N16981

Part: STOP — BROKEN (PAX DOOR) · airframe 43,448 hrs · 33,143 cycles

DURING A MAINTENANCE INSPECTION, THE PAX DOOR FWD LOWER DOOR STOP SEAT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE STOP SEAT, RIGGED THE PAX DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,030 hrs · 32,804 cycles

DURING CREW INSPECTION, THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,178 hrs · 32,102 cycles

DURING A ROUTINE CHECK, FOUND THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES NUMBER 3 AND 4 IAW AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,136 hrs · 32,072 cycles

DURING INSPECTION, THE EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE NR 3 AND 4 EMERGENCY LIGHT BATTERY PACKS. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 41,537 hrs · 31,593 cycles

RIGHT REAR FUSELAGE SKIN CRACKED AROUND RIVETS AT FRAME 75, STRINGER 2R. DAMAGED AREA REPAIRED WITH DOUBLER IAW SRM 53-31-00.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 41,537 hrs · 31,593 cycles

SERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 41,537 hrs · 31,593 cycles

REAR FUSELAGE FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 41,537 hrs · 31,593 cycles

CABIN NR 1 FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,537 hrs · 31,593 cycles

CABIN LT INBOARD SEAT TRACK NR 1 CORRODED. LT INBOARD SEAT TRACK NR 1 REPLACED AS PER 53-01-06.

Part: GUSSET — CORRODED (FRAMES 16-17) · airframe 41,537 hrs · 31,593 cycles

LEFT GUSSET CORRODED AROUND ANCHOR NUT BETWEEN FRAMES 16 AND 17. THE GUSSET WAS REPAIRED IAW SRM 53-21-10, ITEM 2, FIG 201.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO BAY) · airframe 40,011 hrs · 30,403 cycles

PILOT REPORTED EICAS MESSAGE FOR CARGO BAY SMOKE FOR 5 SECONDS, CLIMBING THROUGH 14000 FEET. MX PERFORMED OPS CHECK OF CARGO SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — FAILED (NR 2 NACELLE) · airframe 36,483 hrs · 27,590 cycles

THE CREW REPORTED A NR 2 ENGINE FIRE DETECT FAIL MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE DETECTOR. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,183 hrs · 26,554 cycles

DURING MX INSPECTION THE AFT GALLEY EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL VALVE — INOPERATIVE (BRAKES) · airframe 32,541 hrs · 24,298 cycles

CREW REPORTED ZERO BRAKE EFFECTIVENESS IN LT BRAKE DURING TAXI. MX R & R THE OTBD BRAKE CONTROL VALVE WITH OPS AND TAXI CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

NR 2 RT WALL SEAT TRACK SUPPORT IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. CUT-OUT CORRODED SECTION, FABRICATED AND INSTALLED NEW SEAT TRACK SUPPORT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IS IN FOR A C-CHECK INSPECTION, WHEN A LT SPLICE AT FRAME LBL 15 WAS FOUND CORRODED. MX R & R THE REINFORCEMENT SPLICE AT FRAME IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BRACE — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IS IN FOR A C-CHECK INSPECTION, WHEN THE RT CROSSBRACE WAS FOUND BENT AND CORRODED AT FRAME 17. MX R & R THE CROSSBRACE IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE RT LONGITUDAL SEAT TRACK FROM FRAME 48 THRU 52. MX R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 31,641 hrs · 23,776 cycles

DURING A C-CHECK, CORROSION FOUND AROUND NUTPLATED AT THE BAGGAGE DOOR. MX R & R THE BAGGAGE DOOR INBD ANGLE IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

DURING C-CHECK, LEFT CHANNEL CROSSBEAM AT FRAME 18 WAS FOUND CORRODED. MX BLENDED CORROSION IAW SRM 51-10-03, PERFORMED HFEC, NO CRACKS FOUND AND WAS WITHIN LIMITS IAW SRM 53-21-10. ALL WORK ACCOMPLISHED AND WILL BE RELEASED A THE END OF THE CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

