N16999

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 36,218 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: CONTROL VALVE — FAULTY (BRAKES) · airframe 35,784 hrs · 32,182 cycles

BRAKE INBD INOPERATIVE MESSAGE ON EICAS CAME ON DURING LANDING GEAR EXTENSION. BRAKES WERE MUSHY ON LANDING ROLL & TAXI. MX R & R NR 2 BRAKE CONTROL VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,427 hrs · 24,288 cycles

C-CHECK, STRINGER 17R HAS CORROSION, LOCAL LEVEL 2, BETWEEN FRAMES 21-22. MX PERFORMED, COMPLETED AND COMPLIED WITH ALL WORK IAW EC5330-02798. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 31,427 hrs · 24,288 cycles

DURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT CRACKED. MX R & R ENG NR 1 FWD LOWER YOKE FITTING IAW EC5450-01073. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,427 hrs · 24,288 cycles

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

Part: FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,427 hrs · 24,288 cycles

DURING C-CHECK THE PASSENGER DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,427 hrs · 24,288 cycles

DURING C-CHECK, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 79, STRINGERS 3L-4L. MX REAMED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02796. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (SERVICE DOOR) · airframe 31,427 hrs · 24,288 cycles

DURING C-CHECK THE SERVICE DOOR MAIN HINGE LOWER BRACKET UPPER FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MX REPAIRED THE HINGE ASSY IAW EC5240-01036, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,427 hrs · 24,288 cycles

DURING C-CHECK THE FRAME 75 VERTICAL STAB FITTING WAS FOUND TO HAVE FRETTING CORROSION BETWEEN STRINGERS 2R-2L. MX REMOVED THE CORROSION AND REPAIRED THE FITTING IAW EC5310-01317, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — SHORTED (MLG) · airframe 31,076 hrs · 24,004 cycles

DURING CLIMB OUT, RECEIVED A "LANDING GEAR AIR/GROUND FAIL" MESSAGE. AIR RETURN AND LANDED WITHOUT INCIDENT. EMERGENCY LANDING WAS NOT DECLARED. ISOLATED DISCREPANCY TO A SHORTED RT MLG SHOCK ABSORBER PROXIMITY SWITCH HARNESS. MX R & R THE HARNESS IAW SWPM 20-21-00. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 30,388 hrs · 23,477 cycles

DURING ACCOMPLISHMENT OF EA 5310-01071 FOUND A ONE INCH CRACK ON THE RT SIDE OF THE APU FIREWALL REINFORCEMENT AREA JUST OTBD OF UPPER HORIZONTAL PROFILE OTBD OF LAST RIVET. PERFORMED REPAIR IAW SRM 53-32-13 AND ETD2012-145-6767 AND ETD2013-145-003508.

Part: CONTROL PANEL — FAULTY (FUEL SYSTEM) · airframe 29,666 hrs · 22,878 cycles

CREW REPORTED SMOKE, BURNING ODOR IN COCKPIT BEHIND LT SEAT ALONG WITH FUEL CROSS FEED CIRCUIT BREAKER TRIPPED. MX INSPECTED AND FOUND FUEL CONTROL MODULE PANEL TO BE THE CAUSE. MX R & R FUEL CONTROL MODULE WITH OPS CHECK SUCCESSFUL AND NO BURNING SMELL NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (ZONE 100) · airframe 27,115 hrs · 20,846 cycles

A PASSENGER REPORTED A LOUD POP IN ROW 12C WITH A BURNING SMELL SOON AFTER. FLT DIVERTED TO RIC AND LANDED WITHOUT INCIDENT. RIC MX INSPECTED ACFT AND SUSPECTED NR 2 ACM TO BE THE SOURCE OF BURNING SMELL AND SMOKE. RIC MX PLACED NR2 PACK ON MEL (DEFERED) AND ACFT CONTINUED TO EWR WITHOUT ANY OTHER ISSUE. EWR MX R & R NR 2 ACM IAW AMM 21-51-03 WITH OPS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — FAULTY (SMOKE DETECTION) · airframe 26,889 hrs · 20,672 cycles

