N479AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,461 hrs · 40,805 cycles

SEVERAL CABIN EMERGENCY LIGHTS ARE INOPERATIVE. R & R THE BATTERY PACK.

Part: FRAME — CRACKED (LT MLG WW) · airframe 75,508 hrs · 40,243 cycles

LEFT MLG CRACK IN FRAME 984 AT AFT OTBD CORNER OF WW NEXT TO FLAP BUS CABLE PULLEY BRACKET. SPLICED NEW CHANNEL SECTION IAW SRM 51-70-05 & DWG 5936373.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 75,508 hrs · 40,243 cycles

MID CARGO DOOR CTR STOP PAD SUPPORT BRACKET CRACKED AT FWD SIDE OF CARGO DOOR. INSTALLED NEW SERVICEABLE FWD CTR STOP PAD SUPPORT BRACKET ON MID CARGO DOOR IAW AARD 51-00-05-1 & DWG 5910141.

Part: FORMER — CRACKED (RT WING) · airframe 75,204 hrs · 40,068 cycles

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

Part: FORMER — CRACKED (LT WING) · airframe 75,204 hrs · 40,068 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER REPAIR DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: STRUT — CRACKED (FUSELAGE) · airframe 74,552 hrs · 39,680 cycles

VERTICAL SUPPORT STRUT AFT OF STATION 218 BULKHEAD AT LBL 30 IS CRACKED AT BOTTOM RADIUS. REPAIRED STRUT IAW SRM 53-01-00-001 FIG 2 & AARD 53-10-00-15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,552 hrs · 39,680 cycles

LONGERON 25 LT CRACKED AT LOWER MOUNT HOLE AT FS 160. REPAIRED LONGERON IAW SRM 53-02-00-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,552 hrs · 39,680 cycles

FUSELAGE SKIN HAS A CRACK AT LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUT OUT. REPAIRED SKIN IAW SRM 53-05-00 FIG 57A & AARD 51-60-00-02.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 72,811 hrs · 38,632 cycles

VERTICAL STABILIZER LE SKIN & FRONT SPAR CAP AT STATION ZFS 52.267, LOOSE & DISTRESSED FASTENERS WERE FOUND. ACCOMPLISHED FASTENER REWORK IAW 55-03-00-01 PARAGRAPH 28 FIGURE 30.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 72,811 hrs · 38,632 cycles

CRACK INDICATION WAS FOUND ON 1 FASTENER HOLE, ON THE VERTICAL STABILIZER DURING HFEC INSPECTION IAW SB MD80-55A067. REMOVED HOLE & INSTALLED FREEZE PLUG IAW EA MD80-55-033832.

Part: ENGINE — FAILED (RIGHT) · airframe 72,736 hrs · 38,593 cycles

DFW CREW REPORTED HEARING TWO LOUD BANGS FOLLOWED BY THE RT HAND ENG FAILURE SINGLE ENG TIME 7 TO 8 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT HAND ENG AT DFW ON 02/04/2014. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,331 hrs · 38,380 cycles

EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH THE EMERGENCY EXIT LIGHT PLACED TO ON POSITION. REPLACED COCKPIT OVERHEAD EMERGENCY EXIT BATTERY PACK, OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,097 hrs · 38,244 cycles

FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED B5-23 EMERGENCY LIGHTS POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: SPRING — BROKEN (L2 DOOR) · airframe 72,000 hrs · 38,180 cycles

LT NR 2 DOOR GUST LOCK RETURN SPRING INOPERATIVE. REPLACED LT NR 2 DOOR GUST LOCK SPRING IAW AMM. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,985 hrs · 37,567 cycles

EMERGENCY LIGHT BY AFT GALLEY FAILED TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 29 DEF. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,908 hrs · 36,953 cycles

EMERGENCY LIGHTS NOT ARMED ON ANNUNCIATOR PANEL LAMPS INOPERATIVE. REPLACED LAMPS FOR "EMERGENCY LIGHTS NOT ARMED" ON ANNUNCIATOR PANEL. OPS CHECK NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 69,908 hrs · 36,953 cycles

DFW - CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS DURING CLIMBOUT. SHUTDOWN LEFT ENGINE (SINGLE ENGINE TIME 22 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT DFW ON 04/03/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 69,257 hrs · 36,594 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY FOR 10DEF AND FOR RIGHT AFT LAVATORY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,705 hrs · 36,267 cycles

