N3515

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 65,601 hrs · 34,814 cycles

RIGHT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES ON RIGHT AFT LAVATORY FORWARD BATTERY PACK. OPS CHECK NORMAL.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 65,380 hrs · 34,684 cycles

SAT - INFLIGHT DFW-MEX. CREW REPORTED LEFT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT FAULTED. EMERGENCY DECLARED FLIGHT DIVERTED SAT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT, LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PSEU — INOPERATIVE (LANDING GEAR) · airframe 64,788 hrs · 34,342 cycles

DFW - CREW REPORTED GEAR DOWN INDICATIONS WERE RED. SECOND TIME GEAR INDICATION LIGHTS WERE RED BUT THEN TURNED GREEN. TOWER VERIFIED GEAR WAS IN THE DOWN POSITION. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 63,117 hrs · 33,418 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,117 hrs · 33,418 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED RIGHT AFT LAVATORY FORWARD BATTERY PACK. OPS CHECK NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 62,440 hrs · 33,041 cycles

DFW - CREW REPORTED DURING CLIMBOUT, LEFT ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO WITH QUANTITY NORMAL. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 7 MINS). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT DFW ON 09/26/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,654 hrs · 31,508 cycles

CUSP CRACKED IN ELECTRICAL EQUIPMENT COMPARTMENT JUST AFT OF STATION 157 APROXIMATLEY 18 INCHES OF FORWARD SERVICE DOOR. INSTALLED NEW CUSP SUB-FLOOR AND DOUBLER PER AARD53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,654 hrs · 31,508 cycles

SUBFLOOR DOUBLER UNDER G-1 GALLEY DRAIN PAN CORRODED. REPAIRED SUBFLOOR UNDER G-1 GALLEY DRAIN PAN REFERENCE PRELIMINARY EA DATED 10-8-10 AND FINAL EA MD80-53-013476 AND AARD 53-20-00-16.

Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 59,654 hrs · 31,508 cycles

AIRSTAIR DOOR DEEP DENT RIGHT SIDE. INSTALLED DOUBLER PER SRM 52-01-00 FIGURE 4 SHEET 3.

Part: SKIN — GOUGED (LE SLAT) · airframe 59,654 hrs · 31,508 cycles

LEFT WING SLAT 2 EACH GOUGES ON BOTTOM SIDE OF SLAT AT SLAT TRACK NUMBER 11, MARKED. LEFT WING SLAT CUT OUT DAMAGED AREA AND INSTALLED FLUSH PATCH REPAIR PER AARD 57-50-00-5.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 57,274 hrs · 30,203 cycles

FIRST CLASS EMERGENCY FLOOR LIGHT INOPERATIVE. REPAIRED OPEN WIRE FOR EMERGENCY LIGHT FIRST CLASS GALLEY.

Part: PITOT TUBE — FAILED (RUDDER LIMITER) · airframe 57,023 hrs · 30,073 cycles

INFLIGHT BWI TO DFW. ON CLIMBOUT OF BWI THE RUDDER LIMITER PITOT HEATER FAILED. RESET CIRCUIT BREAKER ONE TIME BUT IT POPPED AGAIN. LANDED LGA WITHOUT INCIDENT. REPLACED THE RUDDER LIMITER PITOT HEATER.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 56,836 hrs · 29,971 cycles

CREW REPORTED YELLOW LANDING GEAR DOOR OPEN LIGHT IN CRUISE. UPON LOWERING LANDING GEAR FOR LANDING GEAR DOOR LIGHT STAYED ON. LANDED LGA WITHOUT INCIDENT. PINNED GEAR ON RUNWAY AND TOWED TO GATE. REPLACED RIGHT MAIN GEAR DOOR PROXIMITY SENSOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,395 hrs · 29,731 cycles

EMERGENCY AISLE BATTERY PACK IS WEAK. REMOVED AND REPLACED WITH SERVICEABLE BATTERY PACK IAW MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,395 hrs · 29,731 cycles

EMERGENCY AISLE BATTERY PACK IS WEAK. REMOVED AND REPLACED WITH SERVICEABLE BATTERY PACK IAW MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,395 hrs · 29,731 cycles

EMERGENCY AISLE BATTERY PACK IS WEAK. REMOVED AND REPLACED WITH SERVICEABLE BATTERY PACK IAW MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,025 hrs

BPS - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS.