DURING C-CHECK INSPECTION, RT OTBD SEAT TRACK SUPPORT FOUND CORRODED AT FR 55. MX REMOVED THE RIVETS AND FABRICATED A NEW SUPPORT AND INSTALL IAW SRM 51-40-02 AND SRM 53-00-11. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IN FOR A C-CHECK, CHECK WHEN THE LT WALL SUPPORT HAD CORROSION ON THE LOWER SIDE OF SUPPORT AT FRAME 60. MX R & R THE LT WALL SUPPORT IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

C-CHECK, GUSSET AT FR 17 WAS FOUND WITH MINOR CORROSION AROUND NUTPLATE. MX BLENDED CORROSION LEAVING REMAINING MATERIAL TO BE WITHIN LIMITS IAW SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BEAM — CORRODED (REAR FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IN FOR A C-CHECK, CHECK WHEN THE CARGO DOOR CUTOUT WAS FOUND. CORRODED ON THE THRESHOLD BETWEEN FRAMES 65 AND 68. MX BLENDED THE CORROSION IAW SRM 51-10-03. R & R THE AREAS OUT OF LIMITS WITH FABRICATED PARTS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

ACFT IN FOR A C-CHECK, WHEN THE NR 4 LT SEAT TRACK WAS FOUND CORRODED IN SEVERAL PLACES. BLENDED AREAS IAW SRM 51-10-03, THE OUT OF LIMIT AREAS IAW SRM 53-00-11 WERE CUT OUT AND FABBED PARTS WERE INSTALL IN THE SEAT TRACK SECTION IAW SRM 53-00-11. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,641 hrs · 23,776 cycles

C-CHECK, CORROSION FOUND AT FRAME 65 AT THE THRESHOLD. MX R & R THE LOWER SECTION OF FRAME 65IAW ETD 2012-145-018140. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

NR 1 LEFT WALL SEAT TRACK SUPPORT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

GUSSET AT FRAME 65 TO 68 AT Y=-479 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

NR 3 LEFT ISLE SEAT TRACK GUSSET IS CORRODED OUT OF LIMITS AFTER BLENDING. R & R GUSSET.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RT OTBD SEAT TRACK SUPPORT CORRODED ON LOWER FOOT. CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.

Part: CHANNEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

PAX DOOR U CHANNEL CORRODED BEYOND LIMITS AFTER BLENDING. R & R U CHANNEL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

FRAME 15 DIGITAL IS CORRODED BEYOND LIMITS. R & R DIGITAL.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

SUPPORT IN THE LAVATORY AREA HAS CORROSION OUT OF LIMITS AFTER BLENDING. REMOVED AND REPLACED DOUBLER.

Part: CHANNEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

PAX DOOR U-CHANNELS ARE CORRODED BEYOND LIMITS AFTER BLENDING. R & R CHANNELS.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

CORROSION AFT LAVATORY LT FLOOR GUSSET CORRODED OUT OF LIMITS AFTER BLENDING. R & R FLOOR GUSSET.

Part: BRACE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RT CROSS BRACE IS CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R BRACE.

Part: SILL — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RIGHT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LEFT ANGLE HAS CORROSION THAT IS OUT OF LIMITS AFTER BLEND OUT. R & R LEFT ANGLE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RT WALL SUPPORT IS OUT OF LIMITS AFTER BLEND-OUT. R & R SUPPORT.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

CROSS BRACE HAS CORROSION OUT OF LIMITS AFTER BLEND-OUT. R & R CROSS BRACE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LT SILL IS COORODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LAVATORY RT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

AFT LAV LT OMEGA BEAM IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. REMOVED DAMAGED SECTION, FABRICATED A FILLER AND DOUBLER AND INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LT FWD SILL HAS CORROSION AROUND NUT-PLATES, OUT OF LIMITS AFTER BLEND-OUT. REMOVED AND REPLACED SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LT SILL CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RT SILL CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

CORROSION OUT OF LIMITS AFTER BLEND-OUT AT FRM 68 RT SIDE AT Z=715.7. R & R TEE ANGLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LT FLOOR SUPPORET CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.

