N16510

Part: FIREWALL — CHAFED (APU BAY) · airframe 11,811 hrs · 11,949 cycles

SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED. MAINTENANCE CLEANED UP THE DAMAGED AREA AND INSTALLED A SHIM IAW EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — ODOR (PITOT SYSTEM) · airframe 11,012 hrs · 11,053 cycles

CREW REPORTED, PITOT 3 INOPERATIVE CAUTION LIGHT ON EICAS AND STRONG BURNING SMELL ON CABIN AND COCKPIT. FOUND PITOT NR 3 CURRENT SENSOR MELTED. REMOVED AND REPLACED PITOT NR 3 CURRENT SENSOR K0057 IAW EMB135 AMM 30-31-00, OPS CHECKED GOOD. NO BURNING SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — FAILED (FUSELAGE) · airframe 10,961 hrs · 11,001 cycles

CLE FLIGHT 2805, THE CREW REPORTED UPON ENTERING ICING CONDITIONS, WINDSHIELD HEAT SELECTED, A STRONG ELECTRICAL SMELL WAS DETECTED. THE AIRCRAFT DIVERTED INTO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,217 hrs · 7,104 cycles

TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 7,217 hrs · 7,103 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FAB AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,217 hrs · 7,103 cycles

TYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 7,217 hrs · 7,103 cycles

TYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 7,217 hrs · 7,103 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FORWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,217 hrs · 7,103 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOOR SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING SERVICE CHECK MAINTENANCE FOUND NR 3 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB135 33-50-04. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 7,057 hrs · 6,926 cycles

DURING RON CHECK MAINTENANCE FOUND THE FORWARD RIGHTHAND OVERWING EMERGENCY LIGHT DOES NOT WORK AND FLOOR PROXIMITY LIGHTS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW EMB135 AMM 33-50-04. EMERGENCY LIGHTS OPS. CHECKED GOOD IAW EMB135 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT)

CREW REPORTED, (VARIOUS EMERGENCY LIGHTS IN FORWARD CABIN ARE INOPERATIVE.) MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB135 AMM NR 33-50-04. OPS. CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN)

THE CREW REPORTED THE EMERGENCY EXIT LIGHTING WOULD NOT REMAIN ILLUMINATED DURING TESTING. MAINTENANCE RECHARGED THE EMERGENCY EXIT LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE THE SECOND AND THIRD EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — OUT OF POSITION (REFUELING PANEL) · airframe 6,829 hrs · 6,719 cycles

CREW REPORTED, FUEL NR 1 LOW LEVEL MESSAGE CAME ON INFLIGHT ON ARRIVAL INTO EWR. NR 1 FUEL QTY INDICATOR SHOWS ZERO FUEL. DECLARED EMERGENCY AND LANDED UNEVENTFULLY IN EWR. MAINTENANCE FOUND REFUELING SWITCH TO BE IN THE OPEN POSITION ON THE REFUELING PANEL. CLOSED SWITCH OPS, CHECKED GOOD IAW EMB135 AMM 28-11-00, INDICATION CHECKS GOOD.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT NR 3160 THE CREW REPORTED THE CABIN SMELLS OF FUMES WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND RAN APU WITH BLEED ON AND OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — FAILED (RIGHT PYLON)

CLE FLIGHT 3052 THE CREW REPORTED THE NR 2 ENGINE SHUT DOWN IN FLIGHT UNCOMMANDED. THEY REPORTED A LOUD BANG AND HIGH ITT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — OUT OF ADJ (EMERGENCY EXIT)

DURING A 2A INSPECTION MAINTENANCE FOUND THE RIGHT HAND OVERWING EMERGENCY EXIT DID NOT PRODUCE A MESSAGE ON THE EICAS WHEN THE DOOR WAS OPEN. MAINTENANCE ADJUSTED THE MICROSWITCH ON THE RIGHT HAND EMERGENCY EXIT DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED MAINTENANCE.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULED INSPECTION A FAIRLEAD FLOOR SUPPORT AT THE CENTER OMEGA BEAM WAS FOUND BROKEN AT FR21. MAINTENANCE R/R THE FAIRLEAD FLOOR SUPPORT AND THE WORK WAS FOUND SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULED MAINTENANCE.