Part: CASTING — CRACKED (SPOILER) · airframe 55,486 hrs · 29,230 cycles

LEFT WING GROUND SPOILER CASTING CRACKED AT FORWARD INBOARD END. INSTALLED DOUBLER PER AARD 57-20-00-15 PAGE 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON LEFT CUSP STATION 1060-1098. INSTALLED DOUBLER PER EA MD80-53-005855 AND AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

FORWARD OUTBOARD G-2 GALLEY MOUNT BRACKET CORRODED AND BLENDED OUT OF LIMITS. INSTALLED NEW G-2 GALLEY MOUNT PER SRM 51-30-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

CRACK ON FLOORBOARD SUPPORT BRACKET AT STATION 927. INSTALLED NEW FLOORBOARD SUPPORT BRACKET PER SRM 51-01-00.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,485 hrs · 29,230 cycles

AFT SERVICE DOOR, FORWARD GIRT BAR FLOOR SUPPORT BRACKET AND SPACERS ARE CORRODED. INSTALLED NEW GIRT BAR SUPPORT BRACKET AND SPACERS PER SRM 51-30-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

FLOORBOARD SUPPORT IS CRACKED AT STATION 845 BELOW NR 4 SEAT TRACK. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,485 hrs · 29,230 cycles

FLOORBOARD SUPPORT CRACKED STATION 886. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-01-06.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON SHEAR TIE IN AFT CARGO AT STATION 1287. INSTALLED NEW SHEAR TIE WITH DOUBLER STRAPS PER SRM 53-03-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,485 hrs · 29,230 cycles

CORROSION ON FLOORBOARD SUPPORT TEE SECTION STATION 1155 TO 1212 LONGERON 23. REMOVED AND REPLACED FLOORBOARD SUPPORT TEE SECTION PER AARD 51-00-00-012.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

FLOORBOARD SUPPORT IS CRACKED AT STATION 972 BELOW NR 5 SEAT TRACK. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

LONGERON 2L CRACKED AT STATION 160. CUT OUT DAMAGED LONGERON AND INSTALLED LONGERON SPLICE PER SRM 53-02-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

CRACKS IN CUSP AT STATION 804 JUST OUTBOARD OF NR 1 SEAT TRACK AT AFT OUTBOARD CORNER OF SEAT TRACK. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,485 hrs · 29,230 cycles

FLOORBOARD SUPPORT CRACKED STATION 864. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,485 hrs · 29,230 cycles

FLOORBOARD SUPPORT CRACKED UNDER NUMBER 4 SEAT TRACK STATION 905. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-01-06.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON FRAME AT STATION 1309 LONGERON 30. REMOVED CORROSION AND INSTALLED DOUBLER AND FRAME REPAIR PER AARD 53-10-00-14.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON FRAME LOWER FLANGE AT STATION 1271 LONGERON 29L- LONGERON 30. INSTALLED J-ANGLE DOUBLER PER AARD 53-10-00-14 REPAIR 1.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION IN LOWER CORNER BRACKET AT STATION 1156 OUTBOARD OF LOWER DOOR BEAM FORWARD END, IN AFT CARGO. INSTALLED NEW BRACKET PER SRM 51-30-5 AND AARD 51-00-00-012.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

CRACK ON INTERCOSTAL ON FORWARD SIDE OF FLOORBEAM STATION 1041. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIGURE 2 SHEET 4.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON UPPER AND LOWER LEG OF MID CARGO DOOR BEAM, STATION 636-693. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

WINDOW PAN CRACKED IN UPPER AFT CORNER AT STATION 1041 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON SUBFLOOR UNDER FORWARD GIRT BAR BRACKET OF AFT SERVICE DOOR AT STATION 1140. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON AFT CARGO DOOR BEAM VERTICAL AND HORIZONTAL LEGS STATION 1158-1209. INSTALLED REPAIR ON DOOR BEAM PER AARD 53-10-00-3.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

TORN CUSP SHEET AT STATION 160 LEFT SIDE AT AIRSTAIR ROD. INSTALLED DOUBLER ON CUSP MEMBRANE PER EA MD80-53-005776.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,486 hrs · 29,230 cycles

RIGHT CUSP HAS CORROSION BETWEEN STATION 1212 AND 1231. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,486 hrs · 29,230 cycles

CRACK IN CUSP FROM LIGHTENING HOLE TO LIGHTENING HOLE RIGHT SIDE STATION 1300. INSTALLED DOUBLER PER EA MD80-53-005822 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

CORROSION ON RIGHT CUSP STATION 1193-1212. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 55,486 hrs · 29,230 cycles

NR 2 GALLEY INBOARD MOUNT FORWARD END AT STATION 200 CORRODED. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,485 hrs · 29,230 cycles

