N7537A

Part: DUCT — RUPTURED (AC BAY) · airframe 64,184 hrs · 33,151 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED Y DUCT AT RIGHT SIDE PACK BAY THAT WAS RUPTURED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BRAKE — DRAGGING (MLG) · airframe 62,984 hrs · 32,489 cycles

DFW - CREW REPORTED UPON THROTTLES BEING SET FOR TAKEOFF, WHEEL NOT TURNING LIGHT ILLUMINATED. AIRCRAFT DID NOT ACCELERATE MORE THAN 10-15 KNOTS. FLIGHT ABORTED TAKEOFF. REMOVED AND REPLACED NUMBER 4 MAIN LANDING GEAR BRAKE ASSYMBLY DUE TO THE BRAKE DRAGGING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,392 hrs · 31,032 cycles

CEILING EMERGENCY LIGHTS FROM ROW 18 TO 21 INOPERATIVE. RESEATED BATTERY PACK AT ROW 20. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,392 hrs · 31,032 cycles

CEILING EMERGENCY LIGHTS AT ROWS 18 TO 21 INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK AT ROW 20. OPS CHECK NORMAL.

Part: HINGE — WORN (EXTERNAL POWER) · airframe 59,784 hrs · 30,725 cycles

JFK - INGLIGHT LGA-DFW. CREW REPORTED BANGING NOISE HEARD COMING FROM NOSE OF AIRCRAFT. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. NOISE WENT AWAY WHEN GEAR WAS LOWERED. INSPECTED AIRCRAFT AND FOUND HINGE PIN OF THE EXTERNAL POWER ACCESS DOOR PARTIALLY MIGRATED OUT. REPLACED DOOR HINGE ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PISTON — MISSING (NLG STRUT) · airframe 59,523 hrs · 30,577 cycles

DFW - CREW REPORTED NOSE GEAR DOORS WOULD NOT CLOSE UPON RETRACTION. SECOND ATTEMPT HAD NOSE LANDING GEAR FAILED TO RETRACT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE LANDING GEAR STRUT PISTON THAT WAS MISSING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FAN BLADE — DAMAGED (LT ENGINE) · airframe 59,188 hrs · 30,400 cycles

IAH - CREW REPORTED LEFT ENGINE COMPRESSOR STALL ON CLIMBOUT. AUTOPILOT KICKED OFF AND AIRCRAFT YAWED SLIGHTLY. EMERGENCY DECLARED FLIGHT RETURNED IAH LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE AND FOUND LEFT ENGINE HAD ICE INGESTION CAUSING FAN FOD TO 8 FAN BLADES. REPLACED BLADES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 57,869 hrs · 29,678 cycles

TUS - CREW REPORTED POWER PORT SYSTEM ON SEAT 12B SPARKED. CIRCUIT BREAKER PULLED TO STOP SPARKS. EMERGENCY DECLARED, LANDED TUS WITHOUT INCIDENT. REPLACED THE IN SEAT POWER SOURCE AND THE OUTLET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

PLOW ANGLE HAS CORROSION AT STATION 1338 LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPLACED CORRODED PLOW ANGLE WITH NEW ANGLE IAW DWG 9915561, SRM 51-30-2 AND SRM 51-30-05.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CARGO AFT CX CORROSION FORWARD SIDE OF AFT PRESSURE BULKHEAD PLOW ANGLE DOUBLER. DOUBLER WAS OUT OF LIMITS PER SRM 53-01. NEW AFT PRESSURE BULKHEAD DOUBLER (DELTA PLATE) WAS INSTALLED PER BOEING DRAWING PL5910130 AND SRM 51-30-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

PLOW ANGLE CORROSION REMOVAL BEYOND LIMITS. REMOVED AND REPLACED PLOW ANGLE PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,766 hrs · 29,100 cycles

CORROSION ON LEFT TIE DOWN TRACK STA 1220 SPLICE TOP AND BOTTOM IN AFT CARGO. INSTALLED NEW SPLICE PER SRM 51-30.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

