N14972

Part: CONTROL PANEL — INOPERATIVE (SMOKE DETECTOR) · airframe 353,582 hrs · 26,735 cycles

THE CREW REPORTED A LAVATORY SMOKE INDICATION IN FLIGHT. LANDED WITHOUT INCIDENT. R & R THE FWD GALLEY SMOKE DETECTOR PANEL, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (FRAME 13) · airframe 35,344 hrs · 26,729 cycles

STRINGER 6R CRACKED AT FRAME 13. R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 34,481 hrs · 26,010 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT AFTER TAKEOFF. BLEEDS CONFIGURED TO E1 & E2 WITH APU OFF. PACK TEMPS SET TO AUTO FULL COLD AND ATTD. PACK 1 ENTERED A FULL HOT CONDITION AND THE CONTROLLOR WAS PULLED TO MANUAL THAT'S WHEN THE SMOKE BILLOWED FROM THE VENTS. MX INSPECTED AND PERFORMED ENGINE RUNS AT VARIOUS SETTINGS AND RAN PACKS NO SMOKE/DEFECTS WERE FOUND. PERFORMED BORESCOPE OF NR 1 ENGINE WITH NO DEFECTS. THE ACFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 33,419 hrs · 25,193 cycles

DURING POST FLIGHT INSPECTION, THE LT WING EMERGENCY LIGHT WAS INOPERATIVE. R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 30,513 hrs · 22,879 cycles

CREW REPORTED THE CAPTAIN'S MFD INTERMITTENT WITH A BURNED WIRE ODOR. MX R & R THE CAPTAIN'S MFD DISPLAY UNIT IAW AMM 34-22-01 WITH OPS CHECKED SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 30,485 hrs · 22,862 cycles

DURING C-CK. SKIN CORRODED FR 12-14 STR 19R-21L. REPAIRED SKIN IAW EC5330-02527. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 30,485 hrs · 22,862 cycles

DURING C-CK. TOILET WASTE DRAIN VALVE SUPPORT CORRODED. REPLACED SUPPORT ASSY IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 30,026 hrs · 22,526 cycles

TYS - A/C DIVERTED TO TYS WHILE EN ROUTE FROM ORD TO CHS WHEN THE NR 1 BLEED VALVE CLOSED. CREW DIVERTED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE BLEED VALVE IAW EMB 145 AMM 36-11-05. OPS CHECK GOOD AND WAS RELEASED, A/C DEPARTED AND UPON TAXI OUT HAD A NR 1 BLEED VALVE CLOSED TO SHOW UP ON THE EICAS AGAIN, RETURN TO BLOCK WHERE MAINTENACE CHANGED NR 2 BLEED VALVE IAW EMB AMM 36-11-05, OPS CHECK GOOD AND CHANGED THE RELAY C7 IAW EMB AMM 20-13-00. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. NO FURTHER ISSUES.

Part: WIRE HARNESS — FAULTY (NR 1 ENGINE) · airframe 30,007 hrs · 22,506 cycles

ORD FLT 5828 THE CREW REPORTED A ENGINE 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL MODULE — MALFUNCTIONED (FIRE WARNING) · airframe 29,855 hrs · 22,383 cycles

SLW - FLIGHT 1760, THE CREW REPORTED AN ENGINE 1 FIRE DETECTOR FAIL ON TAKEOFF ROLL AT 50KTS. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE THE AIRCRAFT WAS INSPECTED AND APPROVED FOR A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE ENGINE ONE FIRE CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 29,835 hrs · 22,363 cycles

IN FLIGHT CREW REPORTED E1 FIRE DETECT FAIL MESSAGE ON EICAS. IAD MX PERFORMED OPERATIONAL CHECK OF E1 FIRE DETECTION SYSTEM SUCCESSFULLY IAW EMB-145 AMM 26-10-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 29,419 hrs · 21,984 cycles

ORD FLT 6165 THE CREW REPORTED JUST BEFORE V1, RECEIVED A STEER INOP MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND SERVICED THE NOSE LANDING GEAR STRUT. OPERATIONAL CHECKS WERE GOOD.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 27,485 hrs · 20,417 cycles

