N15973

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 35,641 hrs · 26,608 cycles

C-CHECK, A SHEAR TIE AT FRAME 26 BETWEEN STR 15R AND 16R WAS FOUND CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-20--01 AND 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 35,641 hrs · 26,608 cycles

C-CHECK, A CRACK WAS FOUND IN A SHEAR TIE AT FRAME 73 BETWEEN STR8L AND 9L. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 35,641 hrs · 26,608 cycles

C-CHECK, A CRACK WAS FOUND IN THE RT OMEGA BEAM INBD SUPPORT BETWEEN FRAMES 47 AND 48. MAINTENANCE R & R THE OMEGA BEAM SUPPORT IAW SRM 53-23-02 AND SRM 51-40-02. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 35,641 hrs · 26,608 cycles

C-CHECK, A CRACKED SHEAR TIE WAS FOUND AT FRAME 24 BETWEEN S15-16R. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 35,641 hrs · 26,608 cycles

CRACK IN LT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAME 50) · corrosion level 2 · airframe 35,641 hrs · 26,608 cycles

RT OTBD FLOOR SUPPORT AT FRAME 50 CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: BEAM — CORRODED (THRESHOLD) · corrosion level 2 · airframe 35,641 hrs · 26,608 cycles

CARGO DOOR CUTOUT THRESHOLD BEAM CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R THRESHOLD BEAM.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 35,641 hrs · 26,608 cycles

CRACK IN RT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 30,721 hrs · 22,700 cycles

DURING C-CHECK, NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REPAIRED YOKE IAW EC5450-01047. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 29,211 hrs · 21,567 cycles

IAH - FLIGHT 2818, THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN AFTER LANDING. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN THE ENGINES, PACKS, AND APU ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FASTENER — LOOSE (WINDSHIELD) · airframe 19,688 hrs · 15,617 cycles

FLIGHT 6061 - IAD - FLIGHT CREW REPORTED LOUD NOISE COMING FROM F/O WINDSHIELD. IAD MX RETORQUED F/O WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONDITIONER — DEFECTIVE (BRAKE TEMP) · airframe 29,045 hrs · 21,439 cycles

FLIGHT 2041 - EWR - FLIGHT CREW REPORTED RT O/B BRAKE OVERTEMP MSG ON EICAS DURING T/O. UPON LANDING MESSAGE CLEARED AND BRAKE INDICATED NORMAL TEMP. EWR MX REMOVED AND REPLACED O/B TEMP SIGNAL CONDITIONER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 25,786 hrs · 19,001 cycles

CLE FLT 2513 THE CREW REPORTED A NR 1 HIGH STAGE BLEED VALVE FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HIGH STAGE VALVE AND THE NR 1 ENGINE INDICATING HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (LANDING GEAR) · airframe 25,725 hrs · 18,955 cycles

SHV - DURING C-CHECK LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPAIRED BROKEN WIRE IAW EMB 145 WM 20-21-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CORRODED (RT MLG) · airframe 25,725 hrs · 18,955 cycles

SHV - DURING C-CHECK RIGHT MLG AFT UPPER TRUNNION HAS PITTING CORROSION AND IS OUT OF LIMITS. REPAIRED RIGHT MLG AFT UPPER TRUNNION IAW EC57350-01406. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED LT OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,725 hrs · 18,955 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,725 hrs · 18,955 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,468 hrs · 17,272 cycles

IAH - FLIGHT 2875 THE FLIGHT ATTENDANT REPORTED A BURNING SMELL WHEN THE HEATER WAS ON. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: STRUT — UNDERSERVICED (NLG) · airframe 23,350 hrs · 17,179 cycles

CLE FLIGHT NR 2847 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG AND A THRUST REVERSE 1&2 DISAGREE MSG ON THE EICAS ON CLIMBOUT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND SERVICED THE NOSE GEAR STRUT. OPS CHECK WAS GOOD.

Part: WIRE — BROKEN (COCKPIT) · airframe 23,185 hrs · 17,048 cycles

IAH - FLIGHT 2434, THE CREW REPORTED A PACK 1 VALVE CLOSED ADVISORY MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE W101-2447-22 AT THE BUSHBUTTON FOR PACK ONE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MUFFLER — LOOSE (AC PACK) · airframe 23,185 hrs · 17,048 cycles

IAH - FLIGHT 2434, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED IN FLIGHT, AND WERE UNABLE TO RESET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE PACK 2 DISTRIBUTION MUFFLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,785 hrs · 15,375 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM WEB AND FLANGE AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19-23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,785 hrs · 15,375 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM AT FR 22 HAS A CRACK IN WEB THROUGH RIVET. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19 AND 23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LOCK — DEFECTIVE (COCKPIT) · airframe 20,030 hrs · 14,836 cycles