Part: FIREWALL — DAMAGED (FUSELAGE) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULE 1-C INSPECTION,MAINTENANCE FOUND A HOLE RUBBED INTO THE FIREWALL BLANKET. MAINTENANCE USED EC5330-01166 FOR THE REPAIR. ALL WORK WAS DONE IAW THE EC AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULE MAINTENANCE.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED MAINTENANCE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULED INSPECTION, SEVERAL AREAS OF CORROSION WAS FOUND ON THE CENTER FLOORBEAM GUSSET BETWEEN FRAMES 18-22. MAINTENANCE REMOVED AND REPLACED GUSSET TOP CAP. IAW-EMB-135/145-SRM-51-40-02. REPAIR PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAL — CORRODED · airframe 3,265 hrs · 3,090 cycles

TYS During a scheduled inspection, corrosion was found on the right floor seal at frame 18. Maintenance removed surface corrosion, alodined, primed and painted. I.A.W.-EMB135/145-CMP-51-21-04,05 and 06. Repair procedure was satisfactory and the aircraft will be released upon complection of inspection.

Part: ANTENNA — CORRODED · airframe 3,265 hrs · 3,090 cycles

TYS During a scheduled inspection the lower TCAS antenna was found with corrosion on the base. Maintenance removed and replaced the antenna, operational checked good. I.A.W.-EMB-AMM-34-43-03. Repair procedure was satisfactory and the aircraft will be released upon complection of inspection.

Part: SWITCH — INOPERATIVE · airframe 3,265 hrs · 3,090 cycles

TYS During a scheduled inspection, When doing inspection task card # 35-20-00-720-001-A00, the cabin oxygen masks did not deploy in auto mode. Maintenance removed and replaced the altitude sensing switch. I.A.W.-EMB-135-AMM-51-40-02. operational checked good. Repair procedures where satisfactory, aircraft will be released upon complection of inspection.

Part: GUSSET — CORRODED · airframe 3,265 hrs · 3,090 cycles

TYS During a scheduled inspection, corrosion was found on the floor gussets at the entrance to the cockpit, between frames 15 and 18. Maintenance removed and replaced gusset and center section of forward digital plate (fabricated doubler, shims and cockpit step bracket),alodined, primed and painted. I.A.W.-EMB135/145-SRM-51-40-02 and CMP-51-21-04,05 and 06., and EC5320-01059. Repair procedure was satisfactory and the aircraft will be released upon complection of inspection.

Part: BUSHING — BACKED OUT (PAX DOOR) · airframe 3,265 hrs · 3,090 cycles

TYS DURING A SCHEDULED INSPECTION THE PAX-DOOR HOLD OPEN PIN LOWER BUSHING WAS FOUND TO BE MIGRATING OUT. MAINTENANCE INSTALLED BUSHING FROM THE BOTTOM IN REFERENCE TO GST-1662/01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED ON COMPLETION OF AIRCRAFT MAINTENANCE INSPECTION.

Part: FLOOR SUPPORT — CORRODED · airframe 3,265 hrs · 3,090 cycles

TYS Several areas of corrosion were found on the aft side of service door aft of frame 22.Maintenance removed floor support and replaced it with a new part IAW emb135/145 SRM 51-40-02 and 51-10-02-Work was satisfactory and aircraft will be released upon completion of scheduled maintenance.

Part: TUBE — BROKEN (LT ENGINE)

MDW-EWR - FLT 3620 - THE CREW REPORTED THE LEFT ENGINE ITT WAS HIGHTER THAN THE RIGHT (APPROX 100 DEGREES) WHILE IN CRUISE. THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE AIR TUBE ASSY FOR THE DIFFUSER TO THE START BLEED CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD IAW ROLLS ROYCE MM 75-31-15 AND 77-00-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)