N488AA

Part: ADC — FAULTY (ZONE 100) · airframe 77,248 hrs · 40,842 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE 30,000 AUTOPILOT & AUTO THROTTLE DISCONNECTED. CAPTAIN HAD FAST & SLOW FAIL LIGHT ON MACH TRIM INOPERATIVE & UNRELIABLE AIRSPEED. R & R NR 1 AIR DATA COMPUTER IAW AMM 34-16-01. PERFORMED OPERATIONAL TEST IAW AMM 22-01-05. SYS CHECKED NORMAL.

Part: HEAT EXCHANGER — LEAKING (AC BAY) · airframe 76,404 hrs · 40,333 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, PASSING FL180 THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. PERFORMED TAIL COMPARTMENT LEAK CHECK IAW MCM36-95-15 & FOUND THE PRIMARY HEAT EXCHANGER LEAKING AT THE UNION WITH DUCT. R & R THE RT PRIMARY HEAT EXCHANGER IAW AMM 21-51-04. PERFORMED LEAK CHECK. SYS CHECKED NORMAL.

Part: SENSOR — FAULTY (ZONE 100) · airframe 76,371 hrs · 40,311 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HIGH SENSORS IAW AMM 36-20-02-201 & MCM 36-95-14. ACCOMPLISHED MCM 36-95-14 & MCM 0930. SYS CHECKED NORMAL. SEE ALSO AALA20150803010 & AALA20150805009.

Part: SENSOR — FAULTY (ZONE 100) · airframe 76,371 hrs · 40,311 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HIGH SENSORS IAW AMM 36-20-02-201 & MCM 36-95-14. ALSO ACCOMPLISHED MCM 36-95-14 & MCM 0930. SYSTEM CHECKED NORMAL. SEE ALSO AALA20150803010 & AALA20150805010.

Part: TUBE — BROKEN (ZONE 200) · airframe 76,371 hrs · 40,311 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HIGH SENSORS IAW AMM 36-20-02-201 & MCM 36-95-14. ACCOMPLISHED MCM 36-95-14 & MCM 0930. SYS CHECKED NORMAL. SEE ALSO AALA20150805009 & AALA20150805010.

Part: PANEL — MISALIGNED (CABIN CEILING) · airframe 76,325 hrs · 40,284 cycles

VENTRAL STAIRWAY RUBS ON CEILING PANEL DURING UP & DOWN TRAVEL. REPAIRED VENTRAL STAIRWAY MOVABLE CEILING IAW AMM 53-20-06. TRIMMED OVERHEAD CEILING PANEL FOR CLEARANCE OF MOVEABLE CEILING, CAT WALK.

Part: RIB — CRACKED (LT WING) · airframe 73,116 hrs · 38,394 cycles

LEFT HAND WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034669.

Part: RIB — CRACKED (RT WING) · airframe 73,116 hrs · 38,394 cycles

RIGHT HAND WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034669.

Part: TRANSMITTER — INOPERATIVE (LT ENGINE) · airframe 69,837 hrs · 36,480 cycles

LAX - INFLIGHT FAT-DFW. CREW REPORTED LEFT ENGINE COMPRESSOR STALL FOLLOWED BY SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE PRESSURATION TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — WORN (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

STATION 1380 LEFT SIDE FRAME WEB HAS WORN AREA FROM COCKPIT TEMP CONTROL VALVE. REMOVED DAMAGED MATERIAL AND INSTALLED FRAME WEB REPAIR AS PER AARD 53-10-00-28.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

FUSELAGE DENTED WITH SCRATCH FROM STATIONS 170 TO 182 LONGERON 25 LEFT. INSTALLED DOUBLER PER SRM 53-04-03, FIGURE 8, SHEET 5.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

RIGHT FORWARD SUBFLOOR CORRODED FROM STATIONS 160 TO 200 RIGHT BUTTLINE 50. INSTALLED SUBFLOOR REPAIR DOUBLER AT STATIONS 160 TO 200, RIGHT BUTTLINES 43 TO 57 PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

FORWARD SERVICE DOOR JAMB PAN, LOWER END CORRODED FROM STATIONS 180 TO 190. ACCOMPLISHED REPAIR PER SRM 53-05-00 FIGURE 55.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

