N16918

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 36,427 hrs · 28,071 cycles

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

Part: FRAME — CRACKED (FRM 10) · airframe 36,427 hrs · 28,071 cycles

DURING C-CHECK THE LT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9L-10L. MAINTENANCE R & R THE FRAME SEGMENT IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 36,427 hrs · 28,071 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE 9 AND 12 O'CLOCK POSITIONS. MAINTENANCE PERFORMED DOUBLER REPAIRS IAW SRM 53-32-13. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 2 ENGINE) · airframe 34,639 hrs · 26,627 cycles

AIRCRAFT WAS IN FOR A NR 2 ENGINE CHANGE WHEN THE FWD LOWER ENGINE YOLK WAS FOUND TO BE CRACKED AND THEN WAS VERIFIED BY NDT TO BE CRACKED. MAINTENANCE R & R THE FWD LOWER YOLK IAW EC 5450-01159. ALL WORK ACCOMPLISHED AND WAS RELEASED.

Part: SLEEVE — TORN (CABIN PRESSURE) · airframe 34,209 hrs · 26,283 cycles

CREW REPORTED LOSS OF PRESSURIZATION IN FLIGHT. LOST PRESSURIZATION AT 5000 FT ON DESCENT DECLARED EMERGENCY. MAINTENANCE R & R MULTIPLE SLEEVES AND CLAMPS ON BOTH PACKS WITH OPS CHECKS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,763 hrs · 24,360 cycles

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

Part: FLAPPER VALVE — LEAKING (RT WING) · airframe 31,492 hrs · 24,142 cycles

PILOT REPORTED AFTER TAKEOFF RT WING LEAKING FUEL TANK NR 2 SHOWING 800 LBS LOWER THAN TANK 1 FUEL IMBALANCE AND TANK NR 2 DASHED OUT. MX R & R THE RT WING FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,332 hrs · 24,016 cycles

DURING ROUTINE MAINTENANCE, THE AFT AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BROKEN CONNECTOR SPLICE ON THE LIGHT STRIP. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE · airframe 27,524 hrs · 21,006 cycles

THE CREW REPORTED AFTER APU START RECEIVED ARUAL WARNING UNIT 1 CHANNEL AND SMOKE BEGAN POURING OUT OF OPENING PLUS ABOVE FMS NR 2. THE ACFT WAS SHUTDOWN AND SMOKE STOPPED. MX INSPECTED AND PERFORMED OPS CHECKS OF BLEED SYS. OPS CHECKS WERE GOOD AND NO SMOKE WAS NOTED AT THIS TIME. THE ACFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,901 hrs · 20,492 cycles

DURING MX INSPECTION, THE CENTER ISLE EMERGENCY LIGHT FLOOR STRIP AT ROWS 5-8 WAS FOUND INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH OPS CHECKED SUCCESSFUL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 25,119 hrs · 19,190 cycles

FLIGHT 2335, CREW REPORTED AN UNCOMMANDED ENGINE NE SHUTDOWN AT 7700FT. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — SHORTED (NR 2) · airframe 25,072 hrs · 19,153 cycles

JAN - FLIGHT 2380, THE CREW REPORTED A LOUD THUD FOLLOWED BY AN ELECTRICAL TYPE BURNING SMELL. THE AIRCRAFT DIVERTED TO JAN, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 2 PACK ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RECIRC FAN, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — FAULTY (NLG) · airframe 24,793 hrs · 18,915 cycles

ORD FLT 5982 THE CREW REPORTED THE NOSE GEAR DOORS OPENED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 24,283 hrs · 18,528 cycles

IAH - FLIGHT 2047, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON CLIMBOUT FROM ATL. THE CREW RAN THE QRH AND THE GEAR RETRACTED. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 23,830 hrs · 18,192 cycles

AUS - FLIGHT 2283, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE PFD1 CIRCUIT BREAKER POPPED WITH AN ELECTRICAL SMELL. THE 31 PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 23,507 hrs · 17,949 cycles

MKE FLT 3004 - THE CREW REPORTED A BANGING NOISE COMING FROM THE FRONT OF AIRCRAFT ON APPROACH. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR DOWN LOCK PROXIMITY SWITCH AND CONNECTOR. ALSO REPLACED THE LEFT MAIN GEAR UPLOCK BOX UPPER PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: BLEED VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 23,083 hrs · 17,644 cycles

