N12934

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 33,210 hrs · 32,434 cycles

DURING MAINTENANCE INSPECTION, LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. R & R FUSE ON POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 31,750 hrs · 31,019 cycles

DURING 4A INSPECTION THE NR 3 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,024 hrs · 30,287 cycles

THE CREW REPORTED THAT THE LT AND RT EXTERNAL OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CRACKED (LT WING) · airframe 30,477 hrs · 29,738 cycles

CRACK AT CENTER HINGE POINT OF LT WING GROUND SPOILER ON WING. DRILLED OUT DAMAGED HOLE, PERFORMED EDDY CURRENT INSPECTION OF HOLE, PERFORMED ROTO PEENING ON THE INNER AND OUTER AREAS OF SPAR 3 AROUND DRILL HOLE, FABRICATED A PLUG FOR DRILLED HOLE IN SPAR 3, FABRICATED FILLER, DOUBLER, AND TRIPLER. PRIMED AND PAINTED ALL FABRICATED PARTS AND INSTALLED WET. RESTORED REPAIRED AREA TO ORIGINAL FINISH.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,477 hrs · 29,738 cycles

DENT AFT OF PAX DOOR BETWEEN FRAME 18 & 20 AND STRINGERS 13 & 15L. CUT OUT CREASED AREA, FABRICATED DOUBLER & FILLER AND INSTALLED.

Part: BULB — FAILED (CABIN LIGHTS) · airframe 30,042 hrs · 29,308 cycles

THE CREW REPORTED A BURNING ODOR IN THE CABIN FROM THE SIDEWALL LIGHTS IN ROW 3 & 4. R & R LIGHT BULB AT SEAT 3BC, OPS TESTED WITH NO DEFECTS, ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 30,003 hrs · 29,266 cycles

DURING C INSPECTION, THE NR 2 ENGINE FORWARD LOWER ENGINE MOUNT YOKE LINKAGE WAS FOUND TO BE CRACKED IN THE INNER RADIUS. CRACK STOP DRILLED.

Part: SKIN — CRACKED (ZONE 500) · airframe 30,003 hrs · 29,266 cycles

DURING A INSPECTION, LT WING SKIN AT THE CENTER HINGE POINT FOR THE GROUND SPOILER WAS FOUND TO BE CRACKED. MX STOP DRILED THE CRACK. MX INSTALLED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5710-01193, ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 30,013 hrs · 29,277 cycles

DURING A-CHECK INSPECTION, SERVICE DOOR EMERGENCY LIGHT SOCKET WAS FOUND TO BE NOT ALLOWING LIGHT BULB TO BE LOCKED IN PLACE. MX R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 2) · airframe 28,894 hrs · 28,175 cycles

DURING APPROACH, THE CREW REPORTED SMOKE IN THE CABIN. THE ACFT LANDED WITHOUT INCIDENT WHERE THE NR 2 AIR CYCLE MACHINE WAS REPLACED, OPERATIONAL CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,019 hrs · 26,251 cycles

IAH - FLIGHT 2330 THE CREW REPORTED AN EXTREMELY STRONG FUEL SMELL IN THE COCKPIT DURING ROTATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN WITH NO FUEL SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MANIFOLD — LEAKING (APU FUEL) · airframe 27,023 hrs · 26,256 cycles

IAH - FLIGHT 2976, THE CREW REPORTED A FUEL ODOR IN THE CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE SECONDARY APU FUEL MANIFOLD, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 26,354 hrs · 25,561 cycles

IAH - FLIGHT 2645, THE CREW REPORTED A BATTERY TWO OVERTEMP IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,113 hrs · 24,297 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE OVERWING CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 13,232 hrs · 7,446 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE OVERWING CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,008 hrs · 24,190 cycles

IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED AN OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,671 hrs · 24,529 cycles

EXIT AISLE AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,896 hrs · 22,985 cycles

SECOND AND THIRD FROM FWD FLOOR PROX LIGHT INOP. REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD, AIRCRAFT STILL IN C-CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,896 hrs · 22,985 cycles

CRACK AND WORKING RIVETS AT FRM 75 STR 1R & 2R AND 1L & 2L. REPAIRED RT SKIN HOLE IAW SRM 53-31-01. REPAIRED LT SKIN HOLES WITH CUTOUTS AND ONE LARGE EXTERNAL DOUBLER IAW SRM 51 & 53. PRIMED AND PAINTED REPAIRED AREA. REFERENCES EC5330-01913, EMB SRM 53-31-01 & CPM51-21-05, 06. AIRCRAFT STILL IN C-CHECK.

