N962TW

Part: COVER — CRACKED (DOOR SLIDE) · airframe 51,381 hrs · 25,580 cycles

FORWARD GALLEY SLIDE IS MISSING, REPORTEDLY IT FELL OUT WHEN CATERING OPENED THE DOOR. THE SLIDE WAS LOCATED AND FOUND PARTLY DEPLOYED. THE DOOR SLIDE COVER IS CRACKED, INSPECTION PORT LOOSE, DOOR IS UNSERVICEABLE. THE SLIDE DOOR COVER WAS REMOVED. REPLACED THE COVER.

Part: SLIDE — DETACHED (GALLEY DOOR) · airframe 51,381 hrs · 25,580 cycles

FORWARD GALLEY SLIDE IS MISSING, REPORTEDLY IT FELL OUT WHEN CATERING OPENED THE DOOR. SLIDE LOCATED AND IS PARTLY DEPLOYED AND IS UNUSEABLE. DOOR SLIDE COVER IS CRACKED, INSPECTION PORT LOOSE, DOOR IS UNSERVICEABLE. SLIDE DOOR COVER REMOVED. REPLACED R1 SLIDE.

Part: BATTERY PACK — INOPERATIVE (PORTABLE LIGHT) · airframe 51,309 hrs · 25,541 cycles

PORTABLE EMERGENCY LIGHT DIM. REPLACED PORTABLE LIGHT BATTERY PACK IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,307 hrs · 25,540 cycles

EMERGENCY LIGHT INOPERATIVE IN AFT TAIL CONE AREA. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: APU — LEAKING (ZONE 300) · airframe 50,830 hrs · 25,223 cycles

AIRCRAFT WAS GROUNDED. SMOKE IN CABIN ACCOUNT AUXILIARY POWER UNIT OIL INGESTION. APU PLENUM DRAIN AT APU AIR INLET BLOWING SMOKE WHICH IS BEING SUCKED INTO APU INLET. REMOVED AND REPLACED APU PER MCM CARD 49-96-83. ACCOMPLISHED PACK BURN PER MCM CARD 21-92-12. OPERATIONAL CHECK GOOD.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 50,103 hrs · 24,783 cycles

THE AIRCRAFT WAS GROUNDED. FOUND R1 DOOR ESCAPE SLIDE IN JETWAY. SLIDE WAS NOT DEPLOYED. REPLACED R1 DOOR ESCAPE SLIDE IAW JOB CARD 25-94-20.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 50,082 hrs · 24,770 cycles

STRONG HYD FLUID SMELL IN CABIN. FLIGHT ATTENDANTS REPORTED CABIN FILLING WITH SMOKE AND FUMES. TURNED PACKS OFF AND DECLARED EMERGENCY. SMOKE FUMES SEEMED TO START TO DISSIPATE. MAINTENANCE FOUND RT ENGINE PRESSURE TO PYLON HYDRAULIC LINE LEAKING. REMOVED AND REPLACED RT HYD LINE AND UNION IAW AMM 20-12-03. REPLACED APU DUE TO HYDRAULIC FLUID INGESTION IAW MCM 49-96-83. PERFORMED PACK BURN IAW MCM 21-92-12. THE AIRCRAFT WAS GROUNDED.

Part: FITTING — CRACKED (LT SPOILER) · airframe 49,675 hrs · 24,516 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT WING GROUND SPOILER CASTING CRACKED INNER WING UPPER TRAILING EDGE AT WING STATION 95. REMOVED AND REPLACED SPOILER FITTING IAW SRM 51-30-02, SRM 51-30-05 AND AMM 27--62-01.

Part: ACM — FAULTY (AC BAY) · airframe 49,564 hrs · 24,446 cycles

AIRCRAFT WAS GROUNDED. DURING CLIMB, THE CREW REPORTED THE AUTO PRESSURIZATION SYSTEM FAILED. NO EMERGENCY DECLARED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. PRESSURIZATION FLOW LIGHT ILLUMINATED AT FL 30000 WITH CRUISE POWER (300-400 FPM). GOOD PACKS, GOOD FLOW, REMAINING CONTROLLER WOULD NOT FULLY COMPLY UNTIL BELOW 12000 AIRCRAFT ALTITUDE, OUTFLOW VALVE FULLY CLOSED. REMOVED AND REPLACED LEFT AND RIGHT COOLING TURBINE ASSEMBLIES. OPERATIONAL CHECK GOOD. SEE ALSO AALA201703209045

