N183AN

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,721 hrs · 18,304 cycles

L1 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY DISCHARGED. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY IAW AMM 25-64-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,721 hrs · 18,304 cycles

THE L4 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY WAS DISCHARGED. REPLACED THE BATTERY IAW AMM 25-64-00.

Part: FLASHLIGHT — INOPERATIVE (ZONE 800 - DOORS) · airframe 69,504 hrs · 18,237 cycles

FLASHLIGHT BATTERY AT THE FLIGHT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 68,909 hrs · 18,073 cycles

THE RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 68,909 hrs · 18,073 cycles

THE LEFT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.

Part: HANDLE — STUCK (L4 DOOR) · airframe 68,712 hrs · 18,025 cycles

L4 DOOR EXTERAL HANDLE, IMPROPERLY STOWED LEAVING THE DOOR STUCK OPEN. RELEASED THE DOOR, CLOSED DOOR, OPS NORMAL.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,519 hrs · 17,984 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT DECK PLATE BETWEEN STA 1709 TO STA 1720. REPAIRED DECK PLATE PER SRM 53-60-51-2R-18.

Part: FLOOR SUPPORT — CORRODED (BS 1620-1640) · airframe 68,519 hrs · 17,984 cycles

CORROSION ON TOP OF THE FLOOR SUPPORT, BS 1620 TO 1640, RBL 20. REPLACED THE FLOOR SUPPORT IAW 51-00-05.

Part: SLIDE — NO TEST (RT OVERWING) · airframe 68,519 hrs · 17,984 cycles

DURING A TEST, RIGHT OVERWING EXIT SLIDE DEPLOYED BUT FAILED TO INFLATE ENTIRELY. THE SLIDE TOOK AN ADDITIONAL 30 SECONDS TO FULLY DEPLOY. SLIDE COMPLETELY DEFLATED 30 MINUTES AFTER DEPLOYMENT. REPLACED INFLATION BOTTLE AND SLIDE.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 68,318 hrs · 17,931 cycles

FIRST OFFICER'S SLIDING WINDOW DIFFICULT TO OPEN & CLOSE, THE HANDLEWAS BINDING. ADJUSTED FIRST OFFICER'S NR 2 WINDOW IAW MM 56-11-02, AND SECURED THE HANDLE MOUNT. OPS CHECKED NORMAL.

Part: IDG — FAILED (RT ENGINE) · airframe 68,242 hrs · 17,912 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, RIGHT HAND ENGINE GENERATOR FAILED AND ACCOUNT ELECTRICAL ISSUE. EMERGENCY DECLARED, AIRCRAFT LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT RIGHT ENGINE INTEGRATED DRIVE GENERATOR PER FIM 24-20-00-810-802 AND REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR PER AMM 24-11-01, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: TIRE — SEPARATED (MLG) · airframe 65,248 hrs · 17,132 cycles

DURING POST FLIGHT WALKAROUND, FOUND THE NR 3 MAIN LANDING GEAR TIRE TREAD SEPERATED. REMOVED AND REPLACED WHEEL ASSY IAW AMM 32-45-01. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SWITCH — DIRTY (R2 GIRT BAR) · airframe 65,179 hrs · 17,116 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE ARMED LIGHT IS ON WITH THE DOOR DISARMED. CLEANED BOTH THE GIRT BAR MICRO SWITCHES AND TARGET. OPERATIONAL CHECKED GOOD IAW AMM 25-66-01.

Part: TARGET — DIRTY (R2 GIRT BAR) · airframe 65,179 hrs · 17,116 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE ARMED LIGHT IS ON WITH THE DOOR DISARMED. CLEANED BOTH GIRT BAR MICRO SWITCHES AND TARGET. OPERATIONAL CHECKED GOOD IAW AMM 25-66-01.

Part: SLIDER — DIRTY (GIRT BAR) · airframe 64,561 hrs · 16,948 cycles

AIRCRAFT WAS NOT GROUNDED. R2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR SHOWS ARMED WHEN PHYSICALLY DISARMED. CLEANED GIRT BAR SLIDERS. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 64,544 hrs · 16,944 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT R4 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — LOOSE (EXIT SIGN) · airframe 64,544 hrs · 16,944 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT L2 DOOR HAS A LOOSE LENS COVER. SECURED LENS COVER IAW AMM 33-24-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — NOT SEATED (SEAT 35D) · airframe 64,536 hrs · 16,942 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 35D IS INOPERATIVE. SEATED THE LIGHT ASSEMBLY IAW AMM 33-51-11. OPERATIONAL CHECKED GOOD.