Part: PAN — CORRODED (LAVATORY) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LAVATORY WATER WASTE PAN IS CORRODED BEYOND LIMITS. R & R PAN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

LAV RT FLOOR GUSSET CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

AFT LAV LT FLOOR GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 31,641 hrs · 23,776 cycles

RT OTBD SEAT TRACK SUPPORT CORRODED BEYOND LIMITS. R & R SUPPORT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,445 hrs · 23,636 cycles

DURING 5A CHECK INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R ROW 12 CEILING EMERGENCY LIGHT BULB WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — SHORTED (APU) · airframe 31,054 hrs · 23,314 cycles

APU FIRE INDICATION ON EICAS AT GATE. CREW DISCHARGED APU FIRE EXTINGUISHER. MX PERFORMED APU FIRE WARNING INSPECTION AND FOUND FIRE TO BE LIMITED TO APU STARTER GENERATOR AND ASSOCIATED DUCTING AND OUTLET SCOOP. APU PLACED ON MEL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,777 hrs · 23,091 cycles

A/C WAS FOUND TO HAVE ALL OF THE FWD EMERGENCY LIGHTS INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD AND WAS RELEASED TO SERVICE.

Part: UNKNOWN — ODOR · airframe 29,160 hrs · 21,811 cycles

THE CREW REPORTED AN ODOR OF JET FUEL AFTER APU START. MX INSPECTED AND PERFORMED OPS CHECKS OF APU. NO FUEL ODOR WAS NOTED. THE ACFT WAS RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,467 hrs · 21,324 cycles

ORD FLT 5843 THE CREW REPORTED FUEL SMELL IN THE COCKPIT AFTER APU START WITH PACK RUNNING ON ENGINE BLEED. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS WITH BLEEDS ON. FOUND NO FUEL SMELL COMING FROM THE PACKS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADAR — INOPERATIVE (NOSE) · airframe 27,663 hrs · 20,632 cycles

ORD FLT 6173 THE CREW REPORTED THE WEATHER RADAR FAILED INFLIGHT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR. OPERATIONAL CHECKS WERE GOOD.

Part: TRANSDUCER — INOPERATIVE (NR 3 WHEEL) · airframe 20,632 hrs · 27,663 cycles

RDU - TYS - BRAKE DEGRADE MESSAGE ON EICAS - MX FRY TO TYS. TYS MX REMOVED AND REPLACED NR 3 WHEEL SPEED TRANSDUCER OPS CHECK GOOD. LP-2781371.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION FRAME 21-23. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FRAME 18-23 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 29 HAS CORROSION AT CROSSBEAM ATTACHMENT AREA. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 29 CROSSBEAM ATTACHMENT AREA BY INSTALLING FABRICATED DOUBLER IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK CORROSION ON DOUBLER WHERE POTABLE WATER LINES EXIT FUSELAGE "EXTERNAL". MAINTENANCE PERFORMED REPAIR ON DOUBLER WHERE POTABLE WATER LINES EXIT FUSELAGE "EXTERNAL" IAW EMB-145 EC5330-02304 ORIG REV. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 38 HAS CORROSION AT CROSSBEAM ATTACHMENT AREA. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 38 AT CARBON CROSSBEAM ATTACHMENT AREA IAW EMB-145 SRM 53-00-10 ITEM 4, FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL) AT CROSSBEAM ATTACHMENT AREA. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CROSSBEAM ATTACHMENT AREA AT FRAME 33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,659 hrs · 19,865 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 29 HAS CORROSION (LOCAL LEVEL 2) AT CROSSBEAM ATTACHMENT AREA. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HANDLE — MISALIGNED (PAX DOOR) · airframe 25,727 hrs · 19,141 cycles

