N14998

Part: FRAME — CRACKED (ZONE 200) · airframe 36,830 hrs · 16,566 cycles

DURING C-CHECK, FOUND FRAME 10 CRACKED UNDER LT DV WINDOW. REMOVED AND INSTALLED NEW FRAME 10 UPPER SECTION LOCATED UNDER LTH DV WINDOW IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (CABIN FLASHLIGHT) · airframe 36,816 hrs · 28,185 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY FLASHLIGHT AFT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,040 hrs · 26,799 cycles

DURING INSPECTION, ACFT MAIN DOOR EMERGENCY LIGHTS FOUND INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 32,915 hrs · 25,165 cycles

CREW REPORTED AN UNUSUAL ODOR IN CABIN WITH NR 2 PACK RUNNING. MAINTENANCE INSPECTED AND FOUND OIL LEAK ON NR 2 ENGINE INLET. MAINTENANCE R & R ENGINE NR 2 ZERO CARBON SEAL AND PERFORMED OPS CHECK OF ENGINE AND NR 2 PACK SYS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,662 hrs · 24,962 cycles

DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 29,014 hrs · 22,094 cycles

REPORTED BURNING ODOR FROM CABIN LIGHT OVER 11A SIDEWALL LIGHT. MX R & R CEILING LIGHT ASSY OVER 11A WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 28,818 hrs · 21,937 cycles

THE CREW REPORTED AN INTERMITTENT SPOILER FAIL MESSAGE IN FLIGHT WITH AN ODOR OF BURNED PLASTIC. ACFT LANDED WITHOUT INCIDENT. MX INSPECTED ACFT, ADJUSTED THRUST LEVER SWITCHES, OPS TESTED WITH NO DEFECTS, INSPECTED FOR BURNED OR DAMAGED COMPONENTS WITH NO DEFECTS NOTED AND NO BURNED PLASTIC ODOR NOTED, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,684 hrs · 21,813 cycles

DURING PRE-FLIGHT INSPECTION, CREW REPORTED THAT THE LAST AISLE PATH EMERGENCY LIGHT STRIP WAS NOT ILLUMINATING. MX R & R THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (NR 1 BLEED SYS) · airframe 27,052 hrs · 20,484 cycles

THE CREW REPORTED A NR 1 BLEED LEAK MESSAGE IN FLIGHT. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND TIGHTENED THE V-BAND CLAMP ON THE NR1 BLEED VALVE. OPS CHECKS WERE GOOD.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 30,170 hrs · 22,386 cycles

PAX DOOR LOWER STRUCTURE HAS CORROSION AROUND NUT PLATE HOLES. FABRICATED AND INSTALLED DOUBLER AFTER BLEND-OUT OF NUT PLATES ON AFT HALF OF MAIN DOOR. BLENDED OUT MINOR CORROSION ON FORWARD HALF OF DOOR IAW EC5210-01154. ACFT STILL IN C-CHECK.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 30,170 hrs · 22,386 cycles

SERVICE DOOR LOWER STRUCTURE CORRODED (LEVEL 1) AROUND NUT PLATES. BLENDED-OUT MINOR CORROSION IAW EC5210-01154. ACFT STILL IN C-CHECK.

Part: CONTACTOR — FAULTY (ELECTRICAL SYS) · airframe 26,693 hrs · 20,181 cycles

DAY FLT 2234 THE CREW REPORTED A ELECTRICAL EMERGENCY ABNORMAL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE ESSENTIAL BUS CONTACTOR 1. ALSO REPAIRED BROKEN WIRE ON OVERHEAD ELECTRICAL PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 25,877 hrs · 19,512 cycles

FLIGHT 5837 - EWR - FLIGHT CREW REPORTED ENGINE NR 2 BLEED LEAK. CREW PERFORMED FLIGHT DIVERSION TO EWR AND LANDED UNEVENTFULLY. EWR MX PERFORMED BLEED AIR DUCTS LEAKAGE TEST SUCCESSFULLY (COULD NOT DUPLICATE MSG/LEAK). ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DUCT — CRACKED (AC PACK) · airframe 25,807 hrs · 19,444 cycles

