N482AA

Part: ADC — FAULTY (ZONE 100) · airframe 77,152 hrs · 40,955 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. AT FL 330, IN ICING CONDITIONS, AUTOPILOT & AUTO THROTTLE DISCONNECTED, ACCOMPANIED BY TAIL BUFFET FROM ICE. TESTED AIRFOIL TAIL ICE PROTECTION SYS IAW AMM 30-10-00 WITH NO FAULTS DETECTED. TESTED 1 & 2 CENTRAL AIR DATA COMPUTER & RECEIVED 1 & 2 CADC COMPARE FAILED. R & R NR 2 CADC IAW MM 34-16-01. SYS TESTED NORMALLY.

Part: PRESSURE SWITCH — ACTIVATED (FUEL) · airframe 76,170 hrs · 40,357 cycles

CREW REPORTED A LT WING INLET PRESSURE LIGHT ILLUMINATED. CREW REQUEST CFR RESPOND & CHECK FOR VISIBLE SIGN OF FUEL LEAK. NO FUEL LEAK WAS FOUND. R & R THE LT ENGINE LOW FUEL INLET PRESSURE SWITCH IAW AMM 733-33-01. PERFORMED OPERATIONAL CHECK. SYS CHECKED GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 75,493 hrs · 39,988 cycles

CORROSION FOUND ON LONGERON STRAP AT L23L & FS 1257. R & R STRAP IAW AARD 51-00-05-1 DWG 5911423.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 74,938 hrs · 39,690 cycles

DURING TAKEOFF NR 1 ENG EPR STUCK AT 1.4. TAKEOFF WAS ABORTED AT UNDER 50 KNOTS. ALL OTHER INDICATIONS UNRESPONSIVE. R & R NR 1 ENG EPR INDICATOR IAW AMM 77-11-01 & NR 1 ENG EPR TRANSMITTER IAW MM 77-11-02. CHECKED DRAIN TRAPS FOR MOISTURE. SYS CHECKED NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,899 hrs · 39,662 cycles

CRACK ON LONGERON AT BS 200, 23 LT. REPAIRED LONGERON IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,899 hrs · 39,662 cycles

CRACK ON LONGERON AT BS 200, STRINGER 24 LT. REPAIRED LONGERON IAW SRM 53-02-00 FIGURE 18.

Part: FORMER — CRACKED (RT WING) · airframe 74,899 hrs · 39,662 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. STOP DRILLED CRACK & INSTALLED RT WING NR 4 SLAT INBD FORMER DOUBLER IAW WORK CARD 57-98-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,158 hrs · 38,035 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 BETWEEN LONGERONS 13 & 14 RT. DYE CHECKED CRACK & STOP DRILLED. INSTALLED DOUBLER IAW SRM 53-01-00 & AARD 53-30-00-02.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,072 hrs · 37,432 cycles

CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED B5-27 BATTERY POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,072 hrs · 37,432 cycles

CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED B5-106 BATTERY POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: VALVE — INOPERATIVE (RT ENGINE) · airframe 71,043 hrs · 37,413 cycles

RDU INFLIGHT DCA-DFW CREW REPORTED RT ENGINE HIGH OIL TEMPERATURE. RT ENGINE SHUTDOWN, SINGLE ENGINE TIME 15 MINUTES. EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE FUEL HEAT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,719 hrs · 36,652 cycles

FUSELAGE SKIN FROM STATIONS 496 TO 500 BETWEEN STRINGERS 28 AND 29 LEFT HAD IMPACT DAMAGE. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER SRM 53-04-03.

Part: CONNECTOR — LOOSE (NR 2 ADC) · airframe 69,719 hrs · 36,652 cycles

MEX - CREW REPORTED FIRST OFFICERS LOST AIR SPEED INDICATOR, ALTIMETER AND AUTO PILOT FAILED. EMERGENCY DECLARED FLIGHT RETURNED MEX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND STATIC PORT QUICK DISCONNECT CONNECTOR LOOSE. RE-SECURED STATIC QUICK DISCONNECT CONNECTOR ON NUMBER TWO CENTRAL AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,966 hrs · 36,262 cycles

CORROSION ON LONGERON 28 RIGHT, STATION 1287. REMOVED CORRODED SECTION OF LONGERON AND INSTALLED SPLICE REPAIR PER 53-02-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

FUSELAGE STATION 750, LONGERONS 29 RIGHT AND 29 LEFT, FUSELAGE SKIN IS BULGING OUT. INSTALLED FUSELAGE SKIN REPAIR PER SRM 53-04-03 FIG 11. INSTALLED 2 REPAIR STRAPS PER EA MD80-53-024926 ON INTERNAL DOUBLER BETWEEN LONGERONS 28 AND 29 BOTH LEFT AND RIGHT SIDES OF AIRCRAFT.

Part: SKIN — DAMAGED (ENRTY DOOR) · airframe 68,198 hrs · 35,810 cycles

FORWARD ENTRY DOOR HOLD OPEN HOOK CUTOUT SKIN DOUBLER DAMAGED. INSTALLED DOUBLER PER EA COMP-52-024852.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,198 hrs · 35,810 cycles

AFT SHEAR TIE AT STATION 1149 BETWEEN LONGERONS 29 AND 30 CORRODED. REPLACED SHEAR TIE.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,198 hrs · 35,810 cycles

RIGHT CUSP STATION 252-256 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

RIGHT CUSP CRACKED AT STATION 1192. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

LEFT CUSP CRACKED STATION 243. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

DENT AND GOUGE IN FUSELAGE SKIN AT STATION 231 LONGERON 8 LEFT. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 11.