Part: ACM — FAULTY (AC BAY)

AIRCRAFT WAS GROUNDED. DURING CLIMB, THE CREW REPORTED THE AUTO PRESSURIZATION SYSTEM FAILED. NO EMERGENCY DECLARED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. PRESSURIZATION FLOW LIGHT ILLUMINATED AT FL 30000 WITH CRUISE POWER (300-400 FPM). GOOD PACKS, GOOD FLOW, REMAINING CONTROLLER WOULD NOT FULLY COMPLY UNTIL BELOW 12000 AIRCRAFT ALTITUDE, OUTFLOW VALVE FULLY CLOSED. REMOVED AND REPLACED LEFT AND RIGHT COOLING TURBINE ASSEMBLIES. OPERATIONAL CHECK GOOD. SEE ALSO AALA20170314007.

Part: SEAL — UNSERVICEABLE (L1 DOOR) · airframe 49,563 hrs · 24,445 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR PORT WINDOW FOGGED OVER AND OBSTRUCTS VISION. REMOVED AND REPLACED WINDOW SEAL IAW AMM 56-30-00. LEAK AND OPERATIONAL CHECK GOOD.

Part: RETAINER — DETACHED (GIRT BAR) · airframe 49,546 hrs · 24,430 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR RETAINING ANGLE IS DETACHED. INSTALLED RETAINING ANGLE IAW AMM 52-41-01 AND SRM 51-03-00 AND 51-30-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,421 hrs · 24,356 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND SIDE SKIN STATION 1474 BETWEEN STRINGER 25L AND 29L. REPAIRED SKIN IAW SRM 53-01-00-001 AND AARD 53-10-00-15.

Part: UNKNOWN — HAZE (CABIN) · airframe 49,420 hrs · 24,355 cycles

AIRCRAFT WAS GROUNDED. HAZE APPEARED IN CABIN PRIOR TO GATE DEPARTURE. PACK BURN IAW WORK CARD 21-92-12. NO HAZE NOTED. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 48,947 hrs · 24,069 cycles

AIRCRAFT NOT GROUNDED. AFT LEFT OVERWING EMERGENCY EXIT LIGHT AT ROW 21A HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER. OPERATIONAL CHECK GOOD.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 48,873 hrs · 24,024 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE PACK DETACHED FROM SLIDE COVER. SECURED SLIDE IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 48,854 hrs · 24,011 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 22D IS INOPERATIVE. FOUND BROKEN WIRE ON SEAT MOUNTED EMERGENCY PATH MARKING WIRE HARNESS. REMOVED AND REPLACED HARNESS IAW SWPM 20-10-01. EMERGENCY PATH MARKING OPERATIONAL CHECK GOOD IAW AMM 33-60-98.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,854 hrs · 24,011 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST CLASS CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.

Part: DUCT — DEFECTIVE (ZONE 100) · airframe 47,722 hrs · 23,324 cycles

DURING DESCENT, HAZE ACCOMPANIED BY AN ELEC ODOR WAS REPORTED IN THE FWD CABIN AREA CONCENTRATED AT ROW 5B. PAX ENTERTAINMENT SYS WAS DE-ACTIVATED & QRH COMPLIED WITH. HAZE DISSIPATED. AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM 21-96-01 & FOUND A DEFECTIVE FWD CARGO HEAT DUCT. R & R DUCT IAW AMM 21-41-01. OPERATIONAL CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 47,354 hrs · 23,112 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SHUT OFF VLVS IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKS NORMAL. SEE ALSO AALA 20160411015, AALA 20160518008 & AALA 20160518010.

Part: SHUTOFF VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 47,354 hrs · 23,112 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL, THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SOV IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKED NORMAL. SEE ALSO AALA 20160411015, AALA 20160518009 & AALA 20160518010.

Part: WARNING SYSTEM — FAULTY (ANTI-ICE SYSTEM) · airframe 47,354 hrs · 23,112 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SOV IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKS NORMAL. SEE ALSO AALA 20160518008, AALA 20160518009 & AALA 20160518010.

Part: SHUTOFF VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 47,354 hrs · 23,112 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SHUT OFF VLVS IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKS NORMAL. SEE ALSO AALA 20160411015, AALA 20160518008 & AALA 20160518009.

