N14514

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,632 hrs · 16,131 cycles

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT IAW 33-50-13. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,570 hrs · 14,634 cycles

DURING ROUTINE CHECK THE GALLEY EMERGENCY LIGHTS FAILED OPS TESTING. MX R & R THE NR 3 INVERTER IAW AMM 33-50-11. THE EMERGENCY LIGHTS OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 17,404 hrs · 14,429 cycles

DURING MX INSPECTION, THE EMERGENCY LIGHT EXIT LOCATING SIGN IN THE GALLEY AISLE CEILING PANEL WAS FOUND TO BE INOPERATIVE. MX INSPECTED THE SIGN, RECONNECTED THE ELECTRICAL CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — DISCONNECTED (CABIN) · airframe 17,138 hrs · 14,209 cycles

IAH - DURING MAINTENANCE INSPECTION LT EMERGENCY EXIT IDENTIFIER AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT, RESECURED THE CONNECTIONS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: WIRE — BROKEN (SERVICE DOOR) · airframe 273,184 hrs · 2,405,856 cycles

IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,982 hrs · 14,085 cycles

SHV - DURING C-CHECK LT OMEGA BEAM FR 21-23 HAS VARIOUS AREAS OF CORROSION ON LWR FLANGE WEB. MX REMOVED LT OMEGA BEAM FROM 17 SPLICE TO FR 26 AND INSTALLED WITH NEW IAW EC5320-01413 ANS CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,877 hrs

IAH - FLIGHT 2452, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LIGHT BALLAST AT ROW SIX. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: CONNECTOR — DIRTY (CABIN) · airframe 16,466 hrs · 13,687 cycles

IAH - FLIGHT 2791, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD SECTION OF AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,280 hrs · 12,765 cycles

DURING SCHEDULED MAINTENANCE THE EMERGENCY STRIP LIGHT AT ROW 3A TO 7A WAS FOUND TO BE INOPERATIVE. THE FLOOR STRIP WIRING WAS FOUND TO BE CHAFED. THE AFFECTED WIRE WAS REPAIRED, THE LIGHTS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,972 hrs · 12,817 cycles

IAH - FLIGHT 2890, DURING PRE-FLIGHT INSPECTION, THE NUMBER ONE ELECTRIC HYDRAULIC PUMP FAILED AND A SMOKE SMELL WAS REPORTED IN THE COCKPIT. MAINTENANCE OPERATIONALLY TESTED THE ELECTRIC HYDRAULIC PUMP WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE SMOKE SMELL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,278 hrs · 11,942 cycles

SLP - FLIGHT 2148, THE CREW REPORTED A BURNING ODOR AT THE COFFEEMAKERS. THE AIRCRAFT RETURNED TO SLP WHERE THE COFFEEMAKERS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2148 WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE THE DISCREPANCY. THE MEL WAS CLEARED, AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 12,718 hrs · 10,691 cycles

LEX - FLIGHT 2671, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER AN ACARS MESSAGE FOR PACK 2 VALVE CLOSED MESSAGE. THE AIRCRAFT DIVERTED TO LEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN) · airframe 12,275 hrs · 10,326 cycles

DURING START, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,170 hrs · 10,240 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (GALLEY) · airframe 9,863 hrs · 8,523 cycles

THE CREW REPORTED A BURNED/HOT ELECTRICAL ODOR COMING FROM THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST FOR THE GALLEY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (COCKPIT) · airframe 9,472 hrs · 8,206 cycles

THE CREW REPORTED THAT THE NR 3 PITOT INOPERATIVE WHILE CLIMBING THROUGH CLOUDS, AND THE COCKPIT FILLED WITH SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY (K0057) FOR THE NUMBER THREE PITOT PROBE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED AND TIMES ARE NOT AVAILABLE.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 8,345 hrs · 7,312 cycles

IAH- FLIGHT 2621, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,125 hrs · 7,137 cycles

IAH - DURING 3A INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 7,333 hrs · 6,477 cycles

AIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21-15, 72-50-00 AND EC7250-01018.

