXTERNAL EMER LIGHT INOPERATIVE. R & R LAMPED IN LIGHT. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,229 hrs · 7,522 cycles

L1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R EMER LIGHT LAMP. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-03. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,765 hrs · 7,444 cycles

LEFT SIDE FUSELAGE EXTERIOR EMER LIGHT AT FUSELAGE STATION 1420 INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,765 hrs · 7,444 cycles

RIGHT SIDE EMER LIGHT AT FUSELAGE STATION 1320 INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,765 hrs · 7,444 cycles

EXTERIOR EMER LIGHT AT FUSELAGE STATION 680 INOPERATIVE. R & R LAMP EMER LIGHT IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,765 hrs · 7,444 cycles

R4 DOOR EXTERNAL EMER LIGHT AT FUSELAGE 1701 INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: DETECTOR — DEFECTIVE (MLG WW) · airframe 46,700 hrs · 7,435 cycles

DURING CRUISE, WHEEL WELL FIRE WARNING INDICATION ILLUMINATED. DIVERTED, EMERGENCY DECLARED, LANDING UNEVENTFUL. ACCOMPLISHED FIM 26-17-00-815 AND RESISTANCE CHECK OF LOOPS PER 26-17-11 WITH NO FAULTS FOUND. REMOVED AND REPLACED DETECTOR LOOPS AND PERFORMED BITE CHECK IAW AMM 26-17-01. SYSTEM CHECKED NORMAL.

Part: CIRCUIT CARD — DEFECTIVE (OVERHEAT SYS) · airframe 46,642 hrs · 7,425 cycles

DURING CRUISE RT MLG WW OVERHEAT INDICATION ILLUMINATED. AIR INTERRUPTION, DIVERTED, EMERGENCY DECLARED & LANDING UNEVENTFUL. INDICATION ON WHILE ON GROUND. R & R WW OVERHEAT DETECTION CARD M691 IAW AMM 26-10-01. PERFORMED GROUND CHECK. SYS CHECKED NORMAL.

Part: TARGET — FAULTY (LE SLAT) · airframe 42,182 hrs · 6,706 cycles

LAX CREW REPORTED LE SLAT ASYMMETRY LIGHT ILLUMINATED & STAYED ON FOR REMAINDER OF FLIGHT. FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND TARGET 282 ON PROXIMITY SWITCH ELECTRONIC UNIT FAULTING. REPLACED NR 1 SLAT INBD INTERMEDIATE TARGET. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED)

Part: ACTUATOR — DAMAGED (LT SPOILER) · airframe 41,584 hrs · 6,613 cycles

LEFT WING SPOILER KNOCK DOWN ACTUATOR SQUIB PINS BENT. REPLACED LT WING SPOILER KNOCK DOWN ACTUATOR ASSY.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 39,433 hrs · 6,289 cycles

LHR - INFLIGHT CDG-DFEW. CREW REPORTED CABIN PRESSURE ONE CONTROLLER EICAS MESSAGE WITH NUMBER TWO CONTROLLER ON PLACARD. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,997 hrs · 6,072 cycles

RIGHT AFT LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,997 hrs · 6,072 cycles

LEFT AFT LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,093 hrs · 5,746 cycles

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

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 36,093 hrs · 5,746 cycles

EMERGENCY LIGHT PANEL AT RIGHT NUMBER 4 DOOR HAS LIGHT OUT. REPLACED LAMP FOR EMERGENCY LIGHT PANEL AT RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,613 hrs · 5,672 cycles

THE 23H TO 27H EMERGENCY LIGHTS SEAT MOUNTED INOPERATIVE. CHARGED PACK, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,760 hrs · 4,555 cycles

RIGHT EXTERIOR EMERGENCY LIGHT CLOSEST TO AFT CARGO DOOR INOPERATIVE. REPLACED LAMP AT RIGHT AFT SLIDE LIGHT. OPS CHECKED NORMAL.

Part: SIGN — UNSERVICEABLE (CABIN) · airframe 28,760 hrs · 4,555 cycles

LEFT AFT EMERGENCY OVERWING EXIT IDENTIFIER UNREADABLE. REMOVED AND REPLACED LT AFT OVERWING EXIT IDENTIFIER. OPS CHECKED NORMAL.

Part: PLACARD — UNSERVICEABLE (CABIN) · airframe 28,760 hrs · 4,555 cycles

LEFT NUMBER 4 DOOR EMERGENCY EXIT IDENTIFIER UNREADABLE. REMOVED AND REPLACED LEFT NUMBER 4 DOOR EXIT IDENTIFIER. OPS CHECKED NORMAL.

Part: LENS — DAMAGED (EXTERIOR)

DFW - LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS FOR LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP FOR LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - RIGHT EXTERIOR EMERGENCY LIGHTS JUST FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR RIGHT SIDE EXTERIOR EMERGENCY LIGHTS JUST FORWARD OF AFT CARGO.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,513 hrs

SFO - EXTERIOR EMERGENCY LIGHT AT AFT RIGHT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT RIGHT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,513 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD SEATS 37HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEATS 37HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,500 hrs

JFK - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,500 hrs

JFK - EMERGENCY LIGHT AT LEFT FORWARD OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M732 FOR EMERGENCY LIGHT AT LEFT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,982 hrs

ORD - EMERGENCY LIGHTS AT SEAT ROWS 35 TO 41 INOPERATIVE. REPLACED CONNECTOR AT SEAT ROW 36AB FOR EMERGENCY LIGHTS AT SEAT ROWS 35 TO 41. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT CEILING LEFT SIDE FIRST CLASS INOPERATIVE. RELAMPED EMERGENCY LIGHT AT CEILING LEFT SIDE FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

LAX - EMERGENCY LIGHTS AT SEATS 24B TO 31B INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 31A FOR EMERGENCY LIGHTS AT SEATS 24B TO 31B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO- EMERGENCY LIGHT AT LEFT FORWARD DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 23H TO 31H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 23H TO 31H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — LOOSE (CABIN)

MAN - EMERGENCY EXIT SIGN COVER AT LEFT NUMBER ONE AFT EXIT SIGN FELL OFF. RESECURED EMERGENCY EXIT SIGN COVER AT LEFT NUMBER ONE AFT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIFE VEST — MISSING (CABIN)

SFO - EMERGENCY LIFE VEST PACKAGE IN FIRST CLASS MISSING ONE LIFE VEST. REPLACED ENTIRE FIRST CLASS EMERGENCY LIFE VEST PACKAGE KIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AFW - EMERGENCY LIGHTS L183 AND L187 INOPERATIVE. REPLACED THREE EACH BATTERY PACKS FOR EMERGENCY LIGHTS AT L183 AND L187. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — SMOKE (GALLEY)

INFLIGHT, OVEN NR 6 IN COACH GALLEY WAS SMOKING FROM BEHIND OVEN. FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL. CLEANED NUMBER SIX OVEN AND RAN NUMBER 6 AND NUMBER 5 OVENS AND AFT GALLEY RIGHT CHILLER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, RIGHT AFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. TIGHTENED RIGHT AFT EMERGENCY EXIT DOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)