N14920

Part: YOKE — CRACKED (NR 1 ENGINE) · airframe 34,245 hrs · 26,798 cycles

DURING ROUTINE MAINTENANCE THE LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE FITTING IAW SB 145-54-0013 AND STS EA 26-2014-063.

Part: INVERTER — FAULTY (CABIN) · airframe 34,152 hrs · 26,722 cycles

DURING ROUTINE MAINTENANCE THE AFT CABIN EXIT SIGN DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE NR4 EMERGENCY LIGHT DC/AC INVERTER. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,076 hrs · 26,365 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY EXIT ROW EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE INVERTER, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (LT AILERON) · airframe 31,799 hrs · 24,983 cycles

DURING C-CHECK,M LT OTBD AILERON PCA BRACKET OTBD TAB HAS WORN LUG HOLE. MAINTENANCE R & R PCA FITTING FOR LT AILERON IAW EC5750-01177(C). THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (YOKE) · airframe 31,799 hrs · 24,983 cycles

DURING C-CHECK. NR 2 ENGINE FWD LOWER YOKE FITTING CRACKED. R & R NR 2 ENGINE FWD LOWER ENGINE YOKE FITTING IAW EC 5450-01073. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — CRACKED (NR 2 PYLON) · airframe 26,440 hrs · 20,637 cycles

THE CREW REPORTED A BLEED NR 2 OVERTEMP MESSAGE IN FLIGHT. ALSO REPORTED A BURNING SMELL. MX INSPECTED AND REPLACED THE NR 2 ENGINE PRECOOLER. OPS CHECKS WERE GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 25,202 hrs · 19,661 cycles

FLIGHT 6030 - SYR - FLIGHT CREW REPORTED BAGG SMOKE INDICATION ON EICAS. SYSTEM RESET WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSE LINE — LOOSE (ANTI-ICE VALVE) · airframe 25,074 hrs · 19,554 cycles

EWR FLT 2609 THE CREW REPORTED A WING ANTI/ICE FAIL MESSAGE DURING ICE TEST ON CLIMBOUT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE INSPECTED AND SECURED SENSE LINE ON THE NR 1 WING ANTI-ICE VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,048 hrs · 19,531 cycles

FLIGHT 2956 - EWR - FLIGHT CREW REPORTED LIGHTNING STRIKE FOLLOWED BY ELECTRICAL SMELL SHORTLY AFTER. EWR MX PERFORMED LIGHTNING STRIKE INSPECTION AND NO DEFECTS WERE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TUBE — FAULTY (NR 1 ENGINE) · airframe 22,395 hrs · 17,165 cycles

BIS FLT 5655 THE CREW REPORTED A "ENGINE NR 1 ATTCS NO MARGIN" MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE COMPRESSOR AIR DISCHARGE TUBE. OPERATIONAL CHECKS WERE GOOD.

Part: TUBE — FAULTY (NR 1 ENGINE) · airframe 22,395 hrs · 17,165 cycles

BIS FLT 5800 THE CREW REPORTED A "ENGINE NR 1 ATTCS NO MARGIN" MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE 14TH STAGE CUSTOMER TUBE. OPERATIONAL CHECKS WERE GOOD.

Part: FUEL CONTROL — LEAKING (APU) · airframe 22,304 hrs · 17,083 cycles

THE CREW REPORTED A FUEL SMELL COMING FROM THE APU. MAINTENANCE INSPECTED AND REPLACED THE APU FUEL CONTROL. OPERATIONAL CHECKS WERE GOOD.

