N12946

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 31,335 hrs · 30,461 cycles

DURING CREW INSPECTION, IT WAS REPORTED THAT NOT ALL CABIN EMERGENCY LIGHTS WERE ILLUMINATING WITH THE BUTTON. MAINTENANCE INSPECTED THE ACFT AND FOUND A LOOSE CONNECTOR ABOVE THE GALLEY CEILING. MAINTENANCE SECURED THE AFFECTED CONNECTOR, OPS TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,846 hrs · 28,997 cycles

LT FLOOR SUPPORT AT FRAME 24 AND 25 HAS CORROSION BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,360 hrs · 28,499 cycles

DURING A-CHECK INSP THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR75 STRINGER 01 LT. MX PERFORMED A DOUBLER REPAIR AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 293,603 hrs · 28,499 cycles

DURING A-CHECK INSPECTION THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FRAME 75 STRINGER 02 RT. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 12/03/2012.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,360 hrs · 28,499 cycles

DURING A-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AFT OF A RIVET AT FRAME 75 STRINGER 01 LT. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,306 hrs · 28,499 cycles

DURING A-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR 75 STRINGER 2 RT. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 26,749 hrs · 25,934 cycles

IAH - FLIGHT 2117 THE CREW REPORTED THAT AFTER SELECTING GEAR UP RECEIVED A LG/LEVER DISAGREE EICAS WARNING FOR THE LEFT MAIN LANDING GEAR. THE CREW RAN THE QRH, CYCLED THE GEAR WITH THE SAME RESULTS, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HYDRAULIC LINE — LEAKING (RT WING) · airframe 26,615 hrs · 25,799 cycles

IAH - FLIGHT 2464, THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED A HYD SYS 1 FAIL MESSAGE FOLLOWED BY ASSOCIATED AIL SYS INOP, EICAS MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED THE RIGHT AILERON SYSTEM PRESSURE LINE IN FRONT OF THE RIGHT O/B FLAP, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — DEFECTIVE (NR 1 ENGINE) · airframe 25,559 hrs · 24,715 cycles

SHV - FLIGHT NUMBER 4921 FROM LFT TO SHV WITH TAKEOFF THRUST ON TAKEOFF ROLL ENGINE NR 1 FIRE DET FAIL MESSAGE PRESENTED ON EICAS. NO OTHER INDICATIONS AND MESSAGE WENT AWAY WITH THROTTLE REDUCTION. MAINTENANCE VISUALLY INSPECTED FIRE LOOP AND VISUALLY INSPECTED ENGINE NR 1 FOR EVIDENCE OF FIRE; NO EVIDENCE NOTED. AIRCRAFT WAS THEN RELEASED FOR FERRY FLIGHT FROM LFT TO SHV FOR FURTHER MAINTENANCE. MAINTENANCE IN SHV REMOVED AND REPLACED ENGINE 1 FIRE DETECTOR IAW EMB-145 AMM 26-11-01, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — INOPERATIVE (NLG) · airframe 25,266 hrs · 24,410 cycles

IAH - FLIGHT 2214 THE CREW REPORTED A LOUD NOISE FROM THE NOSE WHEEL SECTION OF THE AIRCRAFT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE, AND CHECK VALVE ASSEMBLY OPERATIONALLY TESTED WITH NO DEFECTS, TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (NLG)

IAH - FLIGHT 2214 THE CREW REPORTED A LOUD NOISE FROM THE NOSE WHEEL SECTION OF THE AIRCRAFT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE, AND CHECK VALVE ASSEMBLY OPERATIONALLY TESTED WITH NO DEFECTS, TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 25,259 hrs · 24,403 cycles

HRL - FLIGHT 2634, THE CREW REPORTED THAT THE NOSE GEAR DOORS OPENED IN FLIGHT. THE AIRCRAFT RETURNED TO HRL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND APPROVED A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (AILERON) · airframe 24,871 hrs · 24,005 cycles

TYS - A/C WAS IN C-CHECK AND INSPECTION FOUND A HAT BUSHING FIT LOOSELY ON A PCA BRACKET ON LT AILERON. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW E5750--01177. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK.

