N556AA

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,058 hrs · 35,396 cycles

SEVERE LIGHTNING STRIKE STATIC BURNS ON FS SKIN AT STATION 345 BETWEEN LONGERON 26R & 27R IS OUT OF LIMITS. REMOVED DAMAGE & INSTALLED REPAIR DOUBLE IAW SRM 53-04-03.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,721 hrs · 33,473 cycles

CRACK ON TOP CHANNEL AT LONGERON 23 & STATION 200 LT. REPLACED LONGERON SECTION FROM BS 163 TO 218 IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,721 hrs · 33,473 cycles

CRACK ON TOP CHANNEL ON LONGERON 24 AT BS 160 LT. INSTALLED SPLICE & LONGERON REPAIR IAW SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,721 hrs · 33,473 cycles

CRACK ON LONGERON 23 LT AT STATION 200. INSTALLED LONGERON SPLICE IAW SRM 53-02-00.

Part: CSD — FAILED (RT ENGINE) · airframe 61,872 hrs · 31,868 cycles

DFW - CREW REPORTED RIGHT GENERATOR FAILED WITH AUXILIARY POWER UNIT ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,441 hrs · 31,621 cycles

DEEP GOUGE WITH CORROSION AT BOTTOM OF FRAME STATION 1309 BETWEEN LONGERONS 22 AND 23 LEFT. INSTALLED FRAME SPLICE PER SRM 53-03-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 31,413 cycles

THE 1418 CANT FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED REPAIR DOUBLER AND STRAP PER SRM 53-03-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 31,413 cycles

THE 1510 CANT FRAME AT 2 EA TAIL CONE ALIGNMENT PINS ABOVE LEFT LOWER TAIL CONE LATCH CRACKED. STOPPED DRILLED CRACKS AND INSTALLED DOUBLERS PER SRM 53-01-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,541 hrs · 31,146 cycles

AFT EMERGENCY LIGHTS DO NOT TEST. REPLACED AFT BATTERY PACK. OPS CHECK NORMAL.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

CORROSION ON SUBFLOOR AT STATION 216 RIGHT BUTTLINE 12 UNDER G2 MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

FOUND UPPER RIGHT CUSP CRACKED AT STATION 222. INSTALLED NEW CUSP SHEET 218-237 PER AARD 51-10-00-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP CORRODED AT STATION 1169. INSTALLED CUSP REPLACEMENT SHEET AT STATION 1169 TO 1174 PER EA MD80-53-014701.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

NUMBER TWO GALLEY TIE DOWN FITTING HAS CORROSION STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED GALLEY MOUNT AT STATION 218 PER SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

UPPER RIGHT CUSP IS CRACKED AT STATION 222. REPLACED CUSP SHEET PER AARD 53-10-00-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

CORROSION ON OUTBOARD UPPER FLANGE OF NUMBER 5 SEAT TRACK AT STATION 200 TO 218. INSTALLED NEW SECTION OF NUMBER 5 SEAT TRACK STATION 200 TO 247 PER SRM 53-05-00 FIGURE 4F.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

NUMBER ONE GALLEY TIE DOWN FITTING HAS CORROSION AT STATION 160. INSTALLED NEW GALLEY MOUNT PER SRM 51-30-05

Part: MOUNT FITTING — DAMAGED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

GALLEY NUMBER ONE TIE DOWN FITTING ST STATION 160 OUTBOARD FITTING HAS HOLE DRILLED BEYOND MAXIMUM LIMIT PER AARD 53-20-00-19. INSTALLED GALLEY MOUNT PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

CABIN LEFT CUSP CORROSION OUT OF LIMITS AT STATION 597 TO 599. INSTALLED CUSP DOUBLER AT LEFT STATION 598 TO 655 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP CORROSION OUT OF LIMITS STATIONS 1250 TO 1309. REMOVED AND REPLACED CUSP SHEET PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

RIGHT CUSP CORRODED STATION 1174 TO 1250. REMOVED AND REPLACED RIGHT CUSP FROM STATION 1174 TO 1250.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

CORROSION ON CUSP UNDER FORWARD GIRT BAR SUPPORT ANGLE, STATION 1141. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

SUBFLOOR CORRODED, STATION 200 TO 218, BETWEEN SEAT TRACK 5 AND 6. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP CRACKED 3 PLACES BETWEEN STATION 218 AND 237. REMOVED AND REPLACED CUSP SHEET BETWEEN STATION 218 AND 237 LEFT.