ORD FLT 6029 THE CREW REPORTED A WING ANTI-ICE FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 OUTLET DUCT ASSEMBLY ON THE ENVIRONMENTAL CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — OVERHEATED (CABIN) · airframe 23,382 hrs · 17,566 cycles

IAH - FLIGHT 2157 DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE GALLEY FLUORESCENT LIGHT WAS EXTREMELY HOT AND EMITTING A BURNING ODOR. MAINTENANCE REMOVED AND REPLACED THE GALLEY LIGHT ASSY, AND BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 23,382 hrs · 17,566 cycles

IAH - FLIGHT 2157 DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE GALLEY FLUORESCENT LIGHT WAS EXTREMELY HOT AND EMITTING A BURNING ODOR. MAINTENANCE REMOVED AND REPLACED THE GALLEY LIGHT ASSY, AND BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — DEFECTIVE (RT MLG) · airframe 22,473 hrs · 16,910 cycles

FLIGHT 2580 - EWR - FLIGHT CREW REPORTED RIGHT MAIN GEAR RETRACTED SLOWER THAN LEFT, CAUSING SIGNIFICANT YAW MOTION TO RIGHT DURING CLIMBOUT. EWR MX REMOVED AND REPLACED RT MAIN GEAR ACTUATOR AND SOLENOID VALVE. MX PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA09RI220 REPORTS ACTUATOR INFORMATION. SDR C2XA09RI221 REPORTS SOLENOID VALVE INFORMATION.

Part: SOLENOID VALVE — DEFECTIVE (RT MLG) · airframe 22,743 hrs · 16,910 cycles

FLIGHT 2580 - EWR - FLIGHT CREW REPORTED RIGHT MAIN GEAR RETRACTED SLOWER THAN LEFT, CAUSING SIGNIFICANT YAW MOTION TO RIGHT DURING CLIMBOUT. EWR MX REMOVED AND REPLACED RT MAIN GEAR ACTUATOR AND SOLENOID VALVE. MX PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA09RI220 REPORTS ACTUATOR INFORMATION. SDR C2XA09RI221 REPORTS SOLENOID VALVE INFORMATION.

Part: BRACKET — CORRODED (AILERON) · airframe 22,144 hrs · 16,672 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND BOTH LEFT AND RIGHT AILERON PCA BRACKETS CORRODED AND MIGRATED HAT BUSHIONS. MAINTENANCE REMOVED AND REPLACED BOTH AILERON PCA BRACKETS IAW EC5750-01177. ALL WORK WAS ACCOMPLISHED AND OPS CHECK GOOD AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: YOKE — CRACKED (NR 2 NACELLE) · airframe 22,143 hrs · 16,671 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 2 ENGINE FWD/LOWER YOKE WEBBING CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FWD/LOWER YOKE IAW EC 5450-01028 AND TASK CARD 6271001. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SWITCH — INOPERATIVE (ELECTRICAL SYS) · airframe 22,090 hrs · 16,624 cycles

FLIGHT 2452 - ALB - FLIGHT CREW DIVERTED FLIGHT DUE TO ELECTRICAL EMERGENCY ABNORMAL TRANSFER INDICATION. EWR MX REMOVED AND REPLACED PUSH BUTTON ESSENTIAL POWER SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PITOT LINE — DAMAGED (PITOT/STATIC SYS) · airframe 21,069 hrs · 15,853 cycles

CLE FLIGHT NR 2589, THE CREW REPORTED THEY LOSSED ALL AIRSPEED AND ALTITTUDE INDICATIONS ON DESCENT. THE CREW DECLEARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE CAPTAINS AND FO'S PITOT DRAIN ASSEMBLIES, PN QA4-2-42B, AND REPLACED THE CAPTAINS ADC PITOT LINE. OPS CHECKS WERE GOOD.