CHS - FLIGHT 3064, THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND RE-INSTALLED THE MAIN CABIN DOOR INNER HANDLE, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ROLLER — OUT OF ADJUST (MAIN DOOR) · airframe 25,644 hrs · 19,081 cycles

CLE FLT 2989 THE CREW REPORTED THE MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AFT DOOR ROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: FIRE LOOP — CHAFED (NR 1 ENGINE) · airframe 25,521 hrs · 18,987 cycles

FLIGHT 2537 - EWR - FLIGHT CREW REPORTED ENGINE NR 1 FIRE DETECT FAIL CAUTION MESSAGE APPEARED TWICE IN FLIGHT ON EICAS. EWR MX REMOVED AND REPLACED ENGINE NR 1 FIRE LOOP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUT — DEFECTIVE (NLG) · airframe 24,515 hrs · 18,270 cycles

FLIGHT 4931 - IAD - FLIGHT CREW REPORTED AIR GROUND FAIL MESSAGE. RIC MX REMOVED, REPACKED AND INSTALLED NOSE LANDING GEAR STRUT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,509 hrs · 18,263 cycles

CLE FLT 4930 MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT FLOOR STRIP AT THE WING EMERGENCY EXIT DID NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: ROD — WORN (SERVICE DOOR) · airframe 24,509 hrs · 18,263 cycles

DAY FLT 2391 CREW REPORTED THAT THE SERVICE DOOR WOULD NOT CLOSE. MAINTENANCE INSPECTED AND REPLACED THE CRANK ROD ASSY. OPERATIONAL CHECKS WERE GOOD.

Part: LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 24,429 hrs · 18,203 cycles

FLIGHT 2866 - MKE - FLIGHT CREW REPORTED AIR SPEED INDICATION LOSS MOMENTARILY DURING GO AROUND. CREW PERFORMED EMERGENCY DESCENT AND LANDED ACFT UNEVENTFULLY. MX DRAINED BOTH PITOT STATIC LINES AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,379 hrs · 18,163 cycles

CLE FLT 3045 THE CREW REPORTED A VERY STRONG SMELL IN THE COCKPIT WHEN THE ICE PROTECTION CAME ON. SMELL WENT AWAY WHEN THE ICE PROTECTION SYSTEM WAS TURNED OFF. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE ANTI-ICE SYSTEM WITH THE APU AND ENGINE BLEED SYSTEMS ON. NO DEFECTS OR SMELL WERE NOTICED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — BURNED (COCKPIT) · airframe 23,949 hrs · 17,839 cycles

CLE FLT 2309 - THE CREW REPORTED A ELECTRICAL BURNING SMELL AFTER LANDING. THE SMELL WAS STRONGEST IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE UPPER TAXI LIGHT CONTACTOR. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,748 hrs · 17,688 cycles

MCI - FLIGHT 2794, THE CREW REPORTED A SMELL OF SMOKE WHEN THE WINDSHIELD HEAT WAS TURNED ON. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE WINDSHIELD HEAT WITH NO DEFECTS, OR ODORS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 22,777 hrs · 16,970 cycles

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

Part: BOLT — MISSING (CABIN DOOR) · airframe 22,708 hrs · 16,911 cycles

FLIGHT 2093 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. EWR MX FOUND A MISSING BOLT ON INNER HANDLE BOX. MX INSTALLED BOLD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 22,711 hrs · 16,913 cycles

FLIGHT 2530 - GSO - FLIGHT CREW REPORTED THAT DURING CLIMBING, AFTER ENTERING ICING CONDITIONS AT 13000FT, BLEED NR 2 OVERTEMP THEN BLEED NR 1 OVERTEMPED AS BLEED NR 2 BECAME NORMAL, ICING SYSTEM TURNED OFF THEN OVERTEMP WENT AWAY. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 22,711 hrs · 16,913 cycles