LEFT AND CENTER CEILING EMERGENCY LIGHTS, BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED LAMP FOR AFT AISLE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,705 hrs · 36,267 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 21 INOPERATIVE. RECHARGED BATTERY. OPS CHECK NORMAL.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

LONGERON 28 RIGHT CORRODED AFT SIDE OF FRAME STATION 1287. SPLICE IN REPAIR PER SRM 53-02-00, 51-30-05 AND 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

CORROSION ON LEFT CUSP AT STATION 457. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

COCKPIT AREA, MEMBRANE CORRODED AT STATION 133, BELOW CAPTAINS INBOARD SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (OVERWING EXIT) · airframe 68,135 hrs · 35,950 cycles

CABIN SIDEWALL LEFT AFT OVERWING EXIT DOOR HAS CRACK IN DOOR PAN ON AFT SIDE AT TOP STOP FITTING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 51.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

TOOLING MARK ON LEFT FUSELAGE SKIN STATION 211 LONGERON 4 LEFT. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

LONGERON 4 LEFT CRACKED FROM STATIONS 160 AND 200. INSTALLED SPLICE REPAIR FROM STATIONS 148 TO 229 PER SRM 53-02-00 FIGURE 18.

Part: PAN — CRACKED (OVERWING EXIT) · airframe 68,135 hrs · 35,950 cycles

CABIN SIDEWALL LEFT AFT OVERWING EXIT DOOR HAS CRACK IN DOOR PAN ON THE AFT SIDE AT 2ND FROM BOTTOM STOP PAD BRACKET. STOP DRILLED CRACK INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 51.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

RIGHT CUSP IS CRACKED AT STATIONS 466 TO 468. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

RIGHT CABIN UPPER CUSP SHEET AT STATION 1231 TO 1235 WITH HEAVY CORROSION. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

GUSSET AT STATION 210 LONGERON 11 LEFT CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

FUSELAGE SKIN IS CRACKED AT STATION 1309 BETWEEN LONGERONS 6 TO 7 LEFT. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 68,135 hrs · 35,950 cycles

RIGHT FORWARD OVERWING EXIT DOOR CRACKED ON UPPER FORWARD CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 68,135 hrs · 35,950 cycles

RIGHT FORWARD OVERWING EXIT DOOR CRACKED ON UPPER AFT CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.

Part: SKIN — DENTED (LE SLAT) · airframe 68,135 hrs · 35,950 cycles

RIGHT WING, NUMBER 5 SLAT HAS A DENT BETWEEN ATTACHED RIBS NUMBER 15 AND 14 ON OUTBOARD SKIN. REWORKED DENT PER SRM 57-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

RIGHT CABIN UPPER CUSP SHEET FROM STATIONS 1183 TO 1185 WITH HEAVY CORROSION. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

CRACK FOUND AT STATION 1309 BETWEEN LONGERONS 6 AND 7 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4 B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

LEFT CUSP SHEET FROM STATIONS 1250 TO 1309 CORRODED. REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

VERTICAL BRACKET CRACKED JUST ABOVE CENTER FUEL TANK AT STATION 927, RIGHT SIDE AND BELOW NUMBER 5 SEAT TRACK. INSTALLED NEW FLOORBEAM SUPPORT BRACKET PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

LEFT CUSP HAS 2 EACH CRACKS AT THE LIGHTNING HOLE FROM STATIONS 222 TO 226. INSTALLED LEFT CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 53-20-00-16.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

VERTICAL BRACKET CRACKED JUST ABOVE CENTER FUEL TANK AT STATION 927, LEFT SIDE AND BELOW NUMBER 2 SEAT TRACK. INSTALLED NEW FLOORBEAM SUPPORT BRACKET PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,135 hrs · 35,950 cycles

DENT WITH GOUGE IN SKIN AT STATION 239. FINGER DOUBLER INSTALLED PER SRM 53-04-2 AND AARD 51-6-00.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,135 hrs · 35,950 cycles

CORROSION ON SUB FLOOR BRACKET AT STATIONS 212 AND RIGHT BUTTLINE 12. REPLACED NEW MOUNT PER AARD 51-10-00-05.