AFT CARGO HAS CORROSION LEFT TIE DOWN TRACK ATTACH POINTS AND UPPER EDGE TABS STATION 1220 TO 1322. INSTALLED NEW TRACK PER SRM 51-30.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

DENT IN FUSELAGE STATION 206 BETWEEN LONGERON 4 LEFT AND 5 LEFT. COLD WORKED DENT REF: SRM 53-04 FIG 38 DYE CHECKED NO CRACKS FOUND. INSTALLED DOUBLER PER SRM 53-04 FIG 38.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CORROSION ON FRAME 1231 AFT SIDE LONGERON 30. FRAME 1231 FOUND TO BE OUT OF LIMITS ABOVE LONGERON 30. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER PER AARD 53-10-00-17.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

AFT CARGO FRAME 1271 AFT SIDE LONGERON 27 LEFT TO LONGERON 26 RIGHT HAS CORROSION. BLENDED OUT CORROSION UNDER SRM 51-10-03. OUT OF LIMITS. INSTALLED REPAIR "J" ANGLE DOUBLER UNDER AARD 53-10-00-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

CORROSION TOP SIDE OF SUBFLOOR STATION 200 TO 216 OUTBOARD SIDE OF SEAT TRACK NUMBER 5. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

RIGHT CUSP CRACKED STATION 1173. INSTALLED DOUBLER AT STATION 1173 PER EA MD80-53-009531.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

FITTING IN LOWER FORWARD CORNER OF DOOR CUTOUT IS CRACKED STATION 1155 AT AFT CARGO. INSTALLED NEW CORNER SUPPORT PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

RIGHT CUSP CORRODED AT STATION 1183 TO 1186. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

FUSELAGE DENT AT STATION 300 BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CORROSION AT NUT CLIP HOLE ON OUTBOARD FLANGE OF SEAT TRACK NUMBER 5 STATION 204 OUT OF LIMITS. CUT OUT CORROSION AND INSTALLED STRAP PER AARD 53-20-00-13.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CORROSION ON LOWER AFT FITTING AFT CARGO DOOR CUTOUT STATION 1212. REPLACED SUPPORT FITTING PER AARD 51-00-00-12.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CORROSION TOP OF GALLEY TIE DOWN. INSTALLED NEW GALLEY TIE DOWN FITTING PER SRM 51-30-05.

Part: BEAM — CORRODED (CARGO BAY) · airframe 56,766 hrs · 29,100 cycles

CORROSION ON LOWER DOOR CUTOUT BEAM STATION 1155 TO 1212 ON LOWER LEG FOR AFT CARGO. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3 AND SRM 51-30.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CUSP HAS CORROSION BETWEEN NUMBER 10 SEAT TRACKS STATION 1287. REPLACED LEFT CUSP SHEET STATION 1250 TO 1309 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

CORROSION ON SUBFLOOR UNDER GALLEY TIE DOWN AT STATION 218 RIGHT BUTTLINE 11. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

GALLEY FITTING UNDER SUBFLOOR G-2 GALLEY INBOARD AFT MOUNT CORRODED. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 56,766 hrs · 29,100 cycles

FORWARD ENTRY FORWARD END OF NUMBER 2 BEAM CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05-00 SHEET 13.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

NUMBER 2 SEAT TRACK HAS CORROSION STATION 1305. NUMBER 2 SEAT TRACK WAS REPAIRED PER SRM 53-05-00 FIGURE 4F.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 56,766 hrs · 29,100 cycles

FORWARD ENTRY DOOR AFT END NUMBER 2 BEAM CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05 -00 FIGURE 31 SHEET 13.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

LONGERON 3 LEFT CRACKED OUTBOARD SIDE AT RADIUS STATION 160. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

SUBFLOOR CRACKED STATION 155. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,766 hrs · 29,100 cycles

AFT CARGO CORROSION FORWARD SIDE OF AFT PRESSURE BULKHEAD PLOW ANGLE DOUBLER STATION 1338 LONGERON 30. REPLACED DOUBLER PER SRM 51-01-00 AND SRM 51-30-00.

