N11565

Part: DISPLAY — SHORTED (COCKPIT) · airframe 32,857 hrs · 25,276 cycles

THE CREW REPORTED MFD 1 IS OUT WITH BURNING ODOR IN FLIGHT DECK. THE ACFT LANDED IN ECP WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE AFFECTED MFD ON MEL 34-22-01-1 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R & R THE NR 1 MFD, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 32,857 hrs · 25,275 cycles

CREW REPORTED AN ELECTRICAL ODOR AFTER CAPTAINS MFD WENT BLANK. MAINTENANCE R & R CAPTAIN`S MFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 32,565 hrs · 25,041 cycles

THE CREW REPORTED A FUEL ODOR COMING FROM APU BLEED. AFTER ROTATION WHEN APU WAS PROVIDING AIR TO THE PACKS. MAINTENANCE INSPECTED AND REPLACED THE APU FUEL CONTROL ASSY. OPS CHECKED WERE GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,914 hrs · 23,774 cycles

CREW REPORTED A BURNING ODOR BEFORE LANDING. MAINTENANCE PERFORMED TROUBLESHOOTING AND NO UNUSUAL ODORS COULD BE DETECTED OR REPRODUCED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 30,445 hrs · 23,399 cycles

THE CREW REPORTED EMERGENCY LIGHT WAS INTERMITTENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 30,185 hrs · 23,205 cycles

ACFT WAS ON TAKEOFF WHEN A BIRD HIT THE NOSE. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED THE BAD RIVETS AND INSTALL 5 OF A OVERSIZE RIVETS. ALODINED, PRIMED AND PAINTED IAW SRM 51-40-02 AND CPM 51-=21-07. PERFORMED A HIGH FREQUENCY EDDY CURRENT INSPECTION OF AREA. SOP 5711, NO DEFECTS NOTED AND WAS RELEASED BACK TO SERVICE.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 29,683 hrs · 22,827 cycles

DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED BULB, CLEANED DEBRIS FROM SOCKET AND REINSTALLED BULB, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MELTED (TEMP) · airframe 29,458 hrs · 22,653 cycles

THE CREW REPORTED A STRONG SMOKE ODOR, CIGARETTE & PAPER ODOR EMITTING FROM MCD, F/A JUMPSEAT, AROUND EQUIPMENT CLOSET. THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR 1 WINDSHIELD TEMP CONTROLLER TO HAVE MELTED TERMONAL LUGS. MAINTENANCE R & R THE AFFECTED WINDSHIELD TEMP CONTROLLER, OPS TESTED WITH NO DEFECTS, ANDTHE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 28,903 hrs · 22,226 cycles

F/A REPORTED AN ODOR COMING FROM THE GALLEY COFFEEMAKERS. MAINTENANCE CLEANED THE WARMERS ON BOTH COFFEE BREWERS AND PERFORMED AN OPS CHECK, CHECKED GOOD, WITH NO BURNING ODORS DETECTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE ASSY — FAULTY (NR 4) · airframe 28,280 hrs · 21,753 cycles

A "BRAKE DEGRADE" MESSAGE APPEARED ON EICAS DURING LANDING AND REPORTED MORE THAN NORMAL BRAKE PEDAL PRESSURE NEEDED. ACFT PULLED TO THE LEFT. R & R NR 4 BRAKE ASSY, TEMP SENSOR, HYD FUSE AND BRAKE CONTROL VALVE, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WEB — CRACKED (LT WING TE FLAP) · airframe 28,266 hrs · 21,744 cycles

DURING C-CHECK, LT OTBD FLAP INBD ROOT RIB INTERNAL WEBBING CRACKED. MAINTENANCE REPAIRED IAW EC 5750-01562.

Part: FITTING — CORRODED (FRAME 75) · airframe 28,258 hrs · 21,736 cycles

DURING C-CHECK, INSPECTION FOUND VERTICAL STAB SPAR TO FRAME 75 FRETTING AT THE FUSELAGE. MAINTENANCE COMPLIED WITH THE EC 5310-01317 TO REMOVED FITTING, REMOVED CORROSION, CHECK LIMITS AND REINSTALL FITTING.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,180 hrs · 20,914 cycles

PILOT REPORTED A STRONG ODOR OF PLASTIC/ELECTRICAL SMOKE INFLIGHT DURING DESCENT WITH THE TOP OF GLARESHIELD/AVIONICS PANEL EXTREMELY HOT TO THE TOUCH. MX INSPECTED CABIN AND COCKPIT FOR PLASTIC/ELECTRICAL ODOR WITH NONE FOUND OR NOTED. ALSO RAN BOTH ENGINES AND BLEEDS PACKS WITH NO ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAILED · airframe 66,707 hrs · 20,543 cycles