Part: LENS — LOOSE (CABIN) · airframe 48,970 hrs · 24,080 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT AT ROW 7 HAS LOOSE LENS COVER. SECURED LENS COVER IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,107 hrs · 22,383 cycles

DURING MX, EXTENSIVE CORROSION WAS FOUND COMMON TO THE INTERNAL DOUBLER AT THE AFT LAVATORY SERVICE PAN. CORROSION WAS REMOVED IAW SRM & AREA BEYOND ALLOWABLE LIMITS WERE CUT OUT. A TITANIUM REPAIR DOUBLER WAS INSTALLED TO RESTORE STRUCTURAL STRENGTH IAW EA 255445.

Part: VANE — WORN (TE FLAP) · airframe 46,107 hrs · 22,383 cycles

LEFT WING FLAP, TWO EACH WORN SPOTS IN LE AT INBD END OF NR 3 FLAP VANE. REPAIRED IAW SRM 57-03-00-001 FIG 11.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 46,107 hrs · 22,383 cycles

FORWARD CARGO DOOR STOP SUPPORT FITTING AT AFT EDGE OF DOOR, 3RD FROM TOP, IS CRACKED. R & R DOOR STOP SUPPORT FITTING IAW AARD 51-00-05-1, DWG CDK2345 & DWG 4920233.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,639 hrs · 22,079 cycles

EMERGENCY PATH LIGHTS FROM ROW 3 - 19 ARE DIM WHEN POWERED BY EPM BATTERY PACK AB5-2. R & R BATTERY PACK AT AB5-2. SYSTEM CHECKED NORMAL.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 45,148 hrs · 21,788 cycles

EMERGENCY PATH LIGHTING HARNESS DAMAGED AT SEAT 28 DEF & 30 DEF. R & R HARNESS. SYS CHECKED NORMAL.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 44,071 hrs · 21,196 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT HYD PUMPS WERE PLACED TO HIGH, RT HYD PRESS DROPPED & RUDDER CONTROL MANUAL LIGHT ILLUMINATED. ALL QRH PROCEDURES COMPLIED WITH & ALTERNATE GEAR EXTENSION ACCOMPLISHED. R & R NR 2 ENG HYD PUMP IAW AMM 29-10-05 & RT HYD SYS RESERVOIR IAW AMM 29-10-01. PERFORMED OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

CRACK IN RT CUSP AT STATION 1211. ACCOMPLISHED CUSP DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

LOWER FWD FUSELAGE BULKHEAD CRACKED AT LT HAND SIDE OF STATION 37 AT LOWER RADOME ALIGNMENT PIN. INSTALLED DOUBLER IAW AARD 53-10-00-19.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

CABIN SUBFLOOR SUPPORT BRACKET CRACKED AT STATION 864 BELOW NR 4 SEAT TRACK. REMOVED & INSTALLED NEW SERVICEABLE BRACKET IAW AARD 51-00-00-1.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 42,736 hrs · 20,492 cycles

LT WW GEAR DOOR UPPER GREEN ACTUATOR SUPPORT BRACKET CRACKED. REMOVED & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 42,736 hrs · 20,492 cycles

RIGHT WW INTERCOSTAL CRACKED AT FWD KEEL BEAM AT STATION 946. STOP DRILLED CRACK & INSTALLED DOUBLER IAW AARD 53-10-00-6.

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 42,736 hrs · 20,492 cycles

LEFT WW INTERCOSTAL CRACKED AT STATION 946. REMOVED & INSTALLED NEW INTERCOSTAL PART IAW AARD 53-10-00-1.

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 42,736 hrs · 20,492 cycles

LEFT WW LOWER PUMP HANDLE INTERCOSTAL CRACKED. REMOVED & INSTALLED NEW SERVICEABLE INTERCOSTAL IAW AARD 53-10-00-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

LONGERON 2 RT IS CRACKED IN THE INBD RADIUS AT THE AFT SIDE OF STATION 1418. INSTALLED LONGERON & SPLICE AT STATION 1418.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

CRACK IN RADIUS OF STIFFENER ON UPPER FWD SIDE OF STATION 1338 BULKHEAD AFT OF LONGERON 1. R & R STIFFENER AT STATION 1338 BULKHEAD IAW AARD 51-00-05-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

AFT CARGO TIE DOWN TRACK FROM STATIONS 1212 TO 1231 LT CORRODED. INSTALLED 2 NEW TRACK SECTIONS IAW SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

