N489AA

Part: WIRE HARNESS — FAULTY (BOOST PUMP) · airframe 78,732 hrs · 41,517 cycles

UNABLE TO TRANSFER FUEL FROM CENTER TANK AND FORWARD BOOST PUMP CIRCUIT BREAKER WAS FOUND TRIPPED. EMERGENCY WAS NOT DECLARED. UNEVENTFUL LANDING. REMOVED AND REPLACED CENTER FUEL TANK AFT BOOST PUMP HARNESS IAW AMM 28-20-07-201, OPS CHECKED GOOD.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 78,732 hrs · 41,517 cycles

LANDED DUE TO UNABLE TO TRANSFER FUEL FROM CENTER TANK AND FORWARD BOOST PUMP CIRCUIT BREAKER WAS FOUND TRIPPED. EMERGENCY WAS NOT DECLARED. UNEVENTFUL LANDING. PLACARDED THE CENTER TANK BOOST PUMPS IAW MEL 28-01B. THE AIRCRAFT WAS NOT GROUNDED. R & R CENTER FUEL TANK FORWARD BOOST PUMP IAW AMM 28-20-07-201, OPS CHECK GOOD.

Part: PUMP — FAULTED (FUEL BOOST) · airframe 78,732 hrs · 41,517 cycles

UNABLE TO TRANSFER FUEL FROM CENTER TANK AND FORWARD BOOST PUMP CIRCUIT BREAKER WAS FOUND TRIPPED. EMERGENCY WAS NOT DECLARED. UNEVENTFUL LANDING. REMOVED AND REPLACED THE CENTER FUEL TANK AFT BOOST PUMP IAW AMM 28-20-07-201, OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,983 hrs · 41,057 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, NOSE WHEELS APPEARED TO KEEP ROTATING & NOSE GEAR RED LIGHT REMAINED ON. LANDING GEAR WAS EXTENDED NORMALLY & ACFT RETURNED. INSPECTED NOSE GEAR, NOSE GEAR DOORS & NOSE GEAR WW AREA IAW AMM 32-00-00 WITH NO FAULTS FOUND. ACCOMPLISHED NOSE GEAR SWING IAW AMM 32-30-00 WITH NO FAULTS FOUND.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 76,718 hrs · 40,313 cycles

ANGLE CRACKED ON THE FWD UPPER SIDE OF THE RT MAIN GEAR DOOR ACTUATOR MOUNT ON THE CTR WALL OF THE RT MAIN GEAR WW. STRAP DOUBLER INSTALLED IAW SRM 51-70-05 & EA 255478.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,718 hrs · 40,313 cycles

FORWARD CARGO DOOR, CRACKED STOP PAD BRACKET AT AFT LOWER CORNER OF CARGO DOOR. INSTALLED NEW STOP PAD FITTING, PN CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,718 hrs · 40,313 cycles

FORWARD CARGO DOOR CRACKED STOP PAD BRACKET AT AFT SIDE 2ND FROM TOP OF CARGO DOOR. INSTALLED NEW STOP PAD FITTING, PN CDK2345.

Part: CASTING — CRACKED (SPOILER) · airframe 76,718 hrs · 40,313 cycles

LEFT WING, CRACK AT INBD FWD CORNER OF GND SPOILER ACTUATOR CASTING. REPLACED GND SPOILER CASTING IAW AARD 51-00-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,718 hrs · 40,313 cycles

MID CARGO DOOR CRACKED, STOP PAD BRACKET AT FWD UPPER CORNER OF CARGO DOOR. INSTALLED NEW STOP PAD FITTING, PN CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,718 hrs · 40,313 cycles

FORWARD CARGO DOOR CRACKED, STOP PAD BRACKET AT FWD UPPER CORNER OF CARGO DOOR. INSTALLED NEW STOP PAD FITTING, PN CDK2345.

