N14959

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01821. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE CARGO DOOR INTERNAL LOWER SKIN WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ESCAPE HATCH) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE LT AND RT CABIN ESCAPE HATCH DOOR BOTTOM FRAMES WERE FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5220-01052. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 75A AND STRINGER 12R. MX PERFORMED A DOUBLER REPAIR IAW EC5330-02578. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE INNER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-15 AND STRINGERS 19L-19R. MX R & R THE SKIN IAW EC5330-02782. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (ZONE 200) · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK THE LT FRAME 10 SEGMENT BETWEEN STRINGERS 8L-12L WAS FOUND TO HAVE ELONGATED FASTENER HOLES. MX R & R THE FRAME SEGMENT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK, STRINGER 18R WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-23. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,813 hrs · 27,133 cycles

DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,515 hrs · 26,891 cycles

CREW REPORTED SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MX FOUND A BROKEN WIRE SPLICE AND REPLACED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,715 hrs · 26,256 cycles

DURING MX INSPECTION, THE FLOOR PROXIMITY LIGHT STRIPS NR 4 AND NR 5, AND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR5 DC/AC INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,491 hrs · 26,076 cycles

THE LT SIDE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 33,571 hrs · 25,324 cycles

CREW REPORTED CABIN ALTITUDE CLIMBED TO 8400 AT FL370 EXCESSIVE CABIN ALTITUDE CLIMB AND DECENT RATES DURING CLIMBS AND DECENTS +1500FPM -1000FPM MANUAL MODE DID NOT WORK. MX R & R DIGITAL PRESSURE CONTROLLER WITH OPS CHECKS OF AUTO AND MANUAL SYS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 32,258 hrs · 24,242 cycles

DURING ROUTINE MX, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND THE RT OVERWING EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 32,178 hrs · 24,186 cycles

MX REPORTED BOTH AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MX REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — FAULTY (COCKPIT) · airframe 31,033 hrs · 23,286 cycles

ORD FLT 6137 THE CREW REPORTED AN AIR GROUND FAIL MESSAGE EVERY TIME THE GEAR WAS LOWERED FOR ABOUT 10 SECONDS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,890 hrs · 23,165 cycles

SHV - DURING C-CHECK STRINGER 2L WAS FOUND TO BE CRACKED AT FRAME 75. MAINTENANCE REMOVED THE CRACKED SEGMENT AND PERFORMED A STRINGER SPLICE REPAIR IAW EC5310-01563. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,890 hrs · 23,165 cycles

SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AT 2 LOCATIONS BETWEEN FRAMES 79-80 AND STRINGERS 5R-7R. MAINTENANCE REAMED OUT THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02471. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 30,890 hrs · 23,165 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 18-23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,890 hrs · 23,165 cycles

SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R, EMANATING FROM THE FRAME 75 FITTING. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-02353. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (RT WING) · airframe 30,828 hrs · 23,119 cycles

MKE - FLIGHT 2350, THE CREW REPORTED FLUID LEAKING FROM THE TOP OF THE RIGHT AILERON RIGHT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO MKE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING OUTBOARD FLAPPER VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 30,029 hrs · 22,532 cycles

FLIGHT 5817 - BUF - FLIGHT CREW REPORTED BURNING ODOR FOR ABOUT 1 MIN IN THE COCKPIT AND FA REPORTED SMOKE IN COCKPIT IN THE BACK HALF OF CABIN. EWR MX REMOVED AND REPLACED NR 2 RECIRCULATION FAN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 29,945 hrs · 22,458 cycles

ORD FLT 6051 - THE CREW REPORTED WHILE SITTING ON GROUND, PACK 2 WAS SET TO MANUAL MODE TO EXPEDITE COOLING THE CABIN AND COCKPIT FILLED WITH SMOKE. THE APU BLEED WAS OPEN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU AND PACK SYSTEMS. NO SMOKE WAS NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — ODOR · airframe 29,340 hrs · 21,795 cycles

FLIGHT 3155 THE CREW REPORTED A FUEL SMELL DURING APU START. MAINTENANCE PLACED THA APU ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/02/11 MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY TESTED THE APU AND PERFORMED ENGINE RUNS ALL WITH NO FUEL SMELL NOTED. THE MEL WAS REMOVED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE — FAULTY (TE FLAP) · airframe 28,343 hrs · 21,200 cycles

CLE FLT 2243 - THE CREW REPORTED A FLAP FAILURE AFTER TAKEOFF UPON FLAP RETRACTING. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECKS WERE GOOD.

