N436AA

Part: UPLOCK — LEAKING (LT MLG DOOR) · airframe 86,401 hrs · 40,495 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, A LOW HYD PRESS WARNING OCCURRED. FOUND LT MLG DOOR UPLOCK LEAKING. R & R UPLOCK. PERFORMED OPERATIONAL & LEAK CHECK IAW AMM 29-10-05. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,531 hrs · 39,440 cycles

2.5 INCH CRACK ON LT SIDE ABOVE PACK RAM AIR. INSTALLED REPAIR DOUBLER IAW SRM 55-01-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,531 hrs · 39,440 cycles

TWO SKIN CRACKS AT STATION 1436 & STRINGER 3 RT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00.

Part: FORMER — CRACKED (LE SLAT TRACK) · airframe 84,531 hrs · 39,440 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06.

Part: FORMER — CRACKED (LE SLAT) · airframe 84,531 hrs · 39,440 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05.

Part: SPLICE — BURNED (CABIN PRESSURE) · airframe 83,968 hrs · 39,141 cycles

CREW REPORTED BOTH CABIN PRESS CONTROL INOPERATIVE. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. PLACARDED BOTH PRESSURIZATION CONTROLLERS INOPERATIVE IAW MEL. REPLACED SPLICE S9-5J THAT WAS BURNED. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 83,958 hrs · 39,133 cycles

TAIL COMPARTMENT EMER LIGHTS INOPERATIVE. REPLACED POWER SUPPLY FOR TAIL COMPARTMENT EMER LIGHTS. OPERATIONS CHECKED NORMAL.

Part: FITTING — LEAKING (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

CENTER TANK - LEFT BATHTUB FITTING IS LEAKING AT STATION 870 LEFT SIDE OF KEEL BEAM BOX FORWARD OF THE WHEEL WELL. INSTALLED NEW FORWARD AND AFT LEFT BATHTUB FITTINGS PER AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION ON NUMBER 6 SEAT TRACK AT STATION 370 AROUND FASTENER HOLE FOR SIDEWALL SUPPORT. CUT OUT CORROSION AND PERFORMED STRAP DOUBLER REPAIR PER AARD 53-20-00-13.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION AND SHEARED RIVET HEADS AT STATION 646 BETWEEN LONGERONS 30 AND 29 LEFT. CUT OUT CORROSION AND INSTALLED DOUBLER PER EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

CORROSION ON CUSP AT STATION 258 LEFT SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16 AND SRM 51-30-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

CUSP SHEET CRACKED BELOW NUMBER 6 SEAT TRACK FROM STATIONS 218 TO 237. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

RIGHT CUSP FROM STATIONS 503 TO 598 CORRODED. INSTALLED CUSP SHEET PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

FORWARD NUMBER THREE LONGERON LEFT AT STATION 160 CRACKED. INSTALLED NEW LONGERON SECTION PER SRM 53-02-00 FIGURE 18.

Part: SKIN — DENTED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

DENT WITH GOUGE AT STATION 179, LONGERON 30. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 4.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 80,380 hrs · 37,231 cycles

CRACK ON MOUNT BRACKET AT AFT END TIE-DOWN TRACK INTERCOSTAL, STATION 788 BETWEEN LONGERONS 28 AND 27 RIGHT. REMOVED AND INSTALLED NEW BRACKET PER SRM 51-30-05.

Part: RETAINER — DAMAGED (RUDDER) · airframe 80,380 hrs · 37,231 cycles

RUDDER, LEFT SIDE 6 SEAL RETAINER HOLES BORED OUT TO QUARTER INCH IN SIZE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-01A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION ON FLOORBEAM AT STATION 160, RIGHT BUTTLINE 10. REMOVED CORROSION AND INSTALLED A SPLICE ANGLE REPAIR PER SRM 51-70-05-FIGURE 3 SHEET 7.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION ON SUB FLOOR UNDER G-1 GALLEY DRAIN PAN. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION ON SUB FLOOR AT STATION 160, RIGHT BUTTLINE 10 UNDER G1 INBOARD GALLEY MOUNT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,380 hrs · 37,231 cycles