Part: BUSHING — MIGRATED (SPOILER) · airframe 23,896 hrs · 22,985 cycles

RT GROUND SPOILER ACTUATOR UPPER ATTACH FITTING HAS MIGRATED BUSHING. REMOVED AND REPLACED HAT BUSHING IAW EC 5740-01152. AIRCRAFT STILL IN C CHECK.

Part: BUSHING — MIGRATED (SPEED BRAKE) · airframe 23,896 hrs · 22,985 cycles

MIGRATED HAT BUSHING ON LT WING SPEED BRAKE ACTUATOR. REMOVED AND REPLACED HAT BUSHING IAW EC5740-01152.

Part: FRAME — CRACKED (COCKPIT) · airframe 23,896 hrs · 22,895 cycles

TYS - DURING A CURRENT 6C INSPECTION, FOUND A CRACK IN THE COCKPIT AT FR 10L NEAR STR 10 AT THE UPPER END OF THE DV WINDOW CUTOUT. MAINTENANCE REMOVED THE FRAME AND REPAIRED THE FRAME IAW IC 2009-145/03148 AND INSTALL THE FRAME IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CRACKED (SPOILER) · airframe 23,896 hrs · 22,895 cycles

TYS - DURING A CURRENT 6C INSPECTION THE LT UPPER SKIN WAS FOUND CRACKED AT SPAR 3 GROUND SPOILER ACTUATOR ATTACH CUTOUT. MAINTENANCE BLENDED OUT THE CRACK AND PERFORM A NDI INSPECTION AND NO DEFECTS NOTED. A/C WILL BE RELEASED AT THE END OF THE CHECK. WORK WAS ACCOMPLISHED IAW EC 5740-01238.

Part: FRAME — CRACKED (COCKPIT) · airframe 23,896 hrs · 22,895 cycles

TYS - DURING A CURRENT 6C INSPECTION, FOUND A CRACK IN THE COCKPIT AT FR 10 AT THE UPPER END OF THE DV WINDOW CUTOUT. MAINTENANCE REMOVED THE FRAME AND REPAIRED THE FRAME IAW IC 2009-145/03148 AND INSTALL THE FRAME IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FRAME — CRACKED (COCKPIT) · airframe 23,896 hrs · 22,895 cycles

TYS - DURING A CURRENT 6C INSPECTION, FOUND A CRACK IN THE COCKPIT AT FR 10 NEAR STR 10 AT THE UPPER END OF THE DV WINDOW CUTOUT. MAINTENANCE REMOVED THE FRAME AND REPAIRED THE FRAME IAW IC 2009-145/03148 AND INSTALL THE FRAME IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: INLET — CORRODED (NR 2 ENGINE) · airframe 23,896 hrs · 22,985 cycles

TYS - DURING A CURRENT 6C INSPECTION THE NR 2 ENGINE INTAKE MOUNTING FLANGE WAS FOUND WITH SEVERAL BOLT HOLES PITTED AND CORRODED. MAINTENANCE REPAIRED 6 HOLES ON THE NR 2 ENGINE INLET IAW EC 5420-01158. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,896 hrs · 22,985 cycles

TYS - AIRCRAFT IS CURRENTLY IN A 6C INSPECTION. IT WAS FOUND THAT THE FUSELAGE WAS CRACKED AT THE LEFT UPPER CORNER OF THE PILOT WINDSHIELD CUTOUT. MAINTENANCE REPAIRED THE AREA IAW EC 5330-01909 AND IC 2009 -145/02892. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: HOUSING — CORRODED (VERTICAL STAB) · airframe 23,896 hrs · 22,985 cycles

BOTH SPHERICAL BEARING HOUSING'S ON VERTICAL STAB HAVE CORROSION. REAMED HOUSING AND INSTALLED NEW BUSHINGS IAW EMB AMM 55-30-02 AND COMPLIED WITH DIHEDRAL & INCIDENCE CHECKS IAW EMB 145 AMM 51-50-01. AIRCRAFT STILL IN C CHECK.