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 75,681 hrs · 39,721 cycles

ABORTED TAKEOFF AT 90 KNOTS DUE TO RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED. ACFT RETURNED SAFELY TO GATE WITH NO FURTHER INCIDENT. ACCOMPLISHED HIGH ENERGY STOP INSPECTION WITH NO DEFECTS NOTED. REPLACED UPPER & LOWER THRUST REVERSER SWITCH. PERFORMED OPERATIONAL CHECK IAW AMM 78-32-03. SYS CHECKED NORMAL.

Part: TRANSFORMER — FAULTY (ZONE 400) · airframe 75,500 hrs · 39,623 cycles

RIGHT ENG CONSTANT SPEED DRIVE UNIT OUTLET TEMP INDICATED HIGH ABOVE RED LINE. CSD DISCONNECTED DUE TO OVER TEMP. ACFT DIVERTED WITH OVERWEIGHT LANDING. REPLACED ENG TRANSFORMER WITH GOOD OPERATIONAL CHECKS IAW AMM 24-40-01 & AMM 24-10-03.

Part: OIL COOLER — FAULTY (RT ENGINE) · airframe 75,500 hrs · 39,623 cycles

RIGHT ENG CONSTANT SPEED DRIVE UNIT OUTLET TEMP INDICATED HIGH ABOVE RED LINE. CSD DISCONNECTED DUE TO OVER TEMP. ACFT DIVERTED WITH OVERWEIGHT LANDING. REPLACED ENG OIL COOLER WITH GOOD OPERATIONAL CHECKS IAW AMM 24-40-01 & AMM 24-10-03.

Part: GENERATOR — FAULTY (RT ENGINE) · airframe 75,500 hrs · 39,623 cycles

RIGHT ENG CONSTANT SPEED DRIVE UNIT OUTLET TEMP INDICATED HIGH ABOVE RED LINE. CSD DISCONNECTED DUE TO OVER TEMP. ACFT DIVERTED WITH OVERWEIGHT LANDING. REPLACED ENG GEN WITH GOOD OPERATIONAL CHECKS IAW AMM 24-40-01 & AMM 24-10-03.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,721 hrs · 39,212 cycles

SECTION OF OVERHEAD EMER LIGHTS INOPERATIVE IN AFT CABIN. REPLACED EMER LIGHT POWER SUPPLY B5 - 28.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 74,721 hrs · 39,212 cycles

PORTABLE EMER LIGHT FAILS FUNCTIONAL TEST. REPLACED PORTABLE EMER LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,780 hrs · 38,660 cycles

EMERGENCY LIGHT ON SEATS AFT OF OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: BRACKET — CRACKED (RT MLG) · airframe 72,944 hrs · 38,167 cycles

RIGHT MAIN GEAR DOOR ACTUATOR BRACKET IS CRACKED ON INBD SIDE. INSTALLED DOUBLER IAW AARD 53-10-00-38.

Part: RIB — CRACKED (RT WING) · airframe 72,924 hrs · 38,155 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR FITTING IAW MCM 57-98-06 & EA MD80-57-034576.

Part: RIB — CRACKED (LT WING) · airframe 72,924 hrs · 38,155 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR FITTING IAW MCM CARD 57-98-05 & EA MD80-57-034576.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 69,784 hrs · 36,400 cycles

ABQ - CREW REPORTED UNABLE TO PRESSURIZE AIRCRAFT IN AUTO. EMERGENCY DECLARED FLIGHT RETURNED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH PESSURE CONTROLLERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

CORROSION ON FRONT OF FRAME AT STATION 1212 BETWEEN LONGERONS 24 AND 28 RIGHT. INSTALLED DOUBLER PER EA MD80-53-026909.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

CORROSION ON LONGERON 29 RIGHT AT STATION 1287. REMOVED DAMAGED AREA OF LONGERON AND INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,089 hrs · 36,021 cycles

CORROSION ON SHEAR TIE, STATION 1212 FROM LONGERONS 28 LEFT TO 29 RIGHT. REPLACED SHEAR TIE PER AARD 51-00-05-1 AND DRAWING 9936073.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

CRACK AT FASTENER, STATION 1437 BELOW LONGERON 2 RIGHT. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,089 hrs · 36,021 cycles

SEAT TRACK NUMBER SIX CORRODED FROM STATIONS 214 TO 303. INSTALLED SERVICEABLE SEAT TRACK NUMBER SIX FROM STATIONS 214 TO 303 AS PER AARD 51-00-05-1.

