N12922

Part: FIREWALL — CRACKED (APU BAY) · airframe 35,313 hrs · 26,992 cycles

DURING MAINTENANCE INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LT BOTTOM FRAME ATTACHMENT POINT. MAINTENANCE REMOVED THE DAMAGED SECTION OF FIREWALL AND PERFORMED A FILLER/DOUBLER REPAIR IAW SRM 53-32-12, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 35,313 hrs · 26,992 cycles

DURING MAINTENANCE INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT BOTTOM FRAME ATTACHMENT POINT. MAINTENANCE REMOVED THE DAMAGED SECTION OF FIREWALL AND PERFORMED A FILLER/DOUBLER REPAIR IAW SRM 53-32-12, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 35,163 hrs · 26,878 cycles

THE CREW REPORTED A SMOKE INDICATION FROM THE CARGO BAY, THE QRH WAS FOLLOWED AND THE CARGO FIRE BOTTLES WERE DISCHARGED. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, FOUND NO EVIDENCE OF SMOKE OR FIRE, OPERATIONALLY TESTED THE CARGO SMOKE DETECTION SYSTEM, REPLACED THE CARGO FIRE BOTTLES, PERFORMED ENGINE RUNS ALL WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — ODOR (NR 2) · airframe 34,793 hrs · 26,591 cycles

PILOT REPORTED THE F/O PFD CIRCUIT BREAKER TRIPPED IN FLIGHT WITH AN ELECTRICAL BURNING ODOR NOTICED. MAINTENANCE R & R THE NR 2 PFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,664 hrs · 25,705 cycles

CREW REPORTED A BURNING ODOR DURING DECENT AND AGAIN DURING LANDING. MX PERFORMED AN OPS CHECK OF THE AIR CONDITIONING PACKS AND COULD NOT DUPILCATE ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 33,520 hrs · 25,587 cycles

THE CREW REPORTED A MUSTY ODOR WHEN EITHER BLEED ENGINE NR 1 OR NR 2 SELECTED BUT GOES AWAY WHEN APU IS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,518 hrs · 25,585 cycles

THE CREW REPORTED FAINT OIL BURNING ODOR FROM NR 2 PACK DURING CLIMB AND DESCENT. BLEED SOURCE WAS NR 2 ENGINE. OPEN

Part: FRAME — CRACKED (FUELAGE) · airframe 32,115 hrs · 24,506 cycles

DURING C-CHECK, FRAME 10 WAS FOUND CRACKED UNDER F/O WINDOW. MAINTENANCE R & R THE CRACKED FRAME IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FRAME — CORRODED (APU BAY) · airframe 32,115 hrs · 24,506 cycles

DURING C-CHECK. APU GROUNDING SHUNT BAR WAS FOUND CORRODED AT FRAME 80. MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER AT FRAME 80 FOR THE GROUNDING BAR MOUNT IAW EC 5310-01544, REV C. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: THRESHOLD — CORRODED (FRAMES 20-22) · airframe 32,115 hrs · 24,506 cycles

DURING C CHECK, CORROSION WAS FOUND AROUND NUTPLATE HOLES IN SERVICE DOOR THRESHOLD BETWEEN FRAMES 20 - 22. MAINTENANCE R & R THE CORRODED THRESHOLD IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 32,115 hrs · 24,506 cycles

DURING C CHECK, FOUND RT OMEGA BEAM GUSSET AT FRAME 61 WAS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED A NEW OMEGA BEAM IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (FRAME 20) · airframe 32,115 hrs · 24,506 cycles

DURING C-CHECK, A CRACK WAS FOUND AT FRAME 20, S3L IN THE COASTAL REINFORCEMENT. MAINTENANCE R & R COASTAL REINFORCEMENT IAW SRM 51-40-02.