WINDOW PAN CRACKED AT AFT UPPER CORNER AT STATION 1041 RIGHT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: ENGINE — LEAKING (NR 1) · 54,325 cycles

EWR INFLT T1323/27SEP JFK TO ORD CREW REPORTED VIBRATION IN AIRFRAME FOLLOWED BY NR 1 ENGINE OIL QUANTITY LOSS AND OIL TEMPERATURE INCREASE. CREW SHUT DOWN NR 1 ENGINE. LANDED EWR WITHOUT INCIDENT. SINGLE ENGINE TIME 15 TO 20 MINUTES. REPLACED NR 1 ENGINE ON 28 SEP AT EWR DUE TO OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,752 hrs · 53,752 cycles

LGA - EMERGENCY LIGHT AT OVERHEAD TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT RT AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,257 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 20 INOPERATIVE. REPLACED RESET BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BOOT — LOOSE (RT ENGINE)

LBB INFLIGHT T389/31JUL DFW TO ABQ - DURING FLIGHT CREW RECEIVED TAIL COMPARTMENT HIGH INDICATION. LANDED LBB WITHOUT INCIDENT. SECURED BOOT AT RIGHT TEMPERATURE CONTROL VALVE INLET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PISTON — INOPERATIVE (NLG)

ORD INFLIGHT T1462/10FEB - ON RETRACTION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPACKED NOSE GEAR LOWER PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 13, 16, 23 AND 32DEF, AND 12, 16, 23, 25, 27AB AND FIRST CLASS AND FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED BATTERY PACKS FOR ROWS 13, 16, 23 AND 32DEF, AND 12, 16, 23, 25, 27AB AND FIRST CLASS AND FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RDU - EMERGENCY LIGHTS ABOVE AFT STAIRS INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS ABOVE AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAD - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE IN THE FIRST CLASS SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT GALLEY LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTING FROM ROW 13-17 INOPERATIVE. REPOSITIONED CEILING EMERGENCY EXIT LIGHTING BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY ENTRANCE EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS CONNECTOR BACKSHELL BROKEN. REPLACED EMERGENCY EXIT LIGHT CONNECTOR BACKSHELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FS 200-245)

TUL - FOUND SEAT TRACK NR 5 CORRODED STATION 200-245. INSTALLED SEAT TRACK FROM STATION 200-245 NR 5. (M)

Part: SKIN — DENTED (ENTRY DOOR)

TUL - FOUND 6 INCH DENT ON EXTERIOR SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 52-05 FIG 37. (M)

Part: WEB (FS 200-210)

TUL - FOUND ACCESS HOLE REQUIRED TO FOM AT STATION 200-210 BETWEEN SEAT TRACK 5/6 RT. INSTALLED DOUBLER OVER ACCESS HOLE AT STATION 200-210 PER SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP LAYER OF SUBFLOOR RIGHT SIDE STATION 180 TO 179 RBL 48 TO OUTBOARD OF A/C. INSTALLED DOUBLER AND FILLER PER SRM 53-01 FIG 4. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND VARIOUS SPOTS OF CORROSION ON CUSP T FROM STATION 185 TO STATION 232 RIGHT AT FORWARD SERVICE DOOR. SPLICED IN NEW CUSP T ANGLE PER SRM 53-05 PART 1 FIGURE 55 SHEET 2. (M)

Part: ANGLE — CORRODED (FS 951)

TUL - FOUND ANGLE AT TOP OF TRAPEZOIDAL PANEL CORRODED AROUND FASTENERS STATION 951-955. REMOVED AND REPLACED ANGLE SRM 51-01. (M)

Part: SKIN — DENTED (FS 229-264)

TUL - FOUND SEVERAL DENTS AND GOUGES IN FUSELAGE SKIN STATION 229 TO 264 LONGERONS 18 TO 20 LEFT. INSTALLED DOUBLER PER ESO 80559 DATED 5-11-2001. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CANT FRAME 1485 IS CRACKED AT STAIR ACTUATOR CASTING. INSTALLED REPAIR SPLICE AS PER AARD 53-10-00-33. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 1250 THROUGH 1308. INSTALLED NEW CUSP SHEET STATION 1250 THROUGH 1308 SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FS 1164-1309)

TUL - FOUND CORROSION AND GOUGES ON SEAT TRACK NR 3 STATION 1164-1309. REPLACED SEAT TRACK STATION 1164-1309, SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION NR 2 SEAT TRACK STATION 1300, 1251, AND 1287. INSTALLED NEW SECTION OF NR 2 SEAT TRACK FROM STATION 1240 TO 1309 PER SRM 53-05 FIG NR 4F. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED STATION 1174 TO 1250. REPLACED LEFT CUSP STATION 1174-1250 PER SRM 51-01. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO DOOR JAMB BEAM FROM STATION 1160-1208. REPLACED DOOR BEAM PER SRM 51-30-5. (M)