THE CREW REPORTED A BLEED NR 1 OVERTEMP, WING ANTI-ICE FAIL, STAB ANTI-ICE FAIL, ANTI-ICE INOP MESSAGES DURING FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK RT OMEGA BEAM AT FRAME 60-61 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM FRAME 60-61 IAW EMB-145 EC5310-01473. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK CARBON CROSS BEAM SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT LT OMEGA FRAME 59. MAINTENANCE REMOVED AND REPLACED CARBON CROSS BEAM SUPPORT ON LT OMEGA BEAM FRAME 59 IAW EMB-145 SRM 53-00-10 AND EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK RT EXTERNAL FUSELAGE BETWEEN FRAME 73-81 HAS VISUAL INDICATIONS CRACKS AROUND RIVET HEADS. MAINTENANCE PERFORMED REPAIR OF RT EXTERNAL FUSELAGE BETWEEN FRAME 73-81 IAW EC5330-02047. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK LT EXTERNAL FUSELAGE BETWEEN FRAME 73-81 HAS VISUAL INDICATIONS OF CRACKS AROUND RIVET HEADS. MAINTENANCE REPAIRED LT EXTERNAL FUSELAGE BETWEEN FRAME 73-81 IAW EC5330-02067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM DOUBLER AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,525 hrs · 18,850 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM BETWEEN FRAMES 65-68 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68 IAW EMB-145 SRM 51-40-02 AND EC5320-01456 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL FWD SHEAR CLIP AT FRAME 65 IS CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR FOR SHEAR CLIP AT FRAME 65 STRINGER 16L-18L IAW EMB-145 EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,525 hrs · 18,950 cycles

SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER FRAME 22 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM DOUBLER AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLUID — LOW (HYDRAULIC SYS) · airframe 25,482 hrs · 18,920 cycles

NR 2 HYD INDICATOR IN AMBER. FLT DIVERTED AND MX SERVICED HYD SYSTEM, OPS AND LEAK CHECKED GOOD.

Part: FLUID — LOW (HYDRAULIC SYS) · airframe 25,481 hrs · 18,919 cycles

IAH - FLIGHT 2523, DURING CRUISE THE CREW REPORTED THE HYDRAULIC SYSTEM 1 TO BE IN AMBER RANGE. THE AIRCRAFT DIVERTED TO BNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO LEAKS NOTED, SERVICED THE HYDRAULICS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,169 hrs · 18,682 cycles

DURING ROUTINE MAINTENANCE THE AFT EXIT LOCATOR EMERGENCY SIGN WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,169 hrs · 18,682 cycles

DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (EXTERIOR) · airframe 24,641 hrs · 18,283 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND LEFT FORWARD EXTERNAL EMERGENCY LIGHT INOPERATIVE. MX RESECURED CONNECTOR ON EXTERNAL EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 24,112 hrs · 17,882 cycles

FLIGHT 2092 - EWR - FLIGHT CREW REPORTED BAG SMOKE WARNING, GUARDED BUTTON ILLUMINATED. EWR MX REMOVED AND REPLACED AFT BAG SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLUX DETECTOR — MALFUNCTIONED (RIGHT) · airframe 24,045 hrs · 17,833 cycles

IAH - FLIGHT 2228, THE CREW REPORTED THAT THE FIRST OFFICERS HDG WAS OFF MORE THAN 6 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLUX DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,124 hrs · 17,158 cycles

IAH - FLIGHT 2998, THE CREW REPORTED EMERGENCY LIGHTS INOP ON THE BACK LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — SHORTED (COCKPIT) · airframe 22,929 hrs · 17,019 cycles

FLIGHT 2354 - EWR - FLIGHT CREW REPORTED ELECTRICAL SMELL COMING OUT OF THE GLARESHIELD/FRONT AVIONICS PANEL ON APPROACH. EWR MX REMOVED AND REPLACED LT WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 21,866 hrs · 16,275 cycles

YQB FLIGHT 2128 - THE CREW REPORTED PACK 2 PRODUCES SMOKE IN CABIN WHEN TURNED ON. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM IN BOTH MANUAL AND AUTO USING THE APU AND ENGINE BLEED. NO SMOKE WAS DETECTED AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 21,772 hrs · 16,203 cycles

CLE FLIGHT 2039 THE CREW REPORTED ON TAKEOFF FROM CLE THE AIRCRAFT WOULD NOT PRESSURIZE. TRIED MANUAL MODE WITHOUT SUCCESS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE AND REMOVED DEBRIS FROM MANUAL CONTROLLER VENT SCREEN. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,489 hrs · 16,003 cycles

DURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY LIGHT BATTERY WOULD NOT HOLD A CHARGE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 19,624 hrs · 14,659 cycles

MTY - FLIGHT 2702, THE CREW REPORTED A LG AIR/GRD FAIL AFTER T/O MSG WENT AWAY. WE WERE ABLE TO USE DOWN LOCK REL TO RAISE GEAR. THE AIRCRAFT RETURNED TO MTY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NOSE PROX SWITCH AND CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — ODOR (NR 1) · airframe 19,401 hrs · 14,487 cycles

