N468AA

Part: REGULATOR VALVE — ODOR (AC BAY) · airframe 77,379 hrs · 41,251 cycles

SHORTLY AFTER TAKEOFF ROTATION, THERE WAS A FAINT SHORT DURATION, APPROX 1 MINUTE, ODOR, EITHER A BURNING RUBBER OR OIL RESIDUE ODOR. NO SMOKE, JUST SMELL OR ODOR. THE FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. R & R RT AIR CONDITIONING PRESS REGULATING VLV IAW AMM 21-30-01, ALL CHECKED NORMAL. SEE SDR AALA20151106010, AALA20151106011 & AALA20151106012.

Part: WATER SEPARATOR — ODOR (AC BAY) · airframe 77,379 hrs · 41,251 cycles

SHORTLY AFTER TAKEOFF ROTATION, THERE WAS A FAINT, SHORT DURATION, APPROX 1 MINUTE, ODOR, EITHER A BURNING RUBBER OR OIL RESIDUE ODOR. NO SMOKE, JUST SMELL OR ODOR. THE FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. R & R RT WATER SEPARATOR IAW AMM 21-20-02. ALL CHECKED OK. SEE SDR AALA20151106009, AALA20151106011 & AALA20151106012.

Part: WATER SEPARATOR — ODOR (AC BAY) · airframe 77,379 hrs · 41,251 cycles

SHORTLY AFTER TAKEOFF ROTATION, THERE WAS A FAINT, SHORT DURATION, APPROX 1 MINUTE, ODOR, EITHER A BURNING RUBBER OR OIL RESIDUE ODOR. NO SMOKE, JUST SMELL OR ODOR. THE FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. R & R THE LT WATER SEPARATOR IAW AMM 21-20-02. ALL CHECKED NORMAL. ALSO SEE SDR AALA20151106010, AALA20151106011 & AALA20151106012.

Part: REGULATOR VALVE — ODOR (AC BAY) · airframe 77,379 hrs · 41,251 cycles

SHORTLY AFTER TAKEOFF ROTATION, THERE WAS A FAINT, SHORT DURATION, APPROX 1 MINUTE, ODOR, EITHER A BURNING RUBBER OR OIL RESIDUE ODOR. NO SMOKE, JUST SMELL OR ODOR. THE FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. R & R LT AIR CONDITIONING PRESS REGULATOR VLV IAW AMM 21-31-01, ALL CHECKED NORMAL. ALSO SEE SDR AALA20151106010, AALA20151106011 & AALA20151106012.

Part: CLAMP — LEAKING (ZONE 200) · airframe 76,361 hrs · 40,649 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, PACK TRIPPED OFF & THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. REMOVED & REPOSITIONED DUCT. REPLACED LOWER CLAMP & UPPER SHIMS IAW AMM 20-10-11. PERFORMED OPERATIONAL & LEAK CHECK WITH NO TAIL COMPARTMENT TEMP HIGH LIGHT NOTED IAW SIC 0930 & SIC 36-95-14. SYS CHECKED NORMAL.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 76,127 hrs · 40,518 cycles

AT GATE AS 1L DOOR WAS OPENED, UPON ARRIVAL, SLIDE FELL OUT OF HOUSING. REINSTALLED 1L DOOR SLIDE IAW MM 25-62-00.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 75,382 hrs · 40,088 cycles

RIGHT ELEVATOR STATIC WICK SHOWS EVIDENCE OF LIGHTNING STRIKE DAMAGE TO UPPER AFT OTBD SKIN. REPAIRED AREA IAW FEA.

Part: SWITCHING UNIT — DEFECTIVE (SPOILER) · airframe 75,046 hrs · 39,900 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL, NOT OVERWEIGHT. DURING CLIMB THE NLG RED LIGHT REMAINED LIT WITH AUTO SPOILER DO NOT USE & STALL INDICATION FAILURE LIGHTS. NLG STRUT BOTTOMED. PERFORMED NOSE GEAR STRUT SERVICE IAW 32-21-02. REPLACED NOSE GEAR UP POSITION PROXIMITY SENSOR IAW 32-60-05. PERFORMED NOSE GEAR SWING IAW 32-60-00. R & R AUTO SPOILER SWITCHING UNIT IAW AMM 27-62-09. SYS CHECKED NORMAL.

Part: BAND — DAMAGED (DORSAL FIN) · airframe 74,646 hrs · 39,649 cycles

DORSAL FIN BAND AT STATION 52.267 HOLES OUT OF ROUND. REPLACED 503 BAND IAW SRM 55-03-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

DAMAGED FASTENER HOLE IN SKIN AT STATION 151 & STRINGER 26 LT. INSTALLED SLEEVE BUSHING IN SKIN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

DAMAGED HOLE IN SKIN AT STATION 160 & STRINGER 26 LT. INSTALLED SLEEVE BUSHING IN SKIN.

Part: SKIN — WORN (VERTICAL STAB) · airframe 74,646 hrs · 39,649 cycles

LEADING EDGE OF VERTICAL BELOW ZFS 52.267 WORN. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 55-03-00 FIGURE 29.