BULKHEAD SKIN IS CRACKED AROUND LOWER LEFT RADOME ALIGNMENT PIN. INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

SHEAR TIE CRACKED AT 1401 LONGERON 15 LEFT. INSTALLED NEW SHEAR TIE ANGLE PER AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

FOUND CRACK IN CUSP AT STATION 661 LEFT SIDE. REPLACED CUSP SHEET FROM STATIONS 598 TO 712 PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

THE 1485 CANT FRAME CRACKED BELOW STAIR RET ACTUATOR. INSTALLED FRAME SPLICE PER AARD 53-10-00-33.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

CORROSION ON AFT CARGO DOORWAY LOWER FORWARD CORNER FITTING. INSTALLED NEW CORNER FITTING AS PER AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

RIGHT FORWARD SUBFLOOR CORRODED FROM STATIONS 160 TO 200, RIGHT BUTTLINE 50. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

FOUND CRACK IN CUSP AT STATION 581, LEFT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

CORROSION FOUND AT STATIONS 148 TO 160, 6 INCHES RIGHT OF CENTERLINE ON SUBFLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

WINDOW PAN CRACKED, WINDOW 43, UPPER AFT AT STATION 1041. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

CORROSION ON SUBFLOOR AT STATION 200 UNDER G-2 GALLEY OUTBOARD. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

CORROSION ON BOTTOM OF LEFT CUSP FROM STATIONS 554 TO 557. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,228 hrs · 36,149 cycles

CUSP ANGLE CORRODED AT STATIONS 170 TO 210, FORWARD SERVICE DOOR AREA. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 55 AND BOEING DRAWING J060288.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

AFT CARGO CEILING CENTER INTERCOSTAL IS CRACKED AT FWD SIDE OF FLOORBEAM AT STATION 1309. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 69,228 hrs · 36,149 cycles

AFT SERVICE DOOR HAS A CRACK IN FRAME AT LOWER HINGE CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA COMP-52-026822.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

CRACK IN CUSP AT STATION 581 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (TE FLAP) · airframe 69,228 hrs · 36,149 cycles

INBOARD FLAP, INBOARD WEDGE, GOUGED BOTTOM EDGE. REMOVED DAMAGE FROM LOWER SKIN PER SRM 57-01-00 FIGURE 5 SHEET 2. DAMAGE IS 22 INCHES FROM TRAILNG EDGE AND 20 INCHES FROM INBOARD EDGE. DYE PEN INSPECTION REVEALS NO CRACK INDICATION. INSTALLED PERMANENT FLUSH DOUBLER REPAIR PER SRM 57-01-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,228 hrs · 36,149 cycles

FUSE - SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,222 hrs · 35,552 cycles

FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS BATTERY PACK, OPS CHECK NORMAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,379 hrs · 33,969 cycles

CORROSION UNDER STAINLESS DOUBLER ALONG BOTTOM EDGE OF DOOR SILL. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: REGULATOR — MALFUNCTIONED (AC BAY) · airframe 62,315 hrs · 32,306 cycles

DFW - CREW REPORTED FUMES AND SMOKE IN CABIN. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PRESSURE REGULATOR AND ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: REGULATOR VALVE — FAILED (CABIN) · airframe 61,041 hrs · 31,634 cycles

CREW REPORTED SMELL OR ODOR IN CABIN AND COCKPIT AFTER TAKEOFF. RETURNED TO FAT AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT PRESSURE REGULATING VALVES. REPLACED BOTH COALESCER BAGS AND LEFT PNEUMATIC PILOT REGULATOR VALVE.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,532 hrs · 31,345 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23 TO ROW 29. RESEATED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29. OPS NORMAL.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 60,532 hrs · 31,345 cycles

FLASHLIGHT STRAP MISSING FROM FLASHLIGHT BY AFT GALLEY FLIGHT ATTENDANT SEAT. INSTALLED STRAP FOR FLASHLIGHT AT AFT GALLEY FLIGHT ATTENDANT SEAT.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 60,532 hrs · 31,345 cycles

FLASHLIGHT STRAP MISSING FROM FLASHLIGHT OUTSIDE RIGHT LAVATORY. INSTALLED STRAP FOR FLASHLIGHT AT RIGHT LAVATORY.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,532 hrs · 31,345 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK IN TAIL COMPARTMENT. OPS CHECKS NORMAL.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 60,532 hrs · 31,345 cycles