Part: OVERLAY — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

CRACK AT OVERLAY AFT OF FORWARD ENTRY DOOR AT STATION 218 LONGERON 15 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP CRACKED STATION 1094. CUT OUT DAMAGE AND INSTALLED DOUBLER PER IAW AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP SHEET STATION 223 DAMAGED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP STATIONS 1084 TO 1098 12 EACH MISDRILLED IN SHEET. CUT OUT DAMAGE AND INSTALLED DOUBLER PER IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

RIGHT CUSP MEMBRANE CRACKED ON BOTTOM SIDE JUST INBOARD OF CUSP T APPROXIMATELY STATION 1307. INSTALLED NEW CUSP SHEET RIGHT STATIONS 1250 TO 1309 PER AARD 51-10-00-5.

Part: OVERLAY — CRACKED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

CRACK AT OVERLAY LEFT FORWARD ENTRY DOOR JAMB AT STATION 218 LONGERON 11 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

LEFT CUSP CORRODED THROUGH AT STATIONS 569 TO 571. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,678 hrs · 29,568 cycles

CORROSION ON SUBFLOOR BELOW G-1 GALLEY DRAIN PAN. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT UPPER CORNER STATION 370 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT AFT UPPER CORNER STATION 1098 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT FORWARD UPPER CORNER STATION 579 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT FORWARD LOWER CORNER STATION 1041 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT AFT UPPER CORNER AT STATION 1155 RIGHT SIDE. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED ALL PER AARD 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,678 hrs · 29,568 cycles

DENT AT STATION 320 ABOVE LONGERON 18 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIGURE 12-B.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN STATION 1117 CRACKED. INSTALLED DOUBLER.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT UPPER FORWARD CORNER AT STATION 886 LEFT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,678 hrs · 29,568 cycles

WINDOW PAN CRACKED AT FORWARD LOWER CORNER AT STATION 1022 RIGHT HAND SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 57,285 hrs · 29,356 cycles

TPA - CREW REPORTED ON CLIMB OUT AT FL 250 LEFT ENGINE EMITTED LOUD BANG, RPM ROLLED BACK TO SUB-IDLE AND EGT BEGAN TO SLOW CLIMB. SHUTDOWN ENGINE AT THAT POINT (SINGLE ENGINE TIME 13 MINUTES). EMERGENCY DECLARED RETURNED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,384 hrs · 28,857 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 55,207 hrs · 28,207 cycles

PORTABLE EMERGENCY LIGHT WILL NOT CHARGE. RELAMPED LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,403 hrs · 27,768 cycles

CREW REPORTED EMERGENCY LIGHTS REMAIN ON AT ALL TIMES FROM ROW 21 TO BACK OF AIRCRAFT. REPLACED OVERHEAD BATTERY AT POSITION NUMBER 1.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,403 hrs · 27,768 cycles

CREW REPORTED EMERGENCY LIGHTS REMAIN ON AT ALL TIMES FROM ROW 21 TO BACK OF AIRCRAFT. REPLACED OVERHEAD BATTERY AT POSITION NUMBER 4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,298 hrs · 27,707 cycles

BATTERY PACK IN CABIN HAS LOW OUTPUT. INSTALLED SERVICEABLE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,298 hrs · 27,707 cycles

BATTERY PACK IN CABIN HAS WEAK OUTPUT. INSTALLED SERVICEABLE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,298 hrs · 27,707 cycles

BATTERY PACK IN CABIN HAS WEAK OUTPUT. INSTALLED SERVICEABLE BATTERY PACK.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 54,015 hrs · 27,552 cycles

A 2.5 INCH CRACK IN LONGERON 2 RIGHT AT STATION 1418. INSTALLED LONGERON AND SPLICE PER AARD 53-30-00-2.

