N12552

Part: TRANSDUCER — INTERMITTENT (BRAKES) · airframe 36,308 hrs · 28,054 cycles

PILOT REPORTED: AT TAXI SPEED WHEN THE PLANE HITS A BUMP IN THE PAVEMENT, ALSO RANDOMLY WITHOUT PRESSURE CHANGES ON THE BRAKE PEDALS THE PLANE SEEMS TO REDUCE THE PRESSURE BEING DEMANDED AND FEELS LIKE IT IS ROLLING FREELY AS IF THE WHEEL LOCK PROTECTION IS COMING ON. WHEN IT RE-ENGAGES IT ENGAGES GRABBING THE BRAKES AND ACFT SHUTTERS. MX REMOVED AND REPLACED THE NR 2 & 3 WHEEL SPEED TRANSDUCERS AND BLED BRAKES WITH TAXI AND OPERATIONAL CHECKS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — FAULTY (PNUEMATIC SYS) · airframe 33,428 hrs · 25,787 cycles

THE CREW REPORTED ODOR OF JET FUEL COMING THROUGH THE VENTS WHILE APU POWERING THE PACKS. MAINTENANCE INSPECTED AND REPLACED APU BLEED VALVE. OPS CHECKS WERE GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 32,092 hrs · 24,701 cycles

CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE.

Part: WIRE HARNESS — ARCED (CABIN LIGHTS) · airframe 32,092 hrs · 24,701 cycles

CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE. MAINTENANCE R & R THE CABIN LIGHT ASSY AND HARNESS AT ROW 6. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SMOKE (ROW 6) · airframe 32,086 hrs · 24,698 cycles

THE CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE. MAINTENANCE RELEASED ACFT IAW 33-20-00-2. SUPPLEMENT TO FOLLOW.

Part: WIRE — CHAFED (CABIN LIGHTS) · airframe 29,880 hrs · 22,978 cycles

THE CREW REPORTED ELECTRICAL BURNING ODOR COMING FROM THE CEILING AROUND THE COURTESY LIGHT AND COCKPIT. MAINTENANCE INSPECTED AND REPAIRED CHAFED WIRES. OPS CHECKED GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 28,926 hrs · 22,267 cycles

PILOT REPORTED THE EMERGENCY LIGHT BETWEEN ROWS 18 & 20 DID NOT ILLUMINATE DURING TEST. MX R & R EMERGENCY LIGHT SECTION AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 28,440 hrs · 21,913 cycles

CREW REPORTED COFFEE POTS WERE NOT WARMING AND A BURNING ODOR. ODOR DISSIPATED WHEN THEY WERE TURNED OFF. MAINTENANCE INSPECTED AND REPLACED THE COFFEE BREWER LT RAIL AND PUMP ASSEMBLY. OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION BEYOND LIMITS AROUND FASTENERS IN RT OTBD FLOOR SUPPORT AT FRAME 20. R & R FLOOR SUPPORT.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 28,431 hrs · 21,906 cycles

SHEAR TIE CRACKED AT FRAME 24, STRINGERS 16 AND 17R. R & R SHEAR TIE.

Part: SEAT TRACK — CORRODED (FRAMES 47-52) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION IN MULTIPLE AREAS ALONG LT SIDEWALL SEAT TRACK SUPPORT. CORROSION OUT OF LIMITS AFTER BLEND-OUT. R & R SUPPORT.

Part: PROFILE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION AROUND NUTPLATES ON BOTTOM OF PAX DOOR IS OUT OF LIMITS. R & R PROFILE.

Part: FLOOR SUPPORT — CRACKED (FRAME 16-17) · airframe 28,431 hrs · 21,906 cycles

CRACK IN INBD SPLICE ANGLE UNDER FLOOR SUPPORT AT LT OMEGA BEAM BETWEEN FRAMES 16-17. R & R CRACKED SPLICE ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION BEYOND LIMITS ON RAMP ANGLE UNDER LATERAL FLOOR SUPPORT. R & R RAMP ANGLE.

