N424AA

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 87,214 hrs · 47,741 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE MID GALLEY IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — NOT SEATED (CABIN) · airframe 86,871 hrs · 47,501 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS BETWEEN ROWS 12 AND 16 ARE INOPERATIVE. RESEATED BATTERIES IN CHARGER UNIT PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — NOT SEATED (CABIN) · airframe 86,871 hrs · 47,501 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS ABOVE L2 DOOR AND FROM ROW 28 AFT ARE INOPERATIVE. RESEATED BATTERIES ON CHARGER UNITS PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: PROXIMITY SWITCH — DIRTY (CARGO DOOR) · airframe 86,850 hrs · 47,488 cycles

AIRCRAFT WAS NOT GROUNDED. MID CARGO DOOR LIGHT ILLUMINATED AT TAKEOFF. REJECTED TAKEOFF AT APPROXIMATELY 50 KNOTS. CLEANED CARGO DOOR PROXIMITY SWITCH PER AMM 52-70-00. OPERATIONAL CHECK GOOD.

Part: PERISEAL — DEFECTIVE (ZONE 200) · airframe 86,403 hrs · 47,207 cycles

THE AIRCRAFT WAS GROUNDED. AFT TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON DURING CLIMB OUT FL240. MEMORY ITEMS WERE COMPLETED AND THE FLIGHT DECLARED AN EMERGENCY. HIGH TEMP LIGHT WENT OUT AFTER COMPLETING QRH PROCEDURES. REMOVED AND REPLACED RT PACK DUCT CONNECTOR PERI-SEALS PER AMM 21-20-15. OPS AND LEAK CHECK GOOD.

Part: SEAL — DETERIORATED (L1 DOOR) · airframe 86,040 hrs · 46,998 cycles

L1 CABIN DOOR ROUND WINDOW HAS MOISTURE BUILDING UP ON IT. F/A REPORTS IT IS VERY DIFFICULT TO SEE THROUGH AT GATE ARRIVAL. REMOVED AND REPLACED OUTER WINDOW PANE AND SEAL L1 DOOR MM REF 56-30-00. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR AALA201705109019)

Part: SEAL — DETERIORATED (L1 DOOR) · airframe 86,040 hrs · 46,998 cycles

L1 CABIN DOOR ROUND WINDOW HAS MOISTURE BUILDING UP ON IT. F/A REPORTS IT IS VERY DIFFICULT TO SEE THROUGH AT GATE ARRIVAL. REMOVED AND REPLACED INNER WINDOW PANE AND SEAL L1 DOOR MM REF 56-30-00. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR AALA201705119038).

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 85,924 hrs · 46,921 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR LOWER STOP PAD FITTING IS CRACKED AT FORWARD EDGE OF DOOR. INSTALLED NEW DOOR STOP FITTING IAW AARD 51-00-05-1 AND DRAWING 5910141.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 85,924 hrs · 46,921 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. NOSE LANDING GEAR AFT RIGHT DOOR HINGE CUTOUT HAS A SMALL CRACK. REPAIRED IAW SRM 53-05-00, EA 269216, DRAWING 5913421 AND SG09530030.

Part: COVER — LOOSE (SLAT TRACK) · airframe 85,824 hrs · 46,851 cycles

THERE IS A DISTINCT VIBRATION IN BOTH CONTROL WHEELS FROM CRUSE THRU LANDING. LANDING LIGHTS RETRACTED. MAINTENANCE FOUND LOOSE NR 2 SLAT TRACK COVER ON LEFT WING. SECURED COVER. AIRCRAFT WAS GROUNDED.