IAH - FLIGHT 2586 CLIMBING THROUGH 10000 WHILE PERFORMING 2ND PART OF ICE TEST, THE CREW RECEIVED A BLEED 2 VALVE FAIL MESSAGE WITH A BLD 2 VALVE FAIL MESSAGE. THE CREW PERFORMED THE QRH WITH NO HELP, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE BLEED VALVE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 23,083 hrs · 17,644 cycles

IAH - FLIGHT 2586 CLIMBING THROUGH 10000 WHILE PERFORMING 2ND PART OF ICE TEST, THE CREW RECEIVED A BLEED 2 VALVE FAIL MESSAGE WITH A BLD 2 VALVE FAIL MESSAGE. THE CREW PERFORMED THE QRH WITH NO HELP, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HIGH STAGE VALVE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,313 hrs · 17,020 cycles

FLIGHT 2077 - EWR - FLIGHT CREW REPORTED PRESSURIZATION FAIL. EWR MX RE-SECURED NR 1 DUAL CONTROL VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,065 hrs · 16,831 cycles

SHV - DURING C-CHECK THE SHEAR CLIP ATTACHED TO FRAME 65 AT STRINGER 15L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGTO BAY) · corrosion level 2 · airframe 22,065 hrs · 16,831 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION LEVEL 2 LOCAL, FRAME 65-68. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM FRAME 65-68 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: METERING UNIT — DEFECTIVE (NR 2 ENGINE) · airframe 21,498 hrs · 16,393 cycles

FLIGHT 2571 - EWR - FLIGHT CREW REPORTED NR 2 ENGINE ITT / VIBRATION ERRATIC. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FPMU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,398 hrs · 15,577 cycles

CLE FLT 2837 - DURING ROUTINE MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD.

Part: AHRS — MALFUNCTIONED (NR 1) · airframe 20,016 hrs · 15,263 cycles

IAH - FLIGHT 2705, THE CREW REPORTED A CAPTAINS HEADING FLAG ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 19,423 hrs · 14,804 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 18,775 hrs · 14,436 cycles

FLIGHT 3097 - EWR - FLIGHT CREW REPORTED BURNING SMELL COMING FROM FRONT OF CABIN. EWR MX REMOVED AND REPLACED PASSENGER CEILING LIGHT BALLAST NEAR SEAT 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: THERMOSTAT — FAULTY (BLEED SYSTEM) · airframe 18,567 hrs · 14,181 cycles

CLE FLIGHT NR 2293 THE CREW REPORTED A BLEED 1 OVERTEMP MSG ON CLIMB IN ICING CONDITIONS. THE ACFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 FAN AIR VALVE CONTROL THERMOSTAT. OPS CHECKS WERE GOOD.

Part: MODULE — ODOR (PSU)

CLE FLIGHT NR2173 CREW REPORTED A STRONG ELECTRICAL SMELL NEAR THE MAIN CABIN DOOR. MX INSPECTED AND REPLACED THE PASSENGER SERVICE UNIT CONTROL MODULE OPS CHECKS WERE GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,665 hrs · 13,516 cycles

EMERGENCY CEILING LIGHT AT ROW 14 INOPERATIVE. REMOVED AND REPLACED LAMP IAW EMB 145MM 33-50-08. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S)

Part: INVERTER — OVERHEATED (EMERGENCY LIGHTS)

NR 4 EMERGENCY BATTERY INVERTER IS REAL HOT WHEN EMERGENCY LIGHT IS NOT ON. REMOVED AND REPLACED NR 4 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. (S)

Part: INVERTER — OVERHEATED (EMERGENCY LIGHTS)

NR 4 EMERGENCY BATTERY INVERTER IS REAL HOT WHEN EMERGENCY LIGHT IS NOT ON. REMOVED AND REPLACED NR 4 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. (S)

Part: BRACKET — DAMAGED (LT AILERON) · airframe 17,153 hrs · 13,175 cycles

TYS - DURING C-CHECK, THE LEFT AILERON DAMPNER BRACKET WAS FOUND DAMAGED. THE BRACKET WAS REMOVED AND REPLACED IAW EMB 145 SRM 51-40-02. THE A/C IS CURRENTLY STILL IN C-CHECK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,782 hrs · 12,912 cycles

TYS - DURING A SERVICE ROUTINE THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 12 IAW AMM 33-50-15. OPS CHECK GOOD. A/C RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (APU) · airframe 16,838 hrs · 12,953 cycles

IAH - FLIGHT 3144, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL COMING FROM THE APU. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CTL#143170 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/09/08, IAH MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO SMELL OR DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,862 hrs · 12,927 cycles

FLIGHT 4930 - EWR - THE FLIGHT CREW REPORTED AISLE EMERGENCY LOCATOR EXIT LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,782 hrs · 12,912 cycles