MAIN PITCH TRIM INOPERATIVE MESSAGE ON CLIMBOUT, AUTO TRIM FAIL, ELEVATOR MISTRIM. R & R PITCH TRIM SWITCH AND ACTUATOR. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHT) · airframe 24,625 hrs · 18,897 cycles

THE CREW REPORTED SMOKE FROM 4C SIDEWALL LIGHT. MX REPLACED 4 B & C LIGHT ASSY AND 4 B&C LIGHT BALLAST. OPS CHECKS WERE GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 23,373 hrs · 17,884 cycles

EMERGENCY LIGHT FLOOR STRIP INOP. R & R LIGHT STRIP. OPS CHECK GOOD.

Part: CONTACTOR — INOPERATIVE (ZONE 100) · airframe 22,743 hrs · 17,380 cycles

IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BACKUP BATTERY PUSHBUTTON SWITCH, AND CONTACTOR K0305, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,092 hrs · 16,879 cycles

DURING ROUTINE MAINTENANCE THE RIGHT AFT EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 22,743 hrs · 17,380 cycles

IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BACKUP BATTERY PUSHBUTTON SWITCH, AND CONTACTOR K0305, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (SPOILER) · airframe 21,744 hrs · 16,602 cycles

CLE FLT 2521 CREW REPORTED THAT THE SPOILERS OPENED ON TAKEOFF ROLL AT APPROXIMATELY 100 KIAS. THE SPOILERS INDICATED OPEN ON THE EICAS SYSTEM. THE CREW THEN ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. CLE MAINTENANCE CHECKED ALL SPOILER PROXIMITY SWITCHES AND LANDING GEAR WHEEL HUBS FOR PROPER INSTALLATION AND OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. CLE MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY WAS CLEARED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,996 hrs · 16,016 cycles

SECOND FLOOR PROXIMITY EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 20,620 hrs · 15,741 cycles

IAD FLT 3153 THE CREW REPORTED A BLEED NR 1 OVERTEMP INDICATION IN FLIGHT DURING ICING CONDITIONS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FAN AIR CONTROL THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL PANEL — INOPERATIVE (GALLEY) · airframe 20,366 hrs · 15,552 cycles

FLIGHT 2030 - EWR - FLIGHT CREW REPORTED SMOKE DETECTOR SWITCH IN GALLEY NOT WORKING. EWR MX REMOVED AND REPLACED GALLEY SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 20,367 hrs · 15,553 cycles

FLIGHT 2030 - YYZ - FLIGHT CREW REPORTED LAV SMOKE DETECTOR IN GALLEY TEST INOPERATIVE. EWR MX REMOVED AND REPLACED SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK FUSELAGE SKIN HAS CORROSION AT FR 58 POTABLE WATER SUPPORT DOUBLER MATING SURFACE. REPAIRED SKIN IAW EC5330-02079. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK STR 21R HAS CORROSION AT FR 13. REPAIRED STR 21R IAW EC5310-01507. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 18,447 hrs · 14,100 cycles

LT OMEGA BEAM PREVIOUS REPAIR AT FR 20 HAS CORROSION (LEVEL 3). MAINTENANCE REMOVED AND REPLACED PREVIOUS REPAIR WITH NEW REPAIR IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 35-38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (SPOILER) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK LEFT O/B GROUND SPOILER ATTACHMENT HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 AMM 57-51-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION. REPAIRED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (WASTE DRAIN) · airframe 18,447 hrs · 14,100 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM CORROSION FRM 29-34. REPAIRED LEFT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (AILERON) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK LEFT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. REPAIRED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,447 hrs · 14,100 cycles

SHV - DURING C-CHECK RT LOWER EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 18,202 hrs · 13,930 cycles

A 12BC UPPER SIDEWALL EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXIT MARKING SIGN ASSY IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD.