Part: PLATE — CORRODED (VERTICAL STAB)

TUL - FOUND 4 INCH BY 4 INCH CORROSION ON ALL 4 VERTICAL STABILIZER HINGE PLATES FOR HORIZONTAL STABILIZER. REMOVED PLATES AND REPLACED SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND STATION 1170 LEFT CUSP CORRODED UNDER FLOOR. INSTALLED DOUBLER PER AARD 53-00-00-2 AND SRM 53-0 FIG 43. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP 1.5 INCH BY 1 INCH THROUGH CUSP. CUT OUT DAMAGED CORROSION INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FS 1176-1279)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK, 1 INCH BY 103 INCHES. REMOVED AND REPLACED SEAT TRACK NR 1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOORBEAM TOP STATION 1338 AT SCREW HOLES UNDER RIGHT AFT LAV. BLENDED OUT CORROSION INSTALLED WEAT STRIPS PER SRM 53-05 PART 1 PAGE 30A. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP OF 1322 FLOORBEAM RIGHT LAV AFT .25 INCH HOLE. BLENDED OUT CORROSION INSTALLED WEAR STRIPS PER SRM 53-05 PART 1 PAG 30A. (M)

Part: SEAT TRACK — CORRODED (FS 1289)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK AT STATION 1289 AROUND SCREW HOLE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — GOUGED (FS 898)

TUL - FOUND DEEP GOUGES IN NR 3 SEAT TRACK STATION 898. CUT OUT DAMAGE, INSTALLED SEAT TRACK PLUG PER SRM 53-04-4A. (M)

Part: SEAT TRACK — CUT (FS 880)

TUL - FOUND DEEP CUT IN NR 3 SEAT TRACK TIE DOWN LUG INBOARD SIDE STATION 880. CUT OUT DAMAGE, INSTALLED SEAT TRACK PLUG PER SRM 53-05-4A. (M)

Part: SKIN — DENTED (FS 247)

TUL - FOUND DENT 48 INCHES AFT OF FORWARD ENTRY DOOR 3 INCH BELOW RED STRIPE. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38, DAMAGED AND REMOVED. (M)

Part: SEAT TRACK — CORRODED (FS 1284)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1284. CUT OUT CORROSION AND INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTNANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 27 THROUGH 29 DIM. REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSMITTER — MALFUNCTIONED (RT ENGINE)

MSY - FLT 1318 - DURING FLIGHT CREW NOTICED LEFT ENGINE FUEL FLOW INDICATOR INDICATES 2000 LBS HIGHER THAN RIGHT SIDE. SUSPECTED FUEL LEAK. RETURNED AND LANDED MSY WITHOUT INCIDENT. NO FUEL LEAK FOUND. REPLACED FUEL FLOW TRANSMITTER, INDICATOR AND POWER SUPPLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. OVERWING EMERGENCY EXIT LIGHT ASSEMBLY SHORTED TO SIDEWALL GRILL. REPLACED OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: APU — LEAKING (APU COMP)

BOS - FLT 1527 - AFTER TAKEOFF BOS CREW NOTICED SMOKE IN CABIN. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. CHANGED APU AND REPLACED BOTH WATER SEPARATOR BAGS. CLEANED INSIDE OF WATER SEPARATOR AND ACCOMPLISHED PACK BURNOUT OF HIGH PRESSURE DUCTING. ALL WORK ACCOMPLISHED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (CABIN)

DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHTING WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (COCKPIT)

BOS - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE EMERGENCY LIGHTS.

Part: PIPE — CRACKED (AFT FUSELAGE)

DFW - FLT 2030 - AFTER TAKEOFF BDL DURING CLIMB-OUT, OILY ODOR NOTED IN CABIN. ACCOMPLISHED ABNORMAL PROCEDURE AND ODOR DISSIPATED WHEN RIGHT PACK SHUT DOWN. NO OTHER ABNORMAL IND AND A/C PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. REPLACED THRUST REVERSER HYDRAULIC PRESSURE PIPE FOUND CRACKED AND LEAKING HYDRAULIC FLUID WHICH WAS INGESTED INTO APU INLET. ACCOMPLISHED PACK BURNOUT PROCEDURE AND REPLACED BOTH COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEMS LEAK AND GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M)