Part: SENSOR — FAULTY (TAIL COMPARTMENT) · airframe 85,827 hrs · 46,855 cycles

TAIL COMP OVERHEAT LIGHT CAME ON INFLIGHT. LIGHT EXTINGUISHED WHEN PNEUMATIC CROSS FEEDS CLOSED, AIRFOIL ANTI ICE OFF AND A/C SUPPLY HP BLEED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED MCM 36-95-14. REMOVED & REPLACED THE LT & RT TAIL COMPARTMENT OVERHEAT SENSORS. TESTED SENSORS NORMAL IAW AMM 36-20-02. NO LEAKS NOTED. THE AIRCRAFT WAS GROUNDED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 85,602 hrs · 46,710 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BY L1 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: OVERHEAT SENSOR — FAULTY (TAIL) · airframe 84,734 hrs · 46,170 cycles

DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED WORK CARD 36-95-14. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMPERATURE SENSORS IAW AMM 36-20-02.

Part: OVERHEAT SENSOR — FAULTY (TAIL) · airframe 84,734 hrs · 46,170 cycles

DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED WORK CARD 36-95-14. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMPERATURE SENSORS IAW AMM 36-20-02.

Part: BOLT — MISSING (MLG DOOR) · airframe 84,582 hrs · 46,076 cycles

RIGHT MAIN LANDING GEAR INDICATOR UNSAFE (RED) WITH GEAR HANDLE IN THE UP POSITION. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. FOUND LOWER FAIRING FORWARD OF RIGHT HAND GEAR DOOR LOWER AFT LINK BOLT MISSING. INSTALLED NEW BOLT IAW AMM 53-52-00. PSEU AUTOMATIC SYSTEM TEST GOOD PER AMM 32-60-04.

Part: PIN — DISLODGED (L2 DOOR SLIDE) · airframe 84,418 hrs · 45,961 cycles

L2 DOOR EVACUATION SLIDE PACK PINS PULLED OUT ON FORWARD END OF PACK. REMOVED AND REPLACED SLIDE ASSEMBLY IAW MCM CARD 25-94-17.

Part: SWITCH — FAULTY (AC BAY) · airframe 83,601 hrs · 45,478 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, RECEIVED TAIL COMPARTMENT HIGH TEMP INDICATION. ACCOMPLISHED MCM CARD TAIL COMPARTMENT LEAKS CHECK WITH NO LEAKS NOTED. R & R TEMP SWITCHES IAW MCM 36-95-14. ACCOMPLISHED ENG RUNS AT TAKEOFF POWER WITH NO WARNING INDICATIONS RECEIVED. SEE ALSO AALA 20160406014.

Part: SWITCH — FAULTY (AC BAY) · airframe 83,601 hrs · 45,478 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, RECEIVED TAIL COMPARTMENT HIGH TEMP INDICATION. ACCOMPLISHED MCM CARD TAIL COMPARTMENT LEAKS CHECK WITH NO LEAKS NOTED. R & R TEMP SWITCHES IAW MCM 36-95-14. ACCOMPLISHED ENG RUNS AT TAKEOFF POWER WITH NO WARNING INDICATIONS RECEIVED. SEE ALSO AALA 20160408006.

Part: SENSOR — FAULTY (AC BAY) · airframe 81,594 hrs · 44,234 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. RETURNED, ACFT TAIL COMPARTMENT TEMP HIGH LIGHT. DURING TAKEOFF CREW NOTED A TAIL COMPARTMENT TEMP HIGH INDICATION. ACCOMPLISHED TAIL COMPARTMENT LEAK CHECK IAW MCM 36-95-14. R & R PRESS REGULATOR VLV & SENSOR 102-0074. PERFORMED LEAK CHECK IAW MCM 36-95-14 WITH NO LEAKS NOTED. SEE ALSO AALA20150604007.

Part: REGULATOR VALVE — LEAKING (BLEED AIR SYS) · airframe 81,594 hrs · 44,234 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. RETURNED, ACFT TAIL COMPARTMENT TEMP HIGH LIGHT. DURING TAKEOFF CREW NOTED A TAIL COMPARTMENT TEMP HIGH INDICATION. ACCOMPLISHED TAIL COMPARTMENT LEAK CHECK IAW MCM 36-95-14. R & R PRESS REGULATOR VLV & SENSOR 102-0074. PERFORMED LEAK CHECK IAW MCM 36-95-14 WITH NO LEAKS NOTED. SEE ALSO AALA20150608007.