Part: SOLENOID VALVE — MALFUNCTIONED (NLG) · airframe 27,983 hrs · 20,940 cycles

FLT 2267 CREW REPORTED LOUD NOISE FROM NOSE AREA LIKE NOSE GEAR DOORS WERE OPEN. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NLG DOOR SOLENOID VALVE. ALL OPERATIONAL CHECKS WERE GOOD.

Part: RADAR — FAILED (WEATHER RADAR) · airframe 27,783 hrs · 20,788 cycles

FLIGHT 2417 - EWR - FLIGHT CREW REPORTED WEATHER RADAR FAIL IN FLIGHT DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED RADAR UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — LEAKING (RT WING) · airframe 27,112 hrs · 20,302 cycles

TYS - AIR RETURN DUE TO FUEL VENTING FROM RT WING. REPLACED RT WING VENT VALVE, LEAK CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,089 hrs · 20,285 cycles

FLIGHT 2521 - EWR - FLIGHT CREW REPORTED BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED NR 4 EMERGENCY BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,207 hrs · 19,622 cycles

AUTO PRESSURIZATION FAILED IN FLIGHT. REMOVED AND REPLACED DIGITAL PRESSURE CONTROLLER IAW EMB 145 AMM 21-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — FAILED (CABIN) · airframe 25,550 hrs · 19,095 cycles

FLIGHT 2345, FLIGHT CREW REPORTED EMERGENCY LIGHTS STAY ON IN OFF POSITION. MX REMOVED AND REPLACED EMERGENCY LIGHT MODULE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL MODULE — OVERHEATED (CABIN) · airframe 25,156 hrs · 18,812 cycles

IAH - FLIGHT 2057 - DURING TAXI THE CREW REPORTED A BURNING SMELL IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAULTY (CABIN) · airframe 24,028 hrs · 17,998 cycles

FLT 2325 - EWR - FLT CREW REPORTED BURNING SMELL IN CABIN. EWR MX R&R LIGHT BALLAST AT 5A AND 16A SEAT AREAS. PERFORMED OPS CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED WIRE W734-0001-20. OPERATIONAL CHECKS WERE GOOD. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,957 hrs · 17,247 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,039 hrs · 16,640 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND AFT EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SOLENOID VALVE — FAULTY (NLG DOORS) · airframe 21,596 hrs · 16,326 cycles

CLE FLIGHT 3023 - THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE NOSE WHEEL COMPARTMENT. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT. THE NOSE LANDING GEAR SOLENOID VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: TERMINAL BLOCK — SHORTED (WINDOW HEAT) · airframe 21,505 hrs · 16,261 cycles

CLE FLIGHT 2477 - THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BLOCK MELTED ON THE CAPTAINS WINDSHIELD. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — DEFECTIVE (CABIN LIGHTS) · airframe 21,479 hrs · 16,241 cycles

FLT 2322 - EWR - DURING TAXIING OUT OF THE GATE, CREW REPORTED A BURNING ODOR IN CABIN AND GALLEY AREA. CREW RETURNED TO GATE AND EWR MX FOUND BALLAST IN GALLEY AREA DEFECTIVE. MX REMOVED AND REPLACED BALLAST IN GALLEY AREA AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 21,002 hrs · 15,900 cycles

TYS - DURING A CURRENT C-CHECK INSPECTION, THE VERTICAL STAB ATTACH FITTING AT FRAME 75 WAS FOUND FRETTING. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STAB FITTING AT FRAME 75 IAW EC5310-01317. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 20,137 hrs · 15,251 cycles

HRL - FLIGHT 3124, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS. THE CREW INSPECTED THE AIRCRAFT AND PLACED THE BAGGAGE SMOKE DETECTOR ON MEL 26-15-00 CAT-C CTL 119255, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT FROM HRL, WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGAGE SMOKE DETECTORS WITH NO DEFECTS NOT, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,102 hrs · 15,222 cycles

