N472AA

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,566 hrs · 40,183 cycles

CORROSION ON FWD CARGO DOOR PAN LOWER SECTION BETWEEN FS 370 & 427 AT STRINGER 26 RT. R & R SECTION OF PAN IAW EA 53-038391 & SRM 53-05-00 FIG 44.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 75,566 hrs · 40,183 cycles

FORWARD CARGO DOOR, FWD STOP PAD FITTING, SECOND FROM TOP IS CRACKED. R & R FITTING IAW AARD 51-00-05-1, DWG 5910141 & DWG CDK2345.

Part: FORMER — CRACKED (RT WING) · airframe 75,539 hrs · 40,167 cycles

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

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 74,336 hrs · 39,446 cycles

ELECTRICAL ODOR IN CABIN. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND OIL WETNESS IN THE EXHAUST AREA AFTER LANDING. ACFT REMOVED FROM SERVICE. ACFT FERRIED FOR MX. REPLACED RT ENG ON 07/30/2014. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

VERTICAL SUPPORT STRUT ON LT SIDE OF BULKHEAD STATION 218 IS CRACKED AT LOWER END BETWEEN LONGERONS 23 & 24 LT. INSTALLED DOUBLER IAW AARD 53-10-00 FIGURE 15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

STATION 200 AT LONGERON 24 CRACKED. SPLICED IN NEW LONGERON SECTION IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

LONGERON 24 AT STATION 200 CRACKED. INSTALLED NEW LONGERON & SPLICE DOUBLERS IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

LONGERON 25 AT STATION 160 CRACKED. INSTALLED NEW LONGERON & SPLICE DOUBLERS IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

LONGERON 23 AT STATION 200 CRACKED. INSTALLED NEW LONGERON & SPLICE DOUBLERS IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,049 hrs · 39,273 cycles

CRACK IN 1 FASTENER AT LONGERON 22 LT & STATION 188. INSTALL DOUBLER IAW DWG SR09530219.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,510 hrs · 38,386 cycles

AFT SECTION ESCAPE PATH LIGHTING WOULD NOT EXTINGUISH. RECHARGED BATTERIES. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 68,933 hrs · 36,362 cycles

AISLE EMERGENCY LIGHT AT SEAT 28D MISSING RED LENS. REPLACED RED LENS FOR AISLE EMERGENCY LIGHT AT SEAT 28D. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 68,933 hrs · 36,362 cycles

AISLE EMERGENCY LIGHT AT SEAT 28D HAS BROKEN LAMP. REPLACED LAMP FOR SEAT 28D AISLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 68,242 hrs · 35,996 cycles

DFW - FLIGHT ATTENDANT REPORTED PAPER BURNING SMELL IN MID CABIN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT PRESSURE REGULATING SHUT OFF VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,192 hrs · 35,963 cycles

NUMEROUS LIGHTING STRIKES ON OUTER SKIN OF FORWARD CARGO DOOR. REMOVED OLD DAMAGED SKIN AND INSTALLED NEW SKIN PER ESO 80174.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 68,192 hrs · 35,963 cycles

CABIN VERTICAL SUPPORT CRACKED UNDER NR 2 SEAT TRACK AT STATION 927. INSTALLED DOUBLER AND FILLER PER EA MD80-53-022740.

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 68,192 hrs · 35,963 cycles

RIGHT CUSP DAMAGED APPROXIMATELY STATION 212 JUST FORWARD AND INBOARD OF NUMBER 6 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

NUMBER 6 SEAT TRACK FROM BS 214 TO 446 CORRODED. INSTALLED SEAT TRACK SPLICE AND SECTION OF NEW SEAT TRACK PER SRM 53-05-00 FIGURE 4F.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

CORROSION ON TOP OF RIGHT CUSP ANGLE STATION 147. INSTALLED DOUBLER AND FILLER REPAIR PER AARD 53-20-00-14.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

CORROSION ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 68,192 hrs · 35,963 cycles