Part: BALLAST — SHORTED (CABIN LIGHTS) · airframe 18,448 hrs · 13,965 cycles

FLIGHT 2224 - EWR - CREW REPORTED BURNING SMELL IN THE AREA OF SEAT 1A. EWR MX REMOVED AND REPLACED BALLAST AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 18,337 hrs · 13,889 cycles

FLIGHT 2642 - EWR - CREW REPORTED SPS ADVANCE MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED STALL PROTECTION COMPUTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — FAULTY (STALL WARNING) · airframe 18,333 hrs · 13,884 cycles

FLIGHT 1231 - EWR - CREW REPORTED SPS ADV MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED ANGLE OF ATTACK SENSORS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — FAULTY (STALL WARNING) · airframe 18,333 hrs · 13,884 cycles

FLIGHT 1231 - EWR - CREW REPORTED SPS ADV MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED ANGLE OF ATTACK SENSORS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,851 hrs · 13,536 cycles

FLIGHT 2882 - CREW REPORTED GALLEY IDENTIFIER EXIT SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED NR 1 EMERGENCY FLOOR STRIP IAW EMB145 AMM 33-50-12 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 17,649 hrs · 13,391 cycles

RIGHT FUSELAGE SKIN DAMAGE (GROUND DAMAGE) BETWEEN FRM 67 & 71 BETWEEN STR 20L & 15R. REMOVED AND REPLACED SKIN PANEL IAW EMB 145 SRM 51-20-03, 51.40-06, CPM 51-21-04, 05, 06. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 17,215 hrs · 13,078 cycles

IAH - FLIGHT 2145, THE CREW REPORTED AN ELECTRICAL BURNING ODOR COMING FROM ABOVE THE COFFEE POTS. MAINTENANCE OPERATIONALLY CHECKED BOTH COFFEEMAKERS WITH NO DEFECTS, AND FOUND THE ODOR TO BE COMING FROM OLD COFFEE IN THE POTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 13,954 hrs · 10,583 cycles

IAH - DURING MX INSPECTION, SMOKE IN THE COCKPIT WAS REPORTED BY OPS. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING 5A INSPECTION MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT TO NOT BE WORKING. FOUND BROKEN WIRE, RECONNECTED BUTT SPLICE CONNECTION AND OPS CHECKED SYSTEM GOOD.

Part: BATTERY — LOOSE (CABIN)

DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT ROW EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE RESECURED NR 3 EMERGENCY LIGHT BATTERY TO EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 8,007 hrs · 5,965 cycles

SHV- DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,007 hrs · 5,965 cycles

SHV-DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,007 hrs · 5,965 cycles

SHV- DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTANANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,007 hrs · 5,965 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 59 TO 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (COCKPIT)

CLE FLIGHT 2059 THE CREW REPORTED A LAV SMOKE WARNING WITH A LIGHT HAZE OF SMOKE WITH ANTI-ICE SYSTEM ON. THE HAZE CLEARED WITH ANTI-ICE SYSTEM OFF. MAINTENANCE INSPECTED AND RAN ANTI-ICE SYSTEM TESTS AND WAS UNABLE TO DUPLICATE HAZE OR SMOKE. ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED · airframe 5,794 hrs · 4,153 cycles

BTV---CO2002, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND FUSELAGE DAMAGED ON LEFTHAND SIDE AT FRAME #22. MAINTENANCE REMOVED DAMAGED CLIP AT FRAME #22 AND ATTACHING FLOOR CROSS MEMBER, PERFORMED SKIN REPAIR IAW EMB145 SRM #53-21-00, FABRICATED SKIN CLIP IAW EMB LETTER IC2003-145/0103-B, REINSTALLED FABRICATED SKIN CLIP AND FLOOR CROSS MEMBER, AND PRESSURIZATION CHECKED/OPS.CHECKED AIRCRAFT GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

MCI FLIGHT 2248 THE CREW REPORTED A LAV SMOKE WARNING ON TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. NO SMOKE WAS NOTED. MAINTENANCE INSPECTED THE SMOKE DETECTION SYSTEM AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3230 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT#3132 THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE CABIN WAS INOPERATIVE.THE LIGHT WAS AT THE OVERWING EXIT.MAINTENANCE RESECURED THE LIGHT STRIP CONNECTOR AT ROW 11.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (CABIN)

IAH - FLIGHT 4027, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF AISLE PATH EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

IAH - FLIGHT 3749, THE CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PERFORMED OPERATIONAL CHECKS OF THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

IAH - FLT 3749 - THE CREW REPORTED A LAV SMOKE DETECTION LIGHT ILLUMINATED AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, RAN THE ENGINES AND, AIRCONDITIONING PACKS WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)