Part: RIB — CRACKED (LE SLAT) · airframe 69,089 hrs · 36,021 cycles

THE RIGHT WING NUMBER 5 LEADING EDGE SLAT 2ND FROM OUTBOARD TRACK ATTACH BRACKET IS CRACKED. REPLACED DAMAGED RIB PER ESO 80117.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

CORROSION FOUND ON DOUBLER UNDER G2 GALLEY MOUNT AT STATION 218 RIGHT BUTTLINE 8. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

DENT IN FUSELAGE SKIN, STATION 233, ABOVE LONGERON 18 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIGURE 12C .

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,089 hrs · 36,021 cycles

CORROSION ON SUB FLOOR BELOW FORWARD END OF NUMBER 6 SEAT TRACK FROM STATIONS 214 TO 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 69,089 hrs · 36,021 cycles

RIGHT CUSP IS BENT AND CRACKED AT EDGE OF LIGHTNING HOLE AT STATION 746. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CONNECTOR — DEFECTIVE (BRAKE SENSOR) · airframe 66,113 hrs · 34,364 cycles

DFW - CREW REPORTED AFTER TAKEOFF BRAKE TEMPERATURE OVERHEAT LIGHT ILLUMINATED STEADY AND LEFT INBOARD BRAKE SHOWED 3580 DEGREES. ACCOMPLISHED QRH PROCEDURES AND EXTENDED GEAR UNTIL LIGHT EXTINGUISHED. FLIGHT LANDED DFW WITHOUT INCIDENT. REPLACED BAD CONNECTOR ON LEFT INBOARD BRAKE SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,240 hrs · 33,875 cycles

RIGHT FUSELAGE AT STATION 1380 HAS CRACK IN SKIN AT SHEAR TIE AREA JUST ABOVE PYLON. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-30-00-02.

Part: ENGINE — FAILED (LEFT) · airframe 62,895 hrs · 32,601 cycles

DFW - LEFT ENGINE FAILED DURING CLIMBOUT AT ABOUT 23,000 FEET (SINGLE ENGINE TIME 13 MINUTES). SMOKE IN THE CABIN WAS ALSO REPORTED. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON 05/26/2010 AT DFW. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LINK — FAILED (NLG DOOR) · airframe 60,798 hrs · 31,489 cycles

INFLIGHT OMA TO DFW CREW REPORTED NOSE LANDING GEAR WOULD NOT RETRACT WITH VIBRATION AND BURNING RUBBER SMELL IN COCKPIT. AIRCRAFT LANDED MCI DUE TO WEATHER AND WITHOUT INCIDENT. REPLACED BOTH NOSE GEAR DOOR LINKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 59,357 hrs

LGA AFT AISLE OVERHEAD EMERGENCY LIGHT AT AFT LAVATORY INOPERATIVE. RESEATED BATTERY IN PACK FOR EMERGENCY LIGHT AT AFT AISLE OVERHEAD AT AFT LAVATORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,995 hrs

MCO- PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY.