FLT 4219 EWR-CREW REPORTED LAV SMOKE ALARM WARNING WITH NO SMOKE EVIDENT IN LAV. EWR MX REMOVED AND REPLACED SMOKE DETECTOR SENSOR IAW EMB145 AMM 26-14-01 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — SHORTED (RT MLG) · airframe 26,885 hrs · 20,669 cycles

FLT 4415 EWR. CREW REPORTED AFTER TAKEOFF EICAS MESSAGE LG AIR/GND FAIL AND LANDING GEAR WOULD NOT RETRACT. CREW PERFORMED AIR RETURN WITHOUT INCIDENT. EWR MX FOUND CONNECTOR P2835 WITH PINS A, B, AND C SHORTED. EWR MX REMOVED AND REPLACED RIGHT MAIN LANDING GEAR WOW HARNESS IAW EMB145 AMM32-00-03. MX PERFORMED GEAR SWING SEVERAL TIMES WITH NO FAILURES AND OPERATIONAL CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (LANDING GEAR) · airframe 26,791 hrs · 20,593 cycles

THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE THE PROBLEM. RELAYS KO453, KO353, AND KO025 WERE REPLACED. THE NOSE GEAR WAS RESERVICED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS.

Part: PROXIMITY SWITCH — DEFECTIVE (LANDING GEAR) · airframe 26,656 hrs · 20,491 cycles

FLIGHT 6133 - ABE TO ORD - FLIGHT CREW REPORTED LG AIR/GRND FAIL MESSAGE ON EICAS AFTER TAKEOFF AND LANDING GEAR LEVER COULD NOT BE MOVED TO UP POSITION. CREW DIVERTED FLIGHT TO EWR AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT GEAR AND NOSE LANDING GEAR PROX SWITCHES AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,561 hrs · 20,408 cycles

SHV - DURING C-CHECK IT WAS DISCOVERED THAT LT FRAME 10 WAS CRACKED DIRECTLY BELOW THE PILOT'S EMERGENCY ESCAPE HATCH. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (LANDING GEAR) · airframe 26,561 hrs · 20,409 cycles

A/C N16999 FLIGHT 3071 FROM EWR AIR RETURN. L/G/AIR AIR GROUND FAIL AFTER TAKEOFF, GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER RELAY K0024 AND SERVICED NOSE STRUT IAW EMB-145 AMM 32-32-02, 20-13-02 AND 32-20-01. OPERATIONAL CHECK WAS GOOD IAW 32-30-00, COULD NOT DUPLICATE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 26,560 hrs · 20,408 cycles

IAH - FLIGHT 2980, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON TAKEOFF, THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT AND ON LANDING THE CREW REPORTED NO THRUST REVERSER OR SPOILERS, AND AN IC1-2 WOW INOP DURING TAXI TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 26,489 hrs · 20,349 cycles

FLIGHT 2643 - EWR - FLIGHT CREW REPORTED A STRONG SMELL OF FUEL WHILE RUNNING APU. RIC MX REMOVED AND REPLACED FUEL CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHUTOFF VALVE — DEFECTIVE (APU) · airframe 26,407 hrs · 20,285 cycles

FLIGHT 2222 - EWR - FLIGHT CREW REPORTED FUEL SMELL IN COCKPIT WITH APU BLEED OPEN. EWR MX REMOVED AND REPLACED APU FUEL SHUTOFF VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 26,366 hrs · 20,256 cycles

IAH - FLIGHT 2036, THE CREW REPORTED A LANDING GEAR AIR GRND FAIL MESSAGE AND THAT THE LANDING GEAR LEVER COULD NOT BE MOVED UP AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — DEFECTIVE (LANDING GEAR) · airframe 26,364 hrs · 20,253 cycles

IAH - FLIGHT 2346, UPON ROTATION LG AIR/GND FAIL ON EICAS (GEAR STUCK DOWN). UPON RETURN TO IAH DURING APPROACH EICAS SPS FAIL MASTER WARNING SPS ADVANCE MASTER WARNING, IC 1-2 WOW INOP (CAUTION), AHARS 2 BASIC MODE, AND UPON LANDING UNABLE TO PUT IN THRUST REVERSE CAUSING A BRAKE OVERHEAT. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE SOCKETS IN CONNECTOR P2834, OPERATIONALLY TESTED LANDING GEAR EXTEND / RETRACT & WOW SYSTEMS WITH NO DEFECTS NOTED, INSPECTED THE WHEELS AND BRAKES FOR OVERHEAT CONDITION WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (NLG) · airframe 26,212 hrs · 20,143 cycles

