N16571

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,725 hrs · 30,791 cycles

DURING MX INSPECTION, THE EMERGENCY EXIT MARKER FOR LT ESCAPE HATCH WAS NOT ILLUMINATING. MX REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT AC/DC INVERTER WITH OPERATIONAL CHECKED GOOD.

Part: SKIN — CRACKED (FRAME 75) · airframe 38,136 hrs · 29,486 cycles

CRACKS PROTRUDING FROM RIVET HEADS AT FRAME 75 STRINGER 2L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. AIRCRAFT STILL IN C CHECK.

Part: ENGINE — LEAKING (NR 1) · airframe 37,325 hrs · 28,826 cycles

THE CREW REPORTED A STRONG OIL SMELL ON CLIMB AND DESCENT WITH PACKS ON. MAINTENANCE REPLACED THE NR 1 ENGINE

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHTS) · airframe 35,225 hrs · 27,090 cycles

PILOT REPORTED THE FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 8 TO 18, EMERGENCY DOORS AND BACKSIDE OF THE CEILING PANEL ROW 18. MX FOUND NR 3 EMERGENCY LIGHT BATTERY UNSECURE, SECURED AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,224 hrs · 26,309 cycles

THE CREW REPORTED DURING CLIMB OUT, THE PRESSURIZATION WAS CLIMBING 3000 FT PER MINUTE. LEVELED AT 10000 FT CABIN WAS AT 8200FT. THE AIRCRAFT RETURNED TO DEPARTURE. MAINTENANCE INSPECTED AND REPLACED THE MANUAL PRESSURIZATION CONTROLLER, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,224 hrs · 26,308 cycles

DURING ROUTINE MAINTENANCE, THE NR 3 FLOOR EMERGENCY PROXIMITY AISLE LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE THE NR 3 LIGHT STRIP. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,245 hrs · 33,389 cycles

A/C WAS IN FOR A ROUTINE INSPECTION WHEN INSPECTION FOUND THE EMERGENCY STRIP AT ROLL 19 INOP. MAINTENANCE R&R THE LIGHT STRIP IAW AMM 33-50-12; OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: YOKE — CRACKED (NR 1 PYLON) · airframe 31,669 hrs · 24,281 cycles

DURING MAINTENANCE THE NR 1 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE NR 1 ENGINE YOKE FITTING IAW STS EA26-2014-063.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,353 hrs · 22,424 cycles

DURING MX INSPECTION THE FLOOR EMERGENCY LIGHTS AT ROWS 6, 7, 8 WERE INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — SEPARATED (NR 1 COMPRESSOR) · airframe 29,351 hrs · 22,422 cycles

ENGINE NR 1 FAILED AT 2200 MSL. R & R NR 1 ENGINE, OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE. NO N2 ROTATION. 6TH STAGE COMPRESSOR BLADE HAD LIBERATED.

Part: DUCT — LEAKING (CABIN AIR) · airframe 28,669 hrs · 21,907 cycles

THE CREW REPORTED AFTER LANDING THERE WAS A BURNING ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE DUCT ON THE NR 1 PACK HEAT EXCHANGER. OPS CHECKED GOOD.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 28,606 hrs · 21,854 cycles

DURING C-CHECK, THE CARGO DOOR INTERNAL SKIN WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIR IAW EC 5230-01339. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 28,606 hrs · 21,854 cycles

DURING C-CHECK, THE RT ENGINE FORWARD LOWER ENGINE MOUNT YOKE WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE YOKE IAW EC5450-01092. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-60) · airframe 28,606 hrs · 21,854 cycles

DURING C-CHECK, RT OMEGA BEAM HAS CORROSION AT FRAMES 59-60. REPAIRED RT OMEGA BEAM IAW SRM 53-24-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 27,864 hrs · 21,279 cycles

DURING MX INSPECTION, BOTH AFT EXTERIOR EMERGENCY EXIT LIGHTS WERE DISCOVERED INOPERATIVE. MX R & R THE FUSE IN THE NR 4 EMERGENCY LIGHT BATTERY CHARGER TRAY. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — LEAKING (LEFT WING) · airframe 26,749 hrs · 20,443 cycles

A FUEL LEAK REPORTED BY THE TOWER. UNABLE TO CONFIRM, MAINTENANCE INSPECTED AND REPLACED THE LT WING OTBD VENT VALVE IAW AMM 28-12-01. LEAK CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,457 hrs · 20,226 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR COMING OUT OF CAPTAINS SIDE WINDSHIELD. MX PERFORMED OPS CHECKS OF WINDSHIELD HEATING SYS. NO DEFECTS WERE FOUND. PERFORMED GVI OF WIRING BEHIND GLARESHIELD NO DEFECTS FOUND. THE ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 23,750 hrs · 18,072 cycles

FUSELAGE SKIN HAS CRACKS AROUND RIVETS FR 79, STR 5L. REPAIRED SKIN IAW EC 5330-02501. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 22,351 hrs · 16,948 cycles

ON TAXI OUT, CREW REPORTED HEAVY BURNING ODOR IN COCKPIT, NONE IN CABIN. ASSOCIATED PACK OVHT MESSAGE DISPLAYED ON EICAS. MX TROUBLESHOT AND FOUND NR 1 ACM SEIZED. MX R & R NR 1 ACM IAW 145 21-51-00 WITH OPS AND CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,912 hrs · 16,640 cycles

DURING ROUTINE MX THE EMERGENCY LIGHT WAS FOUND INOPERATIVE AT SEATS 15, 16, AND 17. MX REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD.

