N13965

Part: SMOKE WARNING — FALSE INDICATION (LAVATORY) · airframe 35,340 hrs · 26,734 cycles

CREW REPORTED A LAVATORY SMOKE WARNING IN FLIGHT WITH NO ASSOCIATED FIRE OR SMOKE, LANDED WITHOUT INCIDENT, MAINTENANCE INSPECTED THE ACFT, OPS TESTED LAVATORY SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,440 hrs · 25,261 cycles

BOTH LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOP. INTIALLY ITEM WAS MOVED AND PLACED ON MEL 33-50-00-1. LATER IN THE DAY IN IAD MX R & R NR 4 EMERGENCY LIGHT POWER SUPPLY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,198 hrs · 25,062 cycles

DURING MX INSPECTION THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (COMPASS) · airframe 32,847 hrs · 24,766 cycles

CREW REPORTED STRONG ELECTRICAL BURNING ODOR IN COCKPIT. FOUND WIRE TO MAGNETIC COMPASS LOOSE. REINSTALLED AND SECURED WIRE WITH NO ODORS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HARNESS — FAULTY (NR1 ENGINE) · airframe 31,870 hrs · 23,949 cycles

CREW REPORTED ENGINE 1 FIRE DETECT FAIL ON EICAS INTERMITTENTLY AT FL370 IN TURBULENCE. FLIGHT CONTINUED TO DESTINATION WITHOUT INCIDENT. MX R & R ENGINE 1 HARNESS ASSY. ALL OPS CHECKS WERE GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 31,845 hrs · 23,931 cycles

CREW REPORTED SMOKE IN THE COCKPIT FOLLOWED BY LAVATORY SMOKE WARNING ON EICAS. F/A OBSERVED SMOKE IN CABIN. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX R & R THE NR 1 ENGINE. ALL OPS CHECKED GOOD.

Part: WIRE — BURNED (COCKPIT) · airframe 31,191 hrs · 23,445 cycles

THE CREW REPORTED THAT DURING DESCENT, STARTED TO GET WHAT SMELLED LIKE AN ELECTRICAL FIRE. THE ACFT LANDED WITHOUT INCIDENT, WHERE MX INSPECTED THE ACFT AND REPAIRED WIRE W182-2906-24. THE F/O'S AUDIO PANEL OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,921 hrs · 23,227 cycles

SKIN DAMAGED AT FR 65 & FR 67 AND STR 15R. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER.

Part: FAN — INOPERATIVE (AHRS) · airframe 29,778 hrs · 22,261 cycles

IAH - FLIGHT 3044 THE CREW REPORTED AN AHRS 2 OVERHEAT ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AHRS FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,163 hrs · 21,776 cycles

FLIGHT CREW REPORTED BURNING SMELL COMING FROM MIDDLE OF ACFT. EWR MX COULD NOT DUPLICATE THE BURNING SMELL WITH PACKS AND LIGHTS ON. ALSO PERFORMED VISUAL INSPECTION. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,404 hrs · 21,215 cycles

TYS - A/C WAS IN FOR A OVERNIGHT CHECK WHEN MAINTENANCE FOUND THE LT/RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04, OPS CHECK WAS GOOD AND A/C RELEASED TO SERVICE.

Part: COOLING FAN — INOPERATIVE (NR 1) · airframe 26,839 hrs · 20,033 cycles

FLIGHT 2760 - EWR - FLIGHT CREW REPORTED AHRS NR 1 OVERHEAT MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED AHRS NR 1 COOLING FAN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SKIN — CORRODED (COCKPIT) · airframe 25,982 hrs · 19,394 cycles

TYS - A/C CURRENTLY IN C-CHECK, INSPECTION FOUND PITTING ON THE COCKPIT FLOOR SKIN AT FRAME 14 BETWEEN STRINGER 16L TO 16R. MAINTENANCE REMOVED AND REPLACED THE SKIN IN THE EFFECTED AREA AND REMAPPED THE RVSM OF THE LT AND RT REGIONS IAW EC 5330-02058. ALL WORK ACCOMPLISHED AND WILL BE REL AT THE END OF THE CHECK.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 25,981 hrs · 19,394 cycles

TYS - LT ELEVATOR DAMAGED NEAR TIP FAIRING. REMOVED AND REPLACED LT ELEVATOR MOST O/B TIP LEADING EDGE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,981 hrs · 19,394 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LAV AREA CENTER OMEGA BEAM CORRODED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB 145 SRM 51-40-02; 51-20-03, 51-40-06 AND CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,981 hrs · 19,394 cycles