INTERCOSTAL FROM STATIONS 1271 TO 1287 CRACKED. REPLACED INTERCOSTAL IAW AARD 51-00-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

NUMBER 6 SEAT TRACK CORRODED FROM STATIONS 219 TO 589. REPLACED NR 6 SEAT TRACK FROM STATIONS 218 TO 589 IAW SRM 53-05-00.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

CRACKED DOOR STOP SUPPORT BRACKET AT LOWER LT SIDE OF DOOR JAMB. REMOVED SUPPORT BRACKET & INSTALLED SERVICEABLE SUPPORT BRACKET IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

CORROSION ON RT CUSP FROM STATIONS 1098 TO 1174. REPLACE RT HAND CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

CORROSION ON RT CUSP FROM STATIONS 1174 TO 1250. REPLACED RT HAND CUSP IAW AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

INTERCOSTAL CRACKED BETWEEN FLOORBEAMS AT STATIONS 1287 TO 1309 CENTERLINE. REPLACED INTERCOSTAL IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

NUMBER 4 SEAT TRACK CORROSION AT STATION 480. REMOVE CORROSION & INSTALLED REPAIR PLUG IAW SRM 53-05-00-001-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

CORROSION ON NR 4 SEAT TRACK AT STATION 465. REMOVED CORROSION & INSTALLED PLUG IAW SRM 53-05-00-001.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

G1 GALLEY FITTING CORRODED. REPLACE WITH NEW GALLEY FITTING.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

CORROSION UNDER G1 GALLEY DRAIN PAN. CUT OUT CORROSION AREA ON MEMBRANE & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

FOUND EXTENSIVE CORROSION ON RT CUSP FROM STATIONS 1062 TO 1078. PERFORMED CUSP DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

SHEAR TIE CRACKED AT STATION 1429 BETWEEN LONGERONS 16 & 17 RT. REPLACED SHEAR TIE IAW AARD 51-00-05-1.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,736 hrs · 20,492 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

SKIN CRACKED AT 1427 CANT FRAME, 20 INCHES ABOVE AIRSTAIR CUT OUT. INSTALLED EXTERIOR DOUBLER IAW SRM 53-10-00-001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,736 hrs · 20,492 cycles

CRACK ON FWD OTBD SIDE OF FRAME AT STATION 1401. INSTALLED DOUBLER IAW SRM 51-70-5-001.

Part: LENS — MISSING (CABIN) · airframe 42,729 hrs · 20,484 cycles

OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 10D, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,729 hrs · 20,484 cycles

OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 10D INOPERATIVE. REPAIRED LIGHT ASSEMBLY FOR OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 10D, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

FORWARD ZONE SEAT MOUNTED EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR FWD ZONE SEAT MOUNTED EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY EXIT LIGHTS, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,729 hrs · 20,484 cycles

OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 21AB INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 21AB, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY LIGHTS AT STATION 1322R INOPERATIVE. REPLACED BATTERY PACK B5-27, OPERATIONS CHECKED NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY EXIT LIGHT AT SEAT 18D MISSING LAMP. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT 18D, OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY EXIT LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT 18D, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,729 hrs · 20,484 cycles

FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR FWD OVERWING EMERGENCY EXIT LIGHT, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY LIGHTS AT STATION 386R INOPERATIVE. REPLACED BATTERY PACK B5-100, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY LIGHT AT STATION 500R INOPERATIVE. REPLACED BATTERY PACK B5-101, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

OVERWING EMERGENCY EXIT LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS BETWEEN AFT LAVATORIES, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,729 hrs · 20,484 cycles

EMERGENCY LIGHTS AT STATION 1338R INOPERATIVE. REPLACED BATTERY PACK B5-28, OPERATIONS CHECKED NORMAL.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 42,343 hrs · 20,289 cycles

FWD CARGO, LONGERON 30 LT SPLICE PIECE CRACKED AT STATION 228 AFT RT HAND SIDE. INSTALLED FABRICATED SPLICE IAW AARD 55-00-05-1 DRAWING 5911408.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 42,343 hrs · 20,289 cycles

DAMAGED LONGERON 24 LT FROM STATIONS 231 TO 341. REPLACED DAMAGED LONGERON & INSTALLED SPLICED REPAIR IAW SRM 53-02-00 FIGURE 18.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,343 hrs · 20,289 cycles