Part: BLEED VALVE — FAULTY (APU) · airframe 22,274 hrs · 17,057 cycles

FLT 5779 THE CREW REPORTED A FUEL SMELL IN THE CABIN WITH THE APU RUNNING. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,964 hrs · 16,772 cycles

DURING ROUTINE MAINTENANCE THE AFT AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,883 hrs · 16,694 cycles

TYS - FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN SEATS 8 THRU 12 INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 5. OPS CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION AT STRINGER 21R AND SPLICE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REPAIRED THE AREA IAW EMB 145 SRM 51-40-02 AND 51-40-03. RE-STORED SURFACE FINISH IAW EMB 145 CPM 51-21-05 AND 06. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: ANGLE — CORRODED (GALLEY) · corrosion level 2 · airframe 21,883 hrs · 16,694 cycles

AFT GALLEY STEP UP CORRODED AT OUTBOARD END. REPLACED LWR AFT STEP UP ANGLE, FABRICATED, INSTALLED, ALODINED, PRIMED AND PAINTED OUTBOARD ANGLE IAW EMB 145 SRM 51-40-02, 51-00-00 AND CPM 51-21-04, 05 & 06.

Part: SUPPORT — CORRODED (NR 2 GENERATOR) · corrosion level 2 · airframe 21,883 hrs · 16,694 cycles

A COUPLE OF BOLT HOLES OUTBOARD OF THE NR 2 GENERATOR SUPPORT ON THE NR 2 ENG INLET FLANGE HAS CORROSION. REMOVED CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - STRINGER 21R AND SPLICE CORRODED BETWEEN FRAMES 14 AND 15. REPAIRED AREA IAW EMB 145 SRM 51-40-02 AND 51-20-03. RESTORED SURFACE FINISH IAW EMB 145 CPM 51-21-05 & 06.

Part: FITTING — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - SHEAR CLIP CORRODED AT FRM 12 STRINGER 21R. REMOVED AND REPLACED SHEAR CLIP.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - CORROSION ON SUPPORT ASSY FOR AILERON TORQUE TUBE ON SKIN SIDE BETWEEN FRAMES 11 AND 12 BETWEEN STRINGERS 21R AND 20R. REMOVED AND REPLACED SUPPORT ASSY.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - INNER SKIN SPLICE BETWEEN FRMS 12 AND 13 AND BETWEEN STRINGERS 19L AND 19R CORRODED. FOUND TO BE STR 20L AND 20R. REMOVED AND REPAIRED SECTION OF SKIN BUTTSTRAP BETWEEN STR 20L AND 20R.

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,883 hrs · 16,694 cycles

TYS - CORRODED HARDWARE AND EVIDENCE OF CORROSION ON INTERNAL SKIN BETWEEN FRAMES 13 AND 14 AND STRINGERS 21L AND 21R. REMOVED DAMAGED SECTION OF SKIN BUTTSTRAP, REPAIRED BUTTSTRAP BETWEEN STR 20R AND 20L. REMOVED 21R AND 21L SPLICES AND FOUND NO CORROSION TO SKIN, REPLACED STRINGER SPLICES. PRESSURE CHECK GOOD.

Part: DISPLAY — SHORTED (COCKPIT) · airframe 21,558 hrs · 16,396 cycles

IAD FLT 5701 THE CREW REPORTED A EICAS FAIL AND A BURNT SMELL IN THE COCKPIT. THE C/B WAS POPPED AS WELL. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S EICAS /PFD DISPLAY UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 21,183 hrs · 16,093 cycles

DURING ROUTINE 3A INSPECTION THE APU FIREWALL HAD MULTIPLE CRACKS AROUND THE LEFT UPPER SUPPORT AREA. THE FIREWALL WAS REPAIRED IAW SRM 53-32-13, 4 CRACKS TOTAL .53, .52, .68, .73 INCH IN LENGTH.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 21,148 hrs · 16,070 cycles

IAH - FLIGHT 2119, DURING POST FLIGHT INSPECTION THE CREW REPORTED EMERGENCY LIGHTS NOT WORKING BETWEEN ROWS 8-11 WITH WIRES STICKING OUT AT ROW 8. MAINTENANCE RE-SECURED THE LIGHT STRIP AT 7A-11A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 21,033 hrs · 15,984 cycles

IAH - FLIGHT 2989, DURING CRUISE FLIGHT THE CREW REPORTED LOSING THE NUMBER TWO HYDRAULIC SYSTEM. THE CREW DECLARED AN EMERGENCY, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — INOPERATIVE (APU) · airframe 19,635 hrs · 14,880 cycles