Part: GENERATOR — FAULTY (NR 1 ENGINE) · airframe 80,894 hrs · 43,829 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LT GEN OFF BUS LIGHT & LT CSD OIL PRESS LOW ON CLIMB OUT. REPLACED NR 1 ENG GEN IAW AMM 24-20-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,199 hrs · 43,421 cycles

EMERGENCY EXIT LIGHTS ABOVE RT & LT FWD HATCH DOORS INOPERATIVE. R & R BATTERY PACK. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CRACKS IN SKIN AT FWD SERVICE DOOR CUT OUT, FWD UPPER CORNER. INSTALLED DOUBLER TRIPLER IAW DWG SR09530172.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

CUSP T ANGLE FROM STATIONS 170 TO 180 CORRODED. REMOVED & INSTALLED NEW CUSP T ANGLE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

FASTENER HOLES AT STATIONS 190 TO 195 AT RBL DAMAGED. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 160 TO 200 IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

RIGHT CUSP CRACKED FROM STATIONS 200 TO 224 UNDER SEAT TRACK NR 6. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 IAW SRM 51-30-05, SRM 51-30-02 & DWG 9930538.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

HEAVY CORROSION UNDER GALLEY NR 1 DRAIN PAN. INSTALLED DOUBLER UNDER GALLEY NR 1 DRAIN PAN IAW AARD 53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CORROSION ON DOUBLER ON DIAPHRAGM BY FWD SERVICE DOOR FROM STATIONS 200 TO 218. INSTALLED CUSP DOUBLER FROM STATIONS 200 TO 218, OTBD SEAT TRACK NR 5 IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

GALLEY MOUNT IN FWD END OF NR 6 SEAT TRACK CORRODED. REPLACED NEW GALLEY MOUNT IN FWD END OF NR 6 SEAT TRACK IAW AARD 51-00-05-1.

Part: PAN — WORN (CARGO DOOR) · airframe 78,986 hrs · 42,686 cycles

AFT CARGO DOOR OUTER PAN WORN AT NR 4 BEAM FWD STOP PAD. INSTALLED DOUBLER IAW AARD 52-30-00-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

INTERCOSTAL ON CABIN FLOOR ON CTR LINE FRAME 1287 TO 1309 CRACKED. R & R INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

CABIN SEAT TRACK NR 6 FROM STATIONS 36 TO 367 CORRODED. REPLACED CABIN SEAT TRACK NR 6 FROM STATIONS 36 TO 367 IAW SRM 53-05-00-001 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

SEAT TRACK NR 4 FROM STATIONS 1031 TO 1309 CORRODED. INSTALL NEW SEAT TRACK IAW AARD 51-00-05-1 & AARD 51-00-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

SEAT TRACK NR 1 FROM STATIONS 1174 TO 1309 CORRODED. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-40-01-2.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CRACK IN THE CUSP MEMBRANE AT STATION 164, 2 INCHES RT OF ACFT CENTERLINE APPROXIMATELY 1/2 INCH LONG IN THE INBD & OTBD DIRECTION. INSTALLED DOUBLER IAW EA MD80-53-026939.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 78,986 hrs · 42,686 cycles

RIGHT AFT OVERWING EXIT DOOR CRACKED AT THE NR 12 STOP FITTING. INSTALLED DOUBLER IAW SRM 52-05-00-01.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

GALLEY MOUNT CORROSION FWD END OF SEAT TRACK NR 1 & STATION 1174. INSTALLED NEW GALLEY MOUNT TO SEAT TRACK IAW AARD 51-00-05-1 & DWG 5930566.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 78,986 hrs · 42,686 cycles

