N9413T

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 50,350 hrs · 24,823 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NUMBER 1 DOOR PORTABLE LIGHT. OPS CHECK NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 50,350 hrs · 24,823 cycles

ESCAPE PATH LIGHT AT SEAT 22D INOPERATIVE. REPAIRED WIRING FOR ESCAPE PATH LIGHT AT SEAT 22D. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 50,350 hrs · 24,823 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 26 INOPERATIVE. RESEATED BATTERIES AT ROW 25. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,604 hrs · 23,855 cycles

DENT AND SCRATCHES IN FUSELAGE SKIN STATION 464 ABOVE LONGERON 21 RIGHT. DYE CHECKED AND NO CRACKS FOUND. FABRICATED AND INSTALLED CLASS III DOUBLER PER SRM 53-04-03 FIGURE 2 SHEET 5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,604 hrs · 23,855 cycles

DENT AND GOUGE IN FUSELAGE SKIN STATION 241 BETWEEN STRINGERS 21 AND 22 LEFT. DYE CHECKED AND NO CRACKS FOUND. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 02.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,604 hrs · 23,855 cycles

STATIONS 160 TO 200 CORRODED BELOW INBOARD LEG OF FORWARD SERVICE DOOR AREA FLOORBOARD SUPPORT. INSTALLED NEW SUBFLOOR AND OVERLAY DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,604 hrs · 23,855 cycles

LEFT CUSP FROM STATIONS 1171 TO 1176 CORRODED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 48,604 hrs · 23,855 cycles

TOOLING MARK ON CUSP AT STATION 864 LEFT UNDER HORSECOLLAR. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: DOOR — DAMAGED (CARGO DOOR) · airframe 48,604 hrs · 23,855 cycles

EXTERIOR SKIN ON MID CARGO DOOR HAS SEVERAL AREAS OF DAMAGE. REMOVED AND REPLACED OUTER SKIN ON MID CARGO DOOR PER ESO 80174.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,604 hrs · 23,855 cycles

AFT GALLEY SERVICE DOOR JAMB HAS CORROSION ON CUSP UNDER FORWARD AND AFT GIRT BAR SUPPORTS. INSTALLED DOUBLERS PER AARD 53-20-00-16.

Part: DUCT — FAILED (AC BAY) · airframe 48,097 hrs · 23,586 cycles

BNA - INFLIGHT PHL-DFW. CREW REPORTED TAIL TEMPERATURE OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT 1684 AND REPAIRED LEAK ON RIGHT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 45,476 hrs · 22,180 cycles

BHM INFLIGHT DFW-ATL - CREW REPORTED RIGHT ENGINE OIL TEMP INDICATION CLIMBED IN EXCESS OF 190 DEGREES. RIGHT ENGINE WAS SHUTDOWN IN FLIGHT (SINGLE ENGINE TIME 13 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED BHM LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT BHM ON 12/24/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BOOT — CRACKED (AC BAY) · airframe 44,641 hrs · 21,789 cycles

DFW - CREW REPORTED CABIN BEGAN TO DEPRESSURIZE DURING FLIGHT. INICIATED EMERGENCY DESCENT TO 8,000 FT. THE FLIGHT ATTENDANT REPORTED A LOUD AIR LEAK FROM THE AFT GALLEY DOOR. FLIGHT LANDED DFW WITHOUT INCIDENT. REPLACED FLEX BOOT RIGHT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,272 hrs · 21,620 cycles

FRAME 1418 CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER IAW EA MD80-53-011690.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,950 hrs

SFO - BOTH AFT LEFT AND RIGHT OVERWING EXIT DOORS OVERHEAD EXIT LIGHT DIMS THEN BRIGHTENS. REPLACED BATTERY PACK AT B5-105 POSITION.

Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 39,956 hrs · 19,560 cycles

LONGERON 2 RIGHT CRACKED AT STATION 1418. INSTALLED SPLICE PER AARD 53-30-00-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 39,956 hrs · 19,560 cycles

LONGERON 2 LEFT CRACKED AT STATION 1418. INSTALLED SPLICE PER AARD 53-30-00-2.

Part: BEAM — CRACKED (ZONE 200) · airframe 39,956 hrs · 19,560 cycles

HORIZONTAL BEAM CRACKED UNDER INBOARD SUPPORT BOLT. THIRD BEAM UP AT FORWARD ENTRY DOOR. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH AARD 52-10-00-3.

Part: FRAME — CRACKED (ZONE 100) · airframe 39,956 hrs · 19,560 cycles

FRAME 1418 CRACKED AT STRINGER 2 RIGHT AT FORWARD SIDE AND AFT SIDE AT STIFFENER.