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,872 hrs · 24,006 cycles

FUSELAGE SKIN GOUGED IN TWO PLACES INSIDE PYLON ACCESS 414DB. CUT OUT GOUGES FABRICATED AND INSTALLED A FILLER AND A CIRCULAR DOUBLER IAW EC5330-02219. AIRCRAFT RELEASED FROM C-CHECK AND RETURNED TO SERVICE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 24,891 hrs · 24,026 cycles

TYS - LOWER SKIN CORRODED BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 19R AND 21L. REMOVED DAMAGED SECTION OF SKIN AT FRAMES 13 TO 24 AND STRINGERS 18R AND 19L. DRILLED, COUNTERSUNK, AND FITTED NEW SKIN PANEL. INSTALLED NEW SKIN FRAMES 13 TO 24 AND STRINGERS 18R TO 19L, ALODINED, PRIMED, AND PAINTED IAW EC 5330-02218. PLACED ON DMI FOR A GVI OF REPAIRED AREA EVERY 5000 FLIGHT CYCLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,872 hrs · 24,006 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD.

Part: MOUNT — CRACKED (NACELLE) · airframe 24,871 hrs · 24,005 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 1 ENGINE LOWER YOLK MOUNT CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK IAW EC5440-01028. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: MOUNT — CRACKED (NACELLE) · airframe 24,871 hrs · 24,005 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 2 FWD LOWER YOLK CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK IAW EC5450-01028. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: HINGE FITTING — WORN (SPEED BRAKE) · airframe 24,871 hrs · 24,005 cycles

RIGHT WING SPAR 3 SPEED BRAKE CENTER HINGE FITTING HAS ELONGATED BUSHING HOLES. REMOVED AND REPLACED BRACKET IAW EMB 145 SRM 51-40-02.

Part: LEVER — DEFECTIVE (COCKPIT) · airframe 24,131 hrs · 23,250 cycles

IAH - FLIGHT 2709, THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE ON CLIMBOUT. THE AIRCRAFT LANDED AT ISH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PCU — LEAKING (RUDDER) · airframe 23,982 hrs · 23,100 cycles

PILOT REPORTED NR 2 HYDRAULIC LOW QUANTITY ON EICAS ON GROUND IN MSY. MAINTENANCE INSPECTED AND FOUND RUDDER POWER CONTROL UNIT TO BE LEAKING. REMOVED AND REPLACED RUDDER PCU IAW EMB 145 MM 27-22-03. OPERATIONALLY CHECKED AND LEAKED CHECKED GOOD. SERVICED NR 2 HYDRAULIC SYSTEM IAW EMB 145 AMM 12-13-01. AIRCRAFT RETURNED TO SERVICE. RUDDER PCU MISSING BOLTS CAUSING LEAKAGE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 23,778 hrs · 22,890 cycles

OKC - FLIGHT 2204, THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT DOWN LOCK PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 23,772 hrs · 22,885 cycles

IAH - FLIGHT 2748, THE CREW REPORTED A BLEED ONE LOW TEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE HIGH STAGE VALVE, OPERATIONALLY AND LEAK TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN) · airframe 23,494 hrs · 22,586 cycles

JAN - FLIGHT 2833, DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG ELECTRICAL SMELL COMING FROM THE GALLEY COFFEEMAKER. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION THROUGH THE CABIN AND COCKPIT AND FOUND THE CEILING LIGHT AT ROW 5-6 TO HAVE A BURNED ELECTRICAL CONNECTOR. MAINTENANCE DEACTIVATED THE LIGHT, REMOVED THE BULB, AND PLACED THE LIGHT ON MEL 33-20-00/1, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE ELECTRICAL HARNESS AT ROW 5, REPLACED THE BULB, OPERATIONALLY TESTED WITH NO DEFECTS. THE MEL WAS REMOVED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (NR 2 BLEED SYS) · airframe 22,679 hrs · 21,712 cycles