AFT SERVICE DOOR OUTER SKIN AT HOLD OPEN HOOK HAS A CRACK EMITTING OUT OF FASTENER HOLE. STOP DRILLED CRACKS AT OUTER SKIN AT HOLD OPEN HOOK AND INSTALLED DOUBLER REPAIR PER SRM 52-05-00 FIGURE 54.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

CORROSION ON NUMBER 3 SEAT TRACK OUTBOARD FLANGE STATIONS 1193 TO 1212. REPLACED NUMBER 3 SEAT TRACK FROM STATIONS 1170 TO 1309 PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

RIGHT CUSP ROTTED THROUGH STATIONS 1162 TO 1166. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

RIGHT CUSP ROTTED THROUGH STATIONS 1183 TO 1186. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 68,192 hrs · 35,963 cycles

THE SECOND FROM OUTBOARD SLAT TRACK ATTACH BRACKET FOR THE LEFT NUMBER 5 LEADING EDGE SLAT IS CRACKED. REPLACED SECOND FROM OUTBOARD POSITION ATTACH BRACKET FOR THE NUMBER 5 LEADING EDGE SLAT PER ESO 80117.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 68,192 hrs · 35,963 cycles

THE OUTBOARD SLAT TRACK BRACKET FOR THE LEFT NUMBER 5 LEADING EDGE SLAT IS CRACKED. REPLACED OUTBOARD POSITION ATTACH BRACKET FOR THE NUMBER 5 LEADING SLAT PER ESO 80117.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,192 hrs · 35,963 cycles

CORROSION ON RIGHT CUSP AT STATION 246. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 67,683 hrs · 35,673 cycles

COUNTERSINK FASTENER HOLE ON VERTICAL STABILIZER, STATION ZFS=52 LEFT LOWER DOUBLER AREA HAS DIVOT ON OUTER CIRCUMFERENCE OF COUNTERSINK. INSTALLED DOUBLER REPAIR PER SRM 55-03-00 FIGURE 31.

Part: SHUTOFF VALVE — CRACKED (HYDRAULIC SYS) · airframe 64,972 hrs · 34,149 cycles

JFK - INFLIGHT ORD-LGA. CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY VERY LOW. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SPOILER SHUT OFF VALVE CRACKED. REPLACED VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,774 hrs · 32,936 cycles

EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR SIDEWALL LOWER AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR SIDEWALL LOWER AREA, OPS CHECK NORMAL.

Part: LIGHT — DAMAGED (SEAT 16D) · airframe 61,868 hrs · 32,451 cycles

EMERGENCY LIGHT AT SEAT ROW 16D IS DAMAGED. REPLACED SHROUD, LENS, AND LAMPS.

Part: CIRCUIT BREAKER — FAILED (COCKPIT) · airframe 61,455 hrs · 32,208 cycles

DFW - CREW REPORTED AFT CENTER FUEL TANK BOOST PUMP POPPED IN CLIMBOUT. EMERGENCY DECLARED, RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE AFT CENTER BOOST PUMP CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — INCORRECT (CABIN) · airframe 61,296 hrs · 32,121 cycles

LGA - LEFT OVERWING PLACARDS AT ROWS 20 AND 21 INCORRECT. REPLACED EMERGENCY EXIT PLACARDS AT ROWS 20 AND 21.

Part: PLACARD — INCORRECT (CABIN) · airframe 61,296 hrs · 32,121 cycles

LGA - RIGHT OVERWING EXITS PLACARDS AT ROWS 20 AND 21 INCORRECT. REPLACED EMERGENCY EXITS PLACARDS AT ROWS 20 AND 21.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,769 hrs · 31,837 cycles

AFT AISLE BATTERY PACK HAS LOW OUTPUT. REMOVED AND REPLACED BATTERY PACK PER AARD 4289.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,769 hrs · 31,837 cycles

FWD AISLE BATTERY PACK AB5-1 LOW OUTPUT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER MM 33-60-98-4.

Part: SKIN — CRACKED (ZONE 100) · airframe 60,769 hrs · 31,837 cycles

CRACK AT FASTENERS LONG 22L STA 188. INSTALLED DOUBLER PER EA 53-006148 DATED 4/28/09.

