N694AN

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 62,262 hrs · 21,337 cycles

MIA CREW REPORTED MULTIPLE EICAS DISPLAY FAULTS. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH EICAS COMPUTERS, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: WIRE — DAMAGED (HYDRAULIC SYS) · airframe 62,195 hrs · 21,312 cycles

VVI LT HAND HYD QUANTITY INDICATION FLUCTUATED. EMERGENCY DECLARED FLIGHT RETURNED VVI LANDED WITHOUT INCIDENT. PLACARDED LT HAND HYD QUANTITY INDICATION INOPERATIVE IAW MEL 29-07. FLIGHT CONTINUED TO DESTINATION. REPLACED WIRE SEGMENT FROM TRANSMITTER TO KEEL BEAM D40366P AT LAX ON 11/16/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: WIRE — DISCONNECTED (CABIN) · airframe 59,179 hrs · 20,231 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 13DEF INOPERATIVE. FOUND WIRE DISCONNECTED FROM SEAT MOUNTED LIGHT AT ROW 13DEF. REPLACED SEAT MOUNTED SOCKET. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 58,978 hrs · 20,159 cycles

ROW 17 EXIT LIGHT BROKEN. REPLACED LIGHT ASSEMBLY FOR ROW 17 EXIT LIGHT. OPS CHECK NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 58,056 hrs · 19,840 cycles

UPPER SKIN DENT 101 INCHES FROM INBOARD END, FIVE INCHES FROM TRAILING EDGE. CUT OUT DAMAGED SKIN, FILLED CORE WITH RESIN AND APPLIED FIBERGLASS WET LAY-UP REPAIR PLIES PER SRM 51-70-17.

Part: TAT PROBE — INOPERATIVE (ZONE 200) · airframe 57,956 hrs · 19,800 cycles

DFW - CREW REPORTED TOTAL AIR TEMPERATURE PROBE MESSAGE FOLLOWED BY AUTOTHROTTLE DISCONNECT AND LOSS OF FLIGHT MANAGEMENT COMPUTER FLIGHT PLANS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TAT PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TEE FITTING — CRACKED (FLOORBOARD) · airframe 57,166 hrs · 19,493 cycles

STATION 700 FLOORBOARD IS CRACKED ON THE T-CAP RADIUS. REPLACED SECTION OF T-CAP WITH REPAIR PER 53-00-07.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

CORROSION ON WEB STATION 1715 RIGHT BUTTLINE 53. REMOVED AND INSTALLED WEB PER SRM 51-10-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

RIGHT NUMBER 4 DOOR AFT DRAIN SUPPORT CHANNEL CORRODED ON TOP STATIONS 1660 TO 1680. REMOVED AND REPLACED RIGHT NUMBER 4 DOOR AFT DRAIN SUPPORT PER SRM 51-10-02-0G.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

RIGHT NUMBER 4 DOOR FORWARD DRAIN SUPPORT CHANNEL CORRODED ON TOP STATIONS 1640 TO 1660. REMOVED AND REPLACED RIGHT NUMBER 4 DOOR FORWARD DRAIN SUPPORT PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

CORROSION ON LEFT CREASE ANGLE AT STATIONS 760 TO 785. INSTALLED CREASE ANGLE AND SPLICE AT STATIONS 760 TO 810 PER SRM 53-30-13-01 AND AARD 53-30-13-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

INTERGRANULAR CORROSION ON CREASE ANGLE AT LEFT NUMBER 2 DOOR AREA STATION 710. REPLACED CREASE ANGLE AT LEFT NUMBER 2 DOOR PER SRM 51-10-02-0G.

Part: BULKHEAD — CORRODED (LT MLG WW) · corrosion level 3 · airframe 57,166 hrs · 19,493 cycles

BULKHEAD OF LEFT WHEEL WELL CORRODED STATION 1173 LEFT BUTTLINE 7. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-40-14-1 REPAIR 1 FIGURE 2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,166 hrs · 19,493 cycles

SHEAR TIE STATION 1660 AT STRINGER 24 TO 25 LEFT CRACKED. ACCOMPLISHED SHEAR TIE REPAIR.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

RIGHT NUMBER 1 DOOR AFT DRAIN CHANNEL CORRODED. REPLACED CHANNEL PER AARD 51-10-05 REPAIR 1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,166 hrs · 19,493 cycles

CABIN DOOR FORWARD DRAIN SUPPORT CHANNEL CORRODED. REPLACED CHANNEL PER AARD 51-10-05- REPAIR 1.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,166 hrs · 19,493 cycles

LEFT WING NUMBER 1 SLAT HAS AREA OF DELAMINATION ON UPPER TRAILING EDGE WEDGE. INSTALLED DOUBLER PER SRM 51-70-10-2R.