CREW REPORTED A BLEED 2 LEAK IN CLIMB. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR 2 ENGINE BLEED VALVE. OPS AND LEAK CHECKS REVEALED NO DISCREPANCIES, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — FAILED (NR 2 BLEED SYS) · airframe 22,679 hrs · 21,712 cycles

CREW REPORTED A BLEED 2 LEAK IN CLIMB. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR 2 ENGINE BLEED VALVE. OPS AND LEAK CHECKS REVEALED NO DISCREPANCIES, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (NR 2 BLEED) · airframe 22,679 hrs · 21,712 cycles

CREW REPORTED A BLEED 2 LEAK IN CLIMB. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR 2 ENGINE BLEED VALVE. OPS AND LEAK CHECKS REVEALED NO DISCREPANCIES, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POTENTIOMETER — FAULTY (NLG STEERING) · airframe 22,454 hrs · 21,460 cycles

FLIGHT NR 2941, THE CREW REPORTED ON TAKEOFF ROLL, THE ACFT JOLTED TO THE RT AND THEY RECEIVED A STEER INOP MESSAGE ON THE ECIAS. THE TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO THE GATE. MX INSPECTED AND REPLACED THE NOSE GEAR STEERING FEEDBACK POTENTIOMETER. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,213 hrs · 19,206 cycles

DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.

Part: FUEL CONTROL — LEAKING (APU) · airframe 19,134 hrs · 18,094 cycles

CLE FLIGHT 2912 - THE CREW REPORTED A FUEL ODOR WHEN APU BLEED WAS SELECTED. MAINTENANCE REPLACED THE APU FUEL CONTROL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: SELECTOR — FAULTY (COCKPIT) · airframe 18,865 hrs · 17,825 cycles

CLE FLIGHT NR 2092 - THE CREW REPORTED A LANDING GEAR AURAL WARNING AT 8,OOO FT. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR HANDLE. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,942 hrs · 16,845 cycles

DURING ROUTINE MAINTENANCE, THE LEFT EMERGENCY EXIT MARKER SIGN WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL UNIT — INTERMITTENT (WARNING SYSTEM) · airframe 17,345 hrs · 16,211 cycles

CLE FLIGHT 2408 CREW REPORTED AN INADVERTENT LANDING GEAR AURAL WARNING AT 7000 FT WHEN POWER REDUCED TO IDLE. A/C IN CLEAN CONFIGURATION. LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE AURAL WARNING UNIT. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,459 hrs · 15,148 cycles

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

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,382 hrs · 15,052 cycles

IAH - DURING MAINTENANCE INSPECTION, THE NUMBER TWO AND THREE AISLE PATH LIGHTING STRIPS AND THE AFT GALLEY EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 16,370 hrs · 15,039 cycles

OKC - FLIGHT 2378, THE CREW REPORTED SMOKE IN THE COCKPIT FROM THE CAPTAINS WINDSHIELD WHEN THE WINDSHIELD HEAT WAS SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATION CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (FUSELAGE) · airframe 15,774 hrs · 14,326 cycles

SHV - DURING C-CHECK AFT SURFACE OF FR 81 IS CHAFED IN MUTIPLE LOCATION ON LOWER EDGE. MAINTENANCE REPAIRED AFT SURFACED OF FR 81 ON LOWER EDGE IAW EMB 145 EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,774 hrs · 14,326 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM AT FR 45 HAS CORROSION. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 45 IAW EC5320-01276. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,774 hrs · 14,326 cycles

SHV - DURING C-CHECK, THE CENTER OMEGA BEAM HAS CORROSION AT FR 45. MAINTENANCE REPAIRED CENTER OMEGA BEAM @ FR 45 IAW EC5320-01276. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CONTROL UNIT — FAULTY (MLG) · airframe 15,286 hrs · 13,794 cycles

CLE - FLIGHT NR 2623, THE CREW REPORTED A AIR/GROUND FAIL MESSAGE WHEN THE LANDING GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,701 hrs · 13,158 cycles

CLE - THE CREW REPORTED THE EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AND THE OPERATIONAL TESTS WERE GOOD.