Part: OIL SYSTEM — LEAKING (APU) · airframe 52,364 hrs

INFLIGHT, CREW REPORTED SMOKE IN CABIN AND SMELLED LIKE BURNED RUBBER. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND APU OIL LEAK ON LEFT SIDE WITH INGESTION INTO AIR CONDITIONING SYSTEM. REPLACED APU ON 13 DEC AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · 51,761 cycles

LGA EMERGENCY LIGHT AT SEAT 4D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · 51,761 cycles

LGA EMERGENCY LIGHT AT SEAT 4D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - RIGHT AND LEFT HAND EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-23 FOR FORWARD ENTRY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW SEAT MOUNTED EMERGENCY LIGHT AT 7D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: PUMP — FAILED (LT ENGINE)

ORD - FLT 390 - EN ROUTE ORD-LGA, UPON SWITCHING THE LEFT ENGINE HEAT OFF, THE LEFT ENGINE SHUT DOWN. ENGINE IGNITION WAS IN CONTINUOUS AT THE TIME. LEFT FUEL TEMPERATURE FLUCTUATING ON RETURN TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL PUMP, FUEL CONTROL AND FUEL TEMPERATURE BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION FROM STATION 1160-1207. INSTALLED BEAM PER AARD 53-10-00. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE DOUBLER CRACKED ABOVE Y-DUCT FRAME 1445 AFT SIDE BETWEEN STRINGER 1 AND 3L. REMOVED AND REPLACED DOUBLER PER SRM 51-10-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DENTED TWO PLACES AT RIGHT GROUND FLOOD LIGHT STATION 557 LONGERON 21R. REMOVED INTERNAL DAMAGED PARTS AND INSTALLED REPAIRS PER ESO 80559 DATED 10/7/2002. (M)

Part: STRAP — CORRODED (FUSELAGE)

TUL - FOUND FORWARD GALLEY DOOR CUTOUT LOWER SILL STRAP AND SUBPLATE CORRODED. REMOVED AND REPLACED CORRODED SILL STRAP AND SUBPLATE. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 2L CRACKED AT FRAME 1418, JUST FORWARD OF END FITTING OUTBOARD SIDE. REPAIRED PER AARD 53-30-00-2. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

TUL - FOUND ATTACH ANGLE ON AFT SIDE OF FS 1429 FRAME CRACKED, 10 INCHES TO THE LEFT OF LONGERON 1. INSTALLED NEW ATTACH ANGLE ON AFT SIDE OF FS 1429. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN LIGHTENING HOLE CUT OUT, LOWER SIDE OF CUSP. MADE DOUBLER REPAIR PER SRM 53-01. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND LEFT CABIN WINDOW FRAME CRACKED LOWER FORWARD CORNER STATION 984. INSTALLED DOUBLER ON WINDOW FRAME LOWER FORWARD CORNER STATION 984 IAW 53-10-00-25 PAGE 1/2. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP AT STATION 506. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND LEFT CABIN WINDOW FRAME CRACKED LOWER FORWARD CORNER STATION 1022. INSTALLED DOUBLER ON WINDOW FRAME LOWER FORWARD CORNER STATION 1022, PER 53-10-00-25 PAGE 1/2. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY CABIN LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT INOPERATIVE. SPLICED WIRE ON AFT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DEFECTIVE (NR 3 GALLEY)

MIA-YUL - FLT 470 - AFTER TAKEOFF, SMOKE NOTED FROM NR 3 GALLEY OVEN. GALLEY POWER WAS TURNED OFF IN FLIGHT AND AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 3 GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN MID CABIN INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT FLOOR TRACK LIGHTING CONNECTOR AT SEAT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - FLT 0360 - EMERGENCY EXIT FLOOR PATH LIGHT STRIP TORN LOOSE AT ROW 31. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X)