N7531A

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,589 hrs · 31,229 cycles

AFT ACCESS TAIL CONE MOUNT CRACKED AT 5:00 ALIGNMENT PIN MKD. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 51-30-05 AND EA MD80-53-020473.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,589 hrs · 31,229 cycles

AFT ACCESS TAIL CONE MOUNT CRACKED AT 7:00 ALIGNMENT PIN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 51-30-05 AND EA MD80-53-020473.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,307 hrs · 31,048 cycles

ROWS 13 THRU 16 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK FOR ROWS 13 THRU 16 OVERHEAD EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,307 hrs · 31,048 cycles

AFT ACCESSORY COMPARTMENT EMERGENCY OVERHEAD LIGHTS INOPERATIVE. RESEATED BATTERY PACK FOR AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,336 hrs · 30,456 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK ARE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: VALVE — LEAKING (AC BAY) · airframe 59,097 hrs · 30,327 cycles

PHX - CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AIR LEAK AT RIGHT CROSSFEED VALVE. RETORQUED CLAMP NO LEAKS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,746 hrs · 30,134 cycles

CEILING LIGHTS ROW 16 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

THE 1418 FRAME CRACKED AT LONGERON 2 RIGHT. INSTALLED FRAME DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

LONGERON 2 RIGHT CRACKED AT FRAME STATION 1418. PERFORMED LONGERON SPLICE PER AARD 53-30-00-2 FIGURE 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

LEFT ANGLE ON AFT SIDE OF STATION 1418 IS CRACKED AT LONGERON 2 RIGHT. INSTALLED FRAME DOUBLER AT STATION 1418 2 RIGHT PER SRM 53-03-00 FIGURE 31A.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 56,930 hrs · 29,164 cycles

RIGHT SIDE LEADING SLAT CRACKED. LOCATION THE SECOND BRACKET INBOARD FROM OUTERMOST BRACKET. CRACK IS IN THE RADIUS AREA OF OUTBOARD LUG SECOND BRACKET (MARKED). REMOVED 2ND FROM OUTBOARD ATTACH FITTING. LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CORROSION ON NUMBER 5 SEAT TRACK FLOORBOARD SUPPORT OUTBOARD LEG AT STATION 203. INSTALLED STRAP DOUBLER AND FILLER PER AARD 53-20-22-16.

Part: ANGLE — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CORROSION OUT OF LIMITS ON CUSP TEE STATION 208. INSTALLED NEW CUSP ANGLE REPAIR FROM STATION 180 TO STATION 229 RIGHT SPLICE REPAIR PER SRM 53-05-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

DAMAGE ON RIGHT CUSP OUT OF LIMITS STATIONS 1174 TO 1250. INSTALLED NEW CUSP SHEET FROM STATION 1174 TO STATION 1250 PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

CORROSION ON RIGHT CUSP STATION 208. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

CUSP OUT OF LIMITS STATIONS 1155 TO 1174. INSTALLED CUSP REPAIR DOUBLER STATION 1155 TO STATION 1174 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

LEFT CUSP STATIONS 850 TO 857 CORROSION OUT OF LIMITS. INSTALLED REPAIR DOUBLER LEFT CUSP STATIONS 846 TO 863 AS PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CORROSION ON LEFT TIE DOWN STRAP AT STATIONS 1200 TO 1215. INSTALLED TIE DOWN TRACK PER SRM 51-30-01 AND SPLICE PER SRM 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CORROSION ON G-1 GALLEY TIE DOWN FLOOR CENTER FITTING. INSTALLED G-1 GALLEY TIE DOWN FITTING PER SRM 51-30-05.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

REMOVED G-22 MOUNT IN NUMBER 6 SEAT TRACK STATION 217 THAT IS OUT OF LIMITS. INSTALLED G-2 GALLEY MOUNT ON NUMBER 6 SEAT TRACK PER SRM 51-30-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

RIGHT FUSELAGE TO VERTICAL ATTACH ANGLE HAS CRACK. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-2.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

HEAVY CORROSION ON G-1 GALLEY FLOOR TIE DOWN OUTBOARD FITTING. REMOVED AND REPLACED G-1 GALLEY FLOOR TIE DOWN FITTING PER SRM 53-04-00 FIGURE 12B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CABIN LEFT CUSP CORRODED STATIONS 1088 TO 1095. INSTALLED REPAIR DOUBLER ON LEFT CUSP STATIONS 1080 TO 1097 PER AARD 53-20-00-16.

Part: RUB STRIP — WORN (TE FLAP VANE) · airframe 56,930 hrs · 29,164 cycles

RIGHT WING NUMBER 3 FLAP VANE INBOARD END RUB STRIP IS WORN THROUGH AT LEADING EDGE. HOT BOND METAL DOUBLER ON RIGHT WING NUMBER 3 FLAP VANE RUB STRIP TRAILING EDGE PER SRM 51-70-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

LEFT CUSP 888 RIVET HOLE CRACKED. INSTALLED REPAIR DOUBLER LEFT CUSP STATION 888 PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

DENT IN SKIN AT LONGERON 18 LEFT AT STATION 218 AS MARKED. DIMENSIONS ARE 3 INCH BY 3 INCH BY .085 DEPTH. INSTALLED DOUBLER AS PER SRM 53-04-00 FIGURE 12B SHEET 34, CLASS 1 REPAIR.