Part: FITTING — CHAFED (VERTICAL STAB) · airframe 23,896 hrs · 22,985 cycles

FRAME 75 FRETTING AT VERTICAL STAB FITTING. REMOVED FITTING CLEANED AREA AND DYE PEN INSPECTED, NO DEFECTS NOTED AND RE-INSTALLED FITTING IAW EC5310-01317. AIRCRAFT STILL IN C-CHECK.

Part: YOKE — CRACKED (NR 1 NACELLE) · airframe 23,896 hrs · 22,985 cycles

TYS - DURING C-CHECK THE NR 1 ENGINE FWD LOWER YOKE WAS FOUND CRACKED AT THE FWD ATTACH POINT. A DYE PEN TEST WAS PERFORMED IAW EMB NDT PTO 1 AND PTO 2 AND THE CRACK WAS CONFIRMED. THE NR 1 ENG FWD LOWER YOKE INNER PIECE WAS REMOVED AND REPLACED IAW EMB 145 SRM 51-40-02 & EC 5450-01020.

Part: BRACKET — DAMAGED (LT AILERON) · airframe 23,896 hrs · 22,985 cycles

TYS - DURING C-CHECK INSPECTION THE LT AILERON PCA BRACKET OUTBOARD FITTING WAS FOUND DAMAGED/ELONGATED. THE PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-0117 AND SRM 57-60-02. A/C STILL IN C-CHECK.

Part: RESOLVER — INTERMITTENT (NR 2 THROTTLE) · airframe 23,373 hrs · 22,445 cycles

FLIGHT 2070 - IAH-BRO - ON APPROACH INTO BRO THE CREW REPORTED THAT THE "E2 TLA FAIL" MESSAGE ILLUMINATED AND THE NR 2 ENGINE REMAINED AT SET THROTTLE UNTIL THE FADEC CIRCUIT BREAKER WAS RESET PER THE COCKPIT QRH. THE AIRCRAFT DIVERTED TO HRL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FAULTY NR 2 THROTTLE LEVEL THRUST RESOLVER.

Part: BATTERY — OVERTEMP (MASTER) · airframe 22,706 hrs · 21,750 cycles

LCH - FLIGHT 2830, THE CREW REPORTED A BATTERY 2 OVERTEMP WARNING ON EICAS. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: SKIN — CRACKED (RT WING) · airframe 22,058 hrs · 21,124 cycles

WING SKIN CRACK ON RIGHT WING AT I/B SPOILER CENTER HINGE CUTOUT. REPAIRED CRACK IAW IC 2008-145/02561. AIRCRAFT RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 21,579 hrs · 20,638 cycles

IAH - FLIGHT 2191, THE CREW REPORTED THAT THE AIRCRAFT VEERD SHARP LEFT, AND RECEIVED A RUDDER 1&2 INOP EICAS MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RUDDER 1&2 PRESSURE SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,076 hrs · 20,098 cycles

SERVICE ROUTINE EMERGENCY LIGHT AT PANELS 194 AND 195 INOP. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY CHASSIS ASSEMBLY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,076 hrs · 20,098 cycles

DURING SERVICE ROUTINE EMERGENCY LIGHT IN GALLEY AND FLOOR (1-3) INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY (SVC DOOR) IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 20,862 hrs · 19,865 cycles

DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,796 hrs · 19,793 cycles

FLIGHT 2248 - EWR - CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 6 IAW EMB 145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 19,721 hrs · 18,678 cycles

IAH - FLIGHT 2703 THE CREW REPORTED A LAV SMOKE WARNING ON ROTATION WITH A STRONG SMOKE SMELL BUT NO VISUAL INDICATION OF SMOKE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — INOPERATIVE (APU BAY) · airframe 19,719 hrs · 18,676 cycles

DFW - FLIGHT 2811, THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CTL 117353, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT CAME TO IAH ON 03/09/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 19,706 hrs · 18,660 cycles