Part: STRAP — CORRODED (FRAME 20) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION AROUND NUTPLATE IN GUSSET AT RT OMEGA BEAM, CORRODED BEYOND LIMITS. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAME 19-23) · corrosion level 2 · airframe 28,431 hrs · 21,906 cycles

CORROSION BEYOND LIMITS ALONG LT OTBD FLOOR SUPPORT BETWEEN FRAMES 19-23. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (FRAMES 16-17) · airframe 28,431 hrs · 21,906 cycles

CRACK IN OTBD SPLICE ANGLE UNDER FLOOR SUPPORT AT LT OMEGA BEAM BETWEEN FRAMES 16-17. R & R CRACKED SPLICE ANGLE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,334 hrs · 21,827 cycles

DURING MAINTENANCE INSPECTION THE FWD OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,091 hrs · 21,654 cycles

DURING ROUTINE MAINTENANCE, THE ENTRY OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,055 hrs · 21,629 cycles

DURING ROUTINE MAINTENANCE, FORWARD CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 27,161 hrs · 20,937 cycles

CREW REPORTED A BURNING ELECTRICAL ODOR LIKE A SOLDERING IRON OR HAIR CURLER, ABOVE SEAT 1A. DETERMINED THE ODOR TO BE COMING FROM THE SEAT 1A BALLAST. R & R CEILING LIGHT ASSY AT SEAT 1A WITH OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,821 hrs · 20,665 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB. OPS CK GOOD.

Part: FLAPPER VALVE — LEAKING (RT WING) · airframe 26,080 hrs · 20,101 cycles

THE CREW REPORTED A FUEL LEAK FROM RT WING AFTER TAKEOFF. FUEL QTY DROPPED 300LBS AND THEN FUEL LEAK STOPPED. MX INSPECTED AN REPLACED THE RT WING FLAP VALVE. OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,997 hrs · 18,449 cycles

DURING MX INSPECTION, THE LT AFT EXTERIOR, ROW 12, AND 2 AFT CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R BATTERY CHARGER AND BATTERY PACK. OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 23,625 hrs · 18,145 cycles

DURING C-CHECK, EXTERNAL WASTE VALVE SUPPORT CORRODED AROUND WASTE VALVE. MX R & R WASTE DRAIN VALVE DUMP ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,625 hrs · 18,145 cycles

DURING C-CHECK, CARGO DOOR CUTOUT CENTER SILL CORRODED. MX R & R CARGO DOOR CUTOUT CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (ENGINE) · airframe 23,625 hrs · 18,145 cycles

DURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT FITTING CRACKED. R & R FITTING IAW EC5450-01028. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (RT WING) · airframe 22,612 hrs · 17,327 cycles

RT WING LEAKING FUEL DURING CLIMB. CREW DECLARED AN EMERGENCY, RETUNED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND CLEANED THE FLAPPER VALVE ON THE RT WING. OPS CHECKS WERE GOOD. THE ACFT WAS RELEASED FOR SERVICE.

Part: VALVE — LEAKING (FUEL CELL) · airframe 22,510 hrs · 17,252 cycles

DURING FLIGHT IT WAS NOTED THAT FUEL WAS VENTING FROM THE RT WING. THE CREW ELECTED TO DIVERT, WHERE THE ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE RT WING TANK VENT VALVE, OPERATIONALLY CHECKED THE SYS AND CLEARED THE DISCREPANCY.