CRACKED CARGO ANGLE. INSTALLED NEW SERVICEABLE CARGO ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,343 hrs · 20,289 cycles

CARGO ANGLE FROM STATIONS 237 TO 238 CRACKED. INSTALLED NEW SERVICEABLE CARGO ANGLE.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 41,719 hrs · 19,939 cycles

DTW INFLIGHT ORD-LGA CREW REPORTED LT ENGINE GENERATOR FAILED & AUXILIARY POWER UNIT FAILED TO START. FLIGHT DESCENDED & APU START ATTEMPTED AGAIN WITH SUCCESSFUL START. FLIGHT DIVERTED DTW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 40,011 hrs · 19,015 cycles

ORD - INFLIGHT ORD-DFW CREW REPORTED FUEL WAS NOT BURNING OUT OF CENTER TANK AND WING TANKS WERE DECREASING AND CENTER FUEL PRESSURE LOW LIGHT WAS ON. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH CENTER TANK BOOST PUMPS AND PUMP WIRING HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 39,644 hrs · 18,836 cycles

CLE - CREW REPORTED LEFT ENGINE FAILED AT ROTATION AND SHUTDOWN (SINGLE ENGINE TIME 25 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED CLE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT CLE ON 12/24/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,277 hrs · 18,640 cycles

SKIN CRACKED AT STATION 1380, LONGERON 14 RIGHT. INSTALLED DOUBLER REPAIR PER SRM 53-01-00.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 37,945 hrs · 17,974 cycles

EMERGENCY SEAT ESCAPE PATH LIGHTS FROM ROWS 3 TO 19 INOPERATIVE. RECONNECTED LOOSE CONNECTERS AT SEAT 2EF, 3EF AND 4EF AND REPAIRED INSULATION CHAFING AT SIDE WALL 4EF BY SPLICING, OPS CHECK NORMAL.

Part: DUCT — BLOWN (AC BAY) · airframe 33,602 hrs · 15,766 cycles

PHX - CREW REPORTED ON CLIMBOUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT IN LESS THAN 2 MINUTES AFTER RED BOX PROCEDURE. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND CONDITIONED AIR DUCT BLOWN ON THE RIGHT PACK, IN THE TAIL COMPARTMENT. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,838 hrs · 14,886 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS BATTERY PACK. OPS CHECKED NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

CORROSION ON LEFT CUSP STATION 570. INSTALLED DOUBLER AT STATION 570 LEFT CUSP PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

DOOR BEAM HAS CORROSION AT STATION 1155 TO 1211. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

CORROSION ON LEFT CUSP AT STATION 373 TO 376. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

AFT LOWER ANGLE STATION 1309 LONGERON 28 HAS CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-10-00-14.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · 14,627 cycles

RIGHT SKATE ANGLE AT APPROXIMATELY STATION 1474 IS CRACKED BETWEEN THE FASTENERS AND THE AFT FASTENER HEAD IS POPPED. REMOVED DAMAGE AND INSTALLED REPAIR PER AARD 53-10-00-2.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · 14,627 cycles

LEFT SKATE ANGLE AT APPROXIMATELY STATION 1474 IS CRACKED BETWEEN FASTENERS. REMOVED DAMAGE AND INSTALLED REPAIR PER AARD 53-10-00-2.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 31,239 hrs · 14,627 cycles

FORWARD SERVICE DOOR HAS POSSIBLE CRACK AT LOWER HINGE BEAM. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER AND ANGLE PER SRM 52-05 FIG 28. INSTALLED INNER SKIN AND HINGE PER ESO 80177.

Part: PLATE — DAMAGED (HORIZ STAB) · airframe 31,239 hrs · 14,627 cycles

HORIZONTAL STABILIZER LUG PLATES NUMBERS 1, 2, 3, 4, 5, 6, 7 AND 8 BORE OUT OF LIMITS. REPLACED THE EIGHT LUG PLATES PER TASK CARD 55-94-05.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,239 hrs · 14,627 cycles

AFT ACCESSORY SHEAR TIE CRACKED AFT SIDE OF FRAME 1451 AT LONGERON 2 LEFT. REPLACED SHEAR TIE PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

CORROSION REMOVAL BEYOND LIMITS ON CUSP STATION 212 TO 216. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,239 hrs · 14,627 cycles

AFT ACCESSORY SHEAR TIE CRACKED AFT SIDE OF FRAME 1451 AT LONGERON 2 RIGHT. REPLACED SHEAR TIE PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

SEAT TRACK NUMBER 4 AT STATION 1305 TO 1309 CORROSION OUT OF LIMITS. REPLACED NUMBER 4 SEAT TRACK FROM STATION 1241 TO 1309 PER SRM 53-05-00.