EMERGENCY EXIT SIGN AT ROW 12 INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — FAULTY (COCKPIT) · airframe 16,497 hrs · 12,708 cycles

CLE FLIGHT 2080 - THE CREW REPORTD COCKPIT READING LIGHT CIRCUIT BREAKER H-11 POPPED IN FLIGHT. ALSO REPORTED A BURNING SMELL. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 25-12-02. SUPPLEMENT TO FOLLOW. MAINTENANCE REPLACED THE CAPTAIN`S READING LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 16,430 hrs · 12,655 cycles

FLIGHT 2301 - EWR - CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX LUBRICATED MAIN CABIN DOOR SEAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,191 hrs · 11,754 cycles

CLE FLIGHT 2221 - THE CREW REPORTED IN FLIGHT THE F/A AND PASSENGER SMELLED SOMETHING BURNING IN THE MAIN CABIN. NO BURNING SMELL WAS NOTED IN THE COCKPIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM IAW 21-51-00 AND PERFORMED OPERATIONAL CHECK OF THE ANTI-ICE SYSTEM. NO DEFECTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,539 hrs · 10,509 cycles

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT FIND ANY EVIDENCE OF SMOKE SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 12,569 hrs · 9,730 cycles

IAH - FLIGHT 2486, THE CREW REPORTED AN AIR GROUND FAIL ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHOCK ABSORBER — LOW (LT MLG) · airframe 12,357 hrs · 9,562 cycles

CREW REPORTED, LANGING GEAR AIR/GROUND FAILED AFTER TAKEOFF MAINTENANCE REMOVED AND REPLACED THE LGEU DID NOT FIX PROBLEM, INSPECTED AIR/GROUND PROXIMITY SWITCHES AND HARNESS FOR CONDITION AND SECURITY, NO DEFECTS NOTED, PERFORMED LANDING GEAR RETRACTION AND EXTENSION IAW EMB145 MM 32-30-00, NO DEFECTS NOTED; SERVICED LT MAIN LANDING GEAR SHOCK ABSORBER IAW EMB145 MM NR 12-13-05 IAW IAH ENGINEERING AND SERVICED NOSE LANDING GEAR SHOCK ABSORBER IAW MM NR 12-13-04. AFTER RETRACTION AND EXTENSION TEST ON JACKS, TEST FLEW AC SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE.

Part: SHOCK ABSORBER — LOW PRESSURE (MLG) · airframe 12,263 hrs · 9,487 cycles

STL - FLIGHT 2486, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAILURE ON TAKEOFF. THE AIRCRAFT RETURNED TO STL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE LEFT HAND MAIN LANDING GEAR SHOCK ABSORBER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 12,166 hrs · 9,417 cycles

SHV - DURING C-CHECKS FRAME 22 HAS AREA OF CORROSION SURROUNDING NUT PLATE. MAINTENANCE REMOVED CORROSION AND REPAIRED FRAME 22 IAW EC5310-03187. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 12,165 hrs · 9,416 cycles

SHV DURING C-CHECK APU FIREWALL CRACKED AT UPPER RT APU SUPPORT BRACKET. MAINTENANCE REPAIRED APU FIREWALL AT UPPER RT SUPPORT BRACKET IAW EMB 145 SRM 53-32-13 FIG 202 DET B. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 12,165 hrs · 9,416 cycles

SHV DURING C-CHECK CORROSION ON LOWER FRAME OF CARGO DOOR CUT OUT BETWEEN FRAME 65 & 68. MAINTENANCE REMOVED AND REPLACED LOWER FRAME CARGO DOOR CUT OUT AT FRAME 65-68 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,721 hrs · 8,287 cycles

IAH - FLIGHT 3470, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD AND GALLEY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — FAILED (WINDSHIELD) · airframe 7,772 hrs · 5,984 cycles

THE CREW REPORTED THAT THE NR 2 WINDSHIELD HEAT FAILED ACCOMPANIED WITH A BURNING SMELL. MAINTENANCE VERIFIED NORMAL OPERATION OF THE WINDSHIELD HEAT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,547 hrs · 5,817 cycles

SHV - DURING C-CHECK THE LEFT HAND 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: STIFFENER — CHAFED (NR 1 NACELLE) · airframe 7,547 hrs · 5,817 cycles

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

Part: STIFFENER — CHAFED (NR 1 NACELLE) · airframe 7,547 hrs · 5,817 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,547 hrs · 5,817 cycles

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

Part: LIGHT — FAULTY (FUSELAGE)

DURING 4A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT OVER RIGHTHAND WING TO BE INOPERATIVE. REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY LIGHT IAW EMB145 MM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAULTY

BTV---CO2491, DURING SERVICE/ROUTINE FOUND OVERHEAD EMERGENCY LIGHT AT MAIN ENTRANCE DOOR TO BE INOPERATIVE....MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB145 AMM 33-50-06. OPS.CHECKED GOOD.

