N7512A

Part: WIRE — DAMAGED (CABIN) · airframe 63,842 hrs · 33,245 cycles

EGRESS LIGHT WILL NOT COME ON IN FORWARD CABIN. REPAIR DAMAGED WIRE AT SEAT ROW 18DEF.

Part: CLAMP — LOOSE (AC BAY) · airframe 62,063 hrs · 32,231 cycles

MCI - INFLIGHT ORD-AUS. CREW REPORTED RIGHT PACK FAILED AND LEFT PACK FAILED IN DESCENT. EMERGENCY DECLARED FLIGHT DIVERTED MCI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TIGHTENED BOTH CLAMPS FOR RUBBER BOOT JUST OUTBOARD OF GROUND AIR CONDITIONING CHECK VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — BROKEN (CABIN) · airframe 60,167 hrs · 31,191 cycles

ROW 14 SEAT MOUNTED ESCAPE PATH LIGHTING DOES NOT ILLUMINATE. REPLACED PLUG FOR ROW 14 SEAT MOUNTED ESCAPE PATH LIGHTING. OPS CHECKED NORMAL.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,167 hrs · 31,191 cycles

LEFT FORWARD EXIT DOOR JAMB CRACKED AT UPPER STOP. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 32.

Part: PITOT TUBE — INOPERATIVE (ANTI-ICE SYS) · airframe 59,424 hrs · 30,774 cycles

STL - INFLIGHT ORD-DEN. CREW REPORTED PITOT STALL HEATER OFF LIGHT ILLUMINATED. FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY PITOT TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,524 hrs · 30,304 cycles

FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,908 hrs · 29,967 cycles

EMERGENCY LIGHT BATTERY PACK IN OVERHEAD FIRST CLASS AREA FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. SYSTEM TESTS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,908 hrs · 29,967 cycles

EMERGENCY ESCAPE PATH AT SEAT ROWS 5 TO 19 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM CHECKS TESTS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,717 hrs

LGA - INSIDE RIGHT AFT OVERWING HATCH EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT AFT OVERWING HATCH EXIT.

Part: SKIN — DAMAGED (TE FLAP) · airframe 56,138 hrs · 28,970 cycles

FOREIGN OBJECT DAMAGE LOWER SKIN INBOARD WEDGE. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FLUSH PERMANENT REPAIR DOUBLER AND FILLER PER SRM 57-01-00 FIGURE 5 SHEET 2.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

CRACK AT TOP OF STIFFENER FORWARD SIDE PRESSURE BULKHEAD ABOVE VAULT DOOR. REMOVED AND REPLACED STIFFENER PER SRM 51-01-00.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

LEFT TIE DOWN TRACK INBOARD SIDE CORRODED AT STATION 1214 OF AFT CARGO. INSTALLED NEW SPLICE PER SRM 51-10-03.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

CORROSION BOTTOM SIDE OF RIGHT CUSP STATION 1275 TO 1295. INSTALLED NEW CUSP BETWEEN STATION 1250 AND 1309 PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

AFT CARGO LEFT TIE DOWN TRACK CORRODED AT STATION 1117 TO 1212. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,138 hrs · 28,970 cycles

SKIN CRACKED AT CANT STATION 1474 LONGERON 24 LEFT. INSTALLED DOUBLER PER SRM 53-01-00 PG 12.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

CORROSION ON VERTICAL AND HORIZONTAL LEG OF DOOR JAMB BEAM AT MID CARGO. INSTALLED DOUBLER IN ACCORDANCE WITH 53 10 00 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

NUMBER 5 SEAT TRACK BLENDED OUT OF LIMITS. INSTALLED NEW SEAT TRACK AND SPLICE PER SRM 53-05-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,138 hrs · 28,970 cycles

CRACK ON LEFT CUSP BETWEEN STATION 218 AND 237. INSTALLED CUSP SHEET PER AARD 53-20-10-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

RIGHT CUSP CORRODED AT STATION 1161 TO 1174. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (ZONE 100) · airframe 56,138 hrs · 28,970 cycles

DENT IN SKIN AT RIGHT STATION 213 BETWEEN LONGERON 24 RIGHT AND LONGERON 25 RIGHT. AREA OF DISCREPANCY IS 4.3 INCHES AND .248 INCH DEEP. INSTALLED DOUBLER CLASS I PER SRM 53-04-00 FIGURE 12B PAGE 36 SHEET 4.