Part: SIGN — MALFUNCTIONED (EMERGENCY EXIT) · airframe 14,600 hrs · 13,050 cycles

BTV - MX DURING CABIN INTERIOR CHECK EMERGENCY EXIT SIGN AT 12A INOP. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING IAW EMB-145 MM 33-50-00. NO FAULT FOUND.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 14,539 hrs · 12,981 cycles

CLE - THE CREW REPORTED, LOST ALL PRESSURIZATION WHILE CRUISING AT 22,000 FT. THE CREW MADE AN EMERGENCY DESCENT. THE CREW WAS ABLE TO REGAIN CONTROL OF PRESSURIZATION USING MANUAL CONTROL, AND LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PNEUMATIC OUTFLOW VALVE. A SATISFACTORY TEST FLIGHT WAS PERFORMED AND THE ACFT WAS RELEASED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (MLG) · airframe 13,663 hrs · 11,926 cycles

IAH - FLIGHT 2830, THE CREW REPORTED AN AIR/GROUND FAIL IN FLIGHT AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). OPERATIONALLY CHECKED WITH NO DEFECTS, ALL IAW EMB-145 AMM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 13,585 hrs · 11,821 cycles

LCH - FLIGHT 2705, ON DEPARTURE THE CREW REPORTED, RECEIVED AN AIR/GROUND FAILURE MESSAGE AND THE LANDING GEAR LEVER WAS STUCK IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED EXTENSION/RETRACTION CHECKS WITH NO DEFECTS NOTED, ALL IAW EMB-145 MM 32-32-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT SEAT 3B/C WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND FOUND THE ELECTRICAL CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED AND THE LIGHT OPERATIONALLY TESTED.

Part: LEVER — FAULTY (MLG) · airframe 12,096 hrs · 10,262 cycles

CREW REPORTED, AFTER TAKEOFF GEAR HANDLE WOULD NOT RETRACT. DOOR LOCK RELEASED LOUD NOISE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER IAW EMB145 AMM 32-32-02. GEAR SWING PERFORMED, NO FAULTS FOUND. OPS CHECKED GOOD IAW EMB145 AMM 32-32-00. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 11,851 hrs · 10,036 cycles

EWR---CO3256, CREW REPORTED (ON WALKAROUND), THAT THE EMERGENCY EXIT SIGN NEAR THE PASSENGER DOOR IS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE NEAR PASSENGER DOOR, REPAIRED BROKEN WIRE, AND OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: SEAT TRACK — CORRODED · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED 3C INSPECTION, SEAT TRACK RF3 IS CORRODED. MAINTENANCE REMOVED DAMAGED SEAT TRACK, CLEANED AREA, REINSTALLED SEAT TRACK, APPLIED CIC AND PLACED ON DMI FOR 200 FLIGHT CYCLES (REF M-602, 596609). WORK WAS IAW EMB 1C2003-145/2602 AND 53-10-06. A/C WAS REL UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IN THE GALLEY IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED 3C INSPECTION, THE LEFT HAND GALLEY FLOORBEAM WAS CORRODED AND PREVIOUS REPAIR WAS CORRODED. MAINTENANCE REMOVED THE OLD REPAIR, FAB FILLER AND ANGLE, ALODINED AND PRIMED NEW FAB PART. INSTALLED NEW PARTS IAW EMB 135/145 SRM 53-21-04, 05, 10 EMB 145 CPM 51-21-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 114,691 hrs · 9,668 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE CENTER FLOORBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION SEAT TRACK RF2 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW-EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION SEAT TRACK LW4 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK LF5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK LF3 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK RW4 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK RF1 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK LW6 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK LF4 WAS FOUND CORRODED. MAINTENANCE REMOVED THE TRACK, CLEANED THE CORROSION AND REINSTALLED IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK RF5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION, SEAT TRACK LF2 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK LW3 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK RW 5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS- DURING A SCHEDULED INSPECTION, SEAT TRACK LF6 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