RIGHT AFT OVERWING EXIT DOOR CRACKED AT NR 1 STOP FITTING. INSTALLED DOUBLER IAW SRM 52-05-00-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

RIGHT FRAME FOOT AT STATION 200 CORRODED. INSTALLED NEW FRAME FOOT IAW SRM 51-30-05 & SRM 51-30-01.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 78,986 hrs · 42,686 cycles

RIGHT OVERWING EXIT DOOR PAN AT UPPER AFT STOP FITTING CRACKED IN RADIUS. INSTALLED DOUBLER IAW SRM 52-05-00-001 FIGURE 51 & EA COMP-52-035000.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

RIGHT CUSP CRACKED FROM STATIONS 903 TO 905. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 78,986 hrs · 42,686 cycles

LEFT OVERWING EXIT DOOR PAN CRACKED AT FWD UPPER STOP. INSTALLED DOUBLER IAW SRM 52-05-00-01.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 78,986 hrs · 42,686 cycles

LEFT AFT OVERWING EXIT DOOR PAN CRACKED AT AFT UPPER STOP. INSTALLED DOUBLER IAW SRM 52-05-00-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

RIGHT CUSP CRACKED UNDER SEAT TRACK NR 6 AT STATION 804. INSTALLED NEW RT CUSP SHEET FROM STATIONS 788 TO 807 IAW AARD 51-00-05-1, AARD 53-20-00-16 & DAC 9930538.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

CORROSION ON THE LT CUSP INBD OF SEAT TRACK NR 1 & STATION 1176. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

OVERWING FRAME AT STATIONS 886 CRACKED. REMOVED & INSTALLED NEW FRAME.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CORROSION ON WEB FROM STATIONS 1185 TO 1201. INSTALLED NEW WEB SECTION.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CORROSION ON DOOR BEAM WEB FROM STATIONS 1193 TO 1198. INSTALLED NEW STRAP.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

LEFT CUSP CRACKED AT STATION 808 OTBD OF SEAT TRACK NR 1. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

STATION 218 RT CTR GALLEY MOUNT CORRODED. REPLACED MOUNT IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

CORROSION AROUND SEAT TRACK PLUG SEAT TRACK NR 2 AT STATION 1203. REMOVED LIGHT CORROSION & REPLACED PLUG & CHANNEL 7452952-7 IAW AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CRACK IN THE LT CUSP AT STATION 225. INSTALLED NEW CUSP SHEET IAW AARD 53-10-00-5 & AARD 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

AFT CARGO CORROSION ON RT TIE DOWN TRACK Z ANGLE. INSTALLED NEW Z ANGLE IAW AARD 51-00-05-1.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

CRACKED IN SIDE WALL GUSSET AT STATION 207 & LONGERON 15 LT. INSTALLED NEW DOUBLER & FILLER AT FWD ENTRY SIDE WALL GUSSET IAW AARD 53-10-00-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,986 hrs · 42,686 cycles

SEAT TRACK PLUG AT SEAT TRACK NR 6 FROM STATIONS 695 TO 699 CORRODED. REPLACED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: DOUBLER — DEBONDED (FUSELAGE) · airframe 78,986 hrs · 42,686 cycles

LEFT ALTERNATE STATIC PORT DOUBLER DISBONDED. INSTALLED DOUBLER IAW 53-30-00-07.

Part: PORTABLE LIGHT — DAMAGED (CABIN) · airframe 75,616 hrs · 40,717 cycles

FOUND FORWARD PORTABLE EMERGENCY LIGHT LOOSE AND NOT SECURED. FOUND LIGHT ASSEMBLY DAMAGED. REPLACED FORWARD PORTABLE EMERGENCY LIGHT PACK. OPS CHECK NORMAL.