FLIGHT 2530 - GSO - FLIGHT CREW REPORTED THAT DURING CLIMBING, AFTER ENTERING ICING CONDITIONS AT 13000FT , BLEED NR 2 OVERTEMP THEN BLEED NR 1 OVERTEMPED AS BLEED NR 2 BECAME NORMAL, ICING SYSTEM TURNED OFF THEN OVERTEMP WENT AWAY. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 FAN AIR CONTROL THERMOSTAT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,410 hrs · 16,686 cycles

DURING ROUTINE MX THE LOWER EMERGENCY EXIT LIGHT AT 12C WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE LOWER EMERGENCY EXIT LIGHT AT ROW 12C. OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

SHV DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CRACKED AT RIVETS AT FRAMES 21 AND 22. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01426. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

SHV DURING C CHECK THE BAGGAGE DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01198. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

SHV DURING C CHECK THE BAGGAGE DOOR UPPER FRAME WAS FOUND TO BE CORRODED. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01198. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — UNDERSERVICED (NLG) · airframe 19,231 hrs · 14,475 cycles

L/G AIR GROUND FAIL & ENG 1, 2 REV DISAGREE AFTER T/O. SERVICED NLG STRUT IAW EMB 145 MM 32-20-01, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,934 hrs · 13,522 cycles

FLT - 2319 - EWR - CREW REPORTED BURNING ODOR IN COCKPIT FOR ABOUT 5 SECONDS. NO SMOKE OR MESSAGES NOTICED. EWR MX RAN ENGINES AND PACKS, INSPECTED COCKPIT FOR ODOR AND SMOKE BUT NO SMOKE OR ODOR WAS NOTICED. ALL OPERATIONAL TESTS WERE PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,399 hrs · 13,113 cycles

BTV ROUTINE CHECK FLT NR 2043 FOUND COCKPIT CEILING, CEILING AT ROW 3ABC, AND LEFT FWD WING TO FUSELAGE FAIRING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY LIGHT BASE CHARGER IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. CLOSED

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,064 hrs · 12,064 cycles

IAH - FLIGHT 2307 THE CREW DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY LIGHT ON THE BULKHEAD AT ROW THREE TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,234 hrs · 10,633 cycles

STL - DURING MAINTENENCE INSPECTION, THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,140 hrs · 10,560 cycles

LFT - FLIGHT 2551, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE INTERIOR EXIT SIGN AFT OF THE RT EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHT) · airframe 12,403 hrs · 9,193 cycles

ORD FLIGHT NR2758, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. AIRCRAFT WAS FERRIED TO CLE WHERE MAINTENANCE REPLACED THE CONNECTOR AT THE NR 2 EMERGENCY BATTERY. ALL OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,583 hrs · 8,556 cycles

CHS - FLIGHT 3324, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE ON CONTINUOUSLY, AND ROW 5 EMERGENCY LIGHTS WERE INOPERATIVE. THE AIRCRAFT WAS FERRIED TO CLE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,163 hrs · 9,014 cycles

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE RESET THE AIRCRAFT ELECTRICAL SYSTEM, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO PARTS WERE CHANGED.

Part: CONNECTOR — FAULTY (BATTERY CHARGER) · airframe 12,073 hrs · 8,938 cycles

EWR - CREW REPORTED, EMERGENCY LIGHTS STAYED ON IN FORWARD SECTION OF THE CABIN FOR TWO MINUTES WHILE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED CONNECTOR ON NR 2 BATTERY CHARGER P8501 IAW EMB 145 AMM 25-23-09. OPS CHECKED SYSTEM GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 11,834 hrs · 8,750 cycles

DURING CLIMB THE LANDING GEAR LEVER WOULD NOT GO TO THE UP POSITION. USING THE DOWNLOCK RELEASE BUTTON THE GEAR RETRACTED SUCCESSFULLY BUT THE NOSE GEAR DOORS REMAINED OPENED. AIRCRAFT RETURNED TO IAH LANDED WITHOUT INCIDENT. REPLACED THE NLG DOOR SEQUENCE SWITCH AND OPERATIONALLY CHECK GOOD. AIRCRAFT APPROVED FOR SERVICE.