TYS - SMOKING RIVET/TOOL SCRATCH AT FRM 75; STR 1R. PERFORMED DOUBLER REPAIR IAW EC5330-02063.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,983 hrs · 19,395 cycles

TYS - A/C IN FOR A C-CHECK WHEN INSPECTION FOUND CORROSION ON THE AFT SIDE SVC DOOR. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF FR22 IAW EC 5310-01500. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: HOUSING — DAMAGED (VERTICAL STAB) · airframe 25,983 hrs · 19,395 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT AND RT SPHERICAL BEARING HOUSING WITH PITTING AND SCRATCHES. MAINTENANCE REAMED THE SPHERICAL HOUSING TO THE 1ST REWORK AND INSTALL BUSHIONS IAW EMB SRM 55-30-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BALLAST — FAULTY (CABIN) · airframe 25,835 hrs · 19,274 cycles

CLE FLT 2355 THE CREW REPORTED A BURNING ODOR FROM SEAT 1 & 2 AREA. MAINTENANCE INSPECTED AND REPLACED THE NR 4 CABIN LIGHT BALLAST. OPERATIONAL CHECKS WERE GOOD.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 25,832 hrs · 19,270 cycles

FLIGHT 2760 - YUL - FLIGHT CREW REPORTED BURNING ODOR WHEN PACK NR 1 SELECTED. EWR MX FOUND APU OIL OVER SERVICED. MX DRAINED EXCESSIVE OIL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,197 hrs · 18,034 cycles

DURING ROUTINE MAINTENANCE THE FIRST AISLE PATH LIGHT STRIP AND LOWER SERVICE DOOR LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,996 hrs · 17,888 cycles

CLE FLIGHT 2311 - THE CREW REPORTED THE AFT AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY AND THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,113 hrs · 18,508 cycles

MAIN CABIN DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,363 hrs · 17,417 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LAST THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP JUST AFT OF ROW 12, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,314 hrs · 17,380 cycles

RIC - MX - DURING ROUTINE INSPECTION, MX FOUND OVERHEAD EMERGENCY LIGHT AT 12BC SEATS INOPERATIVE. MX REMOVED AND REPLACED LAMP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,209 hrs

IAH - FLIGHT 2499, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING BEYOND ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING LIGHT ASSEMBLY. OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,901 hrs · 16,381 cycles

FWD CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 20,676 hrs · 15,539 cycles

EWR FLIGHT 2261 THE CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED FAULT ISOLATION PROCEDURES IAW 21-20-00-810-801A. RAN ENGINES, PACKS AND APU AT TAKEOFF POWER AND AT VARIOUS SETTINGS. CHECKED LIGHTING AND CABIN ELECTRICAL COMPONENTS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,593 hrs · 15,490 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM FR 17-23 HAS CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: STARTER GEN — FAILED (APU) · airframe 15,044 hrs · 11,178 cycles

CREW REPORTED ON TAXI, APU FAILED AND BURNING ODOR IN THE COCKPIT, AIRCRAFT WAS INSPECTED AND RELEASED IAW MEL 49-00-00 CATEGORY C-CONTROL 057571. IN RIC, REMOVED AND REPLACED APU STARTER/GENERATOR OPS CHECKED GOOD, NO DEFECTS NOTED, MEL ITEM CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAULTY (EMERGENCY LIGHT) · airframe 14,923 hrs · 11,089 cycles

BTV---CO2366, DURING 1A INSPECTION, MAINTENANCE FOUND AFT AISLE PATHWAY EMERGENCY LIGHT TO BE NOT OPERATING. REMOVED AND REPLACED BULB IAW EMB145 AMM NR 33-50-08, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,416 hrs · 9,913 cycles

DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND RIGHT HAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RIGHT HAND EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,120 hrs · 9,691 cycles

CLE FLIGHT 3292 - THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 13,028 hrs · 9,623 cycles

THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM AND REPLACED THE BATTERY AND THE CHARGER ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 13,021 hrs · 9,617 cycles

DURING PREFLIGHT CHECK, CREW REPORTED EXIT ROW EMERGENCY LIGHTS (2) TO BE INOPREATIVE. MAINTENANCE PERFORMED POWER SUPPLY RESET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,021 hrs · 9,617 cycles

CLE FLIGHT 2863, THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS INOPERATIVE. MAINTENANCE RESET ELECTRICAL POWER AND THE SYSTEM OPERATIONAL TEST WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 12,913 hrs · 9,529 cycles

DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (GALLEY FLOOR) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT THE CARBON FIBER GALLEY FLOOR SUPPORT. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB MM 53-21-10 AND CPM 51-21-04/05/06, SRM 53-21-10, 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (GALLEY FLOOR) · airframe 11,422 hrs · 8,377 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE CENTER FLOORBEAM OF FRAME 18. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAE EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WALL FLOOR MOUNT FLANGE AT FRAME 60. MAINTENANCE REMOVED AND REPLACED THE FLOOR MOUNT FLANGE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,422 hrs · 8,377 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 58. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLANGE — CORRODED · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE WALL MOUNT FLANGE THAT SUPPORTS THE GALLEY FLOORBOARD NR 231HF AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE WALL MOUNT FLANGE IAW EMB 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME AFT SILL. MAINTENANCE REMOVED AND REPLACED THE FRAME SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PROFILE — CORRODED (FLOORBEAM) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE Z PROFILE OF THE CENTER FLOORBEAM AT FRAME 24. MAINTENANCE REMOVED AND REPLACED THE Z PROFILE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,422 hrs · 8,377 cycles

DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL YAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (PAX DOOR) · airframe 11,422 hrs · 8,377 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MAIN ENTRANCE DOOR SILL UNDER THE THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR SILL IAW EMB SRM 51-40-02.

Part: MOUNT — CORRODED (LAV SINK DRAIN) · airframe 11,422 hrs · 8,377 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LAVATORY SINK DRAIN CABLE/HOSE MOUNT PLATE. MAINTENANCE REMOVED AND REPLACED THE DRAIN CABLE/HOSE MOUNT PLATE IAW EMB SRM 51-40-02, 51-30-01 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,422 hrs · 8,377 cycles

DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE RT OMEGA BEAM TOP CAP AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE RT OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE LEFT HAND EMERGENCY LIGHT FORWARD OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — FAILED (CABIN)

BTV---CO2316, DURING SERVICE/ROUTINE CHECK FOUND EMERGENCY LIGHT AISLE PATH LIGHTING FROM SEAT ROW 11 THROUGH 19 INOPERATIVE. REMOVED AND REPLACED AC/DC INVERTER IAW AMM NR 33-50-11. OPS. CHECKED LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT)

DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE INOP. MAINTENANCE RESET THE EMERGENCY LIGHTING POWER SUPPLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING)

DURING PREFLIGHT THE CREW NOTED THAT THE RIGHT HAND EMERGENCY OVERWING LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND EMERGENCY OVERWING LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MANIFOLD — OVERHEATED (HYD SYSTEM) · airframe 8,013 hrs · 5,626 cycles

TYS WHILE EN ROUTE FROM IAH TO TYS THE A/C WAS OUT APPROXIMATELY THIRTY MINUTES WHEN THE EICAS GAVE A NR 1 HYD, SYSTEM OVERHEAT MESSAGE FOLLOWED BY 0 PRESSURE INDICATION ON NR 1 SYSTEM. THE CREW FOLLOWED THE QRH PROCEDURE AND LANDED THE A/C AT TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYD MANIFOLD ASSY IAW AMM 27-10-07. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYD PUMP IAW 29-10-03. A/C WAS SERVICED AND ALL OPS CHECKS GOOD AND WAS RELEASED BACK TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING ROUTINE MAINTENANCE THE EXTERNAL FORWARD EMERGENCY LIGHT ON THE LEFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUT — FAULTY (NLG)

RIC FLT 3576-CREW REPORTED AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR CENTERING UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY, AND PERFORMED A SATISFACTORY SYSTEM OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LINER — MISSING (APU)

CLE FLIGHT 3595 THE CREW REPORTED ON LANDING RECEIVED A APU FIRE INDICATION. THE APU WAS SHUT DOWN AND THE INDICATION CLEARED. MAINTENANCE INSPECTED AND FOUND THE EXHAUST SILENCER LINER ASSEMBLY WAS MISSING. THE EXHAUST SILENCER ASSEMBLY WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE PERFORMED APU FIRE INDICATION INSPECTION. NO DEFECTS WERE FOUND.

