N12564

Part: FLOORBEAM — CORRODED (ZONE 100)

FLOOR BEAM AT LBL 18 BETWEEN FRAMES 35 AND 38 IS CORRODED. REMOVED AND REPLACED FLOOR BEAM AT LBL 18 BETWEEN FRAMES 35 AD 38 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: SKIN — CORRODED (ZONE 100)

FUSELAGE SKIN AROUND POTABLE WATER FILL/DRAIN NIPPLES IS CORRODED. REPAIRED SKIN AT PORTABLE WATER FILL/DRAIN NIPPLES IAW EMBRAER ETD 2023-145-013307 AND EMB 145 SRM 51-40-02, SWPM 38-10-50, AMM 38-10-04

Part: BEAM — CRACKED (ZONE 100)

CENTERLINE BEAM CRACKED AT FRAME 23 ON LEFT HAND FLANGE PART REPLACED

Part: BEAM — CORRODED (ZONE 100)

FLOOR BEAM AT LBL -479 BETWEEN FRAME38 AND 45 IS CORRODED. PART REPLACED

Part: BEAM — CORRODED (ZONE 100)

FLOOR BEAM AT LBL 18 IS CORRODED BETWEEN FRAME 45 AND 52. REMOVED AND REPLACED BEAM AT LBL18 BETWEEN FRAME 45 AND 52.

Part: FLOORBEAM — CORRODED (ZONE 100)

FLOOR BEAM AT LBL 18 IS CORRODED BETWEEN FRAMES 25 AND 29. REMOVED AND REPLACED FLOOR BEAM AT LBL 18 BETWEEN FRAMES 25 AND 29 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: UNKNOWN — CORRODED (ZONE 200)

RIGHT EMERGENCY EXIT SURROUND BOTTOM DOOR ALIGNMENT HOLE CORRODED. REMOVED AND REPLACED RIGHT EMERGENCY EXIT LOWER SILL BETWEEN FRAME 43 AND 45 IAW EMB 145 SRM 51-40-02, SRM 51-20-03, AND CPM PART 1 51-21-03

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 40,072 hrs · 31,167 cycles

THE CREW REPORTED DURING CLIMB AND ROTATION E1 POWER RAPIDLY FLUCTUATED BY 1-2% N1 AND ITT BY 20-30 DEGREES. INTERMITTANT MILD PULLING WAS FELT FROM THE ENGINE. NO EICAS MESSAGES. WHEN LEVELED OFF ENGINE STABILIZED AT LOWER THRUST SET. REPORTED SEEMED TO BE A HIGH THRUST THING. NO FURTHER PROBLEMS NOTED. MAINTENANCE INSPECTED AND REPLACED FADEC 1B AND ENGINE 1 FPMU. OPERATIONAL CHECKS WERE GOOD. FADEC P/N 23093345, S/N BX160321

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,389 hrs · 30,614 cycles

IAH - FLIGHT 4060, THE CREW REPORTED TWO EMERGENCY LIGHT FLOOR STRIPS WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACE THE NUMBER NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,639 hrs · 30,001 cycles

EMERGENCY LIGHT FLOOR STRIP AT ROWS 8&9 IS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP AT ROWS 8&9 IAW AMM 33-50-12, OPS CHECK GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,704 hrs · 29,244 cycles

STRINGER 2R CRACKED AT FRAME 75. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW ETD 2018-145-018888. AIRCRAFT STILL IN C CHECK.

Part: LIGHT — CRACKED (CABIN) · airframe 37,020 hrs · 29,243 cycles

A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND 10 OF THE EMERGENCY STRIPS CRACKED OR BROKEN. MAINTENANCE REMOVED AND REPLACED ALL THE LIGHT STRIPS IAW AMM33-50-12 AND OPS CHECK WAS GOOD. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: TRAY — DEFECTIVE (CABIN) · airframe 37,344 hrs · 28,959 cycles

EMERGENCY LIGHTS LT FORWARD OF WING AND 2ND LIGHT AFT OF PAX DOOR INOP. REMOVED AND REPLACED POWER SUPPLY TRAY. OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,384 hrs · 27,425 cycles

PILOT REPORTED A BURNING ODOR AROUND 2A. MX OPENED PSU'S AND OVERHEAD LIGHTING AREAS FROM 1A AND 3A AND INSPECTED FOR EVIDENCE OF ARCING OR BURNING. NO FAULTS NOTED. NO ODORS NOTE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 34,751 hrs · 26,933 cycles

DURING MAINTENANCE INSPECTION, THE RT OUTSIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,018 hrs · 22,443 cycles

THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTING TOWARDS THE BACK OF THE PLANE WERE INOPERATIVE. THE EMERGENCY LIGHT BATTERIES WERE RECHARGED, THE LIGHTS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — FAILED (NR 2 NACELLE) · airframe 28,965 hrs · 22,404 cycles

THE CREW REPORTED NR 2 ENGINE FIRE DETECTOR FAILED MESSAGE DURING CRUISE. MAINTENANCE REPLACED THE NR 2 ENGINE FIRE DETECTOR. OPS CHECKED GOOD.