Part: INDICATOR — FAILED (COCKPIT) · airframe 56,158 hrs · 19,128 cycles

MIA - CREW REPORTED STANDBY ATTITUDE INDICATOR FAILED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STANDBY ATTITUDE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: POWER SUPPLY — FAULTY (NR 2) · airframe 54,560 hrs · 18,538 cycles

MIA - CREW REPORTED EICAS SPOILER MESSAGE IN CRUISE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. FOUND NUMBER 2 POWER SUPPLY UNIT FAULTED. REPLACED UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 54,451 hrs · 18,498 cycles

BULLNOSE AT 2EF INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT 2EF. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 54,451 hrs · 18,498 cycles

RIGHT OVERWING AFT EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE PLACARD. OPS CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 54,451 hrs · 18,498 cycles

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

Part: PLACARD — DAMAGED (ZONE 200) · airframe 54,451 hrs · 18,498 cycles

RIGHT OVERWING FORWARD EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE PLACARD. OPS CHECK NORMAL.

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 54,108 hrs · 18,367 cycles

MIA - TRAILING EDGE FLAP DISAGREE LIGHT CAME ON BEFORE FLAPS EVEN MOVED TO SELECTED POSITION OF 1. SPEED WAS APPX 220KTS. QRH PROCEDURE FOLLOWED AND FLAPS ELECTRICALLY EXTENDED TO 20. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT TRAILING EDGE FLAP TRANSMISSION INBOARD TORQUE LIMITER POPPED. REPLACED TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIMITER — MALFUNCTIONED (TE FLAP) · airframe 54,099 hrs · 18,364 cycles

BOS - FLIGHT CREW OBSERVED A FLAP ASYMMETRY EICAS MESSAGE. QRH PROCEDURES FOLLOWED. EMERGENCY DECLARED LANDED BOS WITHOUT INCIDENT. INSPECTED FLAPS AND FOUND LEFT INBOARD TORQUE LIMITER EXTENDED. SERVICED LEFT INBOARD TORQUE LIMITER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 53,970 hrs · 18,323 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT 5EF INOPERATIVE. SECURED LOOSE CONNECTOR AT 5EF. OPS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,970 hrs · 18,323 cycles

EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 52,971 hrs · 17,948 cycles

CORROSION ON NUMBER 9 SLAT SKIN LOWER TRAILING EDGE AROUND FASTENER AT OUTBOARD AUXILIARY TRACK. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: MODULE — DEFECTIVE (SPOILER) · airframe 52,920 hrs · 17,927 cycles

JFK - INFLIGHT MIA-LGA. CREW REPORTED SPOILER EICAS MESSAGE. DIVERTED TO JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SPOILER CONTROL MODULE M535 STUCK IN TEST MODE AND COULD NOT SHUT OFF. REPLACED MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — FAILED (TACH GENERATOR) · airframe 51,076 hrs · 17,253 cycles

ON CLIMBOUT CABIN ALTITUDE BEGAN TO CLIMB. BEGAN DESCENT AND REGAINED CONTROL OF CABIN PRESSURE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND INTERMITTENT N3 INDICATION FROM RIGHT ENGINE. REPLACED NUMBER TWO ENGINE N3 TACH GENERATOR PLUG.

Part: BATTERY PACK — WEAK (CABIN) · airframe 50,933 hrs · 17,208 cycles

MID COACH SEAT MOUNTED EMERGENCY LIGHT DIM. REPLACED MID COACH SEAT MOUNTED EMERGENCY LIGHT BATTERY PACK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 50,766 hrs · 17,149 cycles

EMERGENCY LIGHT AT AFT RIGHT LAVATORY INOPERATIVE. RESEATED CONNECTOR AT AFT LAVATORY RIGHT FLOOR.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 50,766 hrs · 17,149 cycles

EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RESEATED CONNECTOR AT SEAT 13D LIGHT ASSEMBLY.

Part: MODULE — INOPERATIVE (CABIN)

DFW - MID COACH ZONE EMERGENCY PATH LIGHTS ARE DIM. REPLACED EMERGENCY PATH LIGHTS MODULE AND BATTERY AT MID COACH ZONE.