Part: VALVE — LEAKING (NR 2 FUEL TANK) · airframe 22,510 hrs · 17,252 cycles

FUEL LEAK NR 2 TANK. R & R RT WING VENT VALVE IAW AMM 28-23-04. OPS AND LEAK CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SWITCH — FAULTY (COCKPIT) · airframe 22,136 hrs · 16,997 cycles

ORD FLT 6092 THE CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE AFTER TAKEOFF. MESSAGE DID NOT CLEAR. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE PUSHBUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERTEMP (MAIN) · airframe 21,358 hrs · 16,366 cycles

FLIGHT 6124 - IAD - FLIGHT CREW REPORTED NR 1 MAIN BATTERY OVERTEMP DURING LANDING. IAD MX REMOVED AND REPLACED NR 1 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: MODULE — INOPERATIVE (CABIN PRESSURE) · airframe 20,353 hrs · 15,496 cycles

FLIGHT 2865 - EWR - FLIGHT CREW REPORTED THAT ON DESCENT PRESSURIZATION CABIN ALT STOPPED AT 5800FT AT 16000FT, FOLLOWING QRH IN MANUAL MODE THE CABIN CLIMBED TO 10000FT, WITH CONTROLLER IN FULL DOWN MODE. CREW ATTEMPTED DUMP MODE AND CABIN CLIMBED TO ALTITUDE BEING FLOWN. EWR MX REMOVED AND REPLACED CPAM AND MANUAL CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA11RI030 REPORTS CPAM AND SDR C2XA11RI031 REPORTS MANUAL CONTROLLER INFO.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 20,353 hrs · 15,496 cycles

FLIGHT 2865 - EWR - FLIGHT CREW REPORTED THAT ON DESCENT PRESSURIZATION CABIN ALT STOPPED AT 5800FT AT 16000FT, FOLLOWING QRH IN MANUAL MODE THE CABIN CLIMBED TO 10000FT, WITH CONTROLLER IN FULL DOWN MODE. CREW ATTEMPTED DUMP MODE AND CABIN CLIMBED TO ALTTUDE BEING FLOWN. EWR MX REMOVED AND REPLACED CPAM AND MANUAL CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA11RI030 REPORTS CPAM AND SDR C2XA11RI031 REPORTS MANUAL CONTROLLER INFO.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 20,289 hrs · 15,447 cycles

THE CREW REPORTED THE CABIN PRESSURIZATION DID NOT DESCEND ON SCHEDULE AFTER ENCOUNTERING ICING CONDITIONS IN AUTO MODE. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: PRESSURE SWITCH — FAULTY (BLEED AIR SYS) · airframe 20,284 hrs · 15,445 cycles

THE CREW REPORTED THE CABIN PRESSURIZATION DID NOT DESCEND ON SCHEDULE. MAINTENANCE INSPECTED AND REPLACED THE HIGH STAGE VALVE PRESSURE SWITCH AND CONNECTOR P1203. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,856 hrs · 14,330 cycles

TAM - DURING TAXI THE CREW REPORTED THAT THE EMERGENCY LIGHTS REMAINED ON CONTINUOUSLY. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE RESET THE ELECTRICAL SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,655 hrs · 14,178 cycles

SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 37. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,655 hrs · 14,178 cycles

SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 18,655 hrs · 14,178 cycles

SHV - DURING C CHECK THE CARGO DOOR CUTOUT LOWER 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: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,655 hrs · 14,178 cycles

SHV - DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,655 hrs · 14,178 cycles

SHV - DURING C CHECK THE LT OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 18,273 hrs · 13,908 cycles

SDF - FLIGHT 2815, DURING CLIMBOUT OF SDF, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER VALVE IN THE LEFT WING, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 15,950 hrs · 12,158 cycles

CLE - FLIGHT 2690 THE CREW REPORTED, LOST ALL NR 2 HYDRAULIC SYSTEM FLUID IN FLIGHT. THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,448 hrs · 11,788 cycles

CREW REPORTED AISLE PATH EMERGENCY LIGHTS INOPERATIVE AT ROWS 9 AND 15. MX INSP AND REPLACED THE AISLE PATH LIGHT STRIPS. OPS CHECKS WERE GOOD.