FLASHLIGHT STRAP MISSING FROM FLASHLIGHT BY AFT GALLEY FLIGHT ATTENDANT SEAT. REPLACED STRAP FOR FLASHLIGHT AT AFT GALLEY FLIGHT ATTENDANT SEAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,532 hrs · 31,345 cycles

CEILING EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT BETWEEN AFT LAVATORIES. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,889 hrs

DFW - AFT OVERWING LEFT AND RIGHT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN BIN 20.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,889 hrs

DFW - REMOVED TWO EMERGENCY LIGHT BATTERY PACKS FROM MOUNTS AT BAG BIN 20DEF. INSTALLED BATTERY PACKS IN MOUNTS IN BIN 20DEF.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,889 hrs

DFW - RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,889 hrs

DFW - CEILING EMERGENCY LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 20.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 59,600 hrs · 30,859 cycles

DFW - CREW REPORTED OIL SMELL AND BLUISH COLOR SMOKE IN CABIN AND COCKPIT. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY PACK UNIT AND ACCOMPLISHED A PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (ZONE 200) · airframe 59,359 hrs

LGA - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 14D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,770 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD MAIN ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FORWARD MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SWITCH — INOPERATIVE (RT ENGINE)

ORD - RIGHT HAND ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED ABOUT 12 MINUTES INTO FLIGHT. RETARDED THROTTLE LIGHT REMAINED ON. ENGINE SHUT DOWN BY CREW. ENGINE WINDMILLED 20 MINUTES AT 10 POUNDS PER SQUARE INCH. LANDED ORD WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED OIL FILTER AND TOOK OIL SAMPLE. INSTALLED NEW DIFFERENTIAL SWITCH AND REPLACED BROKEN RIGHT HAND ENGINE ANTI ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

LGA - FORWARD UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD UPPER EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHTS ON CEILING FROM R7 THROUGH R20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILING FROM R7 TO R20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — RUPTURED (RT RNGINE)

DFW - DURING CLIMBOUT FIRE DETECTION LOOP -A- LIGHT ILLUMINATED THEN -B- ILLUMINATED. RETARDED THROTTLE AND LIGHTS EXTINGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE ANTI-ICE DUCT. LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MSP - CEILING EMERGENCY LIGHTS AT ROW 28 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR CEILING EMERGENCY LIGHTS AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACTOR — DIRTY (CABIN)

AUS - AFT EMERGENCY OVERHEAD LIGHTS AT L2 DOOR AND AFT AISLE INOPERATIVE. CLEANED BATTERY CONTACTS AND REINSTALLED BATTERIES FOR AFT EMERGENCY LIGHTS AT L2 DOOR AND AFT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (A/C BAY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FOR TAIL CONE JETTISON INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE FOR TAIL CONE JETTISON LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ODOR — DETECTED (CABIN)

ABQ - FLT 11287 - EN ROUTE PHX-DFW, DURING CRUISE AT 33,000 FEET, A STRONG ELECTRICAL FIRE SMELL ENTER THE COCKPIT FOLLOWED BY REPORTS FROM CABIN OF BURNING ELECTRICAL SMELL. EMERGENCY PROCEDURE WERE FOLLOWED AND THE FLIGHT ATTENDANTS REPORTED THE SMELL SEVERE. DIVERTED ABQ AND LANDED WITHOUT INCIDENT. THE ODOR REMAINED WITH THE AIRCRAFT UNTIL ON THE GROUND AND THEN STARTED TO DISSIPATE. THE FLIGHT ATTENDANTS REPORTED THAT THE ODOR WOULD CHANGE WHEN THE PACKS WERE SHUT OFF, BUT THE SMELL REMAINED. THE SMELL WAS A VERY PRONOUNCED ELECTRICAL BURNING SMELL. PRECAUTIONARY REPLACED NR 1 ENGINE AND WATER SEPARATOR COALESCER BAGS, LEAK CHECKED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. NO FUMES NOTED. (M

Part: PLUG — DAMAGED (APU)

AUS - FLIGHT 1592 - EN ROUTE AUS-ORD, ON TAKEOFF AT AUS A RUBBER / INSULATION / ELECTRICAL ODOR WAS NOTED. IT INCREASED TO A VISIBLE HAZE IN THE CABIN. RETURNED AUS, HAZE DISSIPATED, LANDED AUS WITHOUT INCIDENT. REPLACED APU OIL DRAIN PLUG, LEFT AND RIGHT AUGMENTATION VALVES, AND COALESCERS BAGS. PERFORMED AIRCRAFT PACK BURN OUT. NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