Part: RESERVOIR — LOW PRESSURE (L2 DOOR) · airframe 64,536 hrs · 16,942 cycles

L2 DOOR EMERGENCY POWER RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED RESERVOIR IAW AMM 52-11-30. OPERATIONAL CHECKED GOOD.

Part: FUSE — FAULTY (ZONE 700) · airframe 64,410 hrs · 16,909 cycles

AIRCRAFT WAS GROUNDED. ON APPROACH, MAIN LANDING GEAR DOOR INDICATIONS ON EICAS. FOUND RIGHT MAIN GEAR DOOR DOWN AND RED GEAR DOOR UNSAFE LIGHT ON IN THE WHEEL WELL. REMOVED AND REPLACED MAIN LANDING GEAR EXTENSION HYDRAULIC FLOW FUSE IAW AMM 32-32-19-002-026. OPERATIONAL CHECK GOOD.

Part: SEQUENCE VALVE — FAULTY (RT MLG) · airframe 64,364 hrs · 16,900 cycles

AIRCRAFT WAS GROUNDED. ON FINAL APPROACH AFTER GEAR EXTENSION, GEAR DOORS EICAS MESSAGE AND GEAR DOOR LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT DOWNLOCK OPERATED DOOR SEQUENCE VALVE FOR THE RIGHT MAIN LANDING GEAR IAW AMM 32-32-07. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,491 hrs · 16,672 cycles

AIRCRAFT WAS NOT GROUNDED. 1ST CLASS SEAT MOUNTED EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY AT M10798 IAW AMM 33-51-11. OPERATIONAL CHECK NORMAL.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 63,409 hrs · 16,652 cycles

AIRCRAFT WAS GROUNDED. SJU, AIR INTERRUPT, MIA-UVF. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CRUISE NR 1 ENGINE INDICATED LOW FUEL FLOW AND HIGH EPR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER AND EEC UNIT AND ACCOMPLISHED GROUND OPERATIONAL TEST IAW AMM 77-11-01 AND AMM 73-21-07. SYSTEM CHECKS NORMAL. SEE ALSO AALA20161025003.

Part: TRANSMITTER — FAULTY (NR 1 ENGINE) · airframe 63,409 hrs · 16,652 cycles

AIRCRAFT WAS GROUNDED. SJU, AIR INTERRUPT, MIA-UVF. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CRUISE NR 1 ENGINE INDICATED LOW FUEL FLOW AND HIGH EPR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER AND EEC UNIT AND ACCOMPLISHED GROUND OPERATIONAL TEST IAW AMM 77-11-01 AND AMM 73-21-07. SYSTEM CHECKS NORMAL. SEE ALSO AALA20161025004.

Part: FMC — FAULTY (ZONE 100) · airframe 63,179 hrs · 16,593 cycles

ON CLIMB OUT CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.

Part: FMC — FAULTY (ZONE 100) · airframe 63,179 hrs · 16,593 cycles

DURING CLIMB OUT, CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL, AND THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.

Part: ADC — FAULTY (COCKPIT) · airframe 63,179 hrs · 16,593 cycles

DURING CLIMB OUT CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 62,677 hrs · 16,418 cycles

AIRCRAFT WAS GNDED, AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL, ACAFT NOT OVERWEIGHT. DURING CRUISE, FIRST OFFICERS WINDOW CRACKED & WHOWED ELEC ARCING. T & R FIRST OFFICER, STRINGER R1 WINDOW AS IAW AMM 56-11-0. SYS CHECKED NORMAL.

Part: BATTERY — WEAK (CABIN) · airframe 62,007 hrs · 16,155 cycles

AIRCRAFT WAS NOT GNDED. DURING EMER LIGHT TEST, FOUND EMER AISLE LIGHT DIM AT ROWS 26 - 36. R & R EMER LIGHT BATTERY, BETWEEN AFT LAVATORY CEILING IAW MM 33-51-11.

Part: GOVERNOR — MALFUNCTIONED (FUEL FLOW) · airframe 61,271 hrs · 15,893 cycles

ON CLIMB OUT, RT ENGINE INDICATION FLUCTUATION AT ALL POWER SETTINGS. THE FLIGHT DECLARED AN EMERGENCY & RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R FUEL FLOW GOVERNOR IAW MCM 73-94-01. OPERATIONS & LEAK CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,151 hrs · 15,849 cycles

EMERGENCY LIGHT AT 28 DEF INOPERATIVE. FOUND LOOSE CONNECTOR UNDER SEAT 28 DEF. RESET CONNECTOR & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (RT ENGINE) · airframe 60,789 hrs · 15,741 cycles

DURING CLIMB RT ENG BLEED OFF ILLUMINATED. DIVERTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. R & R RT ENGINE PRESSURE REGULATING & SOV IAW MM 36-11-09. PERFORMED OPERATIONAL CHECKS. SYS CHECKED NORMAL.