Part: SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 28,008 hrs · 21,688 cycles

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

Part: MOUNT — CRACKED (RT ENGINE) · airframe 28,008 hrs · 21,688 cycles

DURING C-CHECK, THE RT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01073, REV B. ACFT APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (LT ENGINE) · airframe 28,008 hrs · 21,688 cycles

DURING C-CHECK, LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01073, REV. B. ACFT APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 28,008 hrs · 21,688 cycles

NR 2 ENGINE FWD LOWER YOKE MOUNT CRACKED. R & R MOUNT IAW EC5450-01073. ACFT APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 28,008 hrs · 21,688 cycles

NR 1 ENGINE FWD LOWER YOKE MOUNT CRACKED. R & R MOUNT IAW EC5450-01073. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CDU — INOPERATIVE (ZONE 100) · airframe 23,275 hrs · 17,922 cycles

FLIGHT MANAGEMENT SYSTEM NR 2 INOPERATIVE AND BURNING ODOR IN COCKPIT REPORTED BY CREW. R & R NR 2 FMS CDU IAW AMM 34-61-02 WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURNED TO SERVICE.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 23,118 hrs · 17,800 cycles

LT AILERON PCA ATTACH BRACKET WORN. R & R ATTACH BRACKET.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 23,118 hrs · 17,800 cycles

AREA AROUND SCREW HOLE ON GUSSET FWD OF RAMP PANEL CORRODED. BLENDED OUT CORROSION, FABRICATED REPAIR DOUBLER, ALODINED , PRIMED AND PAINTED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,116 hrs · 17,798 cycles

AFT 2 ROWS EMERGENCY LIGHTS INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 22,860 hrs · 17,601 cycles

DURING ROUTINE MX THE GALLEY EMEREGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR2 EMERGENCY LIGHT BATTERY. OPS CHECKED WERE GOOD.

Part: HOLDER — FAULTY (COCKPIT) · airframe 22,528 hrs · 17,322 cycles

CLE FLT 4168 THE CREW REPORTED A LIGHT SMOKE WITH AN ELECTRICAL SMELL COMING FROM THE FIRST OFFICER'S YOKE. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S MAP HOLDER. OPERATIONAL CHECKS WERE GOOD.

Part: BUTTON — FAULTY (COCKPIT) · airframe 22,296 hrs · 17,149 cycles

ORD FLT 5810 THE CREW REPORTED A NR 2 BLEED VALVE FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 BLEED VALVE PUSH BUTTON. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERTEMP (NR 2) · airframe 21,750 hrs · 16,668 cycles

ORD FLT 5871 THE CREW REPORTED A BATTERY 2 OVERTEMP WARNING MESSAGE ON THE EICAS WHILE AT THE GATE. MAINTENANCE REPLACED THE NR 2 MAIN BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: BLEED VALVE — FAULTY (APU) · airframe 21,069 hrs · 16,143 cycles

ORD FLT 5876 - THE CREW REPORTED A STRONG FUEL ODOR DURING APU START. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: B-NUT — LOOSE (APU) · airframe 21,059 hrs · 16,133 cycles

IAD FLT 5867 - THE CREW REPORTED A FUEL SMELL ON APU START. MAINTENANCE INSPECTED AND TIGHTENED B-NUT ON THE APU FUEL CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,055 hrs · 16,130 cycles

MCI - DURING MAINTENANCE INSPECTION THE EXIT LOCATOR ON THE AFT GALLEY WALL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 20,912 hrs · 16,005 cycles

FLIGHT 3088 - EWR - FLIGHT CREW REPORTED E1 FIRE DETECT FAIL INDICATION ON EICAS. EWR MX REMOVED AND REPLACED NR 1 ENG FIRE DETECTOR AND PYLON FIRE DETECTOR, AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA11RI040 REPORTS ENGINE FIRE DETECTOR AND SDR C2XA11RI041 REPORTS PYLON FIRE DETECTOR.

Part: FIRE DETECTOR — FAILED (NR 1 PYLON) · airframe 20,912 hrs · 16,005 cycles

FLIGHT 3088 - EWR - FLIGHT CREW REPORTED E1 FIRE DETECT FAIL INDICATION ON EICAS. EWR MX REMOVED AND REPLACED NR 1 ENG FIRE DETECTOR AND PYLON FIRE DETECTOR, AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA11RI040 REPORTS ENGINE FIRE DETECTOR AND SDR C2XA11RI041 REPORTS PYLON FIRE DETECTOR.