DURING OVERNIGHT MAINTENANCE AFT SEAT MOUNTED EMERGENCY EXIT LIGHTS FROM ROW 20-31 INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE IN AFT AIR STAIRS AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DEFECTIVE (CABIN)

DURING OVERNIGHT MAINTENANCE FORWARD DETACHABLE EMERGENCY LIGHT MOUNT PINS WONT ENGAGE MOUNTS. REPLACED FORWARD DETACHABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT FORWARD ENTRY DOOR AND GALLEY SERVICE DOOR VERY DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (BS 1190-1201)

TUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1190-1201. REMOVED DAMAGED AREA OF NR 2 SEAT TRACK AT BS 1190-1201. INSTALLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 53-05 FIG 4A. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND FORWARD DOORWAY WEB IS CRACKED AT LOWER LIGHTING HOLE STATION 1152 BETWEEN LONGERON 27R AND 28R, AFT CARGO. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-24. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 HAS CORROSION AT STATION 625. INSTALLED SEAT TRACK REPAIR PER SRM 53-05. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON INTERCOSTAL BETWEEN LONGERON 28L AND LONGERON 27L FROM STATION 1309 TO STATION 1322. INSTALLED NEW INTERCOSTAL BETWEEN L28L AND L27L FROM STATION 1309 TO 1322 AS PER SRM 53-14. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

TUL - FOUND CORROSION ON RIGHT TIE DOWN TRACK AROUND FASTENER HOLES STATION 1003 TO STATION 1155, AND STATION 1212 TO STATION 1338. REPLACED RIGHT TIE DOWN TRACK FROM STATION 1003 TO 1155 AND STATION 1212 TO 1338 PER SRM 53-05. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

TUL - FOUND CORROSION ON TIE DOWN TRACK AROUND FASTENER HOLES STATION 1003 TO STATION 1338, LEFT TRACK. REPLACED LEFT TIE DOWN TRACK FROM STATION 1003 TO STATION 1338 PER SRM 53-05 FIG 4B. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,542 hrs · 18,176 cycles

TUL - CORROSION ON INTERCOSTAL BETWEEN L28L - L27L, FROM STA 1309 - STA 1322. CORROSION BEYOND LIMITS. INSTALLED NEW INTERCOSTAL BETWEEN L28L - L27L FROM STA 1309 - STA 1322 PER SRM 53-14. (X)

Part: LONGERON — CORRODED (FUSELAGE)

TUL - FOUND CORROSION LONGERON 28L AT STATION 1287 IN BOTTOM OF LONGERON CHANNEL. REMOVED CORROSION AND REPAIRED BY INSTALLING STRAP DOUBLER PER ESO NR 80599, DATED 6-8-2000. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION BOTTOM SIDE STATION 484 LEFT CUSP CORROSION TOP SIDE AND LOWER LIP STATION 490, 450, 430 ALSO STATION 460 T0 470. REMOVED AND REPLACED LEFT CUSP SHEET STATION 427 TO 505 PER AARD 53-20-00-16. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK ON EXTERIOR FUSELAGE SKIN AT STATION 1474 CANTED FRAME RIGHT SIDE 12 INCHES ABOVE AIRSTAIR CUTOUT. STOP DRILLED CRACKED AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT AND SCRATCH ON FUSELAGE SKIN STATION 1309, BETWEEN L18-19 RIGHT, DYE CHECKED AND BURNISHED SCRATCH AT STATION 1309, ADL NR 4880021. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38-20. (M)

Part: FITTING — CORRODED (CARGO BAY)

TUL - AFT CARGO DOOR CUT OUT AFT LOWER SILL ATTACH FITTING HAS CORROSION. INSTALLED NEW AFT DOORWAY JAMB LOWER SILL FITTING PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 4 SEAT TRACK CORRODED FROM STATION 235-237. INSTALLED PLUG PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORROSION AREAS FROM STATION 215 - 303 SRM 53-05. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 3L STATION 160 CRACKED IN RADIUS AT LONGERON TO FRAME ATTACH HI-LOCK, OUTBOARD LEG. INSTALLED NEW LONGERON SECTION AND SPLICE PER SRM 53-02. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED IN RADIUS. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-20. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND TWO GOUGE MARKS IN TOP OF WEB STATION 1214 LONGERON 28 RT. INSTALLED DOUBLER PER AARD 53-10-00-24. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

