N208AA

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,287 hrs · 41,233 cycles

E&E DOOR PAN CORRODED. REMOVED AND REPLACED DOOR PAN PER AARD 53-10-00-14.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,285 hrs · 41,230 cycles

CORROSION ON AFT FACE OF FRAME AT STATION 133 FORWARD SIDE OF E&E DOOR CUTOUT UNDER PAN LONGERON 28L-28R. INSTALLED DOUBLER PER AARD 53-10-00-14 AND REPLACED PAN PER AARD 51-00-00-12.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,287 hrs · 41,234 cycles

CORROSION OUT OF LIMITS AT NUT PLATE FASTENER HOLES. REPLACED LEFT TIE DOWN TRACK PER SRM 51-30-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,287 hrs · 41,234 cycles

CRACK IN SHEAR TIE. SHEAR TIE WAS REPAIRED PER ENGINEERING AUTHORITY MD 80 53-006354, SRM 51-10-04, SRM 51-30.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 77,287 hrs · 41,234 cycles

STIFFENER CRACKED AT UPPER FORWARD. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM 51-01-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,287 hrs · 41,234 cycles

CORROSION IN WEB I/B OF LOWER DOOR BEAM. NEW WEB WAS INSTALLED PER 51-01-00.

Part: PANEL — CRACKED (FUSELAGE) · airframe 77,285 hrs · 41,230 cycles

PANEL CRACKED BETWEEN RIGHT RADOME ALIGNMENT PIN AND RIVET. INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 77,287 hrs · 41,234 cycles

NUMBER 6 SEAT TRACK CORRODED. INSTALLED NEW NUMBER 6 SEAT TRACK PER AMM 53-40-01-2.

Part: STRAP — GOUGED (FUSELAGE) · airframe 77,287 hrs · 41,234 cycles

SCREW GOUGE IN TOP OF STRAP AT STATION 1148 INBOARD OF RIGHT TIE DOWN TRACK. REMOVED AND REPLACED STRAP PER SRM 51-30-05.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 77,325 hrs · 41,267 cycles

LEFT WINDOW PAN FRAME IS CRACKED AT FORWARD LOWER CORNER STATION 845. INSTALLED ANGLE REPAIR AT FORWARD LOWER LEFT CORNER OF WINDOW PAN AT STATION 845 AS PER AARD 53-10-00-25.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,325 hrs · 41,267 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. ACCOMPLISHED SPLICE REPAIR PER AARD 53-30-00-2.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 77,325 hrs · 41,267 cycles

LEFT WINDOW PAN FRAME IS CRACKED AT TOP FORWARD CORNER STATION 946. INSTALLED DOUBLER PER AARD 53-10-00-25 LEFT WINDOW PAN TOP FORWARD CORNER STATION 946.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 77,325 hrs · 41,267 cycles

RIGHT CUSP CRACKED AT STATION 1301 BETWEEN SEAT TRACKS 5 AND 6. INSTALLED RIGHT CUSP SHEET AT STATIONS 1250 AND 1309 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 77,289 hrs · 41,237 cycles

RIGHT CUSP SHEET CRACKED BELOW NR 6 SEAT TRACK. INSTALLED DOUBLER FROM STA 882-887 PER AARD 53-20-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 77,285 hrs · 41,230 cycles

LEFT CUSP CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,285 hrs · 41,230 cycles

SEAT TRACK NR 4 HAS CORROSION. INSTALLED SEAT TRACK PLUG AS PER AARD 53-20-00-10.

Part: VANE — DAMAGED (TE FLAP) · airframe 77,285 hrs · 41,230 cycles

TEMP REPAIR ON L/E OF VANE. INSTALLED HOT BOND REPAIR ON DAMAGED AREA PER ESO8OO95.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,285 hrs · 41,230 cycles

CORROSION ON SEAT TRACK NR 5 BEYOND LIMITS. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 77,285 hrs · 41,230 cycles

TEMP REPAIR INOPERATIVE. REMOVED OLD TEMP REPAIR AND INSTALLED PERMANENT REPAIR AS PER SRM 53-04 FIG 38.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 77,289 hrs · 41,237 cycles

CABIN FORWARD ENTRY AREA HAS CRACK IN STRAP DOUBLER STA 208 LONGERON 15 LEFT. INSTALLED REPAIR DOUBLER PER 53-10-00-11.

Part: LONGERON — WORN (FUSELAGE) · airframe 77,287 hrs · 41,233 cycles

WEAR MARK ON LONGERON 2 LEFT APPROXIMATELY 1 INCH LONG BY .020 DEEP. INSTALLED J-ANGLE DOUBLER, MATERIAL .063 7075T6 ON LONGERON 2 LEFT AT STATION 256 PER SRM 51-10-3.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 76,697 hrs

LGA - AFT CABIN EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EXIT LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 76,697 hrs

LGA - AFT CABIN EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EXIT LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 76,599 hrs

PHX - FORWARD OVERWING EXIT DOOR LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED BATTERY PACK FOR FORWARD OVERWING EXIT DOOR.