Part: DOUBLER — CRACKED (WINDOW PAN) · airframe 56,766 hrs · 29,100 cycles

STATION 1022 LEFT WINDOW PAN DOUBLER IS CRACKED AT UPPER AFT CORNER. REPAIRED PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

A 2 INCH CRACK IN LEFT CUSP AT STATION 227 OUTBOARD OF NUMBER 1 SEAT TRACK. REMOVED DAMAGE INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

EMERGENCY EQUIPMENT COMPARTMENT RIGHT SIDE SUB FLOOR CRACKED BELOW GALLEY 1 WATER DRAIN PAN STATION 155. INSTALLED DOUBLER PER AARD 53-20-00-16

Part: VANE — WORN (TE FLAP) · airframe 56,766 hrs · 29,100 cycles

RIGHT WING WORN AREAS OUTBOARD FLAP INBOARD VANE INBOARD LEADING EDGE. DID HOT BOND REPAIR PER SRM 51-70-02.

Part: FITTING — WORN (LE SLAT) · airframe 56,766 hrs · 29,100 cycles

LEFT NUMBER 4 SLAT OUTBOARD KNUCKLE FITTING WORN. REPLACED WORN KNUCKLE FITTING LEFT NUMBER 4 SLAT PER 27-80-00 REPAIR 2 ESO 80117.

Part: RIB — CRACKED (LT WING) · airframe 56,766 hrs · 29,100 cycles

LEFT WING SLAT TRACK ATTACH RIB ON NUMBER 5 SLAT IS CRACKED AT NUMBER 14 SLAT TRACK. REPLACED 2ND FROM OUTBOARD ATTACH FITTING PER ESO 80117.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,766 hrs · 29,100 cycles

CUSP CRACKED AT STATION 218 JUST OUTBOARD OF SEAT TRACK 2. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: ANTI-SKID SYS — CONTAMINATED (MLG) · airframe 55,839 hrs · 28,618 cycles

WHEN LANDING GEAR WAS LOWERED ALL 4 ANTISKID LIGHTS ILLUMINATED WHEN ANTISKID SYSTEM WAS CYCLED. ALL LIGHTS WENT OUT EXCEPT RIGHT INBOARD. ANTISKID CYCLED AGAIN AND LIGHT WENT OUT. FOUND ANTISKID CONTROL BOX CONTAMINATED WITH COFFEE. REPLACED BOX, PERFORMED ALL CHECKS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,914 hrs · 28,114 cycles

FIRST CLASS EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT. / OPS CHECK GOOD.

Part: TUBE — RUPTURED (NR 2 ENGINE) · airframe 54,007 hrs · 27,598 cycles

MCO - CREW REPORTED NUMBER 2 ENGINE BLEED LIGHT AND FULL FIRE WARNING INDICATION CAME ON. EMERGENCY DECLARED, RETURNED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND ANTI-ICING TUBE RUPTURED. REPLACED TUBE ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (ZONE 100) · airframe 53,100 hrs · 27,100 cycles

CANT FRAME CRACKED AT LOWER TAILCONE ALIGNMENT PIN, STATION 1510, LEFT. REPAIRED PER ESO80559 DATED 11-17-08.

Part: FRAME — CRACKED (BS 1418) · airframe 53,100 hrs · 27,105 cycles

FRAME AT STATION 1418 CRACKED AT LONGERON 2L. REPAIRED PER ESO80559 DATED 11-14-08.