Part: ENGINE — MALFUNCTIONED (NR 2)

MSY INFLIGHT T2224/18AUG DFW TO PBI. CREW REPORTED NR 2 ENGINE OIL LOW PRESSURE INDICATION AT FLIGHT LEVEL 330. CREW SHUT DOWN ENGINE AND LANDED MSY WITHOUT INCIDENT. SINGLE ENGINE TIME 17 MINUTES. REPLACED NR 2 ENGINE ON 20 AUG AT MSY DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,891 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 27D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 14D. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 27D INOPERATIVE. REPLACED THE FORWARD MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX INTERIOR CEILING EMERGENCY LIGHTS AT STATION 650-750 INOPERATIVE. REPLACED BATTERY PACK FOR INTERIOR CEILING EMERGENCY LIGHTS AT STATION 650-750. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SAN FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS OVERHEAD EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

ORD - MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 22 AND 23. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 8D. REPLACED LIGHT SOCKET SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE OVERWING DOOR SECTION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 20 THROUGH 22. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN SKIN IN TWO PLACES AROUND RIVET STATION 1380 BETWEEN LONGERON 16 AND 17L. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M)

Part: CONNECTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT ROW 7-11 INOPERATIVE. CLEANED EMERGENCY EXIT CEILING LIGHT BATTERY CONNECTOR AT SEAT 7-11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS FROM SEAT 12 TO 16 FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (APU BAY)

DFW - FLT 421 - EN ROUTE DFW-SEA, SHORTLY AFTER TAKEOFF, CABIN FILLED WITH SMOKE. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU. PERFORMED PACK BURNOUT PER MM. LEAK CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIR DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT AFT STAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

PHX - FLT 1636 - AFTER TAKEOFF, EN ROUTE PHX-ORD, NOSE GAER WOULD NOT MOVED TO THE UP POSITION UPON RAISING THE GEAR HANDLE. RETURNED PHX AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR SHRADER VALVE. SERVICED NOSE GEAR STRUT WITH FLUID AND AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

DFW - FLT 953 - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED SCHRAEDER VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: VALVE — LEAKING (NLG)

IAD - FLT 1463 - AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT, RECYCLED GEAR AND NOSE GEAR STILL DID NOT RETRACT. REPLACED SERVICE VALVE AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOOR SUPPORT — CORRODED (FWD GALLEY FLOOR) · airframe 34,481 hrs · 18,125 cycles

TUL - STA 148 - STA 150 RBL 8, FLOOR SUPPORT CORRODED BEYOND LIMITS. STA 200 BETWEEN SEAT TRACKS 5 AND 6, FLOOR SUPPORT CORRODED BEYOND LIMITS. REPLACED FLOORBOARD PER SRM 53-05-PARTS. (X)

Part: DOUBLER — CORRODED (GALLEY FLOOR) · airframe 34,481 hrs · 18,125 cycles

TUL - INBOARD OF RIGHT GALLEY DOOR FLOOR SUPPORT, SUB-FLOOR DOUBLER ERODED/CORRODED, 6 INCHES BY 5 INCHES, BEYOND LIMITS. INSTALLED DOUBLER, 7075T6, 0.025 INCH, PER SRM 53-01, FIG 4, SHEET 3. (X)

Part: WEB — DENTED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CUSP DENTED AT STA 733, RIGHT. INSTALLED DOUBLER PER SRM 53-01, FIG 4. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - SEAT TRACK NR 2 CORRODED BEYOND LIMITS FROM STA 1174 - STA 1309. REPLACED NR 2 SEAT TRACK FROM STA 1174 - STA 1309 PER SRM 53-05. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON SEAT TRACK NR 1, BS 960 TO BS 965. REMOVED AND REPLACED SECTION OF NR 1 SEAT TRACK FROM STA 936 TO STA 1031 PER SRM 53--05. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON SEAT TRACK AND BS 700 - BS 703. FINISHED INSTALLING SEAT TRACK NR 1 AND SEAT TRACK SPLICE FROM 541 TO 798 PER SRM 53-05-PART 1. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,481 hrs · 18,125 cycles

TUL - NR 4 SEAT TRACK CORRODED AT STA 237. REMOVED AND REPLACED SECTION OF NR 4 SEAT TRACK FROM STA 200 TO STA 265 PER SRM 53-05, FIG 4F. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON SEAT TRACK NR 1, BS 608. REPLACED SEAT TRACK FROM STA 541 - STA 798 PER SRM 53-05, PART 1. (X)