CORROSION ON AFT SERVICE DOOR SUBFLOOR UNDER AFT GIRT BAR SUPPORT BRACKET. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: EXCITER — FAILED (RT ENGINE) · airframe 74,895 hrs · 34,456 cycles

MCO INFLIGHT TPA-ORD. CREW REPORTED LIGHTNING STRIKE TO RIGHT SIDE OF AIRCRAFT WITH RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 1 MINUTE). EMERGENCY DECLARED DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE EXCITER, BOTH IGNITION LEADS AND IGNITOR PLUGS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL VALVE — LEAKING (HYDRAUILIC SYS) · airframe 74,207 hrs · 34,139 cycles

YYC - CREW REPORTED LOSS OF HYDRAULIC PRESSURE. EMERGENCY DECLARED FLIGHT RETURNED YYC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT THRUST REVERSER CONTROL VALVE AND RUDDER SHUTOFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,256 hrs · 32,340 cycles

EMERGENCY LIGHTS IN SEATS INOPERATIVE. INSTALLED BATTERY PACK FOR EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,256 hrs · 32,340 cycles

EMERGENCY LIGHTING IN SEATS INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK FOR EMERGENCY LIGHTING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,256 hrs · 32,340 cycles

EMERGENCY LIGHTING IN SEATS INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK FOR EMERGENCY LIGHTING IN SEATS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,256 hrs · 32,340 cycles

EMERGENCY LIGHTS IN SEATS INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK FOR EMERGENCY LIGHTS.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 69,652 hrs · 32,041 cycles

DFW - CREW REPORTED AIRCRAFT LOST PRESSURIZATION AND NOTICED THE CABIN ALTITUDE CLIMBING. DECLARED AND EMERGENCY AND DESCENDED, O2 MASKS DID NOT DEPLOY. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH PRESSURE CONTROLLERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,330 hrs

LGA - CEILING EMERGENCY LIGHTS AT ROW 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK AT ROW 8 FOR EMERGENCY LIGHTS.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 68,144 hrs · 31,424 cycles

MID CARGO DOOR UPPER FORWARD STOP BRACKET CRACKED. INSTALLED A SERVICEABLE BRACKET PER ESO 80174.

Part: FRAME — CRACKED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

CRACK IN DOUBLER REPAIR AT BASE OF ACTUATOR CRADLE AT FRAME STATION 1485. INSTALLED SERVICEABLE DOUBLER PER AARD 53-10-00-33.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 68,144 hrs · 31,424 cycles

MID CARGO DOOR UPPER AFT STOP BRACKET CRACKED. INSTALLED SERVICEABLE BRACKET PER ESO80174.

Part: BRACKET — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

LOWER CORNER BRACKET IN AFT CARGO AT STATION 1211 AND LONGERON 27 RIGHT CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET PER SRM 51-30-00.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

LEFT TIE DOWN TRACK IN AFT CARGO HAS CORROSION SEVERAL PLACES FROM STATION 1212 TO STATION 1117. REPLACED LEFT FORWARD TRACK FROM STATION 1212 TO STATION 1117.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 68,144 hrs · 31,424 cycles

FORWARD ENTRY DOOR THIRD FROM BOTTOM INTERCOSTAL CRACKED. REPAIRED PER AARD 52-10-00-3.

Part: BEAM — CRACKED (ZONE 800) · airframe 68,144 hrs · 31,424 cycles

FORWARD ENTRY DOOR, NUMBER 6 DOOR BEAM CRACKED. REPAIRED PER SRM 52-05-00 FIGURE 3.

Part: BRACKET — CORRODED (CARGO DOOR FRAME) · airframe 68,144 hrs · 31,424 cycles

CORROSION IN MID CARGO DOOR JAMB FORWARD LOWER CORNER FITTING. OLD BRACKET WAS REMOVED AND NEW BRACKET INSTALLED.