Part: OVEN — OVERHEATED (GALLEY) · airframe 75,616 hrs · 40,717 cycles

IAD - INFLIGHT DCA-DFW. CREW REPORTED FIRST CLASS GALLEY OVEN OVERHEATED CAUSING SMOKE IN CABIN. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. PLACARD FIRST CLASS GALLEY OVEN PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED FORWARD GALLEY OVEN AT AUS ON 02/16/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,960 hrs · 40,350 cycles

CRACK IN CANT FRAME 1497 BELOW RIGHT LOUVER BOX. INSTALLED DOUBLER PER SRM 53-01-00 AND EA MD80-53-026937.

Part: CLAMP — LOOSE (APU) · airframe 74,058 hrs · 39,811 cycles

LAS - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AUXILIARY POWER UNIT EXHAUST SHROUD LEAKING AT BOTH UPPER AND LOWER CLAMP ASSEMBLIES. TIGHTENED CLAMPS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DEBONDED (RT AILERON) · airframe 73,709 hrs · 39,631 cycles

DISBOND ON UPPER SURFACE OF AILERON, 48 INCHES OUTBOARD OF INBOARD END 7 INCHES FORWARD OF TRAILING EDGE. CUT OUT DAMAGED SKIN AND CORE, POTTED IN NEW CORE PLUG, APPLIED GRAPHITE WET LAY-UP PER SRM 51-70-01A, PARAGRAPH 14.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 73,443 hrs · 39,476 cycles

LEFT OVERWING EMERGENCY LIGHT FOUND ON WITH SWITCH OFF.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,933 hrs · 39,193 cycles

ACCIDENTAL IMPACT TO FRAME STATION 207 LONGERON 23 LEFT. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-00-00 AND EA 021460.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,933 hrs · 39,193 cycles

DURING PUSHBACK AIRCRAFT WAS DAMAGED OCCURED TO LEFT FUSELAGE, AFT OF LEFT NUMBER 1 DOOR AT STATION 207, LONGERON 23 LEFT. REPLACED LONGERON PER SRM 53-04 FIGURE 12C AND PRELIMINARY EA3.

Part: CASTING — CRACKED (SPOILER) · airframe 71,690 hrs · 38,485 cycles

RIGHT WING GROUND SPOILER CASTING CRACKED. INSTALLED CASTING PER AARD 51-10-00-5

Part: ENGINE — FAILED (RIGHT) · airframe 70,035 hrs · 37,575 cycles

SAT - CREW REPORTED, HEARD A BANG FROM RIGHT ENGINE AND EGT BEGAN TO RISE. ENGINE WAS SHUT DOWN (SINGLE ENGINE TIME APPROXIMATELY 14 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED SAT LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE AT SAT ON 11/30/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LINE — LEAKING (BRAKE SYSTEM) · airframe 68,883 hrs · 36,922 cycles

DFW - DURING TAXI IN AFTER LANDING, CREW WAS CONTACTED BY A PASSING AIRCRAFT THAT THE BRAKES APPEARED TO BE SMOKING. CREW NOTED RIGHT HYDRAULIC FLUID QUANTITY HAD DROPPED TO ALMOST ZERO. FOUND NUMBER 1 BRAKE FORWARD BRAKE LINE LEAKING AROUND QUICK CONNECT. REPLACED HOSE AND QUICK CONNECT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CASTING — CRACKED (SPOILER) · airframe 67,879 hrs · 36,346 cycles

LEFT WING TRAILING EDGE CRACKED IN FORWARD INBOARD CORNER OF GROUND SPOILER ACTUATOR MOUNT CASTING. REPLACED LEFT GROUND SPOILER ACTUATOR CASTING PER BOEING DRAWING 5936832.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

FRAME 1322 DAMAGED. INSTALLED SPLICE REPAIR PER SRM 53-03-00 FIGURE 2A.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

LEFT CARGO TIE DOWN TRACK CORRODED. REMOVED AND REPLACED TRACK PER SRM 53-01-01.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

DAMAGE ON FRAME 1309. INSTALLED SPLICE REPAIR PER SRM 53-03-00 FIGURE 2A.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