Part: SKIN — CRACKED (ZONE 200) · airframe 53,100 hrs · 27,105 cycles

2 CRACKS IN SKIN AT STATION 1380 RT BETWEEN LONGERON 13R AND 14R. INSTALLED DOUBLER PER SRM 53-01-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,429 hrs

LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

LGA - COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

LGA - FORWARD SECTION SEAT MOUNTED EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD SECTION SEAT MOUNTED EMERGENCY EGRESS LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT RIGHT OVERWING AFT EXIT INOPERATIVE. REPLACED BATTERY PACK B2505 FOR EMERGENCY LIGHTS AT RIGHT OVERWING AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS IN CEILING ABOVE SEATS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING ABOVE SEATS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — DEFECTIVE (FUEL SYSTEM)

MSP T1510/04 EN ROUTE MSP-DFW AFT CENTER FUEL TANK BOOST PUMP POPPING CIRCUIT BREAKER. RETURNED MSP AND LANDED WITHOUT INCIDENT. PLACARDED AFT CENTER FUEL TANK BOOST PUMP PER MEL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT TAIL COMPARTMENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ORD - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTS AT ROW 20 INOPERATIVE. REPLACED AFT EMERGENCY EXIT PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT ZONE SEAT MOUNTED EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (FWD AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. SECURED EMERGENCY EXIT LIGHT QUICK DISCONNECT AT FORWARD AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION UNDER FASTENERS ON INSIDE FRAME AT STATION 1463. INSTALLED DOUBLER PER ESO DATED 5-30-02, SPOT FACED CORROSION AREAS. STRAP INSTALLED, 2 ROWS OF FASTENERS. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND WEB CORRODED SEVERAL AREAS FS 1213-1215 ABOVE L28R WEB BLOWN OUT. INSTALLED NEW WEB PER SRM 51-01. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CARGO CUT OUT LOWER FRAME HAS CORROSION ON OUTBOARD FACE STATION 1155-1211, SEVERAL AREAS. INSTALLED NEW FRAME PER SRM 51-01. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND TOP FLANGE OF INTERCOSTAL CRACKED AT TWO FASTENER HOLES BELOW CABIN FLOOR, BL0. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW PER SRM 51-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND TWO DEEP DENTS IN SKIN STATION 452 BETWEEN LONGERON 22 AND 23L. INSTALLED PERMANENT EXTERNAL REPAIR PER SRM 53-04 FIG 12B SHEET 4, 5, 6 95 AND 96. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FORWARD CARGO DOOR FRAME, LOWER THRESHOLD AT STATION 405. REMOVED AND REPLACED SECTION OF PAN (THRESHOLD) PER SRM 53-05 FIG 44. (M)

Part: ATTACH ANGLE — CRACKED (EMPENNAGE)

TUL - FOUND CRACK BETWEEN RIVETS ON VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE 8 INCHE FORWARD OF VERTICAL REAR SPAR ATTACH POINT. CUT OUT DAMAGED AREA. INSTALLED DOUBLER ANGLE PER AARD 53-10-00-2. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CREASE IN SKIN ALONG FRAME AND SEVERAL DENTS IN SKIN STATION 277 ABOVE LONGERON 18L. INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND TWO DEEP GOUGES STATION 387-395 LONGERON 23L, STATION 369-374 STATION 370. INSTALLED PERMANENT REPAIR PER SRM 5304 FIG 12B SHEET 4, 5, 6 AND 95, 96. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

TUL - FLOORBEAM CRACKED, STATION 927, LBL 56. REMOVED AND INSTALLED NEW FLOORBEAM PER SRM 51-01. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED AFT SIDE OF 1437 FRAME BETWEEN L1 AND L2R. INSTALLED NEW SHEAR TIE SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1236 AND 1208. REPAIRED DAMAGED AREAS PER AARD 53-20-00-10. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN RUNNING PARALLEL TO LONGERON 23L FROM STATION 387-395. INSTALLED PERMANENT REPAIR (CLAS 1) PER SRM 53-04 FIG 12B SHEET 4, 5, 6 AND 95, 96. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BOTTOM SIDE OF LEFT CUSP STATION 617-622. REMOVED CORROSION AND INSTALLED DOUBLER AS PER SRM 53-01 PAGE 18. (M)