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

CORROSION IN LOWER "J" ANGLE AT STATION 1322 BETWEEN LONGERON 29 LEFT AND LONGERON 29 RIGHT. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-17.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 68,144 hrs · 31,424 cycles

MID CARGO DOOR BEAM VERTICAL LEG CORRODED. INSTALLED 2 DOUBLERS PER AARD 53-10-00-3.

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

CORROSION ON ANGLE FRAME 9 INCHES TO THE RIGHT OF AIRCRAFT CENTER LINE AT STATION 1380, LOWER AFT SIDE OF APU ENCLOSURE. REPAIR DOUBLER INSTALLED PER ESO 80559 DATED 12/01/08.

Part: LONGERON — CRACKED (BS 160) · airframe 68,144 hrs · 31,424 cycles

STATION 160 AT LONGERON LEFT 3 IS CRACKED AT FASTENER. INSTALLED REPLACEMENT SPLICE LONGERON AT STATION 160 AT LEFT 3 PER SRM 53-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,144 hrs · 31,424 cycles

CORROSION ON LOWER SIDE OF RIGHT CUSP STATION 1200. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 68,144 hrs · 31,424 cycles

BRACKET CORRODED, BETWEEN LONGERON 27 AND 28 RIGHT AT AFT CARGO DOOR CUTOUT STATION 1210. REMOVED BRACKET AND INSTALLED SERVICEABLE BRACKET PER SRM 51-01-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,144 hrs · 31,424 cycles

PLOW ANGLE CORRODED IN AFT CARGO STATION 1338. INSTALLED A SERVICEABLE ANGLE PER SRM 53-01.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 68,144 hrs · 31,424 cycles

NUMBER 4 SEAT TRACK TANG BROKEN FROM STATION 928 TO 930. INSTALLED REPAIR PLUG.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 68,144 hrs · 31,424 cycles

NUMBER 4 SEAT TRACK TANG BROKEN FROM STATION 916 TO 919. INSTALLED REPAIR PLUG.

Part: FITTING — CRACKED (AFT PAX DOOR) · airframe 68,144 hrs · 31,424 cycles

VAULT DOOR BELL CRANK FITTING CRACKED. INSTALLED A SERVICEABLE FITTING.

Part: MOUNT — CORRODED (GALLEY) · airframe 68,144 hrs · 31,424 cycles

CORROSION ON INBOARD AFT NUMBER 2 GALLEY MOUNT. INSTALLED SERVICEABLE GALLEY MOUNT.

Part: FITTING — CRACKED (ZONE 200) · airframe 68,144 hrs · 31,424 cycles

DOOR STOP BACK UP FITTING IS CRACKED AT LOWER FASTENER ON LEFT SIDE OF VAULT DOOR OPENING, LOWER FITTING. INSTALLED SERVICEABLE DOOR STOP FITTING PER SRM 51-01.

Part: MOUNT — CORRODED (ZONE 100) · airframe 68,141 hrs · 31,424 cycles

G2 GALLEY INBOARD GALLEY MOUNT CORRODED IN HOLE AND TOP. NEW GALLEY MOUNT WAS INSTALLED PER SRM 51-01.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

CORROSION ON LOWER SIDE OF RIGHT CUSP STATION 560. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,144 hrs · 31,424 cycles

RIGHT CUSP CORRODED STATION 845. REPAIRED PER AARD 53-20-00-10.