TUL - FOUND LIGHTNING STRIKE HAS .3125 INCH NACA STYLE RIVET NOT FILLING COUNTER SINK AT STATION 328, LONGERON 27L REMOVED RIVET, CUT .875 INCH HOLE. INSTALLED DOUBLER AND FILLER PER SRM 53-04 FIG 38. (M)

Part: THRESHOLD — DENTED (PAX DOORWAY)

TUL - MEASURE AND DYE CHECK TWO DENTS AFT OF PASSENGER DOOR SILL 4 INCHES BELOW LONGERON L18 ADL NR 4880014, STATION 227. CUTOUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: FITTING — CRACKED (STRINGER)

TUL - FOUND STATION 1416 L2R CRACKED AT END FITTING. SPLICED L2R LONGERON AT STATION 1416 PER AARD 53-30-00-2. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CUSP CORRODED OUTBOARD OF SEAT TRACK NR 6 STATION 52L. REMOVED CORROSION PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CORROSION ON CUSP. CUTOUT CORROSION AREA AND INSTALLED .025 7075T6 DOUBLER PER SRM 53-01 FIG 4. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,542 hrs · 18,176 cycles

TUL - STATIC DISCHARGES IN FUSELAGE, STA 298 LONGERON 21L. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (X)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CUSP CORRODED OUTBOARD OF SEAT TRACK NR 6 AT STATION 484-503 AROUND FASTENERS. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: FRAME — CRACKED (PAX WINDOW)

TUL - FOUND WINDOW FRAME CRACKED FORWARD LOWER CONER AFT OF STATION 984 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED AT STATION 733. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CUSP CORRODED AT SEAT TRACK NR 6 BOTTOM SIDE STATION 238. REMOVED CORRODED AREA OF CUSP AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED AT STATION 640. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: FITTING — CORRODED (CARGO DOORWAY)

TUL - FOUND AFT CARGO AFT DOORWAY JAMB TO LOWER SILL ATTACH FITTING HAS CORROSION. INSTALLED NEW AFT DOORWAY JAMB LOWER SILL ATTACH FITTING SRM 51-01. (M)

Part: STRUCTURE — DENTED (CABIN)

TUL - FOUND MEASURE AND DYE CHECK TWO DENTS AFT OF PASSENGER DOOR SILL STATION 227 APPROX 4 INCHES BELOW DOOR LONGERON 14L. CUT OUT DAMGE. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: GALLEY TRACK — CORRODED (CABIN)

TUL - FOUND FORWARD GALLEY G1 INBOARD TIE DOWN CORRODED. REMOVED AND REPLACED GALLEY MOUNT PER SRM 53-01. (M)

Part: FRAME — CRACKED (PAX WINDOW)

TUL - FOUND WINDOW FRAME CRACKED FORWARD LOWER CORNER IN RADIUS STATION 946 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — DAMAGED (CABIN)

TUL - FOUND HOLE IN CUPS AT STATION 733 UNDER NR 6 SEAT TRACK. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND TWO HOLES IN SUB-FLOOR INBOARD OF SEAT TRACK NR 1 AT STATION 237-241. INSTALLED DOUBLER ON CUSP PER SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND LEFT CUSP HAS CORROSION AT LIGHTENING HOLE STATION 840. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CUSP CORRODED OUTBOARD SEAT TRACK NR 6 STATION 555 AROUND LIGHTNING HOLE. REMOVED CORROSION, INSTALLED DOUBLER 53-03 SRM FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK HAS CORROSION AT STATION 625. INSTALLED SEAT TRACK PLUG PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 4 SEAT TRACK HAS CORROSION STATION 218. INSTALLED SEAT TRACK PLUG PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,542 hrs · 18,176 cycles

TUL - NR 6 SEAT TRACK CORRODED AT STA 625. INSTALLED SEAT TRACK PLUG PER SRM 53-05. (X)

Part: FRAME — CRACKED (PAX WINDOW)