Part: BRAKE ASSY — WORN (NR 3) · airframe 20,887 hrs · 15,983 cycles

CLE FLT 3073 THE CREW REPORTED A BRAKE DEGRADE MESSAGE ON THE EICAS AFTER LANDING ALONG WITH THE NR 3 BRAKE FELT VERY SOFT AND INEFFECTIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 BRAKE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 18,132 hrs · 13,893 cycles

SHV - DURING C-CHECK FR 65 HAS CORROSION AT CARGO DOOR CUTOUT. REPAIRED FR 65 IAW EC5320-01494. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CARGO BAY) · airframe 18,132 hrs · 13,893 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT SILL HAS CORROSION BETWEEN FR 65 AND 68. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,132 hrs · 13,893 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED BETWEEN FR 19-21. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (MAIN DOOR) · airframe 18,132 hrs · 13,893 cycles

SHV - DURING C-CHECK MAIN DOOR LOWER SECTION NUT PLATE HOLES CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED MAIN DOOR LOWER SECTION NUT PLATE HOLES IAW EC5210-01154A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — SHORTED (CABIN LIGHTS)

DURING APPROACH, THE F/A REPORTED A FAINT ELECTRICAL SMOKE ODOR IN THE FRONT OF THE CABIN. THE AC LANDED WITHOUT INCIDENT WHERE MAINT INSPECTED THE ACFT AND REMOVED AND REPLACED THE FIRST AND SECOND LIGHT BALLASTS ABOVE SEAT 1A, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K)

Part: CONTROL MODULE — ODOR (CABIN LIGHTS)

FLIGHT CREW REPORTED BURNING SMELL IN FWD CABIN AND ELECTRICAL ODOR AS WELL. EWR MX FOUND POOR GROUND AT GS 8008DC. THEN AREA WAS CLEANED AND GROUND RESECURED. MX ALSO REMOVED AND REPLACED CABIN LIGHT CONTROL MODULE. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K)

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 14,803 hrs · 11,383 cycles

FLIGHT 2251 EWR FLIGHT CREW REPORTED SIDE ROW LIGHTS OUT AND BURNING SMELL FROM CONTROL MODULE. EWR MX R&R CONTROL MODULE IAW EMB 145 AMM 33-20 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHOCK ABSORBER — STICKING (RT MLG) · airframe 13,445 hrs · 10,497 cycles

IAH - FLIGHT 2192, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR SHOCK ABSORBER, OPERATIONALLY CHECKED THE EXTENSION / RETRACTION SYSTEM WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (RT SPEED BRAKE) · airframe 13,437 hrs · 10,491 cycles

IAH FLIGHT 3013 - THE CREW REPORTED THE LEFT SPEED BRAKE EXTENDED FASTER THAN THE RIGHT INFLIGHT CAUSING THE AIRCRAFT TO ROLL ABOUT 4 DEGRESS PER SECOND WITH AND WITHOUT AUTOPILOT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT OUTBOARD SPEED BRAKE ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 13,249 hrs · 10,359 cycles

CLE FLIGHT 2932 - THE CREW REPORTED LAV SMOKE DETECTOR OPERATION INTERMITTENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON THE LAV SMOKE DETECTOR AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 12,665 hrs · 9,939 cycles

TYS - MAIN DOOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED FEMALE SPLICE CONNECTOR SP7376 IAW EMB 145 WM 20-50-02. OPS CHECK GOOD.

Part: MODULE — INOPERATIVE (FIRE DETECTION) · airframe 11,369 hrs · 8,985 cycles

FLT 2346 - EWR - CREW REPORTED BAG FIRE EXT LIGHT WILL NOT ILLUMINATE DURING TEST. EWR MX REMOVED AND REPLACED BAG FIRE EXT MODULE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — DEFECTIVE (MLG) · airframe 10,525 hrs · 8,321 cycles

IAH - FLIGHT 2197, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL WITH A LOCKED SELECTOR LEVER AFTER TAKEOFF FROM MCI. THE MESSAGE CLEARED ITSELF, AND THE CREW WAS ABLE TO RETRACT THE LANDING GEAR AND CONTINUE TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU (LANDING GEAR ELECTRONICS UNIT), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,561 hrs · 6,760 cycles

SHV - DURING C CHECK, THE SHEAR CLIP AT FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — LIGHTNING STRIKE (RT ELEVATOR) · airframe 8,561 hrs · 6,760 cycles

SHV - DURING C CHECK, THE RIGHT ELEVATOR WAS FOUND TO HAVE LIGHTNING STRIKE DAMAGE WITH PITTING. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5530-01096. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,302 hrs · 5,751 cycles

CLE FLIGHT 2617 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 12. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 6. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — SMOKE (NR 1) · airframe 6,141 hrs · 4,856 cycles

CLE - FLIGHT 2115 THE CREW REPORTED SMOKE IN CABIN AND FLIGHT DECK FROM PACKS. THE AIRCRAFT RETURNED TO LGA AND MAINTENANCE PLACED PACK NR 1 ON MEL. THE AIRCRAFT HEATING AND AIR CONDITIONING SYSTEM WAS TESTED THE NEXT DAY AND FOUND TO BE OPERATING CORRECTLY, AND THE SOURCE OF THE SMOKE WAS THE NR 1 ENGINE. MAINTENANCE REPLACED THE NR 1 ENGINE AND THE OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE OR FUMES DETECTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,438 hrs · 3,552 cycles

CLE - FLIGHT 2846, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB-145 AMM 33-50-12, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (NR 2 COWLING) · airframe 4,060 hrs · 3,255 cycles

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

Part: STRUCTURE — GOUGED (NR 2 COWLING) · airframe 4,060 hrs · 3,255 cycles

SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,060 hrs · 3,255 cycles

SHV- DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,060 hrs · 3,255 cycles

SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. 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.