Part: RIB — CRACKED (LE SLAT) · airframe 68,198 hrs · 35,810 cycles

THE 2ND FROM OUTBOARD SLAT RIB ON NUMBER 5 SLAT SHOWS A CRACK INDICATION USING HIGH FREQUENCY EDDY CURRENT. REPLACED DAMAGED RIB WITH NEW ONE PER ESO 80117.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

FUSELAGE LEFT SIDE SKIN CRACKED AT STATION 1309 BETWEEN LONGERON 6 AND 7 LEFT. INSTALLED DOUBLER PER SRMS 53-04-03 AND 51-01-00.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

SUBFLOOR UNDER G-1 GALLEY PAN IS CRACKED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

RIGHT CABIN CUSP HAS CRACK AT STATION 1192. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,198 hrs · 35,810 cycles

FUSELAGE SKIN AT STATION 229, LONGERON 29 RIGHT DENTED. INSTALLED REPAIR DOUBLER PER SRM 53-04-03.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 66,812 hrs · 35,039 cycles

RNO - CREW REPORTED RIGHT GENERATOR FAILED AND AUXILIARY POWER UNIT FAILED TO PICK UP LOAD. EMERGENCY DECLARED FLIGHT RETURNED RNO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,712 hrs · 34,418 cycles

FOUND CEILING EMERGENCY LIGHT AT ROW 21 INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT AT ROW 21. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,712 hrs · 34,418 cycles

EMERGENCY LIGHTS ABOVE AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK B5-4 FOR EMERGENCY LIGHTS ABOVE AFT GALLEY. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 65,712 hrs · 34,418 cycles

CEILING EMERGENCY LIGHTS ROW 23 TO 30 INOPERATIVE. RESEATED BATTERIES AT ROW 24 AND 29. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,708 hrs · 33,331 cycles

EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. OPS CHECK NORMAL.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,760 hrs · 31,700 cycles

FORWARD CARGO DOOR BEAM AT STATION 398 HAS CORROSION. BEAM REPAIRED UNDER EA MD80-53-007068.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,437 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,352 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: PISTON — INOPERATIVE (NLG)

ORD INFLIGHT T1718 - COULD NOT RETRACT THE LANDING GEAR AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STRUT LOWER PISTON AND SERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHTING IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - CEILING EMERGENCY LIGHT IN TAIL INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR CEILING EMERGENCY LIGHT IN TAIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY CABIN LIGHTS AT ROWS 4 THROUGH ROW 6 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, 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: MODULE — LEAKING (REVERSER FILTER)

DFW - FLT 1040 - JUST AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED HOT OIL FUMES IN CABIN. DISSIPATED IN 5 MINUTES. DID NOT REPEAT REMAINDER OF FLIGHT. PREVIOUSLY REPORTED ON GROUND WHILE APU RUNNING. TIGHTENED LEFT REVERSER FILTER MODULE. LEAK CHECK OK. REPLACED AIR CONDITIONER COLESCER SOCKS, RAN PACKS WITH APU AND ENGINES RUNNING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: PISTON — FAILED (NLG)

DFW - FLT 1203 - AFTER TAKEOFF DFW, LANDING GEAR WOULD NOT RETRACT, FLAPS ORAL WARNING, AUTO SPOILER DO NOT USE LIGHT ILLUMINATED, PRESSURIZATION MALFUNCTION. GROUND SHIFT MECHANISM APPEARED NOT TO OPERATE NORMALLY. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR PISTON AND CYLINDER ASSEMBLY. LUBED NOSE LANDING GEAR, SERVICED NOSE LANDING GEAR STRUT, PERFORMED NOSE LANDING GEAR SWING. CYCLED SEVERAL TIMES. NOSE LANDING GEAR OPERATIONS CHECK AND LEAK CHECKS NORMAL. TAXIED AIRCRAFT FOR GROUND CHECK. AIRCRAFT TAXIED NORMAL. NOSE LANDING GEAR STEERING OPERATIONS CHECKS NORMAL, RUDDER STEERING OPERATIONS CHECK NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINK — DEFECTIVE (NLG)

BOS - FLT 1197 - AFTER TAKEOFF EN ROUTE PVD-ORD, UNABLE TO RETRACT NOSE LANDING GEAR. AIRCRAFT DIVERTED AND LANDED BOS WITHOUT INCIDENT. REPLACED LOWER TORQUE LINK AND HOLLOW PIN FOR LOWER TORQUE LINK. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CARGO TRACK — CORRODED (BS 1060-1222)

TUL - FOUND AFT CARGO LEFT TIE DOWN TRACK HAS CORROSION FROM STATION 1060 TO STATION 1222. REMOVED AND REPLACED AFT CARGO LEFT TIE-DOWN TRACK FROM STATION 1001 TO 1222. (M)

Part: LONGERON — CORRODED (BS 1155-1174)

TUL - FOUND RIGHT LONGERON CUSP HAS CORROSION STATION 1155 TO 1174 LONGERON 18R ABOVE AFT CX DOOR. INSTALLED DOUBLER STATION 1150-1175 PER 53-01 SRM FIG 4 SHEET 3 PAGE 17. (M)

Part: JAMB — CORRODED (BS 1193)

TUL - FOUND HORIZONTAL AND VERTICAL CARGO DOOR JAMB BEAM HAS CORROSION. AA REPAIR DOCUMENT 53-10-00-8. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING AT PAX SEAT ROW 21D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)