IAH - FLIGHT 2715, THE CREW REPORTED, LANDING GEAR WOULD NOT RETRACT, RECEIVED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BACKSHELL FROM THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR CANNON PLUG, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 26,112 hrs · 20,073 cycles

CLE FLT 2415 THE CREW REPORTED THE AIRCRAFT OVERPRESSURIZED IN CLIMB. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 25,363 hrs · 19,497 cycles

ORD FLT 5891 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 25,273 hrs · 19,421 cycles

ORD FLT 5980 THE CREW REPORTED A LAV SMOKE WARNING ON THE EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED LAV SMOKE OPERATIONAL CHECKS. COULD NOT DUPLICATE PROBLEM AND NO SMOKE WAS NOTED.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 22,803 hrs · 17,503 cycles

CLE FLT 5733 THE CREW REPORTED A BAG SMOKE DETECTOR INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE BAG SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: FAN — MALFUNCTIONED (CARGO BAY) · airframe 22,541 hrs · 16,915 cycles

IAH, ON DESCENT THE CREW REPORTED A BAG FIRE INDICATION WITHOUT SOUNDING THE ALARM OR DISPLAYING EICAS MESSAGE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE BAGGAGE COMPARTMENT RECIRC FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TARGET — OUT OF ADJUST (NLG) · airframe 22,046 hrs · 16,555 cycles

BNA - AIR/GROUND FAIL ON CLIMB LANDING GEAR WOULD RETRACT. AIR RETURNED, MX ADJUSTED THE NOSE PROX SWITCH TARGET AND OPS CHECKED GOOD. A/C WAS RELEASED.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,720 hrs · 16,300 cycles

SHV - DURING C-CK, SERVICE DOOR AFT SILL HAS CORROSION AROUND NUT PLATE. REPAIRED SERVICE DOOR SILL IAW EC5310-01373. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — OUT OF LIMITS (AILERON) · airframe 21,720 hrs · 16,300 cycles

SHV - DURING C-CHECK LT AILERON PCA FITTING IS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV C. ALODINED, PREPPED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (AILERON) · airframe 21,720 hrs · 16,300 cycles

SHV - DURING C-CHECK LT AILERON ATTACHMENT POINT FOR PCA O/B ROD END HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV C. PREPPED, ALODINED, PRIMED, AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — LEAKING (APU) · airframe 21,675 hrs · 16,262 cycles

IAH - FLIGHT 2992, DURING TAXI OUT THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE APU FUEL SOLENOID VALVE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (PITOT HEAT) · airframe 21,147 hrs · 15,853 cycles

IAH - FLIGHT 2822, DURING CLIMB THE CREW REPORTED A PITOT 2 HEAT INOP MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY FOR THE NUMBER TWO PITOT PROBE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 20,872 hrs · 15,653 cycles

IAH FLIGHT 2934 - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE LAV. MAINTENANCE REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 20,341 hrs · 15,261 cycles

CREW REPORTED THAT ON DEPARTURE, AFTER THE GEAR WAS SELECTED UP, AND HAD UP INDICATIONS THE GEAR SOUNDED LIKE IT WAS STILL DOWN. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R&R THE DOOR SEQUENCE PROXIMITY SWITCH, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTY (AHRS) · airframe 20,122 hrs · 15,110 cycles

CLE FLIGHT NR 2475 THE CREW REPORTED THEY LOST THE NR 1 ATTITUDE AND HEADING COMPUTER (AHRS) IN FLIGHT. MX INSPECTED AND REPLACED THE CAPTAINS AHRS COMPUTER AND OPS CHECKS WERE GOOD.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT)

AC WAS ON APPROACH INTO BNA WHEN SMOKE WAS SEEN COMING OUT FROM UNDERNEATH THE FO DASH. MX R&R THE RT WINDSHIELD IAW EMB 145 AMM 56-10-01. PRESSURIZATION CHECK/LEAK CHECK IAW EMB AMM 21-31-00. AC RELEASED, AFTER ALL CHECKS, BACK TO SERVICE.