Part: SKIN — WORN (VERTICAL STAB) · airframe 74,646 hrs · 39,649 cycles

VERTICAL STABILIZER LE JUST BELOW ZFS 52 HAS WORN HOLES. INSTALLED PLUG IAW EA MD80-55-036666.

Part: STRUCTURE — WORN (VERTICAL STAB) · airframe 74,646 hrs · 39,649 cycles

FOUND WEAR IN VERTICAL STABILIZER DORSAL FASTENER HOLES. INSTALLED REPAIR DOUBLER IAW SRM 55-03-00-001.

Part: SKIN PANEL — WORN (VERTICAL STAB) · airframe 74,646 hrs · 39,649 cycles

FOUND WEAR IN FASTENER HOLES ON VERTICAL STABILIZER LE PANEL. INSTALLED REPAIR DOUBLER ON VERTICAL STABILIZER LE PANEL IAW SRM 55-03-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

LONGERON 23 LT AT STATION 200 CRACKED. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

LONGERON 24 LT AT STATION 200 CRACKED. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

LONGERON 26 LT AT STATION 160 CRACKED. INSTALLED SPLICE REPAIR IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,646 hrs · 39,649 cycles

LONGERON 25 CRACKED AT STATION 160. ACCOMPLISHED REPAIR IAW SRM 53-02-00.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 70,486 hrs · 37,145 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 70,486 hrs · 37,145 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO ROW 11 INOPERATIVE. RESEATED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,702 hrs · 35,603 cycles

CUSP FROM STATIONS 145 TO 170 RIGHT BUTTLINE 56 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,702 hrs · 35,603 cycles

RIGHT CUSP AT STATION 342 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,702 hrs · 35,603 cycles

LEFT CUSP AT STATION 1142 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

RIGHT CUSP AT STATION 535 TO 539 CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

TOP BRACKET CRACKED ON AFT PRESSURE BULKHEAD STIFFENER, 34 INCHES ABOVE FLOOR AT LEFT OUTBOARD END. INSTALLED ANGLE BRACKET ON AFT BULKHEAD STIFFENER LEFT OUTBOARD END PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

CARGO AFT CX LT CUSP CRACKED STA 1266. INSTALLED CUSP SHEET AT STA1250-1309 LT SIDE PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

LEFT CUSP SHEET IS DAMAGED FROM STATIONS 1244 TO 1250. INSTALLED DOUBLER PER AARD 53-20-00-16 AND EA MD80-53-021127.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

CUSP AT STATIONS 1244 TO 1250 DAMAGED. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,702 hrs · 35,603 cycles

CORROSION ON SUBFLOOR AT G-2 GALLEY AFT INBD FLOOR TIEDOWN FITTING AT STATION 216. INSTALLED SUB-FLOOR DOUBLER PER AARD 53-20-00-16.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,702 hrs · 35,603 cycles

CORROSION ON G-2 GALLEY AFT INBD FLOOR TIEDOWN FITTING AT STATION 216. INSTALLED UPPER G-2 GALLEY MOUNT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

LEFT CUSP STATIONS 1088 TO 1091 CORROSION BEYOND LIMITS. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 67,702 hrs · 35,603 cycles

CRACK IN LEFT RINGPAN AT UPPER AFT CORNER. REMOVED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,702 hrs · 35,603 cycles

DENTS IN SKIN AT STATION 256. INSTALLED DOUBLER REPAIR PER BOEING DRAWING SG09530002.

Part: GEARBOX — FAILED (NR 2 ENGINE) · airframe 66,876 hrs · 35,148 cycles

BNA - CREW REPORTED NUMBER 2 ENGINE OIL QUANTITY AND OIL PRESSURE LOSS. RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 10 MIN). EMERGENCY DECLARED FLIGHT RETURNED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT BNA ON 07/18/2011 DUE TO GEARBOX FAILURE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: A/C PACK — DIRTY (AC BAY) · airframe 66,520 hrs · 34,947 cycles

LIT - CREW REPORTED ODOR IN FLIGHT DECK AND CABIN. EMERGENCY DECLARED FLIGHT RETURNED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FILTER — CLOGGED (RT ENGINE) · airframe 64,239 hrs · 33,656 cycles

PHL - ON DESCENT RIGHT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED, IDLE POWER WAS NECESSARY TO KEEP LIGHT OUT. EMERGENCY DECLARED, LANDED PHL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OIL FILTER AND DRAINED OIL AND REPLACED WITH CLEAN OIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 63,930 hrs · 33,480 cycles

DFW - CREW REPORTED NUMBER 2 ENGINE FIRE LOOP HAD A FIRE INDICATION FOLLOWED BY WARNING BELL. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTI ICE DUCT THAT WAS BLOWN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TIRE — DAMAGED (NLG) · airframe 62,290 hrs · 32,619 cycles

INFLIGHT DFW TO MEX. CREW REPORTED SEVERE YAW AT ROTATION. FELT LIKE NOSE GEAR PROBLEM. ALSO CAPTAINS SLIDING WINDOW POSSIBLE CRACK. EMERGENCY DECLARED AND LANDED SAT WITHOUT INCIDENT. NO DEFECTS NOTED WITH LANDING GEAR. REPLACED BOTH NOSE LANDING GEAR TIRE ASSEMBLIES AND CAPTAINS SLIDING WINDOW SEAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,032 hrs · 32,475 cycles

EMERGENCY LIGHTS AT FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY CEILING LIGHTS.

