N15985

Part: ACM — LOCKED (NR 2) · airframe 26,820 hrs · 27,889 cycles

THE CREW REPORTED SMOKE IN THE CABIN, STRONGEST NEAR 9D. NR 2 A/C PACK INOPERATIVE, LOCKED UP. MAINTENANCE INSPECTED THE ACFT AND PLACED PACK 2 ON MEL 21-51-00-1 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 36,248 hrs · 27,460 cycles

DURING ROUTINE MAINTENANCE, THE RT OVERWING EXIT EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE RT OVERWING EXIT MARKER SIGN. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (ROW 20) · airframe 36,241 hrs · 27,453 cycles

ROW 20 FLOOR EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE R & R FLOOR EMERGENCY LIGHT ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAMES 75-78) · airframe 35,916 hrs · 27,198 cycles

DURING C-CK, FUSELAGE SKIN CRACKED AROUND RIVET FR 75-78 STR 2R-7R. REPAIRED SKIN IAW EC5330-02981. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 33,165 hrs · 25,038 cycles

DURING ROUTINE MAINTENANCE, THE RT OVER WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT OVERWING EMERGENCY LIGHT ASSY. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,070 hrs · 24,959 cycles

THE CREW REPORTED EMERGENCY PROXIMITY LIGHT STRIP INOPERATIVE AT SEAT 1 & 2. MAINTENANCE REPLACED LIGHT. OPS CHECKED GOOD.

Part: TRUNNION — CRACKED (LT MLG) · airframe 32,980 hrs · 24,869 cycles

ACFT WAS SCHEDULED FOR A GEAR INSPECTION WITH EDDY CURRENT MACHINE, THE LT MLG AFT TRUNION OTBD AREA OF THE TRUNION WAS FOUND TO BE CRACKED. THE LT MLG TRUNION BEARING ASSY WAS CHANGED IAW EC 5710-01218. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED TO SERVICE. ALL OPS CHECK WERE FOUND GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,850 hrs · 24,021 cycles

DURING ROUTINE MX, THE CENTER AILSE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,814 hrs · 23,995 cycles

CREW REPORTED THE ROW 12 EMERGENCY LIGHT INOPERATIVE. MX R & R THE EMERGENCY LIGHT INVERTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CENTER FUSELAGE) · airframe 30,967 hrs · 23,348 cycles

ACFT IS IN FOR A C-CHECK WHEN INSPECTION FOUND CORROSION ON THE INTERNAL SURFACE OF SKIN PANEL BETWEEN FRAME 13 AND 14; STR 18R THRU 20L. MX R & R THE PANEL, ALODINED AREA PRIME AND PAINTED IAW EC 5330-02703. PERFORMED RVSM MAPING REF TASK CARD 34-13-04-280-A00. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: LINE — CHAFED (BRAKE) · airframe 30,576 hrs · 23,051 cycles

LOST ALL HYD FLUID IN THE NR 2 SYS IN FLIGHT. R & R RT OTBD BRAKE LINE. LEAK CHECKED GOOD.

Part: LINE — CHAFED (BRAKE) · airframe 30,576 hrs · 23,051 cycles

LOST ALL HYD FLUID IN THE NR 2 SYS IN FLIGHT. R & R RT OTBD BRAKE LINE. LEAK CHECKED GOOD.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 28,681 hrs · 21,536 cycles

DURING SCHEDULED MX INSPECTION THE LT SIDE EMERGENCY EXIT ROW UPPER SIGN WAS FOUND INOPERATIVE. MX R & R THE NR 4 INVERTER IAW AMM 33-50-01 WITH OPS CHECK SUCCESSFUL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 26,503 hrs · 19,837 cycles

IAH - FLIGHT 2261, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REVIEWED CMC MESSAGES AND FOUND NO WOW MESSAGES, VERIFIED NORMAL OPERATION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK FR 10 IS CRACKED JUST BELOW LT DV WINDOW. REMOVED AND REPLACED FR 10 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK LT OMEGA BEAM LOWER FLANGE HAS CORROSION (LEVEL 3 LOCAL) AT FRAME 20. MAINTENANCE PERFORMED BEAM SPLICE REPAIR ON LT OMEGA BEAM AT FRAME 19-23 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 EC5320-01229 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION AT FR 53-59. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 58-59. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 26,022 hrs · 19,482 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) ON LT OMEGA BEAM CROSSBEAM FLANGE AT FRAME 58-59. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CROSSBEAM AT FRAME 58-59 IAW EC5310-01466 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,022 hrs · 19,482 cycles