Part: DISPLAY — DEFECTIVE (ZONE 100) · airframe 20,338 hrs · 15,414 cycles

THE CREW REPORTED THAT THE CAPTAINS PFD1, MFD1, AND EICAS ALL HAD RED X'S. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE NR 1 IC600, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,291 hrs · 14,628 cycles

SHV - DURING C-CHECK FRAME 10 CRACKED DIRECTLY UNDER DV WINDOW FRAME LT. MAINTENANCE REMOVED AND REPLACED FRAME 10 SECTION UNDER DV WINDOW LT IAW EMB-145 SRM 51-40-02 AND 51-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,291 hrs · 14,628 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) AROUND NUT PLATE HOLES AT FRAMES 19 AND 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 BY INSTALLING FABRICATED DOUBLER AND RESTORED TO ORIGINAL FINISH RT OMEGA BEAM AT FRAME 18 IAW EC5320-01443 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — BENT (FUSELAGE) · airframe 19,291 hrs · 14,628 cycles

SHV - DURING C-CHECK FRAME 21 BENT BETWEEN STRINGER 21L & 21R. MAINTENANCE PERFORMED REPAIR OF FRAME 21 BETWEEN STRINGER 21L & 21R IAW ETD 2010-145/10420. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,291 hrs · 14,628 cycles

SHV - DURING C-CHECK FRAME 10 CRACKED DIRECTLY UNDER DV WINDOW FRAME RT. MAINTENANCE REMOVED AND REPLACED FRAME 10 SECTION UNDER DV WINDOW IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,291 hrs · 14,628 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM IS CORRODED (LEVEL 2 LOCAL) AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FRAME 17-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHOCK ABSORBER — DAMAGED (RT MLG) · airframe 19,291 hrs · 14,628 cycles

SHV - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDING GEAR AIR/GROUND FAIL ON EICAS. REMOVED AND REPLACED RT MAIN LANDING GEAR SHOCK ABSORBER IAW EMB 145 AMM 32-10-02. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — INOPERATIVE (APU) · airframe 19,087 hrs · 14,475 cycles

FLIGHT 2094 - DTW - FLIGHT CREW ABORTED T/O DUE TO LAV SMOKE INDICATION ON T/O ROLL. MX REMOVED AND REPLACED APU BLEED AIR CHECK VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FUSE — BLOWN (CABIN) · airframe 18,263 hrs · 13,845 cycles

MCI - DURING POST FLIGHT INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE IN THE NUMBER ONE EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,897 hrs · 13,572 cycles

LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 17,897 hrs · 13,572 cycles

AFT CEILING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED THE EXIT SIGN ASSY IAW EMB 145 33-50-80, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 17,020 hrs · 12,955 cycles

DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT WING EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY AND THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: CLAMP — DEFECTIVE (FUEL LINE) · airframe 16,466 hrs · 12,527 cycles

FLIGHT 2893 - YHZ-EWR - FLIGHT CREW REPORTED FUEL LEAKING FROM LEFT WING. FLIGHT CREW DIVERTED FLIGHT TO PWM AND LANDED ACFT UNEVENTFULLY. MX FOUND BAD CLAMP ON FUEL SENSOR LINE. MX REMOVED AND REPLACED CLAMP, REFUELED WING AND PERFORMED LEAK CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,320 hrs · 12,421 cycles

FLIGHT 2264 - DTW - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. CREW PERFORMED SYSTEM RESET SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 14,853 hrs · 11,342 cycles

IAH FLIGHT NR 2143 THE CREW REPORTED A RAPID DECOMPRESSION IN FLIGHT @ 36000FT. THE ACFT PERFORMED AN EMERGENCY DESCENT AND DIVERTED INTO MGM AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPS CHECKS WERE GOOD. THE OUTFLOW VALVES WERE ALSO REPLACED FOR PRECAUTIONARY REASONS.