Part: TRANSFER PUMP — FAILED (HYD SYSTEM) · airframe 76,387 hrs · 40,729 cycles

BNA INFLIGHT DCA TO DFW - CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY LOSS AND RIGHT ENGINE DRIVEN PUMP MAKING NOISE. LANDED BNA WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE HYDRAULIC PUMP FAILED. REPLACED NUMBER ONE ENGINE HYDRAULIC PUMP AND LEFT HYDRAULIC SYSTEM FILTERS. NO DEBRIS FOUND IN FILTER BOWLS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 74,889 hrs · 74,889 cycles

DFW - INFLIGHT T493/11JUL - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMB THROUGH FLIGHT LEVEL 180. LIGHT EXTINGUISHED AFTER SHUTTING OFF RT A/C PACK. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RUPTURED DUCT IN AFT COMPARTMENT ON RT SIDE. REPLACED DUCT IN AFT COMPARTMENT ON RT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 73,566 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT AFT POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT AFT POSITION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 73,566 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT FORWARD POSITION MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 9D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 10D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 8D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY SLIDE FLOOD LIGHT AT MIDDLE POSITION TAIL COMPARTMENT INOPERATIVE. RELAMPED EMERGENCY SLIDE FLOOD LIGHT AT MIDDLE POSITION TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 15D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 10D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — CRACKED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT FORWARD EXIT SIGN HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT FORWARD EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 8D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (AIR CONDITIONING)

DFW TO ATL DIVERTED TO LIT DUE TO PRESSURIZATION LOSS AT 29000 FEET. DEPLOYED OXYGEN MASKS. PRESSURIZATION RETURNED AT 20000 BUT DIVERTED TO LIT DUE TO DEPLETED PASSENGER OXYGEN. LANDED LIT WITHOUT INCIDENT. REPLACED BOTH NUMBER ONE AND NUMBER TWO PRESSURIZATION CONTROLLERS AND OUTFLOW VALVE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY CEILING LIGHTS ABOVE ROWS 27 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS ABOVE ROWS 27 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT SERVICE DOOR EMRGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD RIGHT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, BOTH LT AND RT FORWARD EMERGENCY EXIT ESCAPE HATCH LIGHT DIM. RECONNECTED LOOSE CONNECTION AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GASKET — FAILED (ACM BAY)

LAS - FLT 322 - EN ROUTE LAS-DFW TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING ROTATION. TEMPERATURE LIGHT EXTINGUISHED WHEN POWER WAS REDUCED, ILLUMINATED WITH HIGHER POWER SETTING. RETURNED LAS AND LANDED WITHOUT INCIDENT. REPLACED RIGHT AIR CONDITIONING SUPPLY HIGH TEMPERATURE SENSOR GASKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (FUSELAGE)

DFW - FLT 1319 - EN ROUTE DFW-PDX, SHORTLY AFTER DEPARTURE DETECTED AIRCRAFT WOULD NOT PRESSURIZE. AIR INTERRUPTED, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED PRESSURIZATION VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (STAIRWAY)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR FORWARD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 20D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHING AT SEAT 20D INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, MID-CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED MID-CABIN EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: COUPLING — BROKEN (TAIL COMPARTMENT)

BNA - FLT 0691 - DURING CLIMB-OUT AT 18,000 FEET, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. CREW FOLLOWED CHECK LIST AND TAIL COMPARTMENT HIGH TEMPERATURE LIGHT EXTINGUISHED. AIRCRAFT AIR INTERRRUPTED AND RETURNED TO BNA WITHOUT FURTHER INCIDENT. REPLACED BROKEN COALESCER ASSEMBLY COUPLING AND AS A PRECAUTIONARY, REPLACED WATER SEPARATOR BAG. RAN ENGINES AND PACKS WITH NO LEAKS DETECTED AND TAIL COMPARTMENT HIGH TEMPERATURE LIGHT DID NOT ILLUMINATE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SEAT TRACK — CORRODED (BS 205)

TUL - NR 5 SEAT TRACK CORRODED AT LUG AND NUTPLATE HOLES, STA 205, FORWARD END OF TRACK. INSTALLED STRAP AND PLUG ON SEAT TRACK FLANGE PER ESO 80559 DATED 8-21-96 AND REMOVED SEAT TRACK LUGS PER ESO 80359 DATED 8-27-97. TST: 43,793.04. CYCLES, 24,583. (X)

Part: SEAT TRACK — CORRODED (BS 1155-1231)

TUL - CORROSION ON NR 3 SEAT TRACK OUTBOARD FLANGE FROM STA 1155 TO STA 1231. REPLACED SECTION OF SEAT TRACK PER SRM 53-05, FIG 4. TST: 43,793 HOURS. CYCLES, 24,583. X)