DURING A SCHEDULED INSPECTION SEAT TRACK LW5 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EC5340-01048.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS- DURING A SCHEDULED 3C INSPECTION THE FOLLOWING SEAT TRACKS WERE FOUND CORRODED (RW1 THRU RW3 AND LW1 THRU LW2). MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EC 5340-01048 AND EMB 145 AMM53-01-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,469 hrs · 9,668 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT CENTER FLOORBEAM WAS FOUND CORRODED UNDER THE AFT WALL COMPOSIT FLOOR SUPPORT. MAINTENANCE REMOVED AND REPLACED THE CENTER LAV FLOORBEAM CAP. I/A/W-EMB-145-SRM-51-40-02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF THE INSPECTION.

Part: WIRE HARNESS — DEFECTIVE (MLG) · airframe 10,924 hrs · 9,121 cycles

EWR---CO2809, CREW REPORTED, LANDING / AIR GROUND FAILURE INFLIGHT AND ENGINE NR 1 & NR 2 THRUST REVERSER DISAGREEMENT INFLIGHT. DECLARED EMERGENCY AND LANDED IN EWR UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED NOSE GEAR AIR GROUND PROXIMITY SWITCH HARNESS, OPS CHECKED GOOD IAW EMB145 MM 32-65-05 AND EMB 145 MM 78-31-01. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — INOPERATIVE (NLG)

FLIGHT 3075, THE CREW NOTED THAT THE NOSE WHEEL WOULD NOT RETRACT, AIR RETURN TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — FALSE INDICATION (NLG) · airframe 9,342 hrs · 7,553 cycles

TYS AIRCRAFT WAS FERRIED INTO TYS DUE TO A GEAR RETRACTION INDICATION PROBLEM. MAINTENANCE CHANGED THE NOSE UPLOCK BOX AND ALL OPS CHECKS WERE GOOD IAW EMB AMM 32-33-07 AND FUNCTIONAL CHECK 32-41-00-700-801A, AND OPS CHECK WAS GOOD IAW AMM 32-30-00-700-801-A. ALL WORK WAS ACCOMPLISH AND WAS RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

IAH- MAINTENANCE NOTED THAT THE RIGHT FRONT EMERGENCY LIGHT FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — CORRODED (LT FUSELAGE)

DURING A ROUTINE MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMBRAER 145 MM 33-50-07. (M)

Part: BULB — FAILED (CABIN)

CLE - FLT 4169 - DURING PREFLIGHT INSPECTION, THE THIRD EMERGENCY CEILING 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: SKIN — DAMAGED (FUSELAGE)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT SKIN UNDER THE CAPTAINS SIDE WINDOW WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01112, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER LEFT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC-5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC-5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20 LEFT. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REPAIR DOUBLER IAW EMBRAER SCHEME STS1274/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SOCKET — INOPERATIVE (RT EMER EXIT)

BTV - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHTS NOT WORKING. MAINTENANCE CLEANED RT FORWARD OVERWING EMERGENCY LIGHT SOCKET AND OPS CHECKED SYSTEM GOOD. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EWR - FLT CO4130 - CREW REPORTS RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT ASSY. OPS CHECKED, EMERGENCY LIGHTS GOOD. (X)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

BTV - DURING 2A INSPECTION, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT OVER LEFT HAND WING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY OVER THYE LEFT HAND WING AND OPS CHECKED, SYSTEM GOOD. (X)

Part: AIR DIST — ODOR (CABIN)

CLE - FLT 4007 - CREW REPORTED THEY RECEIVED SMOKE IN THE COKPIT AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND FOUND THE SMOKE WAS CAUSED BY EXCESSIVE AMOUNTS OF DE-ICE FLUID IN THE APU COMPARTMENT. THE COMPARTMENT WAS CLEANED AND THE OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 21-00-06. AIRCRAFT RELEASED FOR SERVICE. (X)