Part: CIRCUIT CARD — FAULTY (ENGINE SPEED) · airframe 60,787 hrs · 15,740 cycles

DURING CLIMB, THE RT ENG BLEED OFF EICAS MSG ILLUMINATED. DIVERTED AND MX CHECK PRESOV & RFCC LINE FOR SECURITY IAW FIM 36-10-00 WITH NO LEAKS FOUND. R & R RT ENGINE SPEED CARD IAW FIM 36-10-00 & MM 77-12-04. ACCOMPLISHED CHECK OF LT & RT AIR DISTRIBUTION SYS IAW 36-11-00-710-801. SYS CHECKED NORMAL.

Part: SHUTOFF VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 60,728 hrs · 15,723 cycles

AIR INTERRUPT, RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. THE LT ENG BLEED OFF LIGHT ILLUMINATED, BLEED AIR WOULD NOT RESET & ACFT WOULD NOT HOLD PRESSURIZATION ON SINGLE PACK OPERATION. REPLACED THE LT ENG PRESS REGULATING & PRSOV IAW AMM 36-11-09. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SKIN — CORRODED (RT WING) · airframe 60,685 hrs · 15,711 cycles

OVERWING FILL PORT FAILED BONDING CHECK, FOUND CORROSION BETWEEN PORT FLANGE & WING FAYING SURFACE AS FAULT. REPAIRED IAW EA 252057.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 60,685 hrs · 15,711 cycles

NUMBER 1 ENG PYLON CRITICAL FASTENER HOLE NR 9 SHOWS CRACK INDICATION IAW NDT INSPECTION. REPAIRED HOLE IAW EA 251628.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,685 hrs · 15,711 cycles

LEFT WING SKIN CORRODED AT OVERWING FUEL FILL PORT FAYING SURFACE. REPAIRED SKIN IAW SRM 57-20-01-2R & AMM 28-11-04.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 60,685 hrs · 15,711 cycles

DECK SUPPORT CLIP AT RBL 16.12 & FS 1520 CRACKED. R & R CLIP IAW AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 60,685 hrs · 15,711 cycles

CORROSION ON RT TRANSITION PANEL BETWEEN STATION 1440 - 1640. REPLACED TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,685 hrs · 15,711 cycles

AFT CARGO COMPARTMENT RT TRANSITION PANEL IS CORRODED BETWEEN FS 1380 & 1440. R & R TRANSITION PANEL SECTION IAW AARD 51-00-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,685 hrs · 15,711 cycles

AFT CARGO CEILING AREA, STATION 1320 - 1340, UPPER ANGLE OF CTR WEB IS CRACKED AROUND AFT NUTPLATE LOCATION. REPLACED ANGLE IAW AARD 51-00-05-1.

Part: RIVET — SHEARED (FUSELAGE) · airframe 60,685 hrs · 15,711 cycles

RIVETS SHEARED FOR FLOORBEAM STABILIZER STRAP AT FS 377.7 & LBL 45. ACCOMPLISHED STRAP PLATE & FILLER REPAIR IAW SRM 53-10-51-2R-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,685 hrs · 15,711 cycles

CORROSION ON RT TRANSITION PANEL, FWD OF AFT CARGO DOOR STATION 1320 - 1380. REPLACED RT TRANSITION PANEL FROM STATION 1310 - 1380 IAW AARD 51-00-05.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,685 hrs · 15,711 cycles

SCATTERED HEAVY CORROSION ON AFT DECK PLATE AT 1715 BETWEEN LBL 51 & RBL 50. R & R AFT DECK PLATE IAW SRM 51-20-01, AARD 51-00-05-1 & DWG 146N5300.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 3 · airframe 55,783 hrs · 14,535 cycles

LT INBD MAIN FLAP UPPER SURFACE CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-57-033281.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,115 hrs · 14,367 cycles

MULTIPLE EMERGENCY AISLE LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY AISLE LIGHT BATTERY PACK ABOVE FIRST CLASS LAVATORY. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 55,115 hrs · 14,367 cycles

MULTIPLE EMERGENCY EXIT SEAT LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK ABOVE 9DEF. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,115 hrs · 14,367 cycles

MULTIPLE EMERGENCY EXIT SEAT LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK ABOVE 19DEF. OPERATIONS CHECKED NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,182 hrs · 13,177 cycles