Part: FRAME — DAMAGED (FUSELAGE)

TUL - ROUTED FRAME PREVIOUSLY WITHOUT REPAIR. INSTALLED STRAP REPAIR PER AARD 53-10-00-25. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION TOP CUSP STATION 549-533, LEFT SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01 PAGE 18. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1193. INSTALLED PLUG REPAIR AS PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 CORRODED STATION 451-458. INSTALLED SLAT TRACK REPAIR PER SRM 53-05 FIG 4A SHEET 1 AND 2. (M)

Part: LONGERON — GOUGED (FUSELAGE)

TUL - FOUND STATION 1306 ABOVE LONGERON 19R SKIN GOUGED. CUT OUT GOUGED AREA AND INSTALLED INTERNAL DOUBLER AND PLUG PER SRM 53-04 FIG 38 SHT 24 AND INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M)

Part: OVEN — ODOR (FWD GALLEY)

DFW - FLT 353 - EN ROUTE LGA-ORD, AT 31,000 FEET NR 1 FLIGHT ATTENDANT REPORTED SMOKE AND FUMES COMING FROM CEILING NEAR FORWARD GALLEY. SHUTOFF GALLEY POWER, RE-CIRCULATION FAN PASSENGER PHONES AND POWER PORTS FOR SEATS, RAN SMOKE REMOVAL PROCEDURES. FUMES WERE REDUCED BUT WOULD NOT GO AWAY SMELLED LIKE BURNING ELECTRICAL OR PLASTIC. LANDED BUF WITHOUT INCIDENT. REPLACED FORWARD GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING SIGN INOPERATIVE. REPLACED CONNECTOR PIN ON FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY WALK-AROUND EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REPLACED WALK-AROUND EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE GALLEY DOOR EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REINSTALLED PINS IN QUICK DISCONNECT CONNECTOR FOR GALLEY DOOR EMERGENCY EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (GALLEY)

DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIP AT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (BS 237)

TUL - DENT AND CREASE IN FUSELAGE SKIN, STA 237 BETWEEN LONGERON 18L AND LONGERON 19L. ALSO, INTERNAL DAMAGE TO FUSELAGE FRAME, BENT AND CRACKED, AT SAME LOCATION. REMOVED DAMAGED SECTION OF FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-04, FIG 38. REMOVED DAMAGED FORMER. INSTALLED NEW SECTION. TST: 23,605.42 HOURS. CYCLES: 12,312. (X)

Part: TIE DOWN — CORRODED (BS 1057)

TUL - CORROSION ON AFT ARGO TIE DOWN TRACK FROM STA 1025 TO STA 1155. CORROSION REMOVAL EXCEEDED MAXIMUM ALLOWABLE AT STA 1057. INSTALLED REPAIR STRAP PER AARD 53-20-00-13 AT THIS LOCATION. TST: 23,605 HOURS. CYCLES: 12,312. (X)

Part: TIE DOWN — CORRODED (BS 1212)

TUL - CORROSION ON RT TIE DOWN TRACK, OUTBOARD FLANGE, STA 1212. REMOVED CORROSION. CUT-OUT DAMAGED AREA. INSTALLED FILLER AND STRAP REPAIR PER ESO 80559, DATED 8-20-98 AND SRM AARD 53-20-00-13. TST: 23,605.42 HOURS. CYCLES: 12,312. (X)

Part: FRAME — CORRODED (BS 1287)

TUL - AFT CARGO CORROSION ON FRAME AFT SIDE LOWER LIP FS 1287 FROM LG 29R, LG29L. INSTALLED DOUBLER PER 53-03. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN THE FIRST 10 ROWS OF COACH FOUND INOPERATIVE. REPLACED BROKED EMERGENCY FLOOR LIGHT STRIP CONNECTOR IN FWD PART OF COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)