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

Part: COUPLER — BROKEN (VOR SYS) · airframe 25,928 hrs · 19,412 cycles

EN ROUTE, WHEN CREW RECEIVED A MESSAGE FROM THE VOR/ILS. CDI NEEDLE SHOWING A FULL SCALE DEFLECTION TO LT AND RT, MISSING APPROACH ON 2 OCCASIONS AND LANDED. ACFT FERRIED. MAINTENANCE REMOVED AND REPLACED THE LOWER VOR ANTENNA COUPLER IAW AMM 34-32-03. OPS CHECK WAS GOOD AND RELEASED TO SERVICE.

Part: BRAKE — LOCKED (NR 2) · airframe 25,766 hrs · 19,279 cycles

THE CREW REPORTED NR 2 BRAKE LOCKED UP DURING TAXI. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BRAKE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,800 hrs · 17,021 cycles

EMERGENCY FLOOR STRIP PROX LIGHTS NR 2 AND 3 INOP. REMOVED AND REPLACED NR 3 INVERTER FOR EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 21,855 hrs · 16,313 cycles

EWR - FLIGHT 2685 - THE CREW REPORTED A LOUD BANG AND VIBRATION ON CLIMBOUT, IT WAS REPORTED 2 TIMES. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR UPLOCK BOX NR 1 AND 2 PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 21,721 hrs · 16,208 cycles

FLIGHT 2700 - EWR - FLIGHT CREW REPORTED NR 1 HYD LOW QTY MESSAGE ON EICAS DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX SERVICE HYDRAULIC SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRAKE ASSY — LEAKING (NR 1) · airframe 21,661 hrs · 16,166 cycles

FLIGHT 3115 - EWR - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 1 LOW QUANTITY INDICATION. CREW DECIDED TO PERFORM AN AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRAKE ASSY — LEAKING (NR 4) · airframe 21,661 hrs · 16,166 cycles

FLIGHT 3115 - EWR - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 1 LOW QUANTITY INDICATION. CREW DECIDED TO PERFORM AN AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,600 hrs · 16,121 cycles

FLIGHT 2659 - EWR - FLIGHT CREW REPORTED ELECTRICAL INSULATION BURNING SMELL NOTICED COMING FROM 19A SEAT CEILING LIGHT. EWR MX REMOVED AND REPLACED CEILING LIGHT ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,468 hrs · 16,031 cycles

RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT SERVICE DOOR. RIC MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLANGE — CORRODED (NR 2 INTAKE) · airframe 21,408 hrs · 15,982 cycles

TYS - DURING C-CHECK INSPECTION FOUND THE NR 2 ENG AIR INTAKE MOUNTING FLANGE BOLT HOLES CORRODED. COMPLETED REPAIRS FOR 4 HOLES AT .300 INCH AND 11 HOLES FOR BUSHING INSTALLATION IAW EC 5420-01158. A/C STILL IN C-CHECK.

Part: APU — SMOKE

IAH - FLIGHT 2749 - DURING PRE-FLIGHT THE CREW REPORTED SMOKE IN THE COCKPIT WHEN THE APU WAS STARTED, AND THE CREW SHUT DOWN THE APU. MAINTENANCE INSPECTED ACFT, OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: WIRE — BROKEN (CABIN) · airframe 18,565 hrs · 14,001 cycles

IAH - DURING MAINTENANCE INSPECTION THE LAST THREE AISLE PATH LIGHTING STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE AT SP9221, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,565 hrs · 14,001 cycles

IAH - DURING MAINTENANCE INSPECTION THE LAST THREE AISLE PATH LIGHTING STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER SIX AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,403 hrs · 13,877 cycles

NR 4 EMERGENCY LIGHT INVERTER INOP. REMOVED AND REPLACED INVERTER IAW EMB 145MM 33-50-10 OPS CK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED · airframe 17,172 hrs · 12,967 cycles

FLT 2445 - EWR - CREW REPORTED APU BLEED PRODUCING SMOKE IN CABIN AND COCKPIT. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,712 hrs · 11,885 cycles