Part: ATTACH FITTING — GOUGED (AILERON) · airframe 7,169 hrs · 5,003 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON WAS FOUND TO BE GOUGED AT THE ACTUATOR ATTACHMENT POINT. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND DYE PENETRANT INSPECTION IAW EMBRAER GST 0046/02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FITTING — CHAFED (HORIZ STAB) · airframe 7,169 hrs · 5,003 cycles

TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER LEFT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR INCLUDING DYE PENETRANT INSPECTION IAW EMBRAER GST-0045/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BRACKET — GOUGED (R/H WING) · airframe 7,169 hrs · 5,003 cycles

TYS During a scheduled inspection the right hand aileron PCA rod end attachment bracket was found to be gouged. Maintenance acomplished a blend-out repair including a dye penetrant inspection IAW Embraer GST-0046/02. The repair was found to be satisfactory, the aircraft will be released upon completion of inspection.

Part: FITTING — GOUGED (EMPENAGE) · airframe 7,169 hrs · 5,003 cycles

TYS During a scheduled inspection the right hand horizontal stabilizer bearing forward fitting was found to have a internal gouge. Maintenance accomplished a blend-out repair including dye penetrant inspection IAW Embraer GST-0095/02. The repair was satisfactory, the aircraft will be released upon completion of inspection.

Part: FITTING — CHAFED (HORIZ STAB) · airframe 7,169 hrs · 5,003 cycles

TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER RIGHT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST-0045/02 WHICH INCLUDED THE DYE PENETRANT INSPECTION. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: HINGE FITTING — GOUGED (VERTICAL STAB) · airframe 7,169 hrs · 5,003 cycles

TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE RIGHT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON THE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRACKS FOUND) AND RESTORED PROTECTIVE FINISH IAW EMB-GST-0065/02. REPAIR PROCEDURES ARE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION.

Part: HINGE FITTING — GOUGED (VERTICAL STAB) · airframe 7,169 hrs · 5,003 cycles

TYS, DURING A SCHEDULED 1C/2C INSPECTION THE LEFT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON THE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRACKS FOUND) AND RESTORED PROTECTIVE FINISH IAW EMB-GST-0065/02. REPAIR PROCEDURES ARE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LINE — DENTED (EXTINGUISH SYS) · airframe 7,169 hrs · 5,003 cycles

TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: LINE — DENTED (EXTINGUISH SYS) · airframe 7,169 hrs · 5,003 cycles

TYS DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: LINE — DENTED (EXTINGUISH SYS) · airframe 7,169 hrs · 5,003 cycles

TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 2 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE FIRE EXTINGUISHER LINE IAW-EMB-145-AMM-20-10-03. THE REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR---CREW REPORTED ON FLIGHT 3606 SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS. CHECKED GOOD.

Part: NOZZLE — MALFUNCTIONED (1 ENGINE)

IAH-DURING FLIGHT 3884 THE CREW REPORTED EXTREMELY STRONG JET FUEL FLAMES WHEN THE ANTI-ICE SYSTEM WAS ACTIVATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FUEL NOZZLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DAMAGED (CABIN)

IAH - DURING C-CHECK INSPECTION, ONE SECTION OF AISLE PATH LIGHT STRIPS WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — WORN (COCKPIT)

IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICERS SEAT TRACKS WERE FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — DAMAGED (CABIN)

IAH - DURING C-CHECK INSPECTION, ONE SECTION OF AISLE PATH LIGHT STRIPS WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

IAH - DURING C-CHECK INSPECTION, THE AFT CEILING 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: SEAT TRACK — WORN (COCKPIT)

IAH - DURING C-CHECK INSPECTION, THE CAPTAINS SEAT TRACKS WERE FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB145MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DAMAGED (PAX DOOR)

BNA - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE PASSENGER DOOR SKIN WAS DAMAGED. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REPAIRED THE AFFECTED DOOR SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CLAMP — BROKEN (BLEED AIR)

EWR - FLT 4203 - CREW REPORTED LOUD POP SOUND WAS FOLLOWED BY LOSS OF PRESSURE, DUAL BLEED LEAKS, AND BAGGAGE SMOKE. FURTHER NOTED BAGGAGE SMOKE ILLUMINATED INTERMITTENTLY. MAINTENANCE FOUND BLEED PIPE CLAMP BROKEN, HOLD DOWN NUT PLATE BROKEN. ALSO, FOUND DAU INTERMITTENT CAUSING BAGGAGE SMOKE DETECTOR INTERMITTENTLY ILLUMINATING (PART NUMBER 701-3348-932 S/N 9907204). REMOVED AND REPLACED DUCT CLAMP AND HOLD DOWN AND DAU FOR SMOKE DETECTOR SYSTEM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

EWR - FLT 4228 - CREW REPORTED BAG SMOKE DETECTOR INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES. OPS CHECKED SYSTEM GOOD. (M)