Part: PAN — WORN (SERVICE DOOR) · airframe 31,239 hrs · 14,627 cycles

AFT SERVICE DOOR HANDLE PAN HAS DEEP WEAR. REMOVED OLD CASTING, DRILLED NEW CASTING AND INSTALLED PER ESO 80175.

Part: TAB — DAMAGED (ELEVATOR) · airframe 31,239 hrs · 14,627 cycles

LEFT ELEVATOR GEAR TAB TRAILING EDGE DAMAGED. HOT BONDED METAL DOUBLER PER SRM 51-70-02.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 31,239 hrs · 14,627 cycles

AFT CARGO DOOR AFT BOTTOM STOP FITTING CRACKED. REMOVED OLD FITTING AND REPLACED WITH NEW FITTING PER ESO 80174.

Part: RIB — CRACKED (LE SLAT) · airframe 31,239 hrs · 14,627 cycles

CRACK FOUND IN OUTBOARD RIB ON SLAT ON RIGHT WING. REMOVED OUTBOARD ATTACH FITTING, DRILLED AND INSTALLED NEW FITTING PER ESO 80117.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 31,239 hrs · 14,627 cycles

AFT CARGO DOOR FWD 2ND FROM BOTTOM DOOR STOP FITTING CRACKED. REMOVED OLD FITTING AND REPLACED WITH NEW FITTING PER ESO 80124.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,239 hrs · 14,627 cycles

CORROSION ON SUBFLOOR AT STATION 212 TO 216 FORWARD OF NUMBER 6 SEAT TRACK. REMOVED DAMAGE INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,239 hrs · 14,627 cycles

DENT IN FUSELAGE AT STATION 238 LONGERON 18 LEFT. REMOVED DAMAGE AND INSTALLED DOUBLER FILLER AND FINGER DOUBLER PER SRM 53-04 FIGURE 12B.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 30,083 hrs · 14,123 cycles

IAH - CREW REPORTED YAW DAMPER AND MACH TRIM/ACARS LOST ON APPROACH. EMERGENCY DECLARED, LANDED IAH WITHOUT INCIDENT. FOUND DIGITAL FLIGHT COMPUTER CIRCUIT BREAKER POPPED. RESET ACARS CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ANTI-SKID SYS — INOPERATIVE (MLG) · airframe 29,163 hrs · 13,700 cycles

MCI - ON TAKEOFF WHEEL NOT TURNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND FLIGHT RETURNED TO GATE. REPLACED RIGHT OUTBOARD ANTI-SKID SYSTEM. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT AB5 23 FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DETACHED (CABIN)

DFW - FOUND SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11DEF DETACHED. SECURED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OIL TANK — LEAKING (APU)

YYZ INFLIGHT T1311/11JUN - CREW REPORTED ODOR AND HAZE IN CABIN DURING ROTATION. RETURNED TO YYZ AND LANDED WITHOUT INCIDENT. FOUND OIL DRIPPING FROM APU INLET AND OIL TANK OVER SERVICED. ACCOMPLISHED WORK CARD 21 96 01 FOR CABIN ODOR AND PACK BURN WORKCARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL BOX — MALFUNCTIONED (ANTI SKID)

ORD - FLT 2356 - DFW-ORD, ON LANDING ROLL BOTH RIGHT MAIN TIRES GRABBED AT SPEED OF ABOUT 89 KNOTS. ANTI-SKID FLASHED ON OVERHEAD PANEL. BOTH TIRES WENT FLAT. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (ROW 19) · airframe 5,527 hrs · 2,743 cycles

THE EMERGENCY EGRESS LIGHT AT CABIN ROW 19 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 4-11-00 STL.

Part: BLADE — DAMAGED (COMPRESSOR)

JUST AFTER TAKEOFF THE LEFT ENGINE HAD TWO COMPRESSOR STALLS AND THEN LOST POWER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO DEN. FOUND EVIDENCE OF A BIRD STRIKE CAUSING DAMAGE TO SEVERAL FIRST STAGE COMPRESSOR BLADES. THE ENGINE WAS REPLACED.