TUL - FOUND AFT UPPER CORNER OF WINDOW FRAME CRACKED LEFT STATION 1041-1060. INSTALLED FABRICATED DOUBLER PER AARD 53-10-0025. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,542 hrs · 18,176 cycles

TUL - NR 4 SEAT TRACK HAD CORROSION AT STA 218. INSTALLED SEAT TRACK PLUG PER SRM 53-05. (X)

Part: ACTUATOR — DEFECTIVE (LT MLG)

DFW - FLT 1528 - DURING CLIMB-OUT, THE LEFT RED GEAR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND THE LIGHT WENT OUT. FLIGHT CONTINUED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT AND FOUND THE LEFT RETRACT ACTUATOR CYLINDER WAS AT FAULT. REPLACED LEFT RETRACT ACTUATOR CYLINDER. SYSTEM LEAK CHECKED AND OPERATED NORMALLY DURING GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — MALFUNCTIONED (LT MLG DOOR)

ORD - FLT 1556 - EN ROUTE LAS-ORD, AFTER BRINGING HYDRAULIC PUMPS TO OFF AND LOW, THE LEFT GEAR INDICATION RED LIGHT ILLUMINATED. LIGHT WENT OUT AND STAYED OUT AFTER RECYCLING HYDRAULIC PUMPS TO HIGH AND THEN TO LOW. LIGHT STAYED OUT FOR REMAINDER OF FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED LEFT GEAR DOOR ACTUATOR. ACCOMPLISHED LEAK CHECKS AND CHECKED AND ADJUSTED LEFT MAIN GEAR UP AND LATCHED PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — FAILED (E/E BAY)

DFW - FLT 616 - AFTER TAKEOFF YYC, AFTER GEAR WAS RAISED THE LEFT RED GEAR LIGHT REMAINED ILLUMINATED, AMBER GEAR DOOR OPEN LIGHT EXTINGUISHED. NO UNUSUAL YAW OR VIBRATION. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR UNIT. ACCOMPLISHED REQUIRED TESTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OIL SYSTEM — LEAKING (APU)

DFW - FLT 1718 - AFTER TAKEOFF DFW DURING CLIMB-OUT, SLIGHT SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT PROCEDURE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT AND PROBLEM REPEATED. REPLACED APU. ACCOMPLISHED PACK BURNOUT PROCEDURE AND REPLACED ALL COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (M)

Part: RETRACT CYLINDER — DEFECTIVE (LT MLG)

DFW - FLT 1295 - AFTER TAKEOFF GDL, WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR DOOR RED LIGHT REMAINED ILLUMINATED. SELECTED HYDRAULIC PUMPS TO HIGH AND LIGHT EXTINGUISHED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR RETRACT CYLINDER. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LATCH CYLINDER — DEFECTIVE (LT MLG DOOR)

ORD - FLT 1603 - AFTER T/O FROM SLC EN ROUTE ORD AT ABOUT 14,000 FEET, THE LT MLG RED LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. ALL CONDITIONS WERE CORRECT AFTER INITIAL GEAR RETRACTION. PUMPS RETURNED TO LOW AND OFF AND LIGHTS EXTINGUISHED. WHEN A/C WAS AT 29,000 FT AND 290 KNOTS EXPERIENCED TURBULENCE AND GEAR DOOR OPEN LIGHT CAME ON AND A/C SLOWED RETRACTION WAS HEARD AND FELT. ALL LIGHTS EXTINGUISHED INDICATING NORM RETRACTION. PUMPS WERE LT W/O INCIDENT. REPLACED LT MAIN GEAR DOOR LATCH CYLINDER. ALL GEAR OPERATIONS NORMAL. NO LEAKS NOTED. PERFORMED SEVERAL GEAR SWINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (BS 180-200)

TUL - FOUND CORROSION ON CUSP ANGLE STATION 180 TO 200 AT FORWARD SERVICE DOOR LOWER JAMB. INSTALLED DOUBLER PER ESO 80559, DATED 7-23-96. (M)

Part: PROX SWI UNIT — DEFECTIVE (E/E COMPT)

DFW - FLT 853 - AFTER TAKEOFF DFW WHEN LANDING GEAR HANDLE RAISED, THREE RED LIGHTS ILLUMINATED WITH NO YELLOW GEAR DOOR LIGHT. SELECTED LANDING GEAR DOWN AND GOT THREE GREEN INDICATION. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SWITCH UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT STRIP — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)