Part: SWITCH — OUT OF ADJUST (CABIN)

CLE FLIGHT#2124 THE CREW REPORTED A EMERGENCY EXIT OPEN INDICATION IN FLIGHT ON THE EICAS.THE INDICATION WAS ON THE LEFT SIDE.CABIN PRESSURIZATION WAS MAINTAINED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT EMERGENCY EXIT DOOR MICROSWITCH ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — INOPERATIVE (CABIN)

TYS FLIGHT#2089 THE CREW REPORTED THE EXIT SIGN BY THE GALLEY DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: HOUSING — CORRODED (VERTCAL STAB) · airframe 7,996 hrs · 5,701 cycles

DURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARING HOUSING HAD LITE CORROSION. MAINTENANCE REWORKED BOTH VERTICAL BEARING HOUSINGS IAW EC 5510-01052 AND EMB 145 AMM 51-50-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 7,879 hrs · 5,606 cycles

EWR---CO2442, CREW REPORTED, "FIRST OFFICER'S WINDSHIELD (OUTER PANE) SHATTERED IN FLIGHT." MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD I/A/W EMB145 AMM #56-10-01. HEAT ELEMENT OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 7,556 hrs · 5,355 cycles

TYS AFTER TAKEOFF THE CREW WAS COMPLETING THE AIR PORTION OF THE ICE TEST WHEN A ODOR WAS SMELL IN THE CABIN AFTER A MINUTE THE ICIAS SHOWED SMOKE IN THE LAV BUT NO CABIN INDICATION OR SMOKE WERE NOTED IN THE LAV THE CREW RETURNED TO TYS. MAINT PERFORMED ALL TEST AND COULD'NT DUPLICATE. A DECISION WAS MADE TO R/R THE ENGINE, EVIDENCE SHOWED CARBON SEAL FAILURE. ENG WAS R/R IAW ROLLS-ROYCE MM. AND OPS CHECKS GOOD.

Part: PUMP — FAILED (WING)

CLE FLIGHT#3017 THE CREW REPORTED FUEL PUMP 1A FAILED IN FLIGHT.MAINTENANCE REPLACED THE FUEL PUMP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED · airframe 5,928 hrs · 4,033 cycles

EWR---CO3374, CREW REPORTED BURNING ODOR FROM COFFEE JUG AREA....MAINTENANCE REMOVED AND REPLACED CONNECTOR FOR COFFEE JUG IAW EMB145 WIRING MANUAL 25-31-50. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN · airframe 4,852 hrs · 3,281 cycles

TYS During a scheduled inspection the main cabin door frame skin was found gouged and rubbing on the forward upper cutout. Maintenance blended the gouged and rubbed areas I.A.W.-EMB-GST-3272/01. The repair is satisfactory and the aircraft will be released upon completion of inspection.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SOME EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,587 hrs · 2,410 cycles

CREW REPORTED AFT ROW EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT ROW EMERGENCY LIGHT STRIP IAW EMB145 MM 33-50-08 OPS. CHECKED SYSTEM GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE FLIGHT 3901 THE CREW REPORTED THE AFT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT)

CLT - FLT 4071 - CREW REPORTED THAT DURING THE FLIGHT FROM EWR TO CLT, THE FIRST OFFICERS WINDSHIELD OUTER PANE CRACKED AND SPIDER WEBBED, AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO TYS AND THE FIRST OFFICERS WINDSHIELD WAS REMOVED AND REPLACED IAW EMB-145 MM 56-10-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)