N581AA

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,882 hrs · 34,966 cycles

EMERGENCY LIGHTS IN AFT OF CABIN WONT TEST. REPLACED POWER SUPPLY B5-27.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,725 hrs · 34,262 cycles

RIGHT SHEAR TIE AT STATION 1437 FOUND CRACKED AT LONGERON 2. REPLACED SHEAR TIE ASSEMBLY IAW AARD 51-00-05-1.

Part: RIB — CRACKED (RT WING) · airframe 65,668 hrs · 34,228 cycles

CRACK IN RT WING NR 4 SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR FITTING & HAT BUSHING.

Part: RIB — CRACKED (LT WING) · airframe 65,668 hrs · 34,228 cycles

CRACK IN THE LT WING NR 4 SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR FITTING.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 62,647 hrs · 32,478 cycles

CREW REPORTED STRONG ODOR DURING. EMERGENCY DECLARED FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPAIRED HYD LEAK AT NOSE GEAR STEERING LINE IN MID CARGO COMPARTMENT. SYS GROUND CHECK NORMAL OPERATION.

Part: BALLAST — FAILED (CABIN) · airframe 61,216 hrs · 31,688 cycles

ORD - CREW REPORTED LEFT OVERHEAD LIGHT BALLAST BEHIND ROW 8AB FAILED WITH FUMES AND ELECTRICAL SMELL. PER EMERGENCY PROCEDURE, PULLED CIRCUIT BREAKERS L6, J7, L19, L20, L21 AND F6. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT OVERHEAD LIGHT BALLAST. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (RIGHT) · airframe 60,909 hrs · 31,506 cycles

LIT - INFLIGHT DFW-IND. CREW REPORTED RIGHT ENGINE LOW OIL PRESSURE, ZERO OIL QUANTITY AND OIL TEMP AT 170 DEGREES. CAPTAIN PERFORMED INFLIGHT SHUTDOWN OF RIGHT ENGINE (SINGLE ENGINE TIME 25 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT LIT ON 10/05/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 59,954 hrs · 30,960 cycles

CEILING EMERGENCY LIGHTS ABOVE ROW 30D MISSING LENS. REPLACED LENS FOR CEILING EMERGENCY LIGHT ABOVE ROW 30D. OPS CHECK NORMAL.

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 58,675 hrs · 30,245 cycles

CENTER CEILING EMERGENCY LIGHT JUST FORWARD OF AFT BULKHEAD DOOR INOPERATIVE. RE-SECURED BATTERY PACK AT OVERHEAD CEILING PANEL AFT CABIN ROW 26. OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 58,675 hrs · 30,245 cycles

AFT ESCAPE PATH LIGHT AT SEAT 28D INOPERATIVE. RE-SECURED CONNECTOR AT SEAT 28A. OPS CHECKS NORMAL.

Part: SENSOR — FAILED (NLG) · airframe 58,359 hrs · 30,067 cycles

ORD - INFLIGHT IND-DFW. CREW REPORTED ON TAKEOFF NOSE GEAR DOOR OPEN LIGHT ILLUMINATED. ACCOMPLISHED QRH ALL OTHER INDICATIONS SEEMED NORMAL. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED D1-32 SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

CORROSION ON AFT SIDE OF FRAME, STATION 1231, LONGERON 29 LEFT AND RIGHT. ACCOMPLISHED REPAIR PER AARD 53-10-00-17.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

RIGHT CUSP MEMBRANE CORROSION BEYOND LIMITS. DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

CORROSION ON RIGHT CUSP AT STATION 1305. INSTALLED NEW RIGHT CUSP SHEET FROM STATIONS 1250 TO 1309 PER AARD 51-10-00-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

DEEP BLENDED AREA IN FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER AARD MD80-53-019058, DATED 09/08/11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

BOTTOM OF LEFT CUSP STATION 1287 HAS HEAVY CORROSION. REMOVED CUSP SHEET FROM STATIONS 1250 TO 1309 AND INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

CORROSION IN CENTER OF LONGERON 28 LEFT, STATION 1289. INSTALLED U-CHANNEL PER SRM 53-02-00 FIGURE 19.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

LEFT CUSP STATION 1144 CORRODED. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

CORROSION ON LEFT CUSP STATION 1164. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

CORROSION IN CTR OF LONGERON 29 LEFT, STATION 1289. INSTALLED U-CHANNEL PER SRM 53-02-00 FIGURE 19.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

CRACK IN LEFT CUSP SHEET STATION 1245. DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

CORROSION ON AFT SIDE OF FRAME, LONGERON 30, STATION 1250. INSTALLED J-ANGLE REPAIR PER AARD 53-10-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