Part: VANE — GOUGED (TE FLAP) · airframe 56,930 hrs · 29,164 cycles

LEFT WING NUMBER 3 FLAP VANE HAS 2 EACH GOUGES IN LEADING EDGE NEAR INBOARD END. INSTALLED HOT BOND DOUBLER ON NUMBER 3 OUTBOARD FLAP INBOARD VANE ASSEMBLY PER SRM 51-70-2.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

RIGHT CUSP DAMAGED AT STATION 830. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

DAMAGE ON G-2 GALLEY AFT TIE DOWN FLOOR FITTING. INSTALLED NEW FITTING PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

CORROSION ON SEAT TRACK NUMBER 6 OUT OF LIMITS AT STATION 698. INSTALLED PLUG IN SEAT TRACK NUMBER 6 AT STATION 698 PER SRM 53-10-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,930 hrs · 29,164 cycles

DENT IN SKIN AT LONGERON 18 LEFT AT STATION 218. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B SHEET 34 CLASS 1 REPAIR.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,930 hrs · 29,164 cycles

HEAVY CORROSION ON G1 TIE DOWN FITTING CENTER FITTING. INSTALLED NEW GALLEY NUMBER 1 CENTER MOUNT PER SRM 51-30-05.

Part: CONTROL VALVE — STUCK (AC BAY) · airframe 55,480 hrs · 28,392 cycles

CREW REPORTED HIGH TEMPERATURE LIGHT ON FOR TAIL COMPARTMENT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT FLOW CONTROL VALVE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,667 hrs · 27,396 cycles

FOUR (4) CANT FRAME AT STATION 1480 REPAIR DOUBLER HAS TWO CRACKS. REMOVED CRACKED REPAIR DOUBLER AND INSTALLED INTERIM REPAIR DOUBLER PER ONE TIME ESO 80559 DATED 3/6/09.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,667 hrs · 27,396 cycles

AFT CARGO DOOR JAMB LOWER CHORD ANGLE CORRODED AT STATION 1170. REMOVED CORROSION, INSTALLED REPAIR DOUBLER OVER CONDITION 4 AREA PER AARD 53-10-00-3.

Part: BEAM — CRACKED (PAX DOOR) · airframe 53,667 hrs · 27,396 cycles

FWD ENTRY DOOR SECOND FROM TOP HORIZONTAL BEAM CRACKED IN RADIUS AT FWD END. INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 31.

Part: CSD — INOPERATIVE (LT ENGINE)

ELP INFLIGHT T1540/31JUL TUS TO DFW. CREW REPORTED LT GENERATOR CLICKED OFF AND ON SEVERAL TIMES. UNABLE TO DISCONNECT CONSTANT SPEED DRIVE. SHUT DOWN NR 1 ENGINE AND LANDED ELP WITHOUT INCIDENT. ENGINE WINDMILL TIME 15 MINUTES. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: CLAMP — DEFECTIVE (A/C BAY) · airframe 51,902 hrs

ORD INFLIGHT T1345/25JUN. CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION DURING CLIMB. INDICATION EXTINGUISHED WHEN LT AIR CONDITIONING SWITCH PLACED TO OFF POSITION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED CLAMP AND SHIM AT LT HEAT EXCHANGER INLET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 51,333 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 13 TO 16 INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,333 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT CATWALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT FORWARD GALLEY WALL BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY LIGHT MARKER AT RIGHT AFT EXIT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT MARKER AT RIGHT AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

BOS - FORWARD CABIN PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FORWARD CABIN PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA - COCKPIT AND FORWARD AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT POSITION B523 FOR EMERGENCY LIGHT AT COCKPIT AND FORWARD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA EMERGENCY CEILING LIGHTS AT AFT GALLEY DOOR BACK TO SEATING FROM AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK B5-107. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — BROKEN (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, SEAT 13D EMERGENCY LIGHT SOCKET BROKEN. REMOVED AND REPLACED SEAT 13D EMERGENCY LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 22D THROUGH 26D INOPERATIVE. SECURED EMERGENCY EXIT LIGHTS BATTERY AT SEAT 22-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT SIGN INOPERATIVE. TIGHTENED WIRE ON CONNECTOR TO FORWARD LEFT OVERWING EMEGENCY EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN INTERCOSTAL STATION 1309-1322 BETWEEN LONGERON 28R AND 27R. REPLACED INTERCOSTAL PER SRM 51-10-03. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUPPORT ANGLE BLENDED CUT OUT OF LIMITS. INSTALLED NEW Z-ANGLE FLOORBOARD SUPPORT FROM STATION 1117-1155 IAW SRM 51-10-03. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT AND SCRATCH IN FUSELAGE SKIN LEFT SIDE L26 STATION 162 JUST FORWARD AND BELOW FLAP AIRSTAIR DOOR. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON DOOR BEAM STATION 1155-1212 L28R. FOUND CORROSION BLENDED OUT OF LIMITS. INSTALLED NEW DOOR BEAM STATION 1117 TO 1250 IAW AARD 53-10-00-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 5 CORRODED ON OUTBOARD FLANGE STATION 204. REMOVED SECTION OF TRACK AND SPLICED IN NEW SECTION OF SEAT TRACK STATION 200-247 PER SRM 53-05 FIG 4F. (M)