Part: ADC — FAILED (COCKPIT) · airframe 67,540 hrs · 35,609 cycles

AT ABOUT 300FT AGL AFTER TAKEOFF, F/O`S CADC FAILED WITH FLAGS IN AIRSPEED AND ALTIMETER AND BOTH FLIGHT DIRECTORS FAILED. FOUND C/B F12 POPPED. PLACED BOTH CADCS ON NR 1 AND F/O`S INSTRUMENTS BEGAN TO INDICATE NORMAL. ALTITUDE SELECT WINDOW FLIGHT GUIDANCE PANEL WAS BLANK, AUTOTHROTTLES WOULD NOT TURN ON. SWITCHING FROM AP1 AND AP2 DID NOT HELP. ON FINAL APPROACH 5 MINS LATER FLIGHT DIRECTOR BEGAN TO WORK BUT AUTOTHROTTLES WOULD NOT ENGAGE. BOTH FMAS WENT BLANK AND AFTER 2 MINUTES SELECT WINDOW BEGAN TO WORK. ON FINAL ALL FMA WINDOWS WORKED. FOUND NR 2 CADC BAD. REPLACED NR 2 CADC AND CHANGED CIRCUIT BREAKER FOR NR 2 CADC. ALL TEST CHECKED OK.

Part: COMPUTER — FAILED (NR 2) · airframe 67,540 hrs · 35,609 cycles

CREW REPORTED NUMBER 2 CENTRAL AIR DATA COMPUTER FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 CENTRAL AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,367 hrs · 35,514 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. REPLACED BATTERY PACK BY RIGHT AFT LAVATORY. OPS CHECK NORMAL.

Part: INDICATOR — DEFECTIVE (EGT) · airframe 66,383 hrs · 34,946 cycles

DFW - CREW REPORTED RIGHT ENGINE EXHAUST GAS TEMPERATURE OVERHEAT INDICATION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE AND TWO EGT INDICATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,523 hrs · 33,884 cycles

LEFT CANT FRAME WEB CRACKED ABOVE LEFT LOUVER BOX AT STATION 1463. INSTALLED REPAIR DOUBLER PER EA MD80-53-014696 DATED 01/06/2011 AND SRM 53-01-4.

Part: TURBINE — FAILED (RT ENGINE) · airframe 64,199 hrs · 33,685 cycles

MEX - CREW REPORTED RIGHT ENGINE COMPRESSOR STALL ON DEPARTURE. RIGHT ENGINE SHUTDOWN IN FLIGHT (SINGLE ENGINE TIME 17 MINUTES). EMERGENCY DECLARED RETURNED MWX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RIGHT TURBINE CONTAINED FAILURE. REPLACED RIGHT ENGINE AT MEX ON 11/04/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,250 hrs · 33,126 cycles

LEFT AND RIGHT OVERWING EMERGENCY EXIT MARKER DECALS DAMAGED. REPLACED DECALS.

Part: GUARD — DAMAGED (EMERGENCY LIGHT) · airframe 63,250 hrs · 33,126 cycles

SEAT 15D EMERGENCY LIGHT GUARD DAMAGED. REPLACED LIGHT GUARD.

Part: DOOR — CRACKED (RT MLG) · airframe 60,784 hrs · 31,738 cycles

RIGHT MAIN LANDING GEAR BODY DOOR LOWER AFT END CRACKED. INSTALLED DOUBLER REPAIR PER 52-05-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,525 hrs

LGA FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS AT FORWARD CABIN EMERGENCY LIGHT.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 57,894 hrs

LGA - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. RE-SECURED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — LOOSE (CABIN) · airframe 57,894 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 21 TO 24 INOPERATIVE. RE-SECURED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 21 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,894 hrs

LGA - EMERGENCY EXIT SIGN LIGHT AT RT FORWARD OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,894 hrs

LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 57,250 hrs

TUL - RELEASE HANDLE CABLE ASSEMBLY HAS WORN AND FRAYED CABLE ON LEFT SIDE ABOVE THE MID POINT PULLEY. AREA OF DISCREPANCY WAS .125 INCH BY .125 INCH. REPLACED TAILCONE RELEASE CABLE ASSEMBLY ON LEFT SIDE. OPERATIONS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,861 hrs