Part: SKIN — CRACKED (ZONE 200) · airframe 39,956 hrs · 19,560 cycles

AFT SERVICE DOOR SKIN CRACKED AT HOLD OPEN HOOK CUTOUT. INSTALLED DOUBLER ON AFT SERVICE DOOR IN ACCORDANCE WITH SRM 52 05 00 FIGURE 54 SHEET 1.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 39,326 hrs

SFO - AFT EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS OVERHEAD RIGHT AND LEFT AFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 38,021 hrs

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT 25D AFT TO TAIL CONE INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25D AFT TO TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 38,021 hrs

SFO - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,303 hrs

LAX - OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5 125 FOR OVERWING EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

SFO - FOUND EMERGENCY LIGHTS AT SEAT 28D INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

LAS - EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED FLASHLIGHT BATTERIES FOR EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

IAH - COCKPIT AND GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT AND GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

STL - EMERGENCY PATH LIGHTS AT SEAT 14DEF INOPERATIVE. FOUND CONNECTOR DISCONNECED AT SIDEWALL SEAT 14DEF. RECONNECTED CONNECTOR FOR EMERGENCY PATH LIGHTS AT SEAT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD AND AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

STL - EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY EXIT LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 19 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DTW FRONT ENTRY EMERGENCY EXIT LIGHT UPPER LOCK BROKEN. REPLACED FRONT ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — LEAKING (A/C BAY) · airframe 21,324 hrs · 10,590 cycles

A BURNING ODOR WAS IN CABIN AND COCKPIT ON DESCENT. NO SMOKE. FOUND RT ACM OIL PUDDLING IN ACM OUTLET. THE NEXT STATION REPLACED THE RT ACM.

Part: COMPUTER (NUMBER 1) · airframe 20,444 hrs · 10,097 cycles

THE CAPTAIN'S IAS INDICATOR FROZE AT 180 KNOTS ON CLIMB OUT. CREW MADE AN UNSCHEDULED LANDING AT MCI. REPLACED THE CAPTAIN'S AIR SPEED INDICATOR, PN 4057800-906, AND THE NUMBER 1 CADC. CHECK-C 7-29-01 STL. --CLOSED--

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 19,061 hrs · 9,308 cycles

A LOUD NOISE WAS HEARD FROM THE LT ENGINE AND THE AIRCRAFT SHUTTERED. SMOKE APPEARED IN THE COCKPIT. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED AT SZL. EMERGENCY EVACUATION WAS ACCOMPLISHED. CHECK-C 8-10-00 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,250 hrs · 8,845 cycles

THE EGRESS LIGHT AT SEAT 8D WAS INOPERATIVE DURING TEST. REPLACED THE LAMP. CHECK-C 12-3-00 JFK.

Part: GCU — FAILED (APU) · airframe 17,282 hrs · 8,358 cycles

IN CRUISE FLIGHT WITH RT GEN INOPERATIVE THE APU GEN TRIPPED OFF LINE. THE LT GEN BECAME ERRATIC AND FAILED TO PICK UP THE LOAD, FOLLOWED BY LT AC BUS REPEATEDLY COMING ON AND OFF LINE RAPIDLY THEN COMPLETELY DROPPING OFF LINE. NO GENERATOR WOULD MAINTAIN ANY LOAD. MADE UNSCHEDULED LANDING AT BIS. REPLACED THE RT CSD, PN 696233B, AND GEN PN 976J252-8. FOR APU REPLACED APU GENERATOR CONTROL UNIT PN 947F9453 SERIAL NBR 0704. FOR LT GEN REPLACED THE CROSS TIE RELAY PN 914F567-4 S/N WL 991, AC BUS CONTROL PANEL PN 914F5655 S/N 2T1123, AND LT GENERATOR CONTROL UNIT PN 947F9453 S/N 4296. CHECK-C 8-10-00 STL.

Part: COVER — MISSING (ROW 30)

THE RED EGRESS LIGHT COVER WAS MISSING AT CABIN ROW 30. REPLACED THE RED COVER. CHECK-C 8-11-99 MCI.

Part: BATTERY — DISCHARGED (CABIN)

THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 3, 5, 19, 21, AND 22. REPLACED THE LAMP, MFG PN 1315, FOR ROWS 3 AND 5, AND REPLACED THE BATTERY FOR REMAINING ROWS. CHECK-C 8-11-99 MCI.

Part: SKIN — DENTED (BS 1193)

DURING CHECK-C MAINT, FOUND .5 INCH BY 0.080 DEEP AND .4375 INCH LONG BY 0.076 DEEP DENTS IN SKIN AT STA 1193, LONGERON 20L. TWO DENTS WITHIN .5 INCH OF EACH OTHER. ACCOMP HFEC CHECK PER 51-00-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER SRM 53-04, FIG 38 PAGE 218K.

Part: LONGERON — MISREPAIRED (BS 256)

DURING CHECK-C MAINT, A 9 INCH BY 9 INCH CLASS 3 REPAIR, FOUND INSTALLED WITH BLIND FASTENERS AT STA 256, WL 209 AND LONGERON 17L, WAS DAMAGED. REPAIRED LONGERON 17L, STA 256, PER SRM 53-02 PAGE 48, FIG 18. REPAIRED CLASS 3 REPAIR PER SRM 53-04, PAGE 39 FIG 12B AND SHEET 4.