Part: LIGHT — FAULTY

BTV---CO2491, DURING SERVICE/ROUTINE INSPECTION FOUND OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE.....MAINTENANCE REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT IAW EMB145 AMM #33-50-08. OPS. CHECKED GOOD.

Part: WIRE — LOOSE (CABIN)

IAH FLIGHT#2829 THE CREW REPORTED THE EMERGENCY EXIT LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND RECONNECTED WIRE FOR THE EMERGENCY EXIT LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — GOUGED (FUSELAGE) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

SHV- DURING C CHECK INSPECTION THREE GOUGES WERE FOUND ON SKIN FRAME 20 AT STRINGER 11L. MAINTENANCE REMOVED AND REPAIRED DAMAGE IN IAW EC 5320-01075. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

DURING C CHECK A GOUGE WAS FOUND ON STRINGER 19 RT BETWEEN FRAMES 52 AND 53. MAINTENANCE BLENDED GOUGE, PERFORMED DYE PENATRANT INSPECTION AND INSTALLED AT REINFORCEMENT AT STRINGER 19 RT BETWEEN FRAMES 52 AND 53 IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — DAMAGED (LT NACELLE) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

SHV DURING C CHECK INDENTATION WAS FOUND ON LT ENGINE LOWER NACELLE SKIN OUTBOARD STRINGER 8 INCHES FROM AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE

Part: STRUCTURE — DAMAGED (SPEEDBRAKE) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

DURING C CHECK LT SPEED BRAKE OUTER TRAILING EDGE IS WRAPED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE. OPERATIONAL CHECK GOOD IAW EMB 145 AMM 27-63-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (GALLEY) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

SHV - DURING C CHECK THE GALLEY FLOORBEAM ANGLE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AN REPLACED FLOORBEAM ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (GALLEY) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

DURING C CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED FORWARD SERVICE DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 3,452 hrs · 2,325 cycles

SHV-DURING C CHECK CENTER ISLE CARBON FIBER BEAM WAS FOUND TO HAVE CORROSION UNDER IT LEFT OUTBOUND SIDE. MAINTENANCE REPAIRED DAMAGED AREA IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: APU — BURNED (APU BAY)

MEM FLIGHT 4067 THE CREW REPORTED A APU FIRE INDICATION ON SHORT FINAL FOR 10 SECONDS. MAINTENANCE REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT BY THE GALLEY OTS. INOP. IAH- MAINTENANCE RMOVED AND REPLACED THE #3 INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE FIRST EMERGENCY LIGHTING FLOOR STRIP WAS NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY NR 2 AND PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

BTV---CO3218, DURING SERVICE/ROUTINE INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING AT ROWS THREE AND FOUR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHT AT ROWS THREE AND FOUR IAW EMB145 AMM 33-50-12. OPS CHECKED GOOD.

Part: SPLICE — LOOSE (CABIN)

IAH- DURING PERFLIGHT THE CREW NOTED THAT THE FRONT SECTION OF EMERGENCY LIGHTS NOT WORKING. IAH- MAINTENANCE RESECURED A LOOSE CONNECTOR AT THE FORWARD SECTION OF EMERGENCY LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERFENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCREFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (COCKPIT)

CLE FLIGHT 3738 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. COULD NOT DUPLICATE. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3675 THE CREW REPORTED THE FORWARD EMERGENCY AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY AISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: FIREWALL — CRACKED (FUSELAGE)

CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL WAS CRACKED. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST2706/01. MAINTENANCE REPLACED THE APU FIREWALL. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT#3944 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE AT THE EXIT ROW.MAINTENANCE APPLIED POWER TO AIRCRAFT AND CHARGED THE EMERGENCY LIGHT BATTERIES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COFFEEMAKER — FAULTY (GALLEY)

IAH - FLIGHT 4028, THE CREW REPORTED A SMOKE ODOR COMING FROM THE GALLEY AREA IN FLIGHT. THE POWER FOR THE GALLEY WAS SHUT OFF AND THE CIRCUIT BREAKERS FOR THE GALLEY WERE PULLED, WITH DISSIPATION OF THE ODOR FOLLOWING. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COFFEEMAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.