LEFT TIE DOWN TRACK HAS CORROSION STATION 1250. INSTALLED LEFT TIE DOWN TRACK FROM STATION 1220 TO 1322 AND TRACK SPLICE AT STATION 1220 PER SRM 51-30-01 AND 51-30-05.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

LONGERON 29 LEFT AT STATION 1322 HAS CORROSION. REPLACED LONGERON PER SRM 53-04 FIGURE 38 VIEW G.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

SHEAR TIE AFT SIDE STATION 1322 BETWEEN LONGERON 29 LEFT AND LONGERON 29 RIGHT HAS CORROSION. INSTALLED SHEAR TIE AT STATION 1322 BETWEEN LONGERON 29 AND LONGERON 29 RIGHT PER SRM 53-04 FIGURE 38 VIEW G.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

AFT CARGO DOOR LOWER JAMB AT STATION 1200 SKIN PUSHED UP AT CORNER. COMPLETED INSTALLATION OF QUADRUPLER PER EAMD80-008877.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

LONGERON 3 LEFT CRACKED AT STATION 160. INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

LONGERON 4 LEFT CRACKED AT STATIONS 160 TO 200. INSTALLED NEW SECTION OF LONGERON FROM STATIONS 148 TO 225.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

LOWER FORWARD CORNER BRACKET HAS CORROSION IN DOOR OPENING. REMOVED AND REPLACED BRACKET PER SRM 51-01-00-2 AND 51-30-05.

Part: CASTING — CRACKED (WING) · airframe 67,879 hrs · 36,346 cycles

FOUND PULLEY BRACKET SUPPORT CASTING CRACKED ON FORWARD WING SPAR. REMOVED CASTING PER SRM 51-01.

Part: PAN — WORN (CARGO DOOR) · airframe 67,879 hrs · 36,346 cycles

HANDLE PAN ON CARGO DOOR HAS DEEP WEAR. REMOVED DAMAGED HANDLE PAN, DRILLED AND INSTALLED NEW HANDLE PAN PER ESO 80174.

Part: SKIN — DENTED (LE SLAT) · airframe 67,879 hrs · 36,346 cycles

RIGHT NUMBER THREE SLAT DENTED 22 INCHES FORM OUTBOARD END OF LEADING EDGE. REWORKED DENTED AREA BACK TO ORIGINAL CONTOUR AND NO CRACKS FOUND UNDER ESO 80117.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 67,879 hrs · 36,346 cycles

FORWARD CARGO DOOR HAS CRACKED ANGLE INSIDE UNDER STRAP. REPLACED CRACKED ANGLE UNDER ESO 80174.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 67,879 hrs · 36,346 cycles

CRACK FOUND IN CABIN FORWARD ENTRY DOOR IN CENTER OF NUMBER 6 BEAM AT FASTENER HOLE. INSTALLED DOUBLER AT NUMBER 6 BEAM OF FORWARD ENTRY DOOR PER ESO 80172.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

CRACK IN RIGHT CUSP, THREE INCHES INBOARD OF CUSP TEE STATION 842. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

DENT AND SEVERAL SCRATCHES ON RIGHT SIDE OF FUSELAGE, AT LONGERON 20, STATION 285. BLENDED SCRATCHES AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIGURE 38, SHEET 20.

Part: RIB — CRACKED (RT WING) · airframe 67,879 hrs · 36,346 cycles

CRACK FOUND ON RIGHT WING NUMBER FIVE SLAT OUTBOARD SLAT RIB BY HIGH FREQUENCY EDDY CURRENT INSPECTION. REPLACED CRACKED OUTBOARD MOST ATTACH RIB NUMBER 5 RIGHT HAND SLAT PER ESO 80117.