Part: SKIN — CORRODED (FRAMES 17-19) · airframe 32,115 hrs · 24,506 cycles

DURING C-CHECK, MULTIPLE AREAS OF CORROSION FOUND ON THE INTERIOR BELLY SKIN AT FRAMES 17-19 AND STRINGERS 21L-22R. MAINTENANCE CUTOUT THE DAMAGE AREA, FABRICATED AND INSTALL A FILLER,SHIM AND A REPAIR DOUBLER IAW EC 5320-01890. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,466 hrs · 24,037 cycles

DURING SCHEDULED MX INSPECTION THE LT OVERWING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. MX R & R INVERTER, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHT) · airframe 31,007 hrs · 23,676 cycles

EMERGENCY LIGHTS OVER THE EXIT ROWS WOULD NOT LIGHT, DURING TEST. MX INSPECTED AND PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. OPS CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 30,897 hrs · 23,592 cycles

PILOT REPORTED THE EMERGENCY EXIT LIGHT IN THE CEILING FACING THE FLIGHT DECK WAS DISCOVERED INOPERATIVE. MX PERFORMED AN OPS CHECK OF THE CABIN EMERGENCY LIGHTS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,414 hrs · 21,605 cycles

DENT BETWEEN FRM 15 & 16 AND BETWEEN STRINGER 17L & 18L. REPAIRED DAMAGE, INSTALLED PATCH AND REPLACED SHEAR CLIP IAW ETD2012-145-011674 REV B. ACFT RELEASED AND RETURNED TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 27,197 hrs · 20,633 cycles

ACFT IN FOR A C-CHECK, BAGGAGE DOOR LATERAL L SHAPE BEAM AT FRAME 68 CORRODED. MX REMOVED THE CORROSION IAW THE SRM 51-10-03. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

CROSS MEMBER AT FRM 25 CORRODED. BLENDED CORROSION MATERIAL REMOVED IS WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,633 hrs · 27,197 cycles

CENTER OMEGA BEAM BETWEEN FRM 59 TO 61 CORRODED AT FORWARD NUT PLATE. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLERS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

CAP ON CENTER OMEGA BEAM AT FRAME 18 - FRAME 20 CORRODED. BLENDED CORROSION MATERIAL REMOVED IS WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,196 hrs · 20,633 cycles

CENTER OMEGA BEAM CAP FROM FRM 59 TO FRM 61 CORRODED. REPLACED CENTER OMEGA BEAM CAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,196 hrs · 20,633 cycles

RT OMEGA BEAM CORRODED JUST AFT OF FRM 18. BLENDED CORROSION, MATERIAL REMOVED IS WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

CARGO COMPARTMENT DIGITAL Y-479 HAS CORROSION FROM FRM59 TO FRM61. R & R DIGITAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

CROSS MEMBER FOR POTABLE WATER LT SIDE CORRODED. R & R CROSS MEMBER.

Part: STRUCTURE — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

MAIN DOOR CUT-OUT REAR DIGITAL HAS CORROSION. R & R DIGITAL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

REAR GALLEY RT AFT SILL CORRODED. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

FWD GALLEY SILL CORRODED. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

RT SILL FROM FRAME 59 TO FRAME 61 CORRODED. R & R SILL.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,661 hrs · 20,253 cycles

SEAT 12BC TOP EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 23,789 hrs · 18,114 cycles

CLE FLT 2611 AIR RETURN CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED PRESSURIZATION DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,216 hrs · 17,612 cycles

FLIGHT 2217 - EWR - FLIGHT CREW REPORTED ELECTRICAL SMELL AT ROWS 1-4. EWR MX RAN ELECTRICAL SYSTEMS BUT COULD NOT DUPLICATE ELECTRICAL SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ALTIMETER — STICKING (COCKPIT) · airframe 22,923 hrs · 17,390 cycles

IAH - FLIGHT 2433, ON TAKEOFF THE CREW REPORTED THE STANDBY ALTIMETER TO BE STICKING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE STANDBY ALTIMETER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (FIRE PROTECTION) · airframe 22,222 hrs · 16,889 cycles