Part: BRACKET — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

SEAT TRACK BRACKET CORRODED AT STATION 864. AREA OF DISCREPANCY IS 4 INCHES BY 4 INCHES. REPLACED SEAT TRACK BRACKET PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

CORROSION ON NUMBER 2 SEAT TRACK. REPLACED SEAT TRACK PER SRM 51-01-00.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 56,138 hrs · 28,970 cycles

RIGHT CUSP CRACKED STATION 1244. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,138 hrs · 28,970 cycles

CORROSION ON LEFT CUSP OUTER EDGE AT CENTER LIGHTING HOLE BETWEEN STATION 636 TO 655. REMOVED CORROSION PER SRM 53-01 AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-10.

Part: STOP — CRACKED (ZONE 800) · airframe 56,138 hrs · 28,970 cycles

FORWARD LOWER DOOR STOP PAD CRACKED. INSTALLED NEW DOOR STOP SUPPORT FITTING PER ESO 80174.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,138 hrs · 28,970 cycles

CORROSION AND CRACK ON LEFT CUSP AT STATION 965 TO 984. REMOVED DAMAGE AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 20 00 16.

Part: SKIN — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

ATTACH TAB CRACKED FROM FRAME TO LONGERON 11 LEFT AT STATION 207 AFT OF FORWARD ENTRY DOOR. INSTALLED REPAIR STRAP PER AARD 53-10-00-11.

Part: PAN — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

RIGHT WINDOW PAN AT UPPER CORNER STATION 1231 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

AFT UPPER WINDOW FRAME TAB CRACKED AT LEFT STATION 1022 TO 1041. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25 MSR 018353.

Part: PAN — CRACKED (WINDOW) · airframe 56,138 hrs · 28,970 cycles

RIGHT WINDOW PAN AT STATION 1193 UPPER CORNER CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

LOWER WINDOW FRAME TAB CRACKED AT LEFT STATION 1022 TO 1041. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25, MSR 018352.

Part: PAN — CRACKED (WINDOW) · airframe 56,138 hrs · 28,970 cycles

RIGHT WINDOW PAN AT STATION 1212 CRACKED UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 56,138 hrs · 28,970 cycles

FORWARD LOWER WINDOW FRAME TAB AT LEFT STATION 1079 TO 1098 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25, MSR 018339.

Part: LIGHT — DAMAGED (CABIN) · 54,972 cycles

MSP EMERGENCY LIGHT AT SEAT 7D LIGHT ASSEMBLY MISSING PARTS. REPLACED HARNESS AND LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 21D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 27D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GUARD — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 21D MISSING GUARD. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GUARD — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 21D MISSING GUARD. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD STATION 1400 HAS QUICK DISCONNECT DISCONNECTED. RECONNECTED QUICK DISCONNECT FOR EMERGENCY LIGHT AT OVERHEAD STATION 1400. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — LOOSE (GALLEY DOOR)

MEX - EMERGENCY SLIDE AT AFT GALLEY DOOR LOOSE. REPOSITIONED EMERGENCY SLIDE AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR INOPERATIVE EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SAT - FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS THROUGH FRONT OF COACH SECTION INOPERATIVE. SECURED OVERHEAD EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 19-21 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (TAILCONE)