IAH - FLIGHT 2492, DURING PREFLIGHT INSPECTION, THE CREW REPORTED BURNING SMELL WITH THE PACKS ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AIR CYCLE MACHINE (ACM), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (CHARGER) · airframe 18,237 hrs · 13,614 cycles

CLE FLIGHT 2664 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 16,782 hrs · 12,470 cycles

CLE FLIGHT 2590 THE CREW REPORTED A BURNING SMELL IN THE CABIN OVERHEAD LIGHT AT ROW 9A. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 33-20-00/1. SUPPLEMENT TO FOLLOW.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 16,069 hrs · 11,895 cycles

IAH - FLIGHT 2427, DURING SHORT FINAL, THE CREW REPORTED A BAGGAGE SMOKE WARNING IN SHORT FINAL. BOTH FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFT BAGGAGE COMPT SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 16,069 hrs · 11,895 cycles

IAH - FLIGHT 2427, DURING SHORT FINAL, THE CREW REPORTED A BAGGAGE SMOKE WARNING IN SHORT FINAL. BOTH FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD BAGGAGE COMPT SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO SMOKE) · airframe 16,030 hrs · 11,865 cycles

IAH - THE CREW REPORTED A BAGGAGE SMOKE WARNING ON FINAL APPROACH. THE CREW DISCHARGED BOTH FIRE BOTTLES, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REPLACED BOTH FIRE EXTINGUISHERS, AND COULD FIND NO EVIDENCE OF FIRE/SMOKE. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,603 hrs · 11,534 cycles

IAH - FLIGHT 2121, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST FOUR ROWS OF EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER THREE AISLE PATH LIGHTING STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 13,964 hrs · 10,017 cycles

EWR - FLIGHT 2331 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER STARTING THE APU. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE APU AND AIR DISTRIBUTION SYSTEMS WITH NO DEFECTS BEING NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,300 hrs · 9,720 cycles

THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — FAULTY (CABIN)

CREW REPORTED, EMERGENCY LIGHT (AFT) STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY PATH LIGHT STRIP, OPS CHECKED GOOD IAW EMB145 AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK THE LEFT FORWARD DIGITAL STRAP FROM FRAME 15 TO FRAME 16.5 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CRACKED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE CRACKED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — GOUGED (FUSELAGE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE GOUGED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK THE AFT LEFT CENTER DIGITAL STRAP WAS FOUND TO BE CORRODED AT FRAME 16 TO FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE LEFT BUTTSTRAP AT FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 245 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED FROM FRAME 65 TO 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (NR 2 NACELLE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE AFT EDGE MEMBER OF THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE CROSS MEMBER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCING ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (RT NACELLE) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE RIGHT HAND ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 11,550 hrs · 8,325 cycles

SHV - DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHT ABOVE THE COCKPIT DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE POWER TO THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 10,714 hrs · 7,649 cycles

EWR---CO3418, CREW REPORTED, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. EICAS MESSAGE LDG GEAR DISAGREE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-00, AND PERFORMED SEVERAL LANDING GEAR EXTENSIONS AND RETRACTIONS IAW EMB145 MM 32-30-00. NO FURTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — FAULTY (CABIN)

EWR---CO3453, CREW REPORTED ON POSTFLIGHT CHECK, EMERGENCY LIGHT NEAR EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB IAW EMB145 MM 33-50-00. OPS.CHECKED SYSTEM GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (TE FLAPS)

YYZ FLIGHT 4015 THE CREW REPORTED A LANDING GEAR AURAL WARNING MESSAGE ON LANDING. MAINTENANCE INSPECTED AND REPLACED THE AURAL WARNING UNIT AND THE FLAP SLECTOR LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE FOUND EMERGENCY LIGHT ON MAIN CABIN DOOR INOPERATIVE DURING SERVICE ROUTINE CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN MAIN CABIN DOOR IAW EMB145 AMM 33-50-00. OPS. CHECKED GOOD.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 7,813 hrs · 5,282 cycles

EWR- CREW REPORTED, LATERAL LIGHT AT SEAT 9A SMOKES. MAINTENANCE INSPECTED AND PLACED AIRCRAFT ON MEL. AIRCRAFT RELEASED IAW MEL 33-20-00 CATEGORY C. MAINTENANCE REMOVED AND REPLACED LATERAL PASSENGER CABIN LIGHT ASSY IAW EMB145 MM 33-21-06. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — DAMAGED (LT MLG)