IAH - FLIGHT 2711, THE CREW REPORTED THAT THE CAPTAINS DV WINDOW POPPED OPEN DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE CAPTAINS DV WINDOW LOCK BAR AND ADJUSTED IAW EMB-145 MM56-11-00, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 19,779 hrs · 14,648 cycles

IAH - FLIGHT 2857, THE CREW REPORTED THAT THE BALLAST ABOVE SEAT 4A SMELLED BURNT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHTING IN MEL 33-210-00/1 CAT C CONTROL 128447, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 3145 WHERE MAINTENANCE REPLACED BALLAST, OPS CHECK GOOD. REMOVED FROM MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 19,739 hrs · 14,621 cycles

DURING ROUTINE MAINTENANCE THE EXIT SIGN AT THE RIGHT AFT DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — SHORTED (COCKPIT) · airframe 19,461 hrs · 14,428 cycles

FLIGHT NR 2666 THE CREW REPORTED A TAT 1 HEAT INOP MESSAGE ON THE EICAS WITH A FAINT ELECTRICAL BURNING ODOR THAT LASTED FOR 1 TO 2 MINUTES.MAINTENANCE INSPECTED AND REPLACED THE NR 1 TAT CURRENT SENSOR KO064. OPERATIONAL CHECKS OF THE SYSTEM WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 18,759 hrs · 13,894 cycles

FLIGHT 2882 - EWR - CREW REPORTED NR 2 CARGO SMOKE DETECTOR INOP. EWR MX REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW EMB AMM 26-23-00. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,645 hrs · 13,806 cycles

IAH - FLIGHT 2151, DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 18,486 hrs · 13,686 cycles

EWR FLIGHT 3068 THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES. THE NR 1 ENGINE WAS FOUND TO BE THE CAUSE OF THE LAV INDICATION AND SMOKEY ODOR. THE NR 1 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE ROOT CAUSE OF THE HAZE IN THE CABIN WAS THE NR 4 CARBON SEAL.THE SEGMENTS AND THE TEFLON SEAL NO LONGER RETAINED OIL FROM SEEPING OUT TO THE TIP OF THE FRONT SUMP HOUSING AND INTO THE HP COMPRESSOR"S AIR STREAM.

Part: UNKNOWN — SMOKE (CABIN) · airframe 18,364 hrs · 13,582 cycles

EWR LOG SQUAWK FLT NR 2292 ON CLIMB AT 8000 FT. WE GOT LAV SMOKE WARNING. THE FA CONFIRMED SMOKE IN THE CABIN. INSPECTED ALL OVERHEAD LIGHTS IN CABIN AND LAV. NO DEFECTS NOTED. PERFORMED RR FIM TASK 72-00-00-810-814. RAN BOTH ENGINES INDIVIDUALLY WITH BLEED AND PACKS ON FOR 20 MINUTES AT FULL POWER. COULD NOT DUPLICATE. OPPS CHECK GOOD CLOSED

Part: FRAME — CRACKED (FUSELAGE) · airframe 16,091 hrs · 11,811 cycles

PAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER OUTBOARD HOLE HAS A CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310- 01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOOD

Part: FRAME — CRACKED (FUSELAGE) · airframe 16,091 hrs · 11,811 cycles

PAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER INBOARD HOLE HAS CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310-01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 16,091 hrs · 11,811 cycles

PAX DOOR FRAME CUT-OUT, FWD LOWER STOP STRUCTURE, LOWER INBOARD HOLE HAS TWO CRACKS, ONE ON THE FRAME AND ONE IN THE BACK CASTING. REMOVED CRACKED BRACKET, DRILLED CRACKED HOLE ON SKIN SIDE TO 10MM. DRILLED NEW BRACKET AND INSTALLED. REAMED AND COLD WORKED HOLES FOR DOOR STOP. INSTALLED BUSHING AND FINAL REAMED ALL HOLES. INSTALLED DOOR STOP. ALL WORK DONE IAW EA 5310-01054 AND EC5310-01377.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 15,246 hrs · 11,147 cycles

BNA - CREW REPORTED, ON HEAD START, EXIT ROW OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB145 AMM NR 33-50-04, OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,974 hrs · 10,937 cycles

STL - DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LOCATOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOTOR — FAILED (FLAP DRIVE) · airframe 13,000 hrs · 9,411 cycles

CREW REPORTED FLAP FAILED IN FLIGHT. REPLACED THE NR 1 FLAP DRIVE MOTOR. AIRCRAFT RETURNED TO SERVICE.