Part: RELAY — FAULTY (COCKPIT) · airframe 15,165 hrs · 11,587 cycles

CLE - FLIGHT 2006 - THE CREW REPORTED A WING ANTI-ICE AND A PACK 1 VALVE FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 PACK VALVE AND RELAY KO187. OPERATIONAL CHECKS WERE GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,780 hrs · 10,537 cycles

SHV - DURING C-CHECK FR 15 DAMAGE AT STR 2R FROM COCKPIT DOOR HINGE PIN. MX REPAIRED FR 15 AT STR 2R IAW EMB 145 SRM 53-00-04 FIG 206. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,780 hrs · 10,537 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED UNDER LOWER LT RAMP ANGLE FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 13,780 hrs · 10,537 cycles

SHV - DURING C-CHECK MINOR CRACK AT FWD LOWER CORNER OF CARGO DOOR. MX REMOVED AND REPLACED FWD FRAME ON CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN FOR SERVICE.

Part: ATTACH BRACKET — DAMAGED (HORIZ STAB) · airframe 13,780 hrs · 10,537 cycles

SHV - DURING C-CHECK LT HORIZONTAL STABILIZER ACTUATOR ATTACHMENT POINT O/B LUG O/B HAT BUSHING HOLE IS ELONGATED. MX REMOVED AND REPLACED LT UPPER HORIZONTAL STAB ACTUATOR ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-04 (DRILLING), 51-20-01 (SEALING), SRM 51-40-02 AND AMM 20-10-01 (BOLT TORQUE). NEW ATTACH FITTING INSTALLED WITH NEW HAT BUSHING LUGS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 8,969 hrs · 6,956 cycles

DURING ROUTINE MAINTENANCE FOUND THE AFT OVERWING AND CABIN EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED NR 3 AND NR 4 BATTERY ASSEMBLIES. OPS CHECKED GOOD OF EMERGENCY LIGHTS IAW EMB145 33-50-04.

Part: ODOR — DETECTED (NR 1 A/C PACK) · airframe 8,967 hrs · 6,954 cycles

CLE FLIGHT 2266, THE CREW REPORTED THE NR 1 PACK HAD A OIL LIKE SMELL. MAINTENANCE INSPECTED AND PLACED THE NR 1 PACK SYSTEM ON MEL IAW 21-51-00/02. ON 2/2/06 MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE NR 1 PACK SYSTEM. NO DEFECTS WERE FOUND AND THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 8,809 hrs · 6,837 cycles

SHV - DURING C CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, FIG 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 7,606 hrs · 5,914 cycles

DURING ROUTINE MAINTENANCE THE FIRST OFFICER'S EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,234 hrs · 3,369 cycles

SHV - DURING C-CHECK, THE NUMBER FIVE EMERGENCY AISLE PATH LIGHT WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE AISLE PATH LIGHT ASSEMBLY IAW EMB 145 SRM 33-50-12. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — CRACKED (RT MLG WW) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE RIGHT HAND MAIN LANDING GEAR WHEEL WELL AFT RIB PANEL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PANEL IAW EMB 145 IPC 53-04-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV-DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AT FRAME 22, STRINGER 15 RIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 2 ENGINE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE AFT FLANGE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE MAIN DOOR U-BRACKET AT FRAME 17 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: INTAKE — GOUGED (NR 1 ENGINE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE NR 1 ENGINE AIR INTAKE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. 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) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (RT COWLING) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE RIGHT 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: ANGLE — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 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: STRINGER — GOUGED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND FRAME 53. 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: THRESHOLD — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD U-BRACKET AT FRAME 16 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: FIREWALL — CRACKED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT AND RIGHT UPPER APU MOUNTS. 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: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 cycles

SHV- DURING C-CHECK THE CENTER 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: ANGLE — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,369 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: FIRE LOOP — CHAFED (NR 2 ENGINE)

CLE FLIGHT NR 3242, CREW REPORTED ENGINE NR 2 FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND FOUND THE FIRE LOOP WAS CHAFED. THE NR 2 ENGINE FIRE LOOP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.