Part: FITTING — CORRODED (CARGO BAY) · airframe 34,481 hrs · 18,125 cycles

TUL - CORNER FITTING HAS CORROSION STA 1212, FORWARD SIDE AND OUTBOARD OF LONGERON 28R. REMOVED AND REPLACED FITTING, SRM 51-01. (X)

Part: FRAME — CORRODED (CARGO BAY) · airframe 34,481 hrs · 18,125 cycles

TUL - CORNER FITTING HAS CORROSION, STA 1155 AFT SIDE OF FRAME OUTBOARD L28R. INSTALLED NEW CORNER FITTING AT STA 1155 AFT SIDE OF FRAME PER SRM 51-10-4. FASTENERS 429-8 (BOTTOM) 426-8 (SIDE) NUT 3D006/4. (X)

Part: PAN — CRACKED (CABIN WINDOW) · airframe 34,481 hrs · 18,125 cycles

TUL - WINDOW PAN CRACKED AFT OF BS 807 AND LOWER CORNER AT PREVIOUSLY ROUTED AREA, LEFT. INSTALLED DOUBLER ON CRACKED WINDOW, P/N AT 807 PER SRM 53-10-00-25. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON SEAT TRACK AT CLIPNUT AREAS 1174-1309. INSTALLED NEW SEAT TRACK NR 1 STA 1174 TO STA 1307 PER SRM 51-01. (X)

Part: WEB — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - STA 1174 - STA 1176 TO STA 1250, CORROSION BETWEEN AFT FITTING AND CUSP WEB AT LEFT OUTBOARD END OF CABIN FLOOR BEAM AT PREVIOUS REPAIR. NEW CUSP SHEET INSTALLED PER SRM 51-01 FROM STA 1250 TO STA 1174, LEFT SRM 51-01. (X)

Part: WEB — CRACKED (CARGO BAY) · airframe 34,481 hrs · 18,125 cycles

TUL - WEB CRACKED AT STA 1215 BETWEEN L28R AND 27R, .375 INCH. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-24. (X)

Part: WEB — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - SEVERAL AREAS OF TOOLING DAMAGE ON CUSP AT STA 598 - STA 617, RIGHT SIDE. BLENDED OUT DAMAGE, TREATED AND PRIMED AREA. INSTALLED DOUBLER PER SRM 53-01, FIG 4-3. (X)

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON AFT CARGO DOOR JAMB BEAM FROM STA 1156 TO STA 1210, AREA 2 INCHES BY 54 INCHES. BLENDED OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-03. (X)

Part: WEB — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON LOWER SURFACE OF LEFT CUSP FROM STA 446 - STA 475. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, FIG 4-3. (X)

Part: SHEAR TIE — CRACKED (ACCESSORY BAY) · airframe 34,481 hrs · 18,125 cycles

TUL - SHEAR TIE CRACKED ON AFT SIDE OF BULKHEAD AT STA 1437 BETWEEN LONGERONS 2 AND 3L. REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE. PART NOT VERIFIED IN LRC. SRM 51-01. (X)

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 34,481 hrs · 18,125 cycles

TUL - CANT. STA 1463, LEFT SIDE OF VERTICAL STABILIZER TO FUSELAGE ATTACH POINT ANGLE, ANGLE HAD CRACK, .3750 INCH IN LENGTH, EMITTING FROM RIVET HOLE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-2. (X)

Part: WEB — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - CORROSION ON CUSP WEB, STA 992 - STA 997, RIGHT. REMOVED (CUT OUT) CORRODED WEB AREA AND INSTALLED WEB REPAIR PER SRM 53-01, FIG 4-3. (X)

Part: SEAT TRACK — GOUGED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - NR 1 SEAT TRACK GOUGED, BS 673. BLENDED GOUGE AREA PER SRM 51-10-3, OUT OF LIMITS, ROUTED, INSTALLED PLUG REPAIR AARD 53-20-00-10. (X)