Part: COWLING — CHAFED (NR 1 ENGINE) · airframe 11,759 hrs · 8,452 cycles

DURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT 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: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EC 5310-01270. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (NR 2 NACELLE) · airframe 11,759 hrs · 8,452 cycles

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

Part: SKIN — DENTED (NR 2 INTAKE) · airframe 11,579 hrs · 8,452 cycles

DURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

DURING C-CHECK THE LEFT 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: DOUBLER — CORRODED (FLOORBEAM) · airframe 11,759 hrs · 8,452 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: SILL — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

DURING C-CHECK THE SERVICE DOOR FORWARD 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: SILL — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

SHV - DURING C-CHECK THE LOWER ANGLE ON THE CROSSBEAM BETWEEN THE SERVICE DOOR AFT SILL AND THE CENTER FLOORBEAM AT FRAME 23 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: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

DURING C-CHECK THE RIGHT HAND 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: FIREWALL — CRACKED (APU) · airframe 11,759 hrs · 8,452 cycles

SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP END OF THE RIGHT HAND VERTICAL STIFFENER. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

SHV-DURING C-CHECK THE SERVICE DOOR AFT 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: SILL — CORRODED (FUSELAGE) · airframe 11,759 hrs · 8,452 cycles

SHV-DURING C-CHECK THE LEFT HAND SILL FROM FRAME 18 TO FRAME 22 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: BUTTSTRAP — CORRODED (FUSLEAGE) · airframe 11,759 hrs · 8,452 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 22. 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 (CABIN) · airframe 11,759 hrs · 8,452 cycles

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

Part: CONNECTOR — DISCONNECTED (CABIN)

CREW REPORTED, EMERGENCY LIGHT INOPERATIVE ON SIDE WALL OF CABIN. MAINTENANCE RESECURED CONNECTOR TO THE EMERGENCY LIGHT AND OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — LOOSE (EMERGENCY LIGHT) · airframe 10,750 hrs · 7,680 cycles

ON CREW PREFLIGHT, REPORTED THAT THE EMERGENCY SIDE WALL LIGHT WAS OUT. MAINTENANCE FOUND THE CANNON PLUG LOOSE TO AN INVERTER, RESECURED THE CANNON PLUG ON THE INVERTER ASSY LOCATED LEFT SIDE, JUST AFT OF ST14513.6, OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 10,114 hrs · 7,194 cycles

EWR LOG SQUAWK EMERGENCY EXIT SIGN ROW 12 LEFT SIDE BURNED OUT. RESECURED SPLICE FOR EMERGENCY EXIT SIGN AT ROW 12 LEFT HAND IAW EMB145 MM 33-50-00. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG)

FLIGHT 2819, THE CREW NOTED THAT THE AIRCRAFT HAD NO INDICATION FOR NOSE GEAR DOWN. THE APPROACH WAS ABORTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT NR 3389 THE CREW REPORTED THE LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: WIRE HARNESS — BURNED (CABIN)

CLE FLIGHT 2109 THE CREW REPORTED A BURNING ODOR WHILE TAXIING AND 2BC SIDEWALL LIGHT ASSEMBLY WAS INOPERATIVE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE SIDEWALL LIGHT HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT#2124 THE CREW REPORTED THE AFT AISLE PATH LIGHTING STRIPS #6,#7,#8 WOULD NOT STAY ILLUMINATED.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT#2351 THE CREW REPORTED THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE - FLIGHT 3284, THE CREW REPORTED THE EXIT SIGN AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN)

CLE- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY SIGN LIGHT AT SEAT 12A DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TARGET — OUT OF ADJUST (MAIN GEAR)

CLE FLIGHT#3311 THE CREW REPORTED A LANDING GEAR AIR/GROUND SYSTEM FAILURE AFTER TAKEOFF.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT MAIN LANDING GEAR WOW PROXIMITY SWITCH FRONT TARGETS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS TEST FLOWN GOOD.RELEASED BACK TO SERVICE.LEFT FRONT TARGET P/N 2309-2137-003

Part: BRACKET — DAMAGED (AILERON) · airframe 7,570 hrs · 5,161 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA BRACKET MOUNT HOLE WAS FOUND TO BE ELONGATED DUE TO WEAR. MAINTENANCE REMOVED AND REPLACED THE THE BRACKET IAW CONTINENTAL EXPRESS EC 5750-01177 AND EMB 145 SRM 57-60-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,570 hrs · 5,161 cycles

TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR, FORWARD SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE AFFECTED AREA, PERFORMED DYE-PEN. INSPECTION, ALODINED AND PRIMED IAW-GST-1886/02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — NICKED · airframe 7,570 hrs · 5,161 cycles

TYS, During a scheduled inspection the rudder 2 leading edge on the left side was found nicked. Maintenance blended the affected area, performed dye-pen. inspection, alodined and primed. I/A/W-GST-1886/02 and CPM-51-21-04/05/06. The repair was satisfactory and the aircraft will be released upon complection of inspection.