LGA EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT FOWARD SEAT ROW 20 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,861 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — DAMAGED (NLG)

DFW INFLIGHT T689/17DEC - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR PISTON FLAT DUE TO DAMAGE TO STRUT CYLINDER. REPLACED UPPER AND LOWER NOSE LANDING GEAR STRUTS AND SERVICED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HINGE — INOPERATIVE (FUEL DOOR)

DFW - UNWANTED FUEL TRANSFER DURING FLIGHT. DETERMINED THE LEFT TANK WAS FEEDING INTO THE CENTER. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LEFT FUEL TANK FILL VALVE SWITCH IN OPEN POSITION. WHEN CLOSING FUEL PANEL DOOR GANG BAR DOES NOT SHUT OFF FUEL FILL VALVE SWITCHES. REPLACED HINGE ON FUEL PANEL DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACT — INOPERATIVE (BATTERY PACK)

LGA - EMERGENCY LIGHTS AT ROWS 29 TO 32 INOPERATIVE. CLEANED CONTACTS ON ROW 29 BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 29 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336 INOPERATIVE. REPLACED BATTERY PACK B527 FOR CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336. SYSTEM GROUND CHECKED NORMAL OPERTION.

Part: LATCH — INOPERATIVE (MLG)

MIA - INFLIGHT T1246/02 AFTER TAKEOFF GEAR FAILED TO RETRACT. RAN QRH WITH NO SUCCESS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC BY PASS HANDLE EXTENDED. ADJUSTED LOCK LATCH TAP SPRING IN LOCKING LATCH. STOWED AND LOCKED HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

MIA - FLOOR LEVEL EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED BROKEN WIRE FOR FLOOR LEVEL EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DEFECTIVE (CABIN)

DFW - AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 27D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRAKE — MALFUNCTIONED (RT MLG)

ORD T2301/21 EN ROUTE ORD-DFW ON TAKEOFF RIGHT BRAKE DRAGS AND TEMPERATURE ROSE TO 200 DEGREES. ABORTED TAKEOFF. REPLACED RIGHT WHEEL, BRAKE AND SLEEVE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SIDE WALL HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — MISSING (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN CABIN HAS SEVERAL FEET MISSING. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN CABIN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (ROW 33D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 33D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — CRACKED (BS 1418)

TUL - FOUND LONGERON NR 2 HAS CRACK AND AMAGE FASTENER 2 EACH HOLES. SPLICE IN NEW LONGERON AND INSTALLED DOUBLER ON EXTERNAL FUSELAGE PER 53-01 AND 53-02-12. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED JUMPER STRIP WIRE FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF FIRST CLASS SEATS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF FIRST CLASS SEATS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: PROX SENSOR — DEFECTIVE (NLG)

DFW - FLT 1675 - AFTER TAKEOFF TUL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SWITCH CONTROL UNIT AND PROBLEM CONTINUED DURING LANDING GEAR RETRACTION CHECK. REPLACED NOSE LANDING GEAR UPLOCK PROXIMITY SENSOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (BS 460)

TUL - LIGHTNING STRIKE IN FUSELAGE SKIN STILL INDICATING CRACK. INSTALLED DOUBLER PER SRM 53-04, FIG 38. TST: 23,322.43 HRS. CYCLES, 13,207. ( X)

Part: LIGHT STRIP — DEFECTIVE (CABIN)

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

Part: SPOTLIGHT — DEFECTIVE (FWD ENTRY DOOR)

DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY LIGHT SPOTLIGHT FOUND INOPERATIVE. REPLACED EMERGENCY SPOTLIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRUT — REQUIRED SERVICE (NLG)

ORD - FLT 1387 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NLG DID NOT LOCK UP AND RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR MULTIPLE TIMES WITH SAME RESULT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED NLG STRUT WITH OIL AND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL CONNECTOR — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMEREGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 15 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL TERMINAL — BROKEN (CABIN)

ORD - FLT 224 - DURING PREFLIGHT CHECK, EMERGENCY FLOOR LIGHT TERMINAL FOUND BROKEN AFFECTING LIGHT STRIP FROM PASSENGER SEAT ROW 7 AND AFT. REPLACED EMERGENCY FLOOR LIGHT FEMALE TERMINAL END BY PASSENGER SEAT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)