FLIGHT 2391 - EWR - FLIGHT CREW REPORTED BAGG EXTINGUISHER LIGHT NOT ILLUMINATED DURING TEST. EWR MX REMOVED AND REPLACED RELAY K0629 AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CRACKED (LAV WASTE) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK LAV WASTE DRAIN SUPPORT CRACKED. REMOVED AND REPLACED LAV WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK RT I/B HORIZ STAB HINGE PIN BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RIGHT I/B HORIZ STAB HINGE PIN BUSHING IAW EC5510-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK RT GROUND SPOILER ACTUATOR FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REINSTALLED RT GROUND SPOILER ACTUATOR FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152 CHECKED AND FOUND TO BE WITHIN LIMITS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK RIGHT O/B HORIZ STAB HINGE PIN BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RIGHT O/B HORIZ STAB HINGE PIN BUSHING IAW EC 5510-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (MAIN DOOR) · corrosion level 2 · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK MAIN DOOR HAS CORROSION (LEVEL 2 LOCAL) AROUND NUT PLATE HOLE AT BOTTOM SECTION OF DOOR. MAINTENANCE PERFORMED REPAIR AT MAIN DOOR LOWER NUT PLATE HOLES IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPEED BRAKE) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK RT SPEED BRAKE ACTUATOR FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REINSTALLED RT SPEED BRAKE ACTUATOR FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152, WITHIN LIMITS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK RT GROUND SPOILER O/B HINGE FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND RE-INSTALLED RT GROUND SPOILER O/B HINGE FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152, CHECKED AND FOUND TO BE WITHIN LIMITS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 22,200 hrs · 16,873 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) AROUND SCREW HOLES FOR SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL (THRESHOLD) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 21,689 hrs · 16,479 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING ODOR AT THE SEAT 6-10 AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST AT ROW 8, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DMU — INOPERATIVE (TE FLAP) · airframe 21,274 hrs · 16,155 cycles

FLIGHT 2580 - EWR - DURING LANDING, FLIGHT CREW REPORTED FLAP FAIL WARNING ON EICAS AND FLAP STUCK TO 0. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FECU (SDR C2XA09RI134), FDMU AND FUSE 0098 (SDR# C2XA09RI136). MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ECU — INOPERATIVE (TE FLAP) · airframe 21,274 hrs · 16,155 cycles

FLIGHT 2580 - EWR - DURING LANDING, FLIGHT CREW REPORTED FLAP FAIL WARNING ON EICAS AND FLAP STUCK TO 0. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FECU, FDMU (SDR C2XA09RI135) AND FUSE 0098 (SDR C2XA09RI136). MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FUSE — BLOWN (TE FLAP) · airframe 21,274 hrs · 16,155 cycles

FLIGHT 2580 - EWR - DURING LANDING, FLIGHT CREW REPORTED FLAP FAIL WARNING ON EICAS AND FLAP STUCK TO 0. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FECU (SDR C2XA09RI134), FDMU (SDR C2XA09RI135) AND FUSE 0098. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,600 hrs · 15,652 cycles

IAH - FLIGHT 2117, THE CREW REPORTED AN ELECTRICAL SMELL NOTED DURING CRUISE FOR APPROXIMATELY THREE MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED GROUND RUNS, PRESSURIZED THE AIRCRAFT, ACTIVATED MULTIPLE SYSTEMS ALL WITH NO DEFECTS NOTED, AND UNABLE TO DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (NLG DOOR) · airframe 19,584 hrs · 14,884 cycles

CLE - FLIGHT 2775 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS AFTER SELECTING GEAR DOWN. THE MESSAGE CLEARED IMMEDIATELY AND NO OTHER INDICATIONS WERE NOTICED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (ELECTRICAL SYS) · airframe 15,432 hrs · 11,878 cycles

ICT - FLIGHT 2725, THE CREW REPORTED AN ELEC EMERGENCY ABNORMAL MESSAGE ON EICAS DURING CLIMB. THE CREW PERFORMED AN EMERGENCY DESCENT, AND LANDED AT ICT WITHOUT INCIDENT. THE CREW RESET THE AIRCRAFT POWER AND VERIFIED NORMAL OPERATIONS, MX VERIFIED THAT LANDING WAS LESS THAN 6 FOS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,208 hrs · 11,702 cycles

FLT 2359 - EWR - CREW REPORTED ELECTRICAL EMERGENCY ABNORMAL AND EMERGENCY LIGHT NOT ARMED INDICATIONS CAME ON TAXI. EWR MX REMOVED AND REPLACED RELAY K0097 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,076 hrs · 10,826 cycles

MX DURING AC ROUTINE MAINTENANCE, MX FOUND LT FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED FWD EMERGENCY LIGHT. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 12,472 hrs · 9,548 cycles

IAH - FLIGHT 2511, DURING CRUISE, THE CREW REPORTED THE MAIN PITCH TRIM TO BE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 12,466 hrs · 9,541 cycles

DURING C CHECK, THE FORWARD AND AFT SERVICE DOOR FRAMES WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 12,466 hrs · 9,541 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 12,466 hrs · 9,541 cycles