Part: LENS — INOPERATIVE (EMERGENCY LIGHTS) · 67,593 cycles

DFW EMERGENCY LIGHT BETWEEN RT SEAT ROWS 6 AND 7 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT BETWEEN RT SEAT ROWS 6 AND 7. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 67,593 cycles

DFW EMERGENCY LIGHTS AT AISLE OVERHEAD SEAT ROWS 22 TO 28 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1100 FOR EMERGENCY LIGHTS AT AISLE OVERHEAD SEAT ROWS 22 TO 28. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 67,593 cycles

DFW EMERGENCY LIGHT EXIT SIGNS AT AFT OVERWING LT AND RT INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENCY LIGHT EXIT SIGNS AT AFT OVERWING LT AND RT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · 67,593 cycles

DFW EMERGENCY LIGHT AT SEAT 22D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · 67,593 cycles

DFW EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LGA - FOUND AFT EMERGENCY EXIT FLOOR LIGHT FROM AFT MODULE AB54 INOPERATIVE. REPLACED CONTROL MODULE AND BATTERY FOR AFT EMERGENCY EXIT FLOOR LIGHT FROM AFT MODULE AB54. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (AIR CONDITIONING)

LGA INFLIGHT T1142/24JAN - EN ROUTE TO LGA EXPERIENCED PRESSURIZATION LOSS. INITIATED EMERGENCY DESCENT AND PASSENGER OXYGEN MASKS DROPPED WITH EXCEPTION OF SEAT 23DEF AND FLIGHT ATTENDANT STATION. REPLACED LEFT PACK FLOW CONTROL VALVE, TEMPERATURE CONTROL VALVE, RIGHT PACK AUTO TEMPERATURE CONTROLLER, PACK DISCHARGE SWITCH, AUTO TRIP SWITCHES, AND REPLACED OXYGEN MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADES — DAMAGED (LEFT ENGINE)

ORD - ON TAKE OFF, AIRCRAFT YAWED TO THE RIGHT. FLIGHT ATTENDANTS REPORTED LOUD PBP BEFORE FLIGHT CREW ABORTED TAKEOFF. BRAKE TEMPERATURES DID NOT EXCEED 150 DEGREES. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED NUMBER THREE AND FOUR MAIN LANDING GEAR TIRES AND NUMBER THREE AND FOUR BRAKES. REPLACED LEFT ENGINE ON 07 DECEMBER 2006 AT ORD DUE TO DISTRESSED COMPRESSOR STATE 12 AND 13 BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING EMERGENCY LIGHT CHECK OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, STA 1039 LT AND STATION 1096 RT AND LT WERE INOPERATIVE. REPLACED BATTERY PACK AT STA 1057 RT FOR OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, 1039 LT AND 1096 RT AND LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SIGN — UNSERVICEABLE (CABIN)

DFW - LEFT HAND EMERGENCY LIGHT EXIT MARKER AT FORWARD OVERWING EXIT UNREADABLE. REPLACED LEFT HAND EMERGENCY LIGHT EXIT MARKER AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FORWARD EMERGENCY LIGHT ARROW INOPERATIVE. REPLACED FORWARD EMERGENCY ARROW LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — UNSERVICEABLE (CABIN)

DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT UNREADABLE. REPLACED EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — DAMAGED (ACM BAY)

ORD - FLT 1511 - EN ROUTE ORD-PSP - 15 MINUTES AFTER TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. FOLLOWED PROCEDURES AND LIGHT EXTINGUISHED WITHIN ONE MINUTE. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED AIR CONDITIONING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (A/C BAY)

ORD - FLT 1381 - EN ROUTE ORD-SAT, DURING CLIMB-OUT, THE TAIL COMPARTMENT TEMPERATURE HIGH WARNING LIGHT ILLUMINATED. CHECKLIST WAS RUN AND LIGHT EXTINGUISHED. IAW THE CHECKLIST, THE LEFT SUPPLY SWITCH WAS RETURNED TO THE AUTO POSITION AND DURING CLIMB THE WARNING LIGHT ILLUMINATED AGAIN. IT EXTINGUISHED WHEN HIGH PRESSURE BLEED OFF WAS AGAIN SELECTED. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SENSORS. PERFORMED HIGH POWER RUN UP. CHECKED DUCT COUPLINGS AND VALVES FOR LEAKS DURING RUNUP. NO LEAK NOTED, TAIL COMPARTMENT HIGH TEMPERATURE WARNING LIGHT DID NOT ILLUMINATE DURING HIGH POWER RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — DAMAGED (AFT AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT LEFT SIDE SIDEWALL INOPERATIVE. REPAIRED AFT AIRSTAIR EMERGENCY EXIT SIDEWALL LIGHT WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD HALF OF CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS AND HALF OF COACH EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED BATTERY PACK TO FIRST CLASS EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GENERATOR — DEFECTIVE (ENGINES)