Part: OVEN — DAMAGED (ZONE 900) · airframe 49,238 hrs · 16,620 cycles

MCI - INFLIGHT STL-LAX. CREW REPORTED SMOKE IN CABIN ORIGINATING FROM THE FORWARD GALLEY NUMBER 2 OVEN. EMERGENCY DECLARED, LANDED MCI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BURNED RESIDUE IN OVEN. REPLACED OVEN AND CLEARED CABIN OF SMOKE. NO OTHER GALLEY DAMAGE NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (ZONE 200)

MIA - EMERGENCY EXIT LIGHT ON LOWER FORWARD SIDE OF LEFT PASS ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT FOR LOWER FORWARD SIDE OF LEFT PASS ENTRY DOOR.

Part: STRUCTURE — CORRODED (APU INLET) · corrosion level 2 · airframe 47,963 hrs · 16,178 cycles

CORROSION AROUND NUT PLATE AFT. EDGE OF APU INLET DOOR, REPAIRED IAW EA 53-004951 DATED 11-12-08.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 47,963 hrs · 16,178 cycles

FORWARD AVIONICS DOOR FRAME CRACKED. REPAIRED IAW SRM 51-70-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,963 hrs · 16,178 cycles

INTERCOSTAL CRACKER; REPAIRED INTERCOSTAL IAW SRM 53-60-51-2R1.

Part: WIRE — CHAFED · airframe 46,108 hrs · 15,593 cycles

TUL - WIRE BUNDLE W4104 CHAFED AGAINST BRACKET JUST OUTBOARD OF RIGHT RECIRCULATION FAN AT THE AFT END OF FORWARD CARGO AREA. THREE EACH WIRES WERE BURNED IN HALF. THE BRACKET WAS DAMAGED AND THE INSULATION AROUND AREA WAS BURNED. REPLACED THREE FOOT SECTION OF WIRING, REPLACED INSULATION AND REPAIRED BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS) · airframe 45,596 hrs

DFW - EMERGENCY LIGHT AT SEAT 22D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS) · airframe 45,596 hrs

DFW - EMERGENCY LIGHT AT SEAT 3E MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ANTI-SKID SYS — MULTIPLE FAIL (MLG)

SJU INFLIGHT T883/29DEC BOS TO STT - ANTI SKID EICAS MESSAGE ILLUMINATED AND REMAINED ON UNTIL LANDING. LANDED SJU WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UPPER CONDUIT, RIGHT ANTI SKID MODULE AND NUMBER EIGHT TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 17A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 18F INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — LEAKING (HYD SYSTEM)

JFK INFLIGHT T1298/05MAY - LEFT HYDRAULIC SYSTEM LOST IN FLIGHT. LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR LINE AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP, CASE AND RETURN FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY EXIT LIGHT AT LEFT AFT ENTRY DOOR INOPERATIVE. RELAMPED INOPERATIVE EMERGENCY EXIT LIGHT AT LEFT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY EXIT LIGHT AT CENTER RIGHT DOOR INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - EMERGENCY LIGHTS FROM SEAT ROWS 26D TO 36D ARE DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

TUL - CORROSION FOUND IN RIGHT HAND WHEEL WELL ON LOWER SIDE OF PRESSURE DECK ABOVE SLIDE BOX. SIX SEPARATE CUTOUTS AT STATIONS 1140 TO 1180, RIGHT BUTTLINE 40 TO RIGHT BUTTLINE 70 AND 50. LARGEST IS 2 INCHES BY 2.5 INCHES.

Part: WIRE — SHORTED (CABIN)

BOS - EMERGENCY LIGHTS FROM L2 AND R2 TO SEAT ROW 15 INOPERATIVE. REPAIRED SHORTED WIRE AT SEAT 15DEF FOR EMERGENCY LIGHTS FROM L2 AND R2 TO SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 31D)

DFW - MAINTENANCE OBSERVED SEAT MOUNTED EMERGENCY LIGHTING INOPERATIVE AT ROW 31D. REPLACED THE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SET 9D INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SERVO MOTOR — DEFECTIVE (CENTER PEDESTAL)

ORD - FLT 0096 - AFTER TAKEOFF MIA WHEN REACHING TOP OF CLIMB AT FL 390, AUTOTHROTTLE DISCONNECTED FOLLOWED BY SLIGHT ELECTRICAL ODOR IN COCKPIT. ODOR DISSIPATED AFTER APPROXIMATELY 2 MINUTES AND AUTOTHROTTLES RE-ENGAGED WITH NO FURTHER PROBLEMS NOTED. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AUTOTHROTTLE SERVO MOTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONDUCTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED FLAT CONDUCTOR WIRES AT FRONT AND BACK OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)