DURING C-CHECK, THE FORWARD AND AFT SERVICE DOOR FRAMES WERE FOUND TO BE CORRODED BETWEEN 15R AND 16R. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,466 hrs · 9,541 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, SECTION 7, FIGURE 206 AND EC 5320-1295. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIXTURE — CORRODED (CABIN) · corrosion level 2 · airframe 12,466 hrs · 9,541 cycles

DURING C-CHECK ,THE LAV WASTE DRAIN BASE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE DRAIN BASE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (RT ENGINE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE RIGHT HAND ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/1466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE FORWARD SERVICE DOOR 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: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON FIBER CROSS BEAM. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORM A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK, THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON CROSS BEAM AT FRAME 24. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

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

Part: SILL — CORRODED (CABIN) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE SERVICE DOOR AFT 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: STRAP — CORRODED (FLOORBEAM) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 7,959 hrs · 6,068 cycles

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

Part: STRINGER — GOUGED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE T-REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59 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: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,959 hrs · 6,068 cycles

DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 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: DOUBLER — CORRODED (FLOORBEAM) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE RIGHT FLOORBEAM DOUBLERS AT FRAME 20 AND 22 WERE FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 7,959 hrs · 6,068 cycles

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

Part: SILL — CORRODED (CABIN) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 59. 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 (FLOORBEAM) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE 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) · airframe 7,959 hrs · 6,068 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — FAULTY (EMERGENCY LIGHT)

DURING SERVICE AND ROUTINE INSPECTION OF AIRCRAFT, MAINTENANCE FOUND ROW NR 3 EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 6,929 hrs · 5,266 cycles

DURING WALKAROUND, CREW FOUND EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10-11 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — FAILED (NR 2)

CLE FLIGHT NR 2962 THE CREW REPORTED THE NR 2 ENGINE FALIED ON CLIMBOUT FROM BTV. THE AIRCRAFT DIVERTED INTO SYR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT RELEASED FOR SERVICE.

Part: TOWERSHAFT — DAMAGED (NR 2 ENGINE)

ACFT N12922, FLT NR 2962 (BTV - CLE) DURING CLIMB-OUT THROUGH 18,000 FT, THE NR 2 ENGINE SHUTDOWN UNCOMMANDED. THE CREW WAS UNABLE TO RESTART. ACFT DIVERTED TO SYR AND LANDED SAFETY. MECHANICS WERE DISPATCHED TO ACFT. INITIAL FINDINGS INDICATE METAL ON THE OIL TANK MAG PLUG, WITH NO EVIDENCE OF EXTERNAL DAMAGE OR LEAKAGE. UPDATE 8/27/03 - THE ENGINE WAS INTERNALLY INSPECTED AND DAMAGE WAS FOUND ON THE TOWER SHAFT GEAR. THE ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY)

FLIGHT 2466 PASSENGER REPORTED POSSIBLE BURNING ODOR POSSIBLY CAME FROM GALLEY. ODOR WENT AWAY AFTER TURNING OFF COFFEEMAKERS. SERVICED COFFEEMAKERS WITH H2O, VERIFIED NORMAL OPERATION OF COFFEEMAKERS IAW CMM 25-30-40, NO BURNING ODOR NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (NR 2 ENGINE)

LCH FLIGHT 2218 THE CREW REPORTED NR 2 PACK CREATED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE NR 2 HIGH STAGE VALVE WOULD NOT OPEN. THE HIGH STAGE BLEED VALVE AND THE PRESSURE SWITCH WERE REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

BNA- DURING ROUTINE INSPECTION THE MECHANIC NOTED THAT THE FORWARD ORANGE EMERGENCY LIGHT FLOOR PROXIMITY STRIP FAILED TO ILLUMINATE. BNA- MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 EMERGENCY LIGHT INVERTER, IAW EMB 145 MM 33-50-11,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT FIRST ROW FAILED TO ILLUMINATE. IAH- MAINTENANCE RECONNECTEDA LOOSE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT#2347 THE CREW REPORTED THE 1ST ROW OF EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE EMERGENCY LIGHT STRIP.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — DISCONNECTED

EWR---CO3491, CREW REPORTED, "ON POST FLIGHT INSPECTION, EMERGENCY LIGHT AT MAIN CABIN DOOR IS INOPERATIVE....MAINTENANCE RESECURED LOOSE WIRES ON EMERGENCY LIGHT STRIP IAW EMB145 AMM #33-50-08. (OPS.CHECKED GOOD)