Part: STRUCTURE — CORRODED (CABIN SUBFLOOR) · airframe 34,481 hrs · 18,125 cycles

TUL - SUBFLOOR UNDER G-2 GALLEY MOUNT INBOARD OF TRACK NR 4 HAS CORROSION. INSTALLED DOUBLER, SRM 51-10-3, CORROSION DAMAGE REMOVED. DOUBLER MATERIAL VERIFIED. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,481 hrs · 18,125 cycles

TUL - NR 1 SEAT TRACK CORRODED, BS 762 - BS 767. BLENDED CORROSION OUT, OUT OF LIMITS. INSTALLED PLUG REPAIR AARD 53-20-00-10. (X)

Part: VALVE — DEFECTIVE (NLG)

MIA - FLT 640 - AFTER TAKEOFF, NOSE GEAR UNSAFE UP INDICATOR ILLUMINATED WITH LOUD AIR NOISE. ACCOMPLISHED ABNORMAL PROCEDURE (RED GEAR LIGHT IN FLIGHT, GEAR HANDLE UP) RESULTING IN ALL GEAR DOWN AND GREEN. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SHRADER VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: DOWNLOCK SWITCH — DEFECTIVE (NLG)

MIA - FLT 1722 - DURING LANDING, WHEN GEAR WAS EXTENDED RED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND RED LIGHT REMAINED ILLUMINATED. PERFORMED GO AROUND AND ABNORMAL GEAR PROCEDURES. GEAR INDICATIONS NORMAL. LANDED MIA WITHOUT INCIDENT. REPLACED NOSE GEAR DOWN SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 1066 - DURING APPROACH, ON GEAR EXTENSION NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. RECYCLED GEAR WITH NO HELP. GREEN LIGHT ILLUMINATED FIVE SECONDS AFTER NOSE TOUCHDOWN. LANDED DFW WITHOUT INCIDENT. REPLCED NOSE GEAR DOWNLOCK SWITCH SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: STRUT — REQ'D SERVICE (NLG)

DFW - FLT 1949 - ON TAKEOFF, AUS NOSE LANDING GEAR DID NOT RETRACT WHEN GEAR RETRACT HANDLE RAISED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT ASSEMBLY AND CYCLED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROWS 36 THROUGH 43AB INOPERATIVE. REPAIRED WIRE AT SEAT ROW 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CUSP — CORRODED (BS 1149-1174)

TUL - CUSP MEMBRANE CORRODED RIGHT SIDE. REMOVED CORRODED AREA BY CUTTING OUT A PORTION OF CUSP MEMBRANE FROM STA 1145 TO STA 1174 RT. FABRICATED DOUBLER FROM .31 INCH 7075-T6 AND INSTALLED WET WITH SEALANT PER SRM 53-0, PAGE 17, FIGURE 4, SHEET 3. TST: 23,581 HOURS. CYCLES, 13,157. (X)

Part: TIE DOWN TRACK — CORRODED (BS 1155-1300)

TUL - LEFT CARGO TIE-DOWN TRACK CORRODED FROM STA 1155 - STA 1300 AROUND CENTER FASTENERS AND HOLES. TREATED, PRIMED TIE-DOWN TRACK FROM STA 1155 TO STA 1222. REMOVED OUT OF LIMITS TRACK FROM STA 1222 TO STA 1322. INSTALLED NEW TIE-DOWN TRACK, LT CARGO FROM STA 1222 TO STA 1322. INSTALLED PER SRM 53-05, FIGURE 45. TST: 23,581 HOURS. CYCLES, 13,157. (X)

Part: MEMBRANE — CORRODED (BS 1022-1095)

TUL - CUSP MEMBRANE CORRODED FROM STA 1022 TO STA 1098, LT SIDE. REPLACED CUSP MEMBRANE FROM STA 1022 TO STA 1098 PER SRM 53-01, FIGURE 4, SHEET 3. (X)