Part: PAN — CORRODED (FUSELAGE)

TUL - FOUND FORWARD CARGO LOWER JAMB THRESHOLD PAN IS CORRODED STATION 370 TO 427. REMOVED AND REPLACED THRESHOLD PAN ASSEMBLY PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 CORRODED STATION 213-218. INSTALLED NEW SEAT TRACK FROM STATION 213-303 PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 3 SEAT TRACK CORRODED IN CHANNEL. REPAIRED PER AARD 53-20-00-10 FIG 4A. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON T-ANGLE STATION 1219 L28R OUTBOARD SIDE. REPLACED T-ANGLE PER AARD 53-10-00-3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND HFEC INDICATES CRACKS EMITTING FROM DEEP SCRATCHES AT LOWER FUSE SKIN ANTENNAS AT STATION 390 AND 402. CUT OUT TWO DAMAGE AREA'S AND INSTALLED REPAIR DOUBLER 13 INCH BY 36 INCH PER SRM 53-04 FIG 170. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK HAS CORRODED AT GALLEY BOLT HOLE STATION 1174. INSTALLED NEW NR 1 SEAT TRACK STATION 1174-1309 SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LOWER SIDE OF RIGHT CUSP AT STATION 544. REMOVED CORROSION, INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN RIGHT CUSP FORWARD OF STATION 427 FRAME. INSTALLED DOUBLER RIGHT CUSP STATION 427 AS PER SRM 53-01 FIG 4-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP BETWEEN SEAT TRACK 1 AND 2 CORRODED. INSTALLED NEW CUSP FROM 1279-1309 PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 1174 AFT OF SERVICE DOOR AT SEAT TRACK MOUNT. CUT OUT CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-00-00-02. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN SHEAR TIE. REMOVED AND REPLACED SHEAR TIE SRM 51-01. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME AT STATION 1456 CRACKED WHERE L3L IS ATTACHED TO IT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-17. (M)

Part: WEB — PUNCTURED (FUSELAGE)

TUL - FOUND HOLE PUNCHED THROUGH RIGHT CUSP AT STATION 484 AND 485. CUT OUT DAMAGED AREA AND INSTALLED A DOUBLER ON CUSP PER SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 288-305. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 280. ROUTED DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 43. (M)

Part: SENSOR — LACK OF LUBE (LT WING)

DFW - FLT 1821 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT DISAGREE LIGHT ILLUMINATED. CREW RAN CHECKLIST AND RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FUOND SENSOR ON LEFT WING STUCK. SENSOR WAS LUBRICATED AND OPS CHECKED NORMAL. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CUSP — CORRODED (BS 560)

TUL - FOUND CORROSION CUSP AT FUSELAGE ATTACH ANGLE FS 560, RT FLOOR SIDE. INSTALLED DOUBLER AT STATION 552 TO STATION 560 PER SRM 53-05. (M)

Part: BREAKER — DEFECTIVE (COCKPIT)

PHX - FLT 821 - DURING CRUISE, THE FORWARD CENTER TANK BOOST PUMP CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. FLIGHT AIR INTERRUPTED AND LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED FORWARD CENTER TANK BOOST PUMP CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PISTON — CRACKED (LT MLG)

TUL - LEFT MLG PISTON, LEFT LUG CRACKED. NDT PROCEDURE MD-80/PT/002. REPLACED WITH SERVICEABLE MLG PISTON. TST: 16,454.22 HRS. CYCLES, 9,103. (X)

Part: BALLAST — OVERHEATED (CABIN)

LGA - FLT 0339 - AT THE GATE PRIOR TO PASSENGER BOARDING, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN AT PASSENGER SEAT 27AB NEAR OVERHEAD BIN. FIRE DEPARTMENT SUMMONED AND FIRE EXTINGUISHED. CHECK OF CABIN OVERHEAD REVEALED FLOURESCENT LIGHT BALLAST AT PASSENGER SEAT 27AB HAD FAILED RESULTING IN ELECTRICAL FIRE. AIRCRAFT MAINTENANCE FERRY LGA/TUL FOR REPAIRS TO LIGHT SYSTEM AND OTHER CONSEQUENTIAL DAMAGE TO CABIN INTERIOR AND FUSELAGE. (W)