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE 1ST ROW OF EMERGENCY LIGHTS ON LEFT (SEATS 2A-3A) AND EMERGENCY LIGHTS BY GALLEY DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP ON FIRST ROW. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INACTIVE

EWR---CO3342, CREW REPORTED, "FIRST STRIP OF EMERGENCY AISLE LIGHTS ARE INOPERATIVE....MAINTENANCE RESET AIRCRAFT ELECTRICAL SYSTEM. OPS.CHECKED AILSE PATH EMERGENCY LIGHTS GOOD IAW EMB145 MM #33-50-00 AND #24-36-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2977 THE CREW REPORTED THE GALLEY EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

CLE FLIGHT NR 3282 THE CREW REPORTED SPARKS AND FIRE CAME FROM FLUORESCENT CABIN LIGHT AT SEAT 12C. MAINTENANCE INSPECTED AND REPLACED THE PASSENGER CABIN LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LAMP — FAULTY

BTV---DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND LEFTHAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE.....REMOVED AND REPLACED LAMP IN LEFTHAND OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IN PSU IAW EMB145 AMM #33-50-07. OPS.CHECKED GOOD.

Part: HOSE — DISCONNECTED (HEAT EXCHANGER)

EWR- AIRCRAFT RETURNED TO GATE DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND TWO HOSES DISCONNECTED. REINSTALLED NUMBER TWO RECIRCULATING FAN OUTLET HOSE AND REINSTALLED HEAT EXCHANGER OUTLET HOSE AS REQUIRED. LEAK AND OPERATIONAL CHECK IAW EMB145 MM 21-51-00 GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 3,814 hrs · 2,718 cycles

SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 3,814 hrs · 2,718 cycles

SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR AFT SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (A/C BAY)

IAH- FLIGHT 3724, DURING LANDING THE CREW NOTED THAT SMOKE IN THE CABIN DURING LANDING AND TAXI. MAINTENANCE REMOVED AND REPLACED THE NR 2 ACM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (CABIN)

DAY FLIGHT 3740 CREW REPORTED LAV SMOKE WARNING ON INBOUND TAXI WITH SMOKE IN CABIN. MAINTENANCE RELEASE AIRCRAFT IAW MEL 49-00-00.

Part: LIGHT — INOPERATIVE (CABIN)

DFW FLT 3166 CREW REPORTED EMERGENCY FLOOR PROXIMITY STRIP LIGHTS 2ND STRIP FROM FORWARD TO AFT INOP. MAINTENANCE RELEASED AIRCRAFT IAW MEL 33-50-00.

Part: WIRE — BROKEN (CABIN)

EWR- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS BETWEEN ROWS 9 AND 12 FAILED TO ILLUMINATE. EWR- MAINTENANCE REPAIRED WIRE ON FLOOR PROXIMITY STRIP LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — DAMAGED (CABIN)

CREW REPORTED EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REPAIR DAMAGED WIRING. OPS CHECKED SYSTEM GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: PROXIMITY SENSOR — CRACKED (NLG) · airframe 2,118 hrs · 1,445 cycles

TYS FLIGHT 4148, RECEIVED A LANDING GEAR AIR/GROUND FAULT DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE GEAR PROXIMITY SENSOR FACE TO BE CRACKED. THE SENSOR WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG)

TYS---CO4148, CREW REPORTED LANDING GEAR AIR/GROUND FAIL AND ENGINE 1/2 REVERSER DISAGREE (LIGHTS CAME ON), AIR RETURNED BACK TO TYS AND LANDED UNEVENTFULLY. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SWITCH PROBLEM, PROPERLY INSTALLED NOSE PROXIMITY WOW SWITCH REFERENCE EMB145 MM 32-61-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

BTV---CO3944, DURING RON OF AIRCRAFT MAINTENANCE CLEARED EMERGENCY FLOOR PATH PROXIMITY LIGHT STRIP INOPERATIVE AT SEAT 16 AND 17A MEL (REFERENCE MEL 33-50-00/2 PLACARD 014103). REMOVED AND REPLACED EMERGENCY FLOOR PATH PROXIMITY LIGHT STRIP AT SEAT 16 AND 17A IAW EMB145 MM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.