IAH - FLIGHT 2984, THE CREW REPORTED SMOKE IN THE CABIN DURING FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CTL NUMBER 116866, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. FLIGHT 2272 OUT OF IAH THE CREW REPORTED A SMOKE SMELL AND LAV SMOKE INDICATION, THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE APU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED. THE MEL WAS REMOVED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 19,566 hrs · 18,490 cycles

IAH - FLIGHT 2036, THE CREW REPORTED AN INTERMITTENT LAV SMOKE WARNING ON THE EICAS ONE TIME DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 16,924 hrs · 15,427 cycles

ORD FLIGHT 2243 THE CREW REPORTED A ELECTRICAL/SMOKE SMELL IN THE CABIN DURING CLIMB.THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ROW 1A,2A CABIN LIGHTS TO HAVE ELECTRICAL SMOKE ODOR.THE BULBS WERE REMOVED AND THE A/C WAS RELEASED I/A/W MEL 33-20-00/-1.SUPPLEMENT TO FOLLOW. MAINTENANCE INSPECTED AND FOUND CONNECTOR ON LAMP FIXTURE OVER SEAT 2A LOOSE. RESECURED AND RELAMPED.OPERATIONAL CHECKS WERE GOOD.

Part: PRESSURE SWITCH — CRACKED (HYD SYSTEM)

ROC - FLIGHT NR 2040, THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY IN FLIGHT. REPORTED LOSS OF ALL NR 1 HYDRAULIC FLUID IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE SUPPLY PRESSURE SWITCH. ALSO, REPLACED THE NR 1 HYDRAULIC PUMP AND FILTER.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 16,748 hrs · 15,233 cycles

CREW REPORTED, EMERGENCY LIGHT WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES IAW EMB145 AMM NR 33-50-04, OPS CHECKED GOOD.

Part: WIRE HARNESS — SHORTED (NLG UPLOCK) · airframe 16,501 hrs · 14,957 cycles

CREW REPORTED LANDING GEAR INDICATOR NR 2 C/B POPPED. MX INSP AND REPLACED NOSE GEAR UPLOCK BOX 2 HARNESS. OPS CHECKS GOOD.

Part: LIGHT — DETACHED (LANDING GEAR) · airframe 16,396 hrs · 14,835 cycles

IAH - FLIGHT 3205, DURING DESCENT THE CREW REPORTED LOUD NOISES WHILE EXTENDING THE GEAR. THE CREW HAD THREE GREEN GEAR INDICATIONS, PERFORMED AN EMERGENCY DESCENT AND A FLY-BY WHICH VERIFIED THE GEAR TO BE DOWN AND LOCKED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND UPPER TAXI LIGHT TO BE DETACHED FROM THE GEAR. MAINTENANCE REMOVED AND REPLACED THE TAXI LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 15,504 hrs · 13,692 cycles

CRP - DURING MAINTENANCE INSPECTION, THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION CORRODED AT FRAME 20. REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING VISUAL INSPECTION AT C-CHECK THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WERE CORRORDED. REPAIRED OMEGA BEAM USING DOUBLER REPAIR IAW 53-22-10. AIRCRAFT RETURNED TO SERVICE.

Part: TORQUE BOX — CRACKED (RT WING) · airframe 15,431 hrs · 13,595 cycles

DURING C-CHECK EDDY CURRENT INSPECTION OF THE RIGHT WING INBOARD TORQUE BOX INDICATED A CRACK AT THE FORWARD TWO HI-LOK POSITION. REAMED THE AFFECTED HI-LOK HOLES TO THE NEXT OVERSIZE IAW EMB SRM 51-40-04. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING INSPECTION THE LEFT OMEGA BEAM FOUND TO BE CORRODED AT FRAME 19A-23. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING INSPECTION THE LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 15,431 hrs · 13,595 cycles

DURING INSPECTION THE LAST THREE AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY IAW 33-50-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING VISUAL INSPECTION AT C-CHECK LT OMEGA BEAM AT FRAME 38 WAS CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01157 AND SRM 53-21-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE DEFECTIVE BEAM IAW SRM 51-40-02.