Part: DISPLAY — BURNED (COCKPIT) · airframe 17,668 hrs · 13,523 cycles

CLL - FLIGHT 2593 - DURING FLIGHT THE CREW REPORTED THAT THE PFD1 CIRCUIT BREAKER POPPED WITH A CHECK PFD1 MESSAGE ON EICAS AND SMOKE COMING FROM UNDER THE PFD1. THE AIRCRAFT LANDED AT CLL WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — BURNED · airframe 15,152 hrs · 11,610 cycles

FLIGHT 2654 EWR FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR IN COCKPIT NOTICED AFTER LANDING. EWR MX R&R RELAY KO437 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,566 hrs · 10,543 cycles

IAH - FLIGHT 2656, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,481 hrs · 10,491 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 18-23. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 11,022 hrs · 8,703 cycles

602 NR 482585- RT FWD EXTERIOR EMERGENCY LIGHT AND NR 2 AISLE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY UNIT IAW EMB 145AMM 33-50-04 OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 10,846 hrs · 8,576 cycles

DURING MAINTENANCE INSPECTION THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT) · airframe 10,540 hrs · 8,343 cycles

BRO FLIGHT 3229 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE ARRIVING AT THE GATE. THE WINDSHIELD LEADS WERE RESECURED. LATER THAT DAY AT IAH, FLIGHT 3295, THE AIRCRAFT DISPLAYED A WINDSHIELD NR 2 HEAT FAIL MESSAGE. THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 8,721 hrs · 6,917 cycles

EWR - DURING ROUTINE MAINTENANCE FOUND THE AISLE EMERGENCY LIGHT AT ROW 1 - 3 NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY OVER SERVICE DOOR IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.

Part: BEAM — CORRODED (FUSELAGE) · airframe 8,651 hrs · 6,867 cycles

SHV - DURING C CHECK, THE LOWER BAGGAGE DOOR CUT OUT 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 8,657 hrs · 6,867 cycles

SHV - DURING C CHECK, THE CENTER OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, STEP 4, FIG 203, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,657 hrs · 6,867 cycles

SHV - DURING C CHECK, THE LEFT OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND COMPLETED THE REPAIR IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU) · airframe 8,657 hrs · 6,867 cycles

SHV - DURING C CHECK, THE APU FIREWALL WAS FOUND TO BE CHAFED. DAMAGE WAS FOUND TO BE GREATER THAN 50 PERCENT OF MATERIAL THICKNESS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER AND FILLER REPAIR IAW EC 5330-01359, SEC 1.3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (SERVICE DOOR) · airframe 7,037 hrs · 5,594 cycles

ORF - DURING PREFLIGHT INSPECTION, THE FLIGHT CREW REPORTED THE SERVICE DOOR EXIT SIGN NOT ILLUMINATING WHEN TESTED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM AND THE SERVICE DOOR EXIT SIGN OPERATED NORMALLY WITHOUT ANY DEFECTS NOTED. MAINTENANCE THEN CLEARED THE DISCREPANCY.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

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 (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 7 FIG 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

DURING C CHECK THE RT OMEGA BEAM AFT DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. 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 4,234 hrs · 3,423 cycles

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

Part: SKIN — DENTED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

SHV-DURING C CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 19A AND STRINGER 12L. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-22-01 STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 4,234 hrs · 3,423 cycles

DURING C-CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. 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: STIFFENER — CHAFED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 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: SILL — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

DURING C-CHECK, THE CARGO DOOR LOWER 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: BRACKET — CORRODED (PAX DOOR) · airframe 4,234 hrs · 3,423 cycles

SHV-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: STIFFENER — GOUGED (FUSELAGE) · airframe 4,234 hrs · 3,423 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: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

SHV-DURING C CHECK THE SHELL PLATE ON TOP OF THE CENTER OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 cycles

SHV-DURING C CHECK THE LT OMEGA BEAM 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: BRACKET — CORRODED (PAX DOOR) · airframe 4,234 hrs · 3,423 cycles

SHV-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: FIREWALL — CRACKED (APU BAY) · airframe 4,234 hrs · 3,423 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13 SECTION 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,423 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.

Part: INTAKE — GOUGED (NR 2 ENGINE) · airframe 4,234 hrs · 3,423 cycles

DURING C-CHECK THE NR 2 INTAKE WAS FOUND TO BE GOUGED AT 12 O'CLOCK. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 1 ENGINE) · airframe 4,234 hrs · 3,423 cycles

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 2317 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 2058 THE CREW REPORTED 2 EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

CLT FLIGHT NR 2223 THE CREW REPORTED NR 1 FLOOR PROXIMITY STRIP INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER,OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

THE CREW REPORTED THE FIRST ROW OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE RESECURED WIRE, OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 2104 THE CREW REPORTED THE FIRST SECTION OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: BRAKE — FAILED (T/E FLAP)

CREW REPORTED THAT ON DESCENT THE FLAPS WOULD NOT EXTEND. THE AIRCRAFT ACCOMPLISHED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FLAP TRANSMISSION BRAKE TO HAVE FAILED. THE AFFECTED FLAP BRAKE WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY CHECKED, AND THE AIRCRAFT RETURNED TO SERVICE.