Part: SHROUD — MISSING (EMERGENCY LIGHTS)

EMERGENCY LIGHT AT SEAT 15D MISSING SHROUD. REPLACED SHROUD. GROUND CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHTS)

EMERGENCY LIGHT AT SEAT 15D MISSING LENS. REPLACED LENS. GROUND CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP. GROUND CHECKED NORMAL.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,595 hrs

LGA EMERGENCY LIGHT AT EXTERIOR OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK CONTROL RELAY FOR EMERGENCY LIGHT AT EXTERIOR OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: VALVE — INOPERATIVE (A/C BAY) · airframe 58,248 hrs

DFW INFLIGHT T1550/17 JUN. RT AIR CONDITIONING SUPPLY TEMPERATURE HIGH INDICATION ON CLIMB. CREW REPORTED AN OVERHEAT SMELL. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE TRANSMITTER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: STRAP — MISSING (FLASHLIGHT)

LGA - UPPER EMERGENCY FLASHLIGHT AT FORWARD ENTRY HAS MISSING STRAP. REPLACED STRAP FOR UPPER EMERGENCY FLASHLIGHT AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OXYGEN MASK — DEPLOYED (CABIN)

DFW INFLIGHT - AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS DURING CLIMB AND PASSENGER OXYGEN MASKS DEPLOYED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALL PASSENGER OXYGEN MASKS AND OXYGEN GENERATORS REPLACED AS NECESSARY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL PANEL — INOPERATIVE (LT AC BUSS)

STL IN FLIGHT LOST LT AC BUSS AND LT GENERATOR. HAD ASSOCIATED AC CROSS TIE LOCKOUT. LT SIDE WAS NOT PICKED UP BY THE RT SIDE. SERVICED LT CONSTANT SPEED DRIVE TO PROPER LEVEL AND CHANGED LT BUSS CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BLADE — FAILED (LT ENGINE)

SWF - INFLIGHT/27JUL LGA TO ORD AT FLIGHT LEVEL 210, CREW HEARD A LOUD BANG FOLLOWED BY AIRCRAFT YAW. LEFT HAND ENGINE EXHAUST GAS TEMPERATURE ROSE TO 700C WITH ENGINE ROLLBACK. LANDED SWF WITHOUT INCIDENT. FOUND COMPRESSOR BLADE FAILURE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — FAILED (NLG)

DEN - UPON GEAR RETRACTION GREEN NOSE GEAR LIGHT REMAINED ON, IT STAYED ON FOR THE ENTIRE FIGHT. REPLACED NOSE LANDING GEAR RETRACT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, BOTH EMERGENCY EXIT CEILING LIGHTS INBOARD OF AFT GALLEY DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT SEAT 7D INOPERATIVE. REPLACED SEAT 7D EMERGENCY EXIT SEAT PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK B5-27 INOPERATIVE. REPLACED B5-27 EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ODOR — DETECTED (CABIN)

SJC - FLT 2464 - EN ROUTE SJC-DFW, DETECTED ELECTRICAL BURNING SMELL IN CABIN AND COCKPIT. RETURNED SJC AND LANDED WITHOUT FURTHER INCIDENT. RAN BOTH ENGINES. NO ODOR OR SMOKE NOTED. REPLACED COALESCER BAGS AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (DUCT)

ACA - FLT 426 - AFTER TAKEOFF, TAIL COMPARTMENT OVERHEAT INDICATOR ILLUMINATED. RETURNED AND LANDED ACA WITHOUT INCIDENT. TIGHTENED HEAT EXCHANGER INLET DUCT CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FIRE CONTROLLER — DEFECTIVE (E/E COMPT)

MCI-ORD - FLT 1546 - AFTER TAKEOFF, APU FIRE WARNING LIGHT FLICKERED ON AND OFF. APU WAS SHUT DOWN AND AIRCRAFT LANDED MCI WITHOUT INCIDENT. REPLACED APU FIRE DETECTION LOOP CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 2. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RETRACT CYLINDER — DEFECTIVE (NLG)

SFO - FLT 802 - AFTER TAKEOFF SFO WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO SFO, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACT CYLINDER. SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUID AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)