Part: ACTUATOR — BYPASSING (LT SPOILERS) · airframe 15,186 hrs · 13,337 cycles

BTV LOG SQUAWK LEFT SPOILER REMAINED OPEN IN FLIGHT AFTER SPEED BRAKE LEVER WAS RETURNED TO CLOSE POSITION. THIS LEAD TO UNCOMMANDED LEFT ROLL OF AIRCRAFT ALONG WITH SPOILER FAIL MESSAGE. REMOVED AND REPLACED LEFT SPEED BRAKE ACTUATOR IAW EMB MM 27-62-02. OPS CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT)

CREW REPORTED, ODOR OF WIRE INSULATION BURNING IN COCKPIT AND FLIGHT ATTENDANT JUMPSEAT, ALONG WITH CABIN AND CABIN EMERGENCY PUSHBUTTONS ILLUMINATING. MAINTENANCE FOUND EMERGENCY BATTERY NR 2 NOT INSTALLED CORRECTLY. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY, POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK SENSOR — FAULTY (NLG)

CLE FLIGHT 2104 THE CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT AFTER TAKEOFF. THE GEAR WAS CYCLED AND OPERATED NORMALLY THE 2ND TIME. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK BOX AND THE PROXIMITY SWITCHES ON THE UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. P/N PROXIMITY SWITCHES 8-527-01, S/N A22621 AND 4922.

Part: CHARGER — FAULTY (CABIN)

CLE FLIGHT NR 2158 THE CREW REPORTED A BURNING ODOR COMING FROM THE FORWARD CABIN FLASHLIGHT CHARGING BRACKET. MAINTENANCE INSPECTED AND REPLACED THE FORWARD F/A FLASHLIGHT BASE. OPERATIONAL CHECKS WERE GOOD.

Part: PRESSURE SWITCH — LEAKING (FUSELAGE)

CLE FLIGHT 2779 THE CREW REPORTED A NR 2 HYDRAULIC LOW FLUID MESSAGE IN FLIGHT. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 BRAKE PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: ECU — FAULTY (MLG)

CLE FLIGHT NR 2268) THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER LIFTOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND THE NOSE GEAR WOW PROXIMITY SWITCH HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: SELECTOR — INOPERATIVE (MLG)

CLE FLIGHT 3014 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT UNLESS THE DOWNLOCK RELEASE BUTTON WAS PRESSED. MAINTENANCE REPLACED THE LANDING GEAR LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE CREW RECYCLED THE GEAR AND AFTER 1 MINUTE THE MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 11,454 hrs · 9,457 cycles

EWR---CO3537, CREW REPORTED, AIR GROUND SENSOR FAILED AFTER TAKEOFF. AIR RETURN TO EWR. MAINTENANCE TROUBLESHOT PROBLEM, REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB145 AMM 32-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 11,270 hrs · 9,290 cycles

TYS AIR RETURN, PILOT REPORTED AHRS DISPLAYED ERRONEOUS HEADING. MAINTENANCE OPERATIONAL CHECKED AHRS SYSTEM IAW-EMB-145-MM-34-21-00-700-801A, ALL SYSTEMS OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,261 hrs · 9,281 cycles

TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM JUST FORWARD OF STATION 20793.0 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-145 SRM 51-40-02, 53-24-10, 51-20-03, 53-24-02 AND 51-40-01. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,261 hrs · 9,281 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DOUBLER — CORRODED (FAIRING 191) · airframe 11,261 hrs · 9,281 cycles

TYS During a scheduled inspection corrosion was found on fairing 191 leading edge doublers. Maintenance removed and replaced the leading edge doublers IAW EMB-145 SRM 51-10-02, 51-20-03,04, 05 and 06. The repair was satisfactory, the aircraft will be released upon completion of inspection.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT)

CLE FLIGHT 3234 THE CREW REPORTED A APU FIRE WARNING IN FLIGHT AFTER START. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE WAS EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED APU AND FOUND NO EVIDENCE OF FIRE OR NO DEFECTS. THE APU WAS OPERATIONALLY CHECKED AND NO DEFECTS WERE FOUND. THE FIRE BOTTLE WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — FAULTY (A/C BAY)

CLE - FLIGHT 4378, THE CREW REPORTED A STRONG SMOKE SMELL WHEN OPERATING ONLY PACK ONE ON THE GROUND. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AIR CYCLE MACHINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED PIN IN ACCORDANCE WITH EMB145 MM 55-10-00-400-801-A AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (HORIZONTAL STAB)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER TO VERTICAL STABILIZER OUTBOARD BUSHING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED BUSHING, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (VERTICAL STAB)