Part: RIB — CRACKED (RT WING) · airframe 67,879 hrs · 36,346 cycles

CRACK FOUND ON RIGHT WING NUMBER 5 SLAT 2ND OUTBOARD END SLAT RIB BY HIGH FREQUENCY EDDY CURRENT INSPECTION. REPLACED CRACKED ATTACH RIB 2ND FROM OUTBOARD NUMBER 5 RIGHT SLAT PER ESO 80117.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,879 hrs · 36,346 cycles

NUMBER 6 SEAT TRACK INSIDE TRACK CORROSION. REMOVED CORROSION FOUND SEAT TRACK TO BE OUT OF LIMITS. INSTALLED SEAT TRACK REPAIR PLUG PER 53-05 FIG 4A.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

HOLE IN SUBFLOOR 13 INCHES INBOARD OF FORWARD ENTRY DOOR STATION 200. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

AFT CABIN BULKHEAD DOOR JAMB CENTER BRACKET CRACKED LEFT HAND SIDE. REMOVED AND REPLACED BRACKET PER SRM 51-01.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

RIGHT AFT UPPER WINDOW PAN CRACKED AT STATION 1041. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

AFT BULKHEAD DOOR JAMB CENTER DOOR BRACKET CRACKED ON RIGHT SIDE. REMOVED AND REPLACED BRACKET PER SRM 51-01.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

RIGHT LOWER WINDOW PAN CRACKED AT STATION 1136. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

LEFT WINDOW PAN CRACKED AT UPPER CORNER STATION 1079. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: DIAPHRAGM — CRACKED (FUSELAGE) · airframe 67,879 hrs · 36,346 cycles

DIAPHRAGM SKIN CRACKED AT STATION 200 LEFT, LONGERON 11 LEFT AT DOOR JAMB TAB STA. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,801 hrs

LGA - FORWARD GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

LGA EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8 FOR EMERGENCY LIGHTS AT FORWARD CABIN.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 65,214 hrs

LGA - EMERGENCY LIGHTS AT FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT OVERHEAD AFT FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD AFT FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS FROM FIRST CLASS TO ROW 20 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF FOR EMERGENCY LIGHTS FROM FIRST CLASS TO ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHX - EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING INOPERATIVE. REPLACED BATTERY PACK B523 FOR EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL MODULE — FAILED (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 21 TO THE TAIL INOPERATIVE WHEN THE EMERGENCY LIGHT SWITCH IS IN THE ON POSITION. REPLACED THE BATTERY PACK AND CONTROL MODULE AB5-4 FOR THE EMERGENCY PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 20D, 21D AND 28D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT 20D, 21D, AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — LEAKING (NR 1)

EN ROUTE SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. AIRCRAFT DIVERTED TO AMA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT AND CREASE IN SKIN ABOVE LONGERON 22L, STATION 400 (ADL). CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-00 VIEW H. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED FROM FASTENER HOLE STATION 1380, 19 INCHES ABOVE ENGINE, LEFT ENGINE PYLON. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 (SHEET 3). (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR CUTOUT LOWER BEAM HAS HEAVY CORROSION STATION 1165 TO 1211. REMOVED CORRODED DOOR BEAM AND INSTALLED NEW ONE PER SRM 51-01. ALSO INSTALLED/SPLICED IN NEW WEB SECTION (PREVIOUSLY REPAIRED) PER AARD 53-10-00-24 ON E58 NR 4042956. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LONGERON 11L AT STATION 579. INSTALLED DOUBLER IN LONG 11L AT STATION 579 AND APPROX 13 INCH LONGERON 11 PER SRM 53-02 FIG 3. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 2L CRACKED JUST AFT OF STATION 1418. REPAIRED LONGERON 2L PER AARD 53-30-00-2. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CRACKED APPROXIMATELY AT STATION 1280. REPLACED SEAT TRACK FROM STATION 1171 TO 1307 LEFT SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1203-1205. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - FOUND WEAR MARK ON FRAME 1401 AT L15L. BLENDED OUT WEAR, INSTALLED DOUBLER PER AARD 53-10-00-14. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND LEFT INTERCOSTAL CRACKED AT STATION 988 ON BOTTOM OF KEEL BEAM LBL 4.5 INCH IN UPPER BEND RADIUS. REPLACED LEFT INTERCOSTAL AT STATION 988 AS PER SRM 51-01. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGE IN FUSELAGE AT L19L STATION 223. INSTALLED DOUBLER PER SRM 53-04 FIG 38, VIEW E. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CREASE IN FUSELAGE SKIN STATION 408 BETWEEN L29R AND L30. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: BELTFRAME — CHAFED (FUSELAGE)