Part: SKIN — GOUGED (BS 217)

DURING CHECK-C MAINT, FOUND FUSELAGE SKIN GOUGED AT STA 217, STRINGER 5L AND 6L. AN INTERIM REPAIR HAD BEEN INSTALLED PER ARA 15461. REPAIRED PER SRM 53-04, FIG 12B, SHEET 5.

Part: SKIN — MISREPAIRED (BS 229-245)

DURING CHECK-C MAINT, FOUND FUSELAGE SKIN REPAIR INSTALLED WITH BLIND FASTENERS AT STA 229 TO 245, STRINGER 18L. REPAIRED PER SRM 53-04, FIG 12B, WITH SOLID FASTENERS AND ADDING FINGER DOUBLER.

Part: COVER — MISSING (CABIN)

DURING PREFLIGHT INSPECTION FOUND ESCAPE PATH LIGHTING COVER MISSING. REPLACED COVER. CC-01 9-1-98 STL.

Part: COVER — MISSING (CABIN)

THE EGRESS LIGHTS AT AFT CABIN WAS MISSING THE COVER AND THE RED LENS. REPLACED THE COVER 0105601-003PA40, LAMP 7732, LEN 0105607-301, AND THE END PIECE 015609-001. CHECK-C 9-1-98 STL.

Part: WIRE — LOOSE (ROW 2)

THE EGRESS LIGHT AT CABIN ROW 2 HAD WIRE LOOSE FROM THE LIGHT AND THE COVER WAS MISSING. REPLACED THE WIRE SEGMENT AND INSTALLED COVER. CHECK-C 9-1-98 STL.

Part: LAMP — LOOSE (ROW 3 & 21-24)

FOUND EGRESS LIGHTS INOPERATIVE ON TEST AT ROW 21 TO 24, AND ROW 3. SECURED A LOOSE LIGHT SOCKET AT ROW 24, AND INSTALLED A LOOSE LAMP AT ROW 3. CHECK-C 9-1-98 STL.

Part: WIRE — WORN (ROW 17)

FOUND EMERGENCY EGRESS LIGHT COVER STRIP MISSING AT CABIN ROW 17. REPLACED COVER (P/N 5778-1), AND LIGHT CABLE. CHECK -C 9-1-98 STL.

Part: LENSE — DAMAGED (ROW 3-29)

PARKED AT THE GATE IT WAS NOTED THAT THE EMERGENCY EGRESS LIGHT SYSTEM TRACK COVER/LENSE WAS DAMAGED AT ROWS 3 AND 29. REMOVED AND REPLACED LIGHT COVER/LENSE.

Part: WIRE — LOOSE (ROW 2)

FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM THE FORWARD GALLEY TO CABIN ROW 2. FOUND WIRE PULLED OUT OF LIGHT MODULE. REPLACED MODULE. CHECK-C 10-13-98 MCI.

Part: LIGHT — INOPERATIVE (CABIN)

STL - FLT 296 - DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP AT ROW 3C. REPLACED LAMP MODULE ASSEMBLY MFG P/N 0105606-003. (M)

Part: SENSOR — FAILED (RT MLG BRAKE)

CMH - FLT 167 - DURING TAKEOFF ROLL, GOT TEMPERATURE OVERHEAT LIGHT ON BRAKES. TAKEOFF REJECTED. REPLACED RIGHT OUTBOARD BRAKE TEMPERATURE SENSOR. OPERATIONAL CHECK OK. CC-02 LAX 8-26-97. (X)

Part: DUCT — FAILED (LT PACK)

JFK - DURING TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REINSTALLED SEPARATED RUBBER DUCT AT LEFT PACK. ENGINE RUNS AND LEAKS CHECKS NORMAL. (M)

Part: BULB — FAILED (CABIN)

STL - FLT 401 - DURING INSPECTION, FOUND ROW 2 AND ROW 3 EGRESS LIGHTS NOT OPERATING. REPLACE BULBS TW NR 93-2832, MFG 7732. OPERATIONAL CHECK OF EGRESS LIGHTS, CHECK NORMAL. NEW AIRCRAFT 8-25-95.

Part: OVEN — MALFUNCTIONED (GALLEY)

PDX - DURING CRUISE 'D' GALLEY OVEN, MFG P/N 8203-11-0000 EMITTED SMOKE. OVEN WAS TURNED OFF AND CIRCUIT BREAKER PULLED. TROUBLESHOOTING UNDERWAY TO DETERMINE CAUSE. INVESTIGATION REVEALED OVEN HAD INTERNAL MALFUNTION AND WAS RETURNED TO THE MANUFACTURE. (M)

Part: OVEN — SMOKING (GALLEY)

PDX - FLT 173 - DURING CRUISE, 'D' GALLEY OVEN, MFG P/N 8203-11-0000, EMITTED SMOKE. OVEN WAS TURNED OFF AND CIRCUIT BREAKER PULLED. TROUBLESHOOTING UNDERWAY TO DETERMINE CAUSE. OP-16 - 8-25-95 - MCI.