DURING C-CHECK INSPECTION, RT HORIZONTAL STABILIZER TO VERTICAL STABILIZER OUTBOARD BUSHING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED BUSHING AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — CORRODED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED BEARING IN ACCORDANCE WITH EMB145 MM55-37-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — CORRODED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND VERTICAL STABILIZER SHERICAL BEARING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED BEARING IN ACCORDANCE WITH EMB145 MM 55-37-00-400-801-A AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE)

REFERENCE OPEN SDR C2XAOOIA384 IAH-DURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT. MX PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01144, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (VERTICAL STAB)

DURING C-CHECK INSPECTION THE LEFT HAND SKIN ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. THIS SDR FILED OPEN AWAITING FINAL CORRECTIVE ACTION.(CLOSED BY C2XA00IA394)

Part: SKIN — CRACKED (VERT STAB)

REFERENCE OPEN SDR C2XAOOIA383 DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABLILIZER WAS FOUND TO BE CRACKED. MX PERFORMED AN INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANMGE EC5530-01045, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE)

DURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT.

Part: FRAME — DAMAGED (FUSELAGE)

REFERENCE OPEN SDR C2XA00IA384 DURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT. MX PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-001144, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (VERTICAL STAB)

REFERENCE OPER SDR C2XA00IA383-DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABILIZER WAS FOUND TO BE CRACKED. MX PERFORMED INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING EC5530-01045, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,431 hrs · 13,595 cycles

DURING VISUAL INSPECTION AT C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRORDED BETWEEN FRAMES 24 AND 25. REPAIRED THE OMEGA BEAM USING A DOUBLER REPAIR IAW 53-22-10.

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPROT. MAINTENANCE REMOVED THE CORROSION, AND INSTALLED A REPAIRE DOUBLER ON THE FLOORBEAM. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, A SECTION OF AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. THE AIRCRAFT WAS RELEASED ON MEL 33-50-002 CONTROL NUMBER 212062. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 4267 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB-145 MM 33-50-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: ENGINE — FAILED (LEFT)

AFTER LANDING IN YUL, REPORTED NR 1 ENGINE HIGH ITT AND ENGINE AUTO SHUTDOWN. MAINTENANCE TROUBLESHOT ENGINE FOUND NO DEFECTS WITH BOROSCOPE AND POWER ASSURANCE RAN ENGINE WITHIN LIMITS. MAINTENANCE FERRIED AIRCRAFT TO BTV AND PERFORMED ENGINE CHANGE. OPS CHECKED ENGINE GOOD. (M)

Part: FLOORBEAM — CORRODED (FRAME 20)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPORT. MAINTENANCE REMOVED THE CORROSION, AND INSTALLED A REPAIR DOUBLER ON THE FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01101. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND THE NR 1 CABIN FLOOR EMERGENCY LIGHTS STRIP TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FRAME 20)

IAH - DURING C-CHECK INSPECTION, FOUND THE CENTER FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPORT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRCKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF THE DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL MOD — INOPERATIVE (COCKPIT)

BURNING SMELL IN FORWARD HALF OF CABIN WHENEVER LIGHTS ARE ON. EMERGENCY LIGHTS ARE ON WHEN COCKPIT SWITCH IS IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT CONTROL MODULE, OPS CHECKED GOOD. (M)

Part: BRAKE — LOCKED UP (LT MLG)

EWR - FLIGHT 4111 - CREW REPORTED THAT DURING TAXI, SMOKE WAS SEEN COMING FROM THE LEFT MAIN LANDING GEAR AREA, AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE LEFT MAIN LANDING GEAR, THEN REMOVED AND REPLACED THE NR 2 BRAKE ASSEMBLY IAW EMB-145 MM 32-49-03. OPERATIONAL AND LEAK CHECK WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

CLE - DURING A SCHEDULED INPSECTION, THE LEFT HAND ENGINE OIL PRESSURE EXCEEDED MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. (X)

Part: ENGINE — FAILED (RIGHT)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE OIL PRESSURE EXCEEDED MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)