FLT 2335 - CREW REPORTED BURNING SMELL WHEN ANTI-ICE SYSTEM WAS ON IN ICING. MX RAN BOTH ENGINES, WITH ANTI ICE SYSTEM ON AND COULD NOT DUPLICATE THE SMELL. AC WAS APPROVED TO RETURN TO FLIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,452 hrs · 13,146 cycles

IAH - DURING MAINTENANCE INSPECTION, THE RIGHT EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PCU — MALFUNCTIONED (RUDDER) · airframe 17,235 hrs · 12,981 cycles

IAH - FLIGHT 2840, THE CREW REPORTED A RUDDER TRIM RUN-AWAY AT 50-100 FEET ABOVE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RUDDER PCU, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 17,194 hrs · 12,946 cycles

DURING ROUTINE MAINTENANCE 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT THE MAIN CABIN DOOR. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,532 hrs · 12,421 cycles

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,407 hrs · 12,323 cycles

IAH - DURING MAINTENANCE INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (LEADING EDGE) · airframe 16,204 hrs · 12,160 cycles

SHV - DURING C-CHECK, RT LEADING EDGE NR 3 HAS DENT BETWEEN 2ND AND 3RD VORTILLON. MAINTENANCE REPAIRED RT LEADING EDGE NR 3 BETWEEN 2ND AND 3RD VOTILLON IAW EMB 145 SRM 57-40-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 16,204 hrs · 12,160 cycles

SHV - DURING C-CHECK, RT APU FIRWALL REINFORCED REGION O/B 3 O'CLOCK POSITION IS CRACK. MAINTENANCE REPAIRED RT APU FIREWALL REINFORCED REGION O/B 3 O'CLOCK POSITION IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 16,204 hrs · 12,160 cycles

SHV - DURING C-CHECK, CARGO DOOR LOWER BEAM AT FS 65-68 HAS CORROSION. MAINTENANCE REMOVE AND REPLACED CARGO DOOR LOWER BEAM AT FS 65-68 IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 15,485 hrs · 11,573 cycles

BNA - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANTS SEAT IS NOT WORKING. REMOVED AND REPLACED NR 1 INVERTER IAW EMB AMM NR 33-50-11, OPS CHECKED GOOD.

Part: SUPPORT — WORN (BEARING) · airframe 15,437 hrs · 11,540 cycles

TYS A/C WAS IN FOR A 5A INSPECTION AND IT WAS OBSERVED THAT THE RIGHT SPHERICAL HOUSING SHOWED SIGNS OF WEAR. MAINTENANCE REAMED THE SPHERICAL HOUSING AND REPLACED THE BEARINGS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 5A CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,684 hrs · 10,970 cycles

IAH - CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE F/A JUMPSEAT WAS INOP. MAINTENANCE RESECURED THE LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED).

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 14,690 hrs · 10,975 cycles

CRP - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ON THE BULKHEAD NEAR THE MAIN PAX DOOR WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE WIRE ON THE LIGHT ASSY, OPS CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. PART HAS NO SERIAL NUMBER.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 14,626 hrs · 10,923 cycles

EWR LOG SQUAWK EMERGENCY EXIT LIGHT ABOVE ROW 1C WILL NOT ILLUMINATE. RESET EMERGENCY LIGHT ABOVE ROW 1C IAW EMB MM 33-50-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,456 hrs · 10,788 cycles

MCI - DURING ROUTINE INSPECTION THE REAR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY POWER SUPPLY IN ACCORDANCE WITH EMB-145 AMM 33-50-04 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 14,456 hrs · 10,788 cycles

MCI - DURING ROUTINE INSPECTION THE FORWARD LEFT HAND OUTBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY IN ACCORDANCE WITH EMB-145 AMM 33-50-10 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,378 hrs · 10,728 cycles

CLE FLIGHT NR 2266, THE CREW REPORTED THE AISLE PATH LIGHT STRIP AT ROW 7/8 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,148 hrs · 10,545 cycles

CREW REPORTED OVERWING EMERGENCY LIGHT AND GALLEY EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. OPS CHECKED GOOD.