CORROSION ON BOTTOM OF LEFT CUSP, STATION 1088. REMOVED CUSP SHEET AND INSTALLED NEW SHEET AT STATIONS 1079 TO 1098 PER BOEING DRAWING SG09530019.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

SMALL HOLE IN RIGHT CUSP STATION 570. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

DOUBLER AT STATION 239 LONGERONS 17 TO 18 LEFT DAMAGED. INSTALLED NEW DOUBLER, FILLER, FINGER DOUBLER, LOWER FILLER AND EXTERNAL REPAIR STRAP PER SRM 53-04-05 FIGURE 2 SHEET 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

WEBBING CRACKED STATION 208 LONGERON 11 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

WEBBING CRACKED STATION 208 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

FLOOR BEAM DAMAGED, LOWER SIDE, STATION 665, 1 INCH RIGHT OF CENTER LINE. BLENDED OUT DAMAGE ON LOWER SIDE OF FLOOR BEAM AT STATION 665 1 INCH RIGHT OF CENTER LINE AND INSTALLED DOUBLER PER AARD53-20-00-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,161 hrs · 29,957 cycles

SEAT TRACK NUMBER 3 AT STATION 1201 AT INBOARD FLANGE OUT OF LIMITS. INSTALLED REPAIR PLUG PER SRM 53-05-00 FIGURE 4A.

Part: PAN — CRACKED (WINDOW) · airframe 58,161 hrs · 29,957 cycles

AFT LOWER WINDOW PAN TAB CRACKED RIGHT STATION 1060. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 58,161 hrs · 29,957 cycles

AFT UPPER WINDOW PAN TAB CRACKED RIGHT STATION 1060. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,161 hrs · 29,957 cycles

AFT UPPER WINDOW PAN TAB CRACKED RIGHT STATION 1079. INSTALLED NEW DOUBLER PER AARD 53-10-00-25.

Part: STRUT — LOW (NLG) · airframe 56,571 hrs · 29,052 cycles

DFW - CREW REPORTED NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. GEAR HANDLE WAS LOWERED AND NORMAL THREE GREEN WITH LANDING. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR SHORT SEALS AND ACCOMPLISHED NOSE LANDING GEAR STRUT REPACK. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 55,867 hrs · 28,682 cycles

JFK - INFLIGHT LGA-DFW. CREW REPORTED SMOKE AND ODOR IN THE CABIN. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIRY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 54,458 hrs · 27,870 cycles

3 STOP PAD FITTINGS CRACKED ON AFT CARGO DOOR. REPLACED FITTINGS.

Part: SUPPORT ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 54,458 hrs · 27,870 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL FRETTING CORROSION ON SUPPORT ANGLE ABOVE ACCUMULATOR. INSTALLED CHORD ANGLE PER SRM 51-30-1.

Part: CIRCUIT BREAKER — TRIPPED (FUEL SYSTEM) · airframe 53,854 hrs · 27,540 cycles

DFW - CREW REPORTED LEFT AFT FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED. LEFT FORWARD FUEL BOOST PUMP ON PLACARD. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET AFT LEFT FUEL CIRCUIT BREAKER AND REPLACED LEFT FORWARD FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,316 hrs · 27,237 cycles

EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 DIM. REPLACED BATTERY PACK.

Part: LENS — DAMAGED (CABIN) · airframe 53,316 hrs · 27,237 cycles

SEAT 7D EMERGENCY PATH LIGHT LENS DAMAGED. REPLACED LENS AND CHECKS NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 52,217 hrs

LGA - LEFT NUMBER ONE DOOR EMERGENCY LIGHT WILL NOT SHUT OFF. REPLACED LEFT NUMBER ONE DOOR EMERGENCY LIGHT ASSEMBLY.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 52,203 hrs

LGA PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT.

Part: CONNECTOR — CORRODED (CABIN) · airframe 51,964 hrs

PHL - FORWARD ZONE SEATS 3 TO 19 INOPERATIVE. REPLACED CORRODED CONNECTORS FOR LIGHT ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,964 hrs

PHL - FORWARD ZONE SEAT 3 TO 19 INOPERATIVE. REPLACED BATTERY AT CONTROL MODULE AB5-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,470 hrs · 25,594 cycles

TUL - SKIN CRACKED AT CANTED FRAME IN AFT FUSELAGE AT STATION 1474. LENGTH OF CRACK IS 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 53 01 00.

Part: FRAME — CRACKED (TAILCONE) · airframe 50,470 hrs · 25,594 cycles

CANTED FRAME IN AFT ACCESSORY AT TAIL CONE ALIGNMENT PIN BELOW MAINTENANCE LIGHT SWITCH WAS CRACKED. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 30 SEP 2008.