Part: MASTER SWITCH — DIRTY (COCKPIT) · airframe 14,419 hrs · 11,009 cycles

FLIGHT 2706 - GSO - FLIGHT CREW REPORTED DURING CLIMBOUT LOST PFD NR 2, MFD NR 1, RRMU NR 2, TRANSPONDER, RA ON EICAS MESSAGE. PFD NR 2, FMS NR 2 ALSO WAS LOST. AVIONICS SWITCH LIGHT ON DESCENT. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. MX CLEANED AVIONICS MASTER SWITCH NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — WORN (LT SPOILER)

SHV - DURING C-CHECK, THE LT GROUND SPOILER CENTER HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BRACKET — WORN (RT AILERON)

SHV - DURING C-CHECK. THE RT AILERON TO PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: SILL — CORRODED (CARGO DOORWAY)

SHV - DURING C-CHECK THE CARGO DOOR LOWER SILL CUTOUT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL CUTOUT STRUCTURE IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BRACKET — FAULTY (CABIN) · airframe 13,064 hrs · 10,067 cycles

CLE FLIGHT 2866 - THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT WAS NOT CHARGING. MAINTENANCE REPLACED THE FORWARD CABIN FLASHLIGHT BRACKET. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 12,657 hrs · 9,793 cycles

IAH - FLIGHT 3102, THE CREW REPORTED A BURNING SMELL WITH PACK 2 ON THE GROUND. MAINTENANCE PLACED THE NUMBER 2 PACK ON MEL 21-51-00/2 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. EWR MAINTENANCE OPERATIONALLY CHECKED THE NUMBER TWO PACK WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 03/03/08.

Part: FLAPPER VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 12,470 hrs · 9,673 cycles

IAH - FLIGHT 2582 - THE CREW REPORTED THAT THE PRESSURIZTION FAILED IN AUTO AND MANUAL AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GROUND AIR CONDITIONING FLAPPER VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 12,264 hrs · 9,545 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,104 hrs · 9,428 cycles

TYS - DURING ACCOMPLISHMENT OF EA5310-01061 (LR WEIGHT INCREASE), THE SKIN WAS MISDRILLED BETWEEN FRAMES 45 AND 46, STRINGERS 4R & 5R. THE DAMAGED AREAS OF SKIN AND SKIN SPLICE STRAP WERE CUT OUT. A NEW SPLICE STRAP, FILLER, AND DOUBLER WERE FABRICATED AND THE PARTS WERE ALODINED AND PRIMED. THE FILLER AND DOUBLER WERE INSTALLED WET WITH SEALANT AND THE REPAIR AREA WAS PRIMED AND PAINTED IAW EC5330-01757, AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAULTY (NLG) · airframe 11,994 hrs · 9,347 cycles

FLT 2966, OKC - CLE. INBOUND TO CLE, AN AIR/GROUND FAIL MESSAGE ILLUMINATED DURING GEAR EXTENSION. THE RIGHT NOSE LANDING GEAR DOOR ACTUATOR WAS REMOVED AND REPLACED. CLE FLIGHT# 2966 THE CREW REPORTED ON FINAL APPROACH @1000 FT. GEAR WAS SELECTED DOWN AND EICAS MESSAGE "LG GEAR AIR/GROUND FAIL MESSAGE APPEARED.MESSAGE WENT AWAY ONCE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,739 hrs · 8,448 cycles

FLT 2550 - EWR - CREW REPORTED NR 2 EMERGENCY CEILING PANEL LIGHT AND RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BATTERY CHARGER ASSY NR 2 IAW EMB AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 10,709 hrs · 8,424 cycles

SHV - DURING CRUISE THE AIRCREW EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE ON FLIGHT 3062 FROM TYS TO IAH. AN EMERGENCY WAS DECLARED, DIVERTED TO JAN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE IAW EXPRESSJET TASK CARD 6271001. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR IS BEING FILED OPEN PENDING FINAL DETERMINATION OF ENGINE FAILURE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 12,466 hrs · 9,670 cycles

ELP - FLIGHT 2311, THE CREW REPORTED AIRCRAFT PRESURIZATION FAILED IN AUTO AND MANUAL AFTER T/O. THE AIRCRAFT RETURNED TO ELP WHERE IT LANDED WITHIOUT INCIDENT. THE CABIN PRESSURIZATION SYSTEM WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. FLIGHT 2311 THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHECKED THE PRESSURIZATION SYSTEM WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 9,078 hrs · 7,129 cycles

IAH - FLIGHT 2380, THE CREW REPORTED A BAGGAGE SMOKE INDICATION DURING CLIMB. BOTH BAGGAGE FIRE EXTINGUISHERS WERE DISCHARGED IN ACCORDANCE WITH THE QRH, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED THE BAGGAGE FAN RELAY, SMOKE TEST RELAY, THE FORWARD AND AFT SMOKE DETECTORS AS A PRECAUTION, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 10,701 hrs · 8,419 cycles

IAH - FLIGHT 2145, DURING CRUISE, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY) · airframe 7,953 hrs · 6,229 cycles

CLE FLIGHT 2622, THE CREW REPORTED A MOMENTARY BAG SMOKE INDICATION INFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE BAG SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 5,025 hrs · 3,949 cycles

DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT FLOOR STRIPS NR 6, 7, AND 8 WERE INOP. MAINTENANCE REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 4,101 hrs · 3,212 cycles

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

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LAMP. OPERATIONAL CHECKS WERE GOOD.