MSP - FLT 1103 - EN ROUTE ORD-SEA - LEFT GENERATOR TRIPPED IN FLIGHT. RESET AND TRIPPED AGAIN AFTER FIVE MINUTES. AIR INTERRUPTED AND LANDED MSP WITHOUT INCIDENT. REPLACED LEFT AND RIGHT GENERATOR CONTROL UNITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND TEMPORARY REPAIR INSTALLED AT LONGERON 21R STATION 500. INSTALLED DOUBLER PER SRM 53-04 FIG 38, SHEET 24 AND ESO 80559 DATED 4/10/2001. (M)

Part: FRAME — CHAFED (FUSELAGE)

TUL - FOUND STATION 1401 L21R FRAME WORN FROM INCORRECT LINE STAND OFF. BLENDED OUT WEAR AREA. TREATED, PRIMED AND INSTALLED DOUBLERS PER 53-03 P5 FLT 32 SHEET 4. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CRACK AT BASE OF CANT FRAME 1485 RIGHT JUST OUTBOARD OF STAIR ACT. REMOVED DAMAGE (CRACK), AND INSTALLED WEB SPLICE PER ESO 80559 DATED 2-23-01. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

TUL - FOUND RIGHT AFT LAVATORY STATION 1338 FLOORBEAM DAMAGED, CORROSION AROUND FASTENER HOLE. REPAIRED FLOORBEAM PER SRM 53-05 PART 1. (M)

Part: SKIN PANEL — DAMAGED (VERTICAL STAB)

TUL - FOUND VERTICAL STAB SKIN WORN 50 PERCENT THROUGH BY DAMAGED SEAL BRACKET JUST AFT OF RIGHT ROLLER TRACK. PART REPLACEMENT. REMOVED AND REPLACED STAB SKIN PANEL WITH NEW TREATED PRIMED AND PAINTED PER SRM 51-10-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK 6 AT STATION 215. REMOVED CORRODED SECTION AND SPLICED IN NEW SEAT TRACK FROM STATION 215 TO 303 PER 53-05 PT 1 FIG 4F. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT WITH SHARP CREASES DOWN INSIDE, LEFT FUSELAGE STATION 290 L22L, MARKED. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AND WEAR ON SEAT TRACK NR 1 FROM 1118-1121. INSTALLED SEAT TRACK PLUG STATION 1110-1123 PER SRM 53-05 PART 1, FIG 4A. APPLIED COAT OF WHITE POLYURETHANE PAINT. (M)

Part: OVEN — SMOKING (GALLEY)

BOS - FLT 449 - EN ROUTE BOS-MIA, DURING CLIMB-OUT FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN CABIN. SMOKE STARTED IN BACK OF THE AIRCRAFT AND WORKED FORWARD, THEN SMOKE DISSIPATED. AIRCRAFT RETURNED BOTH AND LANDED WITHOUT INCIDENT. INSPECTED APU AREA FOR OIL LEAKS, ENGINE INLETS AND EXHAUSTS, AND BOTH ENGINE CROSSOVER DUCTS. NO EVIDENCE OF OIL LEAKS NOTED. CHECKED RECIRCULATION FAN AND FILTERS, CHECKED GALLEY OVENS OPERATION AND FOR RESIDUE. NO FAULTS FOUND, FLIGHT ODOR FROM NR 3 OVEN. PRECAUTIONARY REPLACED WATER SEPARATOR COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PER MM. PRECAUTIONARY REPLACED NR 3 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT PART OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT AFT PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)