DURING APU START, APU FIRE INDICATION ON EICAS WITH SMOKE COMING FROM APU TAIL CONE. APU CUT, NO FIRE NOTICED. EWR MX REMOVED AND REPLACED APU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,247 hrs · 15,415 cycles

IAH - DURING A-CHECK INSPECTION THE NUMBER TWO AND THREE EMERGENCY LIGHT AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,963 hrs · 15,194 cycles

CREW REPORTED VERIOUS EMERGENCY LIGHTS INOPERATIVE. MX RESET FWD EMERGENCY LIGHT POWER SUPPLY. CHECKS WERE GOOD AND ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,328 hrs · 14,719 cycles

IAH - FLIGHT 2850, AFTER LANDING THE CREW REPORTED A FUEL SMELL IN THE AIRCRAFT AFTER STARTING THE APU. THE AIRCRAFT MADE IT TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE APU BLEED SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,201 hrs · 13,895 cycles

FLIGHT 2516 EWR FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHTS VERY DIM AND STAYS ON WHILE SWITCH IS IN OFF POSITION. EWR MX R&R EMERGENCY LIGHT BATTERY NR 2 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,936 hrs · 13,707 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: ATTACH BRACKET — DAMAGED (AILERON) · airframe 17,323 hrs · 13,311 cycles

LEFT DAMPER ATTACHMENT BRACKET ON AILERON SPAR O/B HAT BUSHING IS MIGRATED. MX REMOVED AND REPLACED LEFT AILERON DAMPER ATTACH BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 17,323 hrs · 13,311 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER BEAM HAS CORROSION. MX REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: THERMAL SWITCH — TRIPPED (ZONE 900) · airframe 14,358 hrs · 11,138 cycles

FLT 2807, F/A NOTED THERMAL SWITCH FOR GALLEY POPPED IN FLIGHT WITH ASSOCIATED BURNING ODOR. AC RELEASED IAW MEL 25-60-02 (3) CAT D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,516 hrs · 10,495 cycles

RIC MX - DURING ACFT ROUTINE MAINTENANCE, MX FOUND RT OVERWING LIGHT INOP. MX REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 13,506 hrs · 10,486 cycles

EWR LOG SQUAWK LAV SMOKE WARNING AFTER DEPARTURE. NO SMOKE NOTICED. WARNING WENT AWAY AFTER 1 MINUTE. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB-145 AMM 26-14-01. OPS CHECK GOOD.

Part: LEVER — LOOSE (PAX DOOR)

CLE - FLIGHT NR 3264 - THE CREW REPORTED, THE MAIN CABIN DOOR IS VERY HARD TO OPEN. IT STICKS AND CAN TAKE SEVERAL TRIES TO OPEN. MAINTENANCE INSPECTED AND RE-SECURED THE MAIN CABIN DOOR LOCKING LEVER. OPERATIONAL CHECKS WERE REPORTED GOOD.

Part: PROXIMITY SWITCH — FAILED (NLG)

LOUD RUMBLING SOUND FROM NOSE. CAME SUDDENLY DURING CLIMB-OUT. SOUNDED LIKE NOSE GEAR DOOR OPENED UP. MAINTENANCE INSPECTED AND FOUND NOSE GEAR DOORS WOULD NOT CLOSE ON GEAR RETRACTION. REPLACED NOSE GEAR DOOR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 8,458 hrs · 6,473 cycles

EWR - CREW REPORTED, EMERGENCY LIGHTS AT EXIT ROWS ARE REAL DIM. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY UNDER FLOORBOARD IAW EMB145 MM 333-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 12A)

CLE FLIGHT 2314 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE AT 12A ON CEILING. MAINTENANCE REPLACED THE EMERGENCY LIGHT ON THE CEILING AT ROW 12A. OPERATIONAL CHECKS WERE GOOD.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C CHECK THE CENTER BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED AROUND THE NUTPLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01118. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (LT NACELLE) · airframe 7,567 hrs · 5,755 cycles