ANGLE CRACKED AT STATION 680 LEFT BUTTLINE 46. REPLACED ANGLE PER AARD 51-00-05-1 REPAIR 1.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 50,182 hrs · 13,177 cycles

AFT ATTACH ANGLE ON INTERCOSTAL AT STATION 680 LEFT BUTTLINE 46 DAMAGED. INSTALLED WEB ATTACH ANGLE PER AARD 51-00-05-1 REPAIR 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,182 hrs · 13,177 cycles

AFT CARGO, BELOW THE CABIN FLOOR BETWEEN STATIONS 1580 TO 1600, THE INTERCOSTAL AT BUTTLINE 0 TOP L-ANGLE IS CRACKED AT THE AFT NUT PLATE. INSTALLED NEW L-ANGLE PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,182 hrs · 13,177 cycles

CORROSION ON LEFT GUTTERBOX FLOOR SUPPORT AT STATION 1677 AND LEFT BUTTLINE 53. INSTALLED NEW LEFT AFT GUTTERBOX PER AARD 51-00-05-1, REPAIR 1, AND SRM 51-10-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,182 hrs · 13,177 cycles

AFT FLOOR STRUCTURE FROM STATIONS 1640 TO 1672 AT RIGHT BUTTLINE 55 HAS CORROSION AT FASTENER HOLES. INSTALLED NEW AFT GUTTER SUPPORTS AT RIGHT NUMBER 4 DOOR PER AARD 51-00-05-1.

Part: SKIN — GOUGED (FUSELAGE) · airframe 50,182 hrs · 13,177 cycles

SHARP EDGES ON BLENDED GOUGE AT STATION 648 BETWEEN STRINGERS 1 AND 2 RIGHT. INSTALLED SKIN DOUBLER PER EA B757-53-025376.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,430 hrs · 12,985 cycles

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

Part: SKIN — DENTED (FUSELAGE) · airframe 47,391 hrs · 12,422 cycles

DENT IN FUSELAGE SKIN BETWEEN STATIONS 720 TO 740. REPAIRED DENT PER SRM 53-00-01-2R AND EA B757-53-020175.

Part: FMC — MALFUNCTIONED (NR 1) · airframe 45,357 hrs · 11,918 cycles

SFO - CREW REPORTED BOTH FLIGHT MANAGEMENT COMPUTERS DISPLAYED "STANDBY ONE" AND ALL NAV FUNCTIONS (INPUTS) WERE LOCKED OUT. BOTH ROUTE 1 AND 2 UNUSABLE. FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. REPLACED THE NUMBER 1 FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLACARD — PEELING (CABIN) · airframe 42,131 hrs · 11,132 cycles

AFT LEFT OVERWING HATCH EXIT MARKER STICKER PEELING. REMOVED AND REPLACED LEFT AFT OVERWING HATCH EXIT MARKER STICKER. OPS CHECKED GOOD.

Part: SHROUD — MISSING (CABIN) · airframe 39,711 hrs · 10,570 cycles

EMERGENCY LIGHT AT SEAT 23D MISSING SHROUD. REPLACED SHROUD AT SEAT 23D.

Part: WIRE — LOOSE (CABIN) · airframe 39,652 hrs · 10,557 cycles

EMERGENCY LIGHT AT SEAT ROW 1EF INOPERATIVE. SECURED EMERGENCY LIGHT WIRING AT SEAT 1EF.

Part: PLACARD — DAMAGED (OVERWING EXIT)

DFW - LEFT FORWARD EMERGENCY OVERWING EXIT SIGN DECAL PEELED BACK. INSTALLED NEW PLACARD AT LEFT FORWARD EMERGENCY OVERWING EXIT.

Part: PLACARD — DAMAGED (CABIN)

DFW - RIGHT AFT EMERGENCY OVERWING EXIT SIGN DECAL PEELED BACK. INSTALLED NEW PLACARD AT RIGHT AFT EMERGENCY OVERWING EXIT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

ORD - EXTERIOR EMERGENCY LIGHT AT RIGHT MID PASSENGER ENTRANCE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT MID PASSENGER ENTRANCE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

LAS - EMERGENCY LIGHT AT AFT GALLEY LEFT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

MIA EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - EMERGENCY LIGHTS AT SEAT 36D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 36D FOR EMERGENCY LIGHTS AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — OVERTEMP (LEFT)

PHL - INFLIGHT LEFT ENGINE FAILURE ON TAKEOFF. ENGINE HAD LARGE VIBRATION FOLLOWED BY WHAT FELT LIKE SEIZURE. ENGINE GENERATOR TEMPERATURE 975C. REPORTS OF FIRE AND SMOKE BY AIR TRAFFIC CONTROL, OTHER AIRCRAFT AND PASSENGERS. NO FIRE WARNING. ENGINE SHUTDOWN PER QRH PROCEDURE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (LT ENGINE)