MCI - DURING MAINTENANCE INSPECTION THE FORWARD CABIN AND LEFT HAND FORWARD EXTERIOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — FAULTY (EMERGENCY LIGHT) · airframe 13,043 hrs · 9,772 cycles

DURING 5A/3A INSPECTION AND SERVICE AND ROUTINE CHECK MAINTENANCE FOUND THE PASSENGER AND SERVICE DOOR EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED LAMPS IN SERVICE DOOR EMERGENCY LIGHT ASSEMBLY AND RECONNECTED WIRE SPLICE FOR PASSENGER DOOR EMERGENCY LIGHTS IAW EMB145 33-50-00, OPS CHECKED SYSTEM GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 12,300 hrs · 9,190 cycles

SHV - DURING C-CHECK 2 RIVET HOLE CRACKED ON FUSELAGE SKIN UNDER AFT RAR 2 SUPPORT. MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN UNDER RAR 2 ANTENNA SUPPORT IAW EC5330-01475. THE AIRCRAFT WAS APPROVED TO RETURNED FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS OVER THE SERVICE DOOR AND THE FIRST TWO AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — WEAK (GALLEY AREA)

CREW REPORTED, EMERGENCY LIGHTS IN FORWARD PART OF CABIN ARE WEAK. MAINTENANCE REMOVED AND REPLACED GALLEY EMERGENCY LIGHT BATTERY PACK IAW EMB145 MM 33-50-04. OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE FORWARD SECTION OF EMERGENCY LIGHTING ON THE FLOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LIGHTING STRIP BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE AFT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING ROUTINE CHECK, THE FORWARD AISLE PATH LIGHTING STRIP WAS FOUND TO BE DIM WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK, OPERATIONALLY CHECKED THE LIGHTING SYSTEM, AND THE DISCREPANCY WAS CLEARED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: BATTERY — INOPERATIVE (CABIN)

CREW REPORTED, EMERGENCY LIGHTS, FORWARD STRIP, GALLEY AND MAIN EXIT DOOR EXIT INDICATORS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP SEAT 1A IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

THE CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FORWARD EMERGENCY LIGHT POWER SUPPLY TO BE INOPERATIVE. THE AFFECTED POWER SUPPLY WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: CONNECTOR — DIRTY (CABIN)

EWR FLIGHT#3272 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY AISLE PATH LIGHT STRIP CONNECTOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT)

CLE FLIGHT 3201 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD HAD SHATTERED ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OUTER GLASS PLY HAD SHATTERED. THE WINDSHIELD WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ATTACH FITTING — SEPARATED (ELEVATOR) · airframe 4,752 hrs · 3,277 cycles

TYS, DURING A SCHEDULE INSPECTION THE LEFT ELEVATOR ATTACH FITTING WAS FOUND SEPARATING FROM THE HORIZONTAL STABILIZER ON THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE RIVETS WITH NEW OVERSIZED AND USING THE REMAINING RIVET PROTRUDING HEAD PART AS SHIM TO THE NEW ONE AS A PERMANENT REPAIR IAW-EMB-GST-0580/02. AIRCRAFT RELEASED TO SERVICE.

Part: CONNECTOR — BURNED (CABIN)

IAH- WHILE AT THE GATE THE CREW NOTED A BURNT RUBBER SMELL THROUGHOUT THE AIRCRAFT, WITHOUT PACKS OR APU OPERATING. IAH- MAINTENANCE REMOVED AND REPLACED THE COFFEE POT RECEPTACLE/CONNECTOR,PERFORMED A OPERATIONAL CHECK ,NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE AISLE PATH EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF AISLE PATH LIGHTING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — BROKEN (PNEUMATIC SYS)

MKE - THE CREW REPORTED A NUMBER ONE ENGINE BLEED LEAK WARNING. THE AIRCRAFT RETURNED TO MKE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RINGS ON THE NUMBER ONE ENGINE T-TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2)

BDL - FLT 4015 - THE CREW REPORTED A LAVATORY SMOKE INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO BDL WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED AIRCRAFT IAW MEL 36-11-05. UPON ARRIVAL IN CLEVELAND, MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 2 ENGINE DUE TO AN INTERNAL OIL LEAK (CARBO SEAL) IAW CONTINENTAL EXPRESS GENERAL MM TASK CARD 6271001. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)