SHV - DURING C-CHECK THE LEFT HAND LOWER COWLING RIB AT STATION NX-2180.0 WAS FOUND TO HAVE A HOLE CHAFED IN IT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 54-10-07 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · airframe 7,567 hrs · 5,755 cycles

SHV - DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED ON THE LEFT HAND SIDE AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01121. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

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

Part: STIFFENER — CHAFED (NR 1 NACELLE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE NR 1 ENGINE LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE SERVICE DOOR CENTER 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: GUSSET — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

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

Part: GUSSET — CORRODED (CABIN) · airframe 7,567 hrs · 5,755 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE AFT DIGITAL BUTTSTRAP 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: REINFORCEMENT — CHAFED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. 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: SKIN — DENTED (FUSLAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C- CHECK THE OUTER SKIN WAS FOUND TO BE DENTED AT FRAME 20 AND JUST BELOW STRINGER 11L. MAINTENANCE BLENDED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

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

Part: FIREWALL — CRACKED (APU BAY) · airframe 7,567 hrs · 5,755 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. 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 (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAMES 20 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE NUMBER 5 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK, THE SUPPORT PLATE FORWARD OF FRAME 61 AT STRINGER 15L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (CABIN) · airframe 7,567 hrs · 5,755 cycles

DURING C-CHECK, THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 6,725 hrs · 5,110 cycles

CREW REPORTED, BURNING ODOR WHEN PACKS ARE ON. MAINTENANCE INSPECTED AIRCRAFT AND RAN PACKS, NO ODOR DETECTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — LOOSE (CABIN)

THE CREW NOTED THAT THE EMERGENCY LIGHTS POP THE CIRCUIT BREAKER WHEN SELECTED ON DURING POST-FLIGHT. STL- MAINTENANCE RESECURED WIRE TO THE EMERGENCY LIGHT BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

During scheduled maintenance the overwing emergency exit lights were found to be inoperative. Maintenance removed and replaced the emergency light battery charger assembly. The emergency light system operationally tested good and the aircraft was approved for return to service.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT NR 3027 THE CREW REPORTED THE EXIT LIGHT WAS INOPERATIVE ON THE GALLEY DOOR. MAINTENANCE INSPECTED AND RESECURED THE LOOSE CONNECTOR ON THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,645 hrs · 2,641 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED THE DAMAGED AREA AND FABRICATED NEW ANGLE SHIM AND FILLER IAW EMB-145 SRM 63-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,645 hrs · 2,641 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD CENTER TOP CAP BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — NICKED (FUSELAGE) · airframe 3,645 hrs · 2,641 cycles

TYS DURING A SCHEDULED INSPECTION A NICK WAS FOUND ABOVE THE AFT AVIONICS DOOR. MAINTENANCE MEASURED AND BLENDED THE DAMAGE, PERFORMED DYE PENETRANT INSPECTION IAW-GST2491/02 AND CMP-51-21-02,05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: INVERTER — INOPERATIVE

BNA - Crew reported that the aft ceiling emergency exit light was found to be inoperative. Maintenance removed and replaced the #4 inverter and the aircraft was approved for return to service.

Part: BEARING — DISINTEGRATED (NLG) · airframe 925 hrs · 666 cycles

EWR FLIGHT 4142 CREW REPORTED THAT ON TOUCHDOWN THE NOSE GEAR IMMEDIATELY BEGAN TO VIBRATE. ON THE POST FLIGHT INSPECTION THE NOSE WHEEL BEARING WAS DISCOVERED TO BE DISINTEGRATED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY IAW EMB-145 MM 32-20-01. THE NOSE GEAR WHEELS ASSEMBLIES WERE ALSO REMOVED AND REPLACED IAW EMB-145 MM 32-49-05. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — BROKEN (CABIN)

BNA-CLE FLIGHT 4034 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS WERE NOT WORKING AT ROWS 1 AND 2. MAINTENANCE INSPECTED AND REPAIRED A BROKEN WIRE ON THE AISLE PATH LIGHTING. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (CABIN)

CLE FLIGHT 3897 THE CREW REPORTED THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED AND RESEATED THE CANNON PLUG ON THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.