MIA - INFLIGHT LEFT HAND ENGINE BEGAN HIGH FREQUENCY VIBRATION AND OVER TEMPERATURE AT 230 IN HEAVY PRECIPITATION. POWER WAS REDUCED TO IDLE AND DESCENT ACCOMPLISHED BUT OVER TEMPERATURE CONTINUED TO MAX ENGINE GENERATOR TEMPERATURE OF 900C. ENGINE WAS SHUTDOWN PER QRH PROCEDURE AND UNEVENTFUL FOR SINGLE ENGINE APPROACH. VISUALLY INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. ACCOMPLISHED BOROSCOPE OF HPC HPT IPT AND LPT ACCOMPLISHED BITE CHECK OF EEC BVCU TPU AND AVM MONITOR. REPLACED AVM MONITOR AND ACCELORMETER. REPLACED BVCU AND TPU. REPLACED TPU SENSOR AND DEDICATED GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — MALFUNCTIONED (APU BAY)

MCO - AFTER INTERMEDIATE LEVEL OFF AT FL220 SMOKE IN COCKPIT VERY SUDDEN & EVIDENT. FIRST CLASS F/A SMELLED SMOKE, ROW 26 PASSENGER INFORMED AFT F/A SMOKE SMELLED. ACCOMPLISHED CABIN SMOKE FIRE PROCEDURE TURNING OFF BOTH UTILITY BUS SWITCHES, BOTH RECIRCULATION FAN SWITCHES & RT PACK CONTINUE SELECT. SMOKE PERSISTED 20 PLUS MINUTES THROUGH LANDING. SMOKE DETECTED COCKPIT THEN FIRST CLASS F/A THEN MID CABIN. F/A REPORTED SEEING HAZE IN CABIN. WHILE PREPARING FOR DIVERSION TO MCO NOTICED LEFT HAND ENGINE VIBRATION 3.0 (AMBER) IN NR 1 POSITION. ALL SYSTEMS OPERATED NORMAL IN DESCENT TO MCO. REPLACED APU, & REPLACED VIBRATION ACCELEROMETER TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACTOR — DISPLACED (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27 INOPERATIVE. ADJUSTED LAMP CONTACTS AT OVERHEAD STORAGE BIN 27ABC FOR OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 29D)

DFW - MAINTENANCE OBSERVED EMERGENCY LIGHTING INOPERATIVE AT SEAT 29D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — FAILED (L2 DOOR)

SNA - FLT 1599 - FLIGHT ATTENDANT OPENED THE L2 DOOR WITHOUT DISARMING THE SLIDE. SLIDE SEPARATED FROM PACK. NO DEPLOYMENT OF INFLATION OF THE SLIDE. DOOR ASSIST BOTTLE WAS FOUND TO BE FLAT. REPLACED THE L2 DOOR SLIDE AND DOOR ASSIST BOTTLE. GROUND CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT CHECK, RIGHT AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 16 AFT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TACH GENERATOR — FAILED (RT ENGINE)

LAX - RIGHT ENGINE N3 INDICATION. RIGHT N3 INOPERATIVE. REPLACED RIGHT ENGINE N3 TACH GENERATORS, GROUND CHECKS NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM SEAT 3E TO 63. REPLACED BROKEN AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT 3F AND 6F. REMOVED AND REPLACED BROKEN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - AFT LAVATORY EMERGENCY PATH FLOOR TRACK EXIT MARKER LIGHT OUT. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT AND RIGHT SERVICE DOORS. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FROM SEAT ROW 17 THROUGH 34. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - LEFT AND RIGHT EMERGENCY LIGHTS AND EMERGENCY EXITS ARE INOPERATIVE. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

CCS - FLT 2155 - EN ROUTE DFW-CCS, SHORTLY AFTER LANDING CAPTAIN REPORTED PROBLEMS WITH NOSE LANDING GEAR STEERING SYSTEM. ARRIVED CCS GATE WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING WHEEL STEERING VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4 THROUGH 12 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTORS AT SEAT 4 AND 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. RE-CONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (ROW 6 AND 9)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 9 AND ROW 6 INOPERATIVE. REPLACED BAD CONNECTORS AT ROW 9. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT NEAR OVERHEAD BIN AT SEAT 10D INOPERATIVE. TIGHTENED LOOSE WIRES AT SEAT 10D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 3 AND 12 INOPERATIVE. REPLACED END CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)