Part: WINDSHIELD — MELTED (COCKPIT)

ACFT WAS ON APPROACH INTO BNA WHEN SMOKE WAS SEEN COMING OUT FROM UNDERNEATH THE F/O DASH. MX R&R THE RT W/S IAW EMB 145 AMM 56-10-01. PRESSURIZATION CHECK/LEAK CHECK GOOD. IAW EMB 145 AMM 21-31-00. ACFT RELEASED AFTER ALL CHECKS BACK TO SERVICE.

Part: SWITCH — FAULTY (NR 1 PACK)

MCI FLIGHT 2986 - THE CREW REPORTED A PACK 1 OVERLOAD IN FLIGHT EVEN AFTER 5 RESETS. THE MESSAGE REOCCURRED EVEN WHEN PACK 1 WAS DESELECTED. THE ACFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. THE SYSTEM WAS PLACED ON MEL. ON 7/13/08 THE NR 1 PACK OVERTEMP SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. (S)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,075 hrs · 14,376 cycles

FLIGHT 2014 - FLIGHT CREW REPORTED STRONG SMOKE ODOR IN COCKPIT DURING FLIGHT. MX PERFORMED OPERATIONAL CHECK OF WINDSHIELDS 1 AND 2 HEAT, RAN PACKS, RAN BOTH ENGINES AND PERFORMED INSPECTION OF ELECTRICAL COMPONENTS. ALL CHECK WERE PERFORMED SUCCESSFULLY AND NO SMOKE ODOR WAS NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A)

Part: BLEED VALVE — FAULTY (APU) · airframe 18,164 hrs · 13,759 cycles

CLE FLIGHT 2890 - THE CREW REPORTED A FUEL SMELL WHEN THE PACKS WERE OPERATING FROM THE APU. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,421 hrs · 12,548 cycles

IAH - FLIGHT 2115, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE AT 1500 FT ON FINAL APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, WITH NO DEFECTS, OR MESSAGES FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,001 hrs · 12,227 cycles

FLT 2951 - EWR - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP INOP. EWR MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 15,905 hrs · 12,148 cycles

IAH - FLIGHT 3083, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR KEPT GOING OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (APU BAY) · airframe 15,770 hrs · 12,054 cycles

JAN - FLIGHT 2395, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN WITH THE APU RUNNING. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 04/27/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,266 hrs · 11,661 cycles

BTV FLT 2874 DURING ROUTINE INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 12,121 hrs · 9,185 cycles

IAH - DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE 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: ODOR — DETECTED (CABIN) · airframe 9,895 hrs · 7,469 cycles

CREW REPORTED FUEL SMELL IN THE COCKPIT DURING FLIGHT. MAINTENANCE PERFORMED GROUND RUNS ON BOTH ENGINES AND APU WITH BLEEDS ON . NO DEFECTS NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

THE MAIN PASSENGER DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LIGHT ASSEMBLY, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 7,317 hrs · 5,450 cycles

TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKS I/A/W EMB-145-SRM-53-32-13 AND EC5330-01287.

Part: LAMP — BURNED OUT (CABIN INTERIOR)

DURING SERVICE/ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 12A TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LAMP AT SEAT 12A IAW EMB145 AMM 33-50-50. OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: FUEL NOZZLE — COKED (NR 2 ENGINE)

CLE FLIGHT 3244 THE CREW REPORTED A PUNGENT SMELL IN THE CABIN DURING ICE PROTECTION SYSTEM OPERATION. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BRAKE — BYPASSING (LANDING GEAR)

CLE FLIGHT#3738 THE CREW REPORTED AFTER TAKEOFF FROM CLE THEY RECEIVED A #1 HYDRAULIC SYSYTEM LOW QUANTITY INDICATION.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 AND #4 BRAKE ASSEMBLIES.THEY SUSPECTED THE #1 HYDRAULIC SYSTEM FLIUD WAS TRANSFERING TO THE #2 SYSTEM THROUGH THE BRAKES.THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE.#4 BRAKE S/N 0663 TSO:3444 TT:3444 CSN:2403