Part: FRAME — CRACKED (TAILCONE) · airframe 50,470 hrs · 25,594 cycles

CANTED FRAME CRACKED AT TAIL CONE ALIGNMENT PIN AT 9 O`CLOCK POSITION. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 30 SEP 2008.

Part: APU — LEAKING · airframe 49,278 hrs

JFK INFLIGHT T2275/02MAY LGA TO BNA - CREW REPORTED SMOKE IN CABIN AND COCKPIT. DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION AND REPAIR. FOUND AUXILLIARY POWER UNIT (APU) LEAKING OIL. REPLACED APU ON 04 MAY AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,081 hrs

LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5102 FOR CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - COCKPIT, FORWARD ENTRANCE, AND SERVICE ENTRANCE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B523 FOR COCKPIT, FORWARD ENTRANCE AND SERVICE ENTRANCE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414 ARE INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B5100 FOR CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS IN CEILING AT ROW 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING AT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING INOPERATIVE, ON CEILING AT SEAT ROWS 16 THROUGH 22. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE ON THE AFT CEILING. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (TAIL CONE)

DURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED TAIL CONE EMERGENCY EXIT LIGHT BATTERY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (R1 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (MLG)

SAT - FLT 1636 - DURING TAKEOFF ROLL, MAIN LANDING GEAR WHEEL NOT TURNING ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. RESECURED LOOSE CONNECTOR TO NR 1 MAIN LANDING GEAR ANTI-SKID TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — PUNCTURED (RT WING)

TUL - FOUND HOLE DAMAGED FOR NR 3 ACCESS PLATE BOTTOM OF RT WING (SCREW HOLE). CLEANED UP HOLE (MADE ROUND). INSTALLED PLUG PER ESO 80559. (M)

Part: SKIN — PUNCTURED (BS 1433)

TUL - FOUND HOLE IN FUSELAGE SKIN 18 INCHES UP FROM AFT STAIR CUT OUT RIGHT SIDE STATION 1433. CUT OUT DAMAGE. INSTALLED FLUSH REPAIR PER SRM 53-40 FIG 1. (M)

Part: SKIN — DAMAGED (BS 237)

TUL - FOUND DENT/CREASE IN SKIN AND FRAME STRUCTURE .39 INCHES AFT OF FORWARD ENTRY, BELOW RED STRIPE, BETWEEN LONGERON 17L AND 18L, STATION 237. REMOVED DAMAGED AREA. INSTALLED FLUSH PLUG AND FINGER DOUBLER PER SRM 53-04 FIG 38. (M)

Part: LONGERON — CRACKED (BS 1418)

TUL - FOUND CRACK IN LONGERON 2R AFT OF STATION 1418, ROUTED OUT TO .5 BY .25 PER ESO 80559, DATED 4/3/98. INSTALLED REPAIR PER AARD 53-30-00-2, LONGEORN SPLICE. (M)

Part: ACTUATOR — DEFECTIVE (NLG)

PHX - FLT 1538 - AFTER TAKEOFF, GEAR FAILED TO RETRACT. CREW ACCOMPLISHED CHECKLISTS AND RETURNED PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR RETRACT ACTUATOR. ACCOMPLISHED EXTENSION AND RETRACTION CHECKS AND LEAK CHECKS WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — DEFECTIVE (NLG)

PHX - FLT 1538 - AFTR TAKEOFF, GEAR FAILED TO RETRACT. CREW ACCOMPLISHED CHECKLISTS AND RETURNED PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR OVER CENTER ACTUATOR. ACCOMPLISHED EXTENSION AND RETRACTION CHECKS AND LEAK CHECKS WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CYLINDER — DEFECTIVE (RT MLG)

SFO - FLT 1917 - UPON ARRIVAL SFO, NECESSARY TO RECYCLE GEAR THREE TIMES TO GET DOWN AND LOCKED INDICATION. REPLACED RIGHT MAIN LANDING GEAR BUNGEE CYLINDER. ACCOMPLISHED GEAR SWING WITH NO PROBLEMS NOTED. LEAK CHECKED OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT — REQ'D SERVICE (NLG)

ORD - FLT 1025 - AFTER TAKEOFF, HAD TO CYCLE GEAR TO GET NOSE LANDING GEAR LIGHT TO EXTINGUISH. SERVICED GEAR WITH FLUID AND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRUT — REQ'D SERVICING (NLG)

ORD - FLT 267 - ON TAKEOFF ORD, NOSE GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED STRUT, LUBRICATED GEAR. ACCOMPLISHED GEAR RETRACTION CHECK SEVERAL CYCLED WITH NO DEFECTS, COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)