Part: SKIN — DENTED (PAX DOOR) · airframe 7,570 hrs · 5,161 cycles

TYS DURING A 1C/2C INSPECTION THE MAIN DOOR FWD OF THE HANDLE HAD A DENT IN IT, MAINTENANCE TO REMOVED THE PAINT, RECONTOUR THE DENTED AREA, PERFORM A DYE PENENTRANT INSPECTION AND NO CRACK WAS FOUND. CONTOURED DENT, ALODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED IAW GST 1609/02--EMB 135/145 CPM 51-21-04-05-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: STRINGER — CHAFED (STA.17727.0) · airframe 7,570 hrs · 5,161 cycles

TYS DURING A 1C/2C INSPECTION,STRINGER 19R AT STA.17727.0 WAS FOUND CHAFED. MAINTENANCE MEASURED AREA(L=.4670" XW=.1495" X D=.016") FOUND TO BE WITHIN LIMITS,BLENDED DYE PENTRANT INSPECTION,ALODINE,PRIMED AND RESORED TOPCOAT IAW EMB.135/145 SRM 53-24-02 AND CPM 51-21-04-05-06.ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: SKIN — DENTED (PAX DOOR) · airframe 7,570 hrs · 5,161 cycles

TYS DURING A SCHEDULED 1C/2C INSPECTION,THE PAX DOOR HAD TWO DENTS IN THE MIDDLE OF THE DOOR. A GST WAS USED TO MAKE THE REPAIR (GST 1906/02) WHICH STATED REMOVE PAINT, RECONTOUR THE DENTED AREA, PERFORM A DYE-PENETRANT INSPECTION, NO CRACK WAS FOUND. AREA WAS ALODINED, PRIMED AND PAINTED IAW WITH THE GST AND EMB 135/145 CPM 51-21-04-05-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL 1C/2C INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,570 hrs · 5,161 cycles

TYS, DURING A SCHEDULE INSPECTION, THE PAX DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS, ALODINED AND PAINTED IAW-EMB-SRM-53-21-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,570 hrs · 5,161 cycles

TYS, DURING A SCHEDULE INSPECTION, THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS, ALODINED AND PAINTED IAW-EMB-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 7,570 hrs · 5,161 cycles

TYS During a scheduled inspection the left hand sidewall floor support at station 5292.0 was found to be corroded in several areas. Maintenance removed and replaced the flooor support IAW EMB-145 SRM 51-40-02, the repair was satisfactory. The aircraft will be released upon completion of inspection.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,570 hrs · 5,161 cycles

TYS, DURING A SCHEDULE INSPECTION, THE AFT SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS, ALODINED AND PAINTED IAW-EMB-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: MODULE — INOPERATIVE (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ARM. IAH- MAINTENANCE REMOVED AND REPLACED THE CABIN CONTROL MODULE FOR LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (COCKPIT)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT NOT ARMED INTERMITTENT ON EICAS. MAINTENANCE CLEANED THE CANNON PLUG ON THE CABIN LIGHT CONTROL UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,907 hrs · 4,031 cycles

TYS DURING A SCHEDULED INSPECTION THE MOST FORWARD SECTION OF THE CABIN EMERGENCY ISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE THE FORWARD EMERGENCY ISLE PATH LIGHT STRIP IAW EMB-145 MM 33-50-08, OPERATIONAL CHECKS WERE SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,907 hrs · 4,031 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IN THE LEFT HAND OVERWING EMERGENCY LIGHT ASSY IAW EMB-145 MM 33-50-10, OPERATIONAL CHECKS WERE SATISFACTORY.

Part: ENGINE — FAULTY · airframe 5,513 hrs · 3,752 cycles

EWR/BTV---CO3626, CREW REPORTED "AIRCRAFT FILLED WITH FUMES DURING FLIGHT. A CONSTANT LIGHT SMELL OF FUEL/OIL SOMETIMES IT GOT STRONG"...MAINTENANCE TROUBLESHOT TO INTERNAL ENGINE OIL LEAK AIRCRAFT MAINTENANCE FERRIED TO BTV FOR ENGINE CHANGE. REMOVED AND REPLACED ENGINE IN BTV. GROUND RUN OPS.CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE

Part: LIGHT — BURNED OUT (CABIN)

TYS - DURING A SCHEDULED INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB-145 MM 33-50-10. OPS CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: UNKNOWN — ODOR (CABIN)

CLE FLIGHT 3896- THE CREW REPORTED A BURNING SMELL IN CABIN AFTER TAKEOFF WHEN THEY SWITCHED FROM APU BLEED TO ENGINE BLEED. MAINTENANCE PERFORMED ENGINE RUNS I/A/W EMBRAER 145 MAINTENANCE MANUAL 71-00-01 AND FOUND NO DEFECTS. THE A/C WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)