Part: SEAL — TORN (PAX DOOR) · airframe 59,957 hrs

DFW INFLIGHT RIC TO DFW - CREW REPORTED MODERATE BUMP IN FLIGHT FOLLOWED BY FORWARD ENTRY DOOR NOISE. CABIN ALTITUDE ROSE TO 9500 FEET. DESCENDED TO FL190. FLIGHT ATTENDANTS PUT WET BLANKETS IN THE DOORWAY AND CABIN ALTITUDE WENT TO NORMAL. LANDED DFW WITHOUT INCIDENT. FOUND FORWARD ENTRY DOOR SEAL TORN IN LOWER CORNER. REPAIRED DOOR SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: REGULATOR — MALFUNCTIONED (A/C BAY) · airframe 58,520 hrs

DEN INFLIGHT T1055/23JUN. CREW REPORTED ODOR AND HAZE IN CABIN. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND. REPLACED RT AIR CONDITIONING PILOT PRESSURE REGULATOR AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — DISLODGED (EMERGENCY LIGHT) · airframe 57,847 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 28 TO AFT OF CABIN INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 28 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,847 hrs

LGA - EMERGENCY LIGHT AT TAIL COMPARTMENT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — DIRTY (NLG STRUT)

ORD INFLIGHT T1349/16FEB - CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CLEANED AND REPLACED SEALS, BEARING PLATE, AND SCHRADER VALVE. SERVICED STRUT WITH NEW FLUID. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — LEAKING (NOSE GEAR)

ORD INFLIGHT - UNABLE TO RETRACT LANDING GEAR. THREE GREEN INDICATION AT ALL TIMES. GEAR HANDLE WOULD NOT MOVE FULL RANGE. LANDED ORD WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT NOT FULLY EXTENDING. REPACKED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION ARE DIM. REPLACED NUMBER ONE CONTROL MODULE AND BATTERY AND REPLACED NUMBER TWO BATTERY FOR SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA - CEILING EMERGENCY EXIT LIGHTS AT ROW 19 AND 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHTS AT ROW 19 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA - EMERGENCY EXIT PATH LIGHTS AT ROWS 4 THROUGH 19 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT PATH LIGHT AT ROWS 4 THROUGH 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE)

TUL - FLT 1704 - EN ROUTE ORD-EWR, AT 33,000 FEET, CREW REPORTED DROP IN ALTITUDE TO 10,000 FEET. DEPLOYED OXYGEN MASKS, AND LANDED EWR WITHOUT FURTHER INCIDENT. FERRIED AIRCRAFT TUL. REPLACED NR 1 CABIN PRESSURE CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER BAG — DIRTY (AC BAY)

ORD - FLT 1326 - EN ROUTE ORD-TPA - SHORTLY AFTER TAKEOFF, CABIN FILLED WITH SMOKE. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PER MAINTENANCE MANUAL. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 9 INOPERTIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — DEFECTIVE (MLG)

ORD - FLT 792 - EN ROUTE ORD-EWR - DURING INSPECTION, BEFORE FLIGHT, CO-PILOT DETECTED SMOKE IN WHEEL WELL AREA. REPLACED AUXILIARY ELECTRIC HYDRAUIC PUMP. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (ROW 3 DEF)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH LIGHTING WIRE AT SEAT ROW 3DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

DFW - FLT 1284 - DURING APPROACH TO DFW, BURNING ODOR NOTED IN AFT CABIN AND RT LAVATORY SMOKE DETECTOR SOUNDED SEVERAL TIMES. ODOR DISSIPATED AND DETECTOR ALARM STOPPED. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED SMOKE DETECTOR IN AFT RT LAVATORY. ACCOMPLISHED GROUND ENGINE RUN AT HIGH POWER WITH NO DEFECTS OR ODOR NOTED. PRECAUTIONARY CHECKED GALLEY OVENS AND LIGHT BALLAST WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER — DIRTY (ACM BAY)

DFW - FLT T1341 - AFTER TAKEOFF MEM DURING INITIAL CLIMB-OUT, SLIGHT ODOR NOTED IN COCKPIT AND CABIN. ODOR DISSIPATED AFTER 10 MINUTES OF FLIGHT AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CSD — DEFECTIVE (LT ENG)

OAK - FLT 1769 - DURING CRUISE, THE LEFT ENGINE FIRE WARNING CAME ON. LEFT THROTTLE WAS RETARDED AND FIRE WARNING EXTINGUISHED. LANDED OAK WITHOUT INCIDENT. REPLACED LEFT CSD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)