IAH- FLIGHT 4172, AFTER TAKEOFF LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND REMAINED ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES IN FLIGHT. NORMAL LANDING OCCURRED AT IAH. MAINTENANCE FOUND THAT THE LEFT GEAR WEIGHT ON WHEELS PROX SWITCH FOR LEFT MLG STRUT CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE PROX SWITCH ON LEFT MLG IAW EMB 145 M/M 32-63-01, NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (COCKPIT)

IAH- FLIGHT 4172, AFTER TAKEOFF, LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND, REMAINED ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES INFLIGHT. NORMAL LANDING OCCURRED IN IAH. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED A OPERATIONAL CHECK IAW EMB145 M/M 32-32-01. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GARLOCK SEAL — LEAKING (#1 ENGINE)

LCH- DURING FLIGHT 3788, THE CREW NOTED NUMBER 1 ENGINE LOW OIL QUANTITY AND PRESSURE, DECLAIRED EMERGENCY, AND DIVERTED TO LCH, (ACTUAL DESTINATION WAS HSV). LCH- MAINTENANCE REMOVED AND REPLACED THE #3 GENERATOR GARLOCK SEAL, SERVICED THE ENGINE OIL SYSTEM,AND,PERFORMED A ENGINE RUN UP,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BLOWN (CABIN) · airframe 7,066 hrs · 4,778 cycles

TYS, During a scheduled routine check the emergency light at seat 12A was found not working, Maintenance removed and replaced the bulb I/A/W-EMB-145-AMM-33-50-00. operational checks good, aircraft released to service.

Part: BULB — MALFUNCTIONED (GALLEY)

iah- during flight 3955 the crew noted a strong burning smell coming from the galley courtesy lights. IAH- MAINTENANCE REMOVED AND REPLACEDTHE GALLEY COURTESY LIGHT BULBS, PERFORMED A OPERATIONAL CHECK OF THE GALLEY LIGHTS, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LOOP — FAULTY (ENGINE COWLING)

CLE FLT.#3743 THE CREW REPORTED RIGHT ENGINE FIRE DETECTOR FAILED TESTMAINTENANCE REPLACED RIGHT ENGINE FIRE DETECTOR LOOP. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — FAULTY (GALLEY) · airframe 5,400 hrs · 3,632 cycles

EWR--CO4228, CREW REPORTED BURNING SMELL COMING FROM COFFEE POT.....MAINTENANCE REMOVED AND REPLACED COFFEE POT RECEPTACLE IAW EMB145 MM #25-31-00....OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DAU — FALSE INDICATION (E&E BAY) · airframe 4,823 hrs · 3,233 cycles

CREW REPORTED, BAGGAGE FIRE EXT WARNING LIGHT WILL NOT EXTINGUISH. MAINTENANCE RERACKED THE NR 1 DAU BAGGAGE FIRE EXT WARNING LIGHT EXTINGUISHED AND REMAINED OUT. OPS CHECKED GOOD IAW EMB145 MM 26-15-01. AIRCRAFT RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED (TAIL)

IAH - FLIGHT 3781, THE CREW REPORTED A VERY STRONG FUEL SMELL IMMEDIATELY AFTER STARTING THE APU IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE FUEL SMELL WAS AGAIN REPORTED, THE APU WAS STARTED ON THE GROUND AND MAINTENANCE PLACED THE APU ON MEL 49-00-00 CONTROL NUMBER 009774, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 02/21/01 WHERE MAINTENANCE REMOVED AND REPLACED THE APU. CLEARED MEL 49-00-00 CONTROL NUMBER 009774, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL LINE — LOOSE (APU)

STL/EWR - FLT 4271 - CREW REPORTED ''STRONG SMELL OF FUEL AFTER STARTING THE APU IN FLIGHT''. MAINTENANCE CONTROL MEL''D AIRCRAFT PER MEL 49-00-00 PLACARD PLACARD NR 009259. AIRCRAFT RETURNED TO EWR. MAINTENANCE SECURED FUEL LINE AT FUEL FILTER, AND GROUND RUN CHECKED GOOD IAW EMB 145 MM 49-00-00. MEL CLEARED, AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — BLOWN (FUSELAGE)

EWR C04254, MAINTENANCE REPORTED DURING SERVICE CHECK THAT THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMRGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECKED GOOD.

Part: APU — LEAKING (TAIL SECTION)

IAH - FLT 4055 - THE CREW REPORTED SMOKE IN THE CABIN WITH THE APU RUNNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL CONTROL NR 307952, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 4198, AND MAINTENANCE REMOVED AND REPLACED THE AFFECTED APU, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE)

IAH - DURING MAINTENANCE INSPECTION, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)