ORD - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT CEILING LIGHT RIGHT SIDE DOES NOT ILLUMINATE PROPERLY. REPAIRED EMERGENCY EXIT TAIL CONE SLIDE EMERGENCY EXIT LIGHT HOUSING WIRES AND REPLACED AFT AIRSTAIR EMERGENCY EXIT CEILING LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT LOWER EMERGENCY EXIT SLIDE LIGHT DID NOT ILLUMINATE. REPLACED AFT LOWER EMERGENCY EXIT SLIDE LIGHT BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SMALL DENT IN SKIN AT STATION 237 BETWEEN LONGERON 18-19L. INSTALLED DOUBLER AT DENT PER SRM 53-04 FIG 12B. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME CRACKED AT AIRSTAIR ACTUATOR BRACKET, STATION 1485. REPAIRED FRAME PER ESO 80559 DATED 2/16/2001. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 1401, 8 INCHES ABOVE THE NR 2 ENGINE PYLON. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND STATION 1200R FLOOR CUSP HAS HOLE OUTBOARD OF NR 6 SEAT TRACK. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP WEB AT STATION 795. REMOVED DAMAGED AREA AND INSTALLED REPAIR DUOBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK STATION 1174-1309. REMOVED AND REPLACED SECTION OF NR 2 SEAT TRACK STATION 1174-1309 SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND 2 INCHES BY 76 INCHES CORROSION ON LEFT CUSP STATION 1174. INSTALLED NEW SERVICEABLE LEFT CUSP STATION 1174-1250 PER SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FUOND SEAT TRACK NR 6 CORRODED FROM STATION 303-798. INSTALLED NEW SEAT TRACK NR 6 FROM STATION 303-798 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK FROM 1174-1309. INSTALLED SERVICEABLE SEAT TRACK FROM STATION 1170-1309 AS PER SRM 51-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 2R CRACKED AT STATION 1418. INSTALLED NEW SECTION OF LONGERON EXTRUSION AS PER AARD 53-30-00-2, PAGE NR 1 AND NR 2. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND CRACKED AT STATION 486 AND 570. REMOVED DAMAGED AT STATION 486 AND 570 AND INSTALLED DOUBLER PER AARD 53-00-00-02 FIG 1. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND HORIZONTAL SCRATCH 4 INCHES IN LENGTH 2 FEET AFT OF POSS ENTRY DOOR EVEN WITH BUTTON OF DOOR AND SHEAR TIE CRACKED. DAMAGED AREA CUTOUT AND SHEAR TIE REMOVED DOUBLER AND NEW SHEAR TIE INSTALLED PER SRM 53-04 FIG 12B AND 51-01. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP WEB AT STATION 513-608 CRACKED. REMOVED DAMAGE AT 513 AND 608 AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 735. REMOVED MATERIAL THAT WAS BEYOND LIMITS AND INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND .5 INCH CRACK AT FRAME 160 FASTENERS. LONG SPLICE SECTION PER SRM 53-02. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN SEAT TRACK NR 4 STATION 340. REMOVED GOUGE SEAT TRACK NR 4 STATION 340. INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED STATION 1290 JUST OUTBOARD NR 1 SEAT TRACK. INSTALLED NEW CUSP SHEET FROM STATION 1250-1309 LEFT PER SRM 51-01. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND RIGHT CUSP AT STATION 722. 6 INCHES INBOARD FROM WALL HAS CRACK. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: GENERATOR — DEFECTIVE (NR 2 ENGINE)

DFW - FLT 1758 - EN ROUTE AUS-ORD, RIGHT SIDE GENERATOR FAILED. DIVERTED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE AIRCRAFT GENERATOR. REPLACED AIRCRAFT GENERATOR CONTROL UNIT. SYSTM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

ORD - FLT 1512 - LEFT ENGINE FAILED ON TAKEOFF AT ABOUT 300 AGL. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — FAILED (ROW 21)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 21 TO AFT INOPERATIVE. REPAIRED SHORTED WIRE IN AFT SLIDE HANDLE LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

PHX - FLT 2084 - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED CONNECTOR FOR FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY INOPERATIVE. REPAIRED WIRING TO EMERGENCY FLOOR PATH LIGHTING STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — CORRODED (BS 1340)

TUL - FORWARD SIDE FRAME 18, STR 44R, HAS CORROSION ON FRAME 18. CORROSION REMOVED PER SRM 51-74-10, AND REPAIRED PER SRM 51-71-50. TST: 29,628.53 HOURS. CYCLES: 10,098. (X)