Part: HEATER — SMOKE (WINDSHEILD)

DURING DESCENT THE CREW REPORTED THAT THE WINDSHIELDS FOGGED UP WITH A BURNING ODOR. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE DEFERRED THE WINDSHIELD HEATING SYSTEM. THE FIRST OFFICER'S WINDSHIELD WAS LATER REMOVED AND REPLACED AND THE DEFERRAL CLEARED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

CLE FLIGHT 2031, THE CREW REPORTED THE EMERGENCY EXIT SIGN NEXT TO MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN AND RESECURED THE INVERTER CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INTERMITTENT (EMERGENCY LIGHT)

CVG FLIGHT 2931 THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST AND NO DEFECTS WERE FOUND. WHEN AIRCRAFT GOT TO IAH THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — LEAKING (NLG) · airframe 12,237 hrs · 9,046 cycles

CREW REPORTED, THUMPING NOISE HEARD ON DESCENT AND APPROACH. ALMOST SEEMS THAT NOSE GEAR DOOR WAS CYCLING. MAINTENANCE TROUBLESHOT AND FOUND A LEAKING ACTUATOR AT NOSE LANDING GEAR DOOR NR 2. REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR IAW EMB145 AMM 32-33-03, OPS CHECKED GOOD. ALSO, FOUND CORROSION ON THE NOSE LANDING GEAR WOW PROXIMITY SWITCH. REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH (PART NUMBER: 80-057-01 SERIAL NUMBER: 1374) IAW EMB145 AMM 32-63-02, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,927 hrs · 8,807 cycles

SHV-DURING C-CHECK THE NR 2 EMERGENCY LIGHT BATTERY WAS FOUND TO HAVE NO OUTPUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 11,927 hrs · 8,807 cycles

SHV-DURING C-CHECK THE AFT AISLE EMERGENCY PROXIMITY LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED THE LIGHT STRIP WIRING IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV-DURING C-CHECK THE LT CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 22-23 AND FRAME 24-25. MAINTENANCE REMOVED DAMAGED AREAS AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 25 AND 16 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: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 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: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 23 AND 29 WAS FOUND TO BE CORRODED. 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 (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 203 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

DURING C-CHECK THE LT SILL AT FR 18 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

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

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

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: RIB — DENTED (NR 1 NACELLE) · airframe 11,927 hrs · 8,807 cycles

DURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT RIB WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 54-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LONGERON — GOUGED (NR 2 NACELLE) · airframe 11,927 hrs · 8,807 cycles

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

Part: RIB — GOUGED (NR 1 COWLING) · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE NR 1 LOWER ENGINE COWLING AFT RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (NR 2 COWLING) · airframe 11,927 hrs · 8,807 cycles

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

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK THE UPPER CROSS BEAM AT FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE UPPER CROSS BEAM AT FR 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (NR 2 COWLING) · airframe 11,927 hrs · 8,807 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,927 hrs · 8,807 cycles

DURING C-CHECK THE CENTER BUTTSTRAP AT FR 59-60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,927 hrs · 8,807 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: STRINGER — GOUGED (FUSELAGE) · airframe 11,927 hrs · 8,807 cycles

SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 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: LIGHT — INOPERATIVE (CABIN)

FLIGHT NR 2448 THE CREW REPORTED 2 ADJACENT EXIT ROW LIGHTS WERE INOPERATIVE IN MIDDLE OF CABIN. MAINTENANCE INSPECTED AND RESET EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — LOOSE (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. IAH- MAINTENANCE RESECURED THE NR 2 BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — LOOSE (CABIN)

CLE - DURING PREFLIGHT INSPECTION THE CREW NOTICED THAT THE FORWARD 3 STRIPS OF FLOOR PROXIMITY LIGHTING DID NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 BATTERY TO BE LOOSE IN THE BATTERY CHARGER. THE BATTERY WAS RE-SECURED AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD.