TUL - FOUND BELL FRAME HAS DEEP CUT, RUB MARK STATION 522 AT LONGERON L6. BLENDED OUT DAMAGE AD INSTALLED DOUBLER REPAIR PER 53-10-00-14 FIG 1. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED AT STATION 1103. CUT OUT CRACKED AREA DYE CHECKED TO CONFIRM CRACK. REMOVAL AND INSTALLED DOUBLER PER SRM 53-30. (M)

Part: LIGHT — INOPERATIVE (SEAT 5)

LAX - DURING OVERNIGHT MAINTENANCE, L2 EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. REPLACED L2 EMERGENCY EXIT LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ENGINE — MALFUNCTIONED (RIGHT)

PHX - FLT 1267 - EN ROUTE DFW-LAX, RIGHT ENGINE LOW OIL PRESSURE ILLUMINATED. OIL QTY READ ZERO. SHUT ENGINE DOWN. CREW DECLARED EMERGENCY AND LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED NUMBER 6 PUMP CARBON SEAL ASSEMBLY AND BEARING ASSEMBLY AS A PRECAUTION AND REPLACED MAIN ENGINE OIL FILTER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: BOLT — FAILED (SPOILER)

TUL - FOUND THE GRUOND SPOILER MOUNT BOLT WAS FOUND SHEARED. HALF OF THE BOLT WAS STILL ATTACHED, THE OTHER HALF WAS LAYING ON THE PANEL UNDER ACTUATOR. REPLACED BOLT PER MM 27-62-02-2. (M)

Part: WINDOW — DEFECTIVE (LT COCKPIT)

IAD- FLT 731 - EN ROUTE DCA- ORD SHORTLY AFTER TAKEOFF, NOTED ELECTRICAL/BURING WIRE TYPE FUMES IN THE COCKPIT. FUMES BECAME STRONGER AFTER APPROXIMATELY TWO MINUTES IN FLIGHT. FLIGHT ATTENDANTS REPORTED FUMES IN REAR OF AIRCRAFT UPON GATE ARRIVAL. AIR INTERRUPTED AND LANDED IAD WITHOUT INCIDENT. REPLACED CAPTAINS CLEAR VIEW WINDOW, RAN PACKS NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY AISLE AND OVERWING EMERGENCY EXIT LIGHTS MID-CABIN WERE INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY AND AS A PRECAUTIONARY, REPLACED BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ENGINE — FAILED (RIGHT)

SWF - FLT 1339 - AFTER TAKEOFF SWF, DURING INITIAL CLIMB-OUT, SMOKE NOTED IN CABIN AND COCKPIT. ACCOMPLISHED ABNORMAL PROCEDURES AND SMOKE CLEARED WHEN LEFT PACK TURNED OFF. AIRCRAFT RETURNED TO SWF AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT PROCEDURE AND OIL NOTED IN RT ENGINE BLEED CAPS. AIRCRAFT MAINTENANCE FERRY SWF/LGA. REPLACED RT ENGINE DUE TO OIL LEAK. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (TAIL CONE)

DFW - DURING OVERNIGHT CHECK, FORWARD OVERHEAD EMERGENCY LIGHT IN TAIL CONE AREA FOUND INOPERATIVE. REPAIRED BROKEN OVERHEAD EMERGENCY LIGHT WIRE AT LIGHT ASSEMBLY CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)