Part: UPLOCK — INOPERATIVE (NLG)

IAH - FLIGHT 2368, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT FULLY RETRACT WITH A LANDING GEAR DISAGREE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NOSE LANDING GEAR UP-LOCK BOX IAW EMB-145 M/M 32-33-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — UNDERSERVICED (NLG)

FLT 2825 - DURING CLIMB THE CREW NOTICED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED AND LANDED AT IAH WITHOUT FURTHER INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE AND THE DISCREPANCY REOCCURED ON FLIGHT 2810. MAINTENANCE INSPECTED AND FOUND THE NOSE LANDING GEAR STRUT TO REQUIRE SERVICING. THE NOSE LANDING GEAR STRUT WAS SERVICED, THE AIRCRAFT SUCESSFULLY TEST FLOWN, AND THE AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: PIN — BENT · airframe 10,555 hrs · 7,694 cycles

EWR---CO2409, CREW REPORTED, "NOSEWHEEL GEAR DOORS WILL NOT RETRACT, VIBRATE....MAINTENANCE FOUND PIN#31 AT CANNON PLUG P0778 TO BE BENT, REPAIRED PIN #31 IAW EMB145 AMM #20-00-00. PERFORMED GEAR SWING IAW EMB145 AMM #32-30-00, OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LOCK — LACK OF LUBE (PAX DOOR)

CLE FLIGHT 3260, THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO LOCK CLOSED. MAINTENANCE INSPECTED, CLEANED AND LUBRICATED THE MAIN CABIN DOOR ROLLER AND LOCKING MECHANISM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UPLOCK — INOPERATIVE (RT MLG)

IAH - FLT 4215 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW PERFORMED AN AIR-RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB-145 AMM 32-33-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (CABIN) · airframe 3,924 hrs · 2,947 cycles

IAH - DURING C-CHECK INSPECTION, LEFT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC531001126, AND ACFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: BEAM — CORRODED (FUSELAGE) · airframe 3,924 hrs · 2,947 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01127, AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: STRAP — CORRODED (FUSELAGE) · airframe 3,924 hrs · 2,947 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01125, AND ACFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

BTV - FLT 4218 - DURING SERVICE CHECK, FOUND RIGHT EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE ADJUSTED AND CLEANED RIGHT EMERGENCY LIGHT AND OPS CHECKED SYSTEM GOOD. (M)

Part: BULB — FAILED (FUSELAGE)

BTV - FLT 4218 - DURING 3A INSPECTION MAINTENANCE, FOUND BOTH OVERWING EMERGENCY EXTERIOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BOTH BULBS AND OPS CHECKED SYSTEM GOOD. (M)

Part: BULB — INOPERATIVE (PAX DOORWAY)

IAH - DURING 2A INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: APU — SMOKING (AFT FUSELAGE)

SMOKE IN CABIN WITH PACK NR 2 OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED THE APU FOUND APU SOURCE OF SMOKE. OPS CHECKED OF APU AND PACK NR 2 GOOD. (M)

Part: BULB — FAILED (EMERGENCY EXIT)

IAH - FLT 4173 - THE PILOT REPORTED THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: BULB — FAILED (LT EMER EXIT)

EFD - DURNG MAINTENANCE INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (RT EMER EXIT)

EFD - DURING MAINTENANCE INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMLBY IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (SPOILER SYSTEM)

IAH - FLT 4278 - THE CREW REPORTED THAT AT 14,000 FEET AFTER THE SPEED BRAKE LEVER WAS CLOSED, THE AIRCRAFT ROLLED TO THE RIGHT, AND SPOILER WARNING MESSAGE ON EICAS WAS DISPLAYED. THE CREW DISENGAGED THE AUTOPILOT, AND PULLED THE CIRCUIT BREAKERS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENNACE REMOVED AND REPLACED THE SPOILER CONTORL UNIT IAW EMB145 MM 27-63-02. THE AIRCRAFT WAS TEST FLOWN WITH NO DISCREPANCIES NOTED, AND WAS THEN APPROVED FOR RETURN TO SERVICE. (X)

Part: BULB — FAILED (LT OVERWING)

IAH - FLT 4206 - CREW INFORMED MAINTENANCE THE LEFT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AS REQUIRED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)