Part: SILL — CORRODED (CABIN) · airframe 7,255 hrs · 6,407 cycles

SHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 7,255 hrs · 6,407 cycles

SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 7,255 hrs · 6,407 cycles

SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 51-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED T-SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (CABIN) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE CARGO DOOR LOWER CUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CRACKED (CABIN) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 2 ENGINE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 1 ENGINE) · airframe 7,255 hrs · 6,407 cycles

SHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DISTORTED (LT MLG)

FLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MAIN LANDING GEAR PROXIMITY SWITCH MOUNT BRACKET TO BE DISTORTED. THE AFFECTED BRACKET WAS REMOVED AND REPLACED. THE LANDING GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (TAIL)

CLT FLIGHT#3177 THE CREW REPORTED A RUDDER 1/2 FAIL MESSAGE ON CLIMBOUT.THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 AND #2 RUDDER PRESSURE SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICES.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

CLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED AND PERFORMED AUTO PILOT CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (CABIN)

CLE FLIGHT#3133 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE EMERGENCY AISLE PATH LIGHTING STRIP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — CRACKED (NLG) · airframe 3,057 hrs · 2,639 cycles

TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 135MM 32-63-05. AIRCRAFT WAS RELEASED.

Part: PROXIMITY SWITCH — CRACKED (NLG) · airframe 3,057 hrs · 2,639 cycles

TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 135 MM 32-63-05. AIRCRAFT RETURNED TO SERVICE.

Part: ANTENNA — CORRODED (TCAS) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE LOWER TCAS ANTENNA WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE TCAS ANTENNA IAW EMB 135 AMM34-43-03, PERFORMED OPS CHECK IAW EMB 135AMM 34-43-00. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.

Part: RIVET — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION TWO RIVETS WERE FOUND CORRODED UNDERNEATH THE SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED THE TWO RIVETS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK INSPECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 3,057 hrs · 2,639 cycles

TYS, DURING A SCHEDULED 1C INSPECTION, THE NR 6 EMERGENCY TRACK LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE NR 6 TRACK LIGHTING IAW EMB-135-AMM-33-50-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF THE FORWARD DIGITAL. MAINTENANCE REMOVED FORWARD DIGITAL AND CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED, REINSTALLED DIGITAL IAW-EC5320-01059, EMB-135/145-SRM-51-20-03/51-40-02 & 06/51-21-04/05/06. REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: SWITCH — FAULTY · airframe 3,057 hrs · 2,639 cycles

TYS, During a scheduled 1C inspection, the oxygen deployement on step 13 of task card #35-20-00-770-001-A00 failed. Maintenance removed and replaced the altitude sensing switch. IAW-EMB-135-AMM-35-20-02, operational checked good. Aircraft will be released upon complection of the inspection.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS DETECTED ON CENTER SUPPORT RAMP NEXT TO THE CARBON FIBER CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AND REINSTALLED THE CARBON FIBER CROSSBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION.

Part: BYPASS JACKET — CORRODED (NR 1 ENGINE) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE NR 1 FANCASE TO BYPASS HAD CORROSION. MAINTENANCE CLEANED UP THE CORROSION. APPLIED CHEMICAL FILM COATING TO THE MAGNESIUM IAW RR AE3007A MM 70-00-00-300-818 AND APPLIED CORROSION RESISTANT PAINT IAW EC7220-01009. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.

airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE EMERG./PARKING BRAKE SYSTEM FAIL A OPS. CHECK. MAINTENANCE R/R THE #2 BRAKE CONTROL VALVE AND PERFORMED A LEAK AND OPS. CHECK.ALL WORK WAS ACCOMPLISHED IAW EMB 135 AMM 32-41-06 AND WILL BE REL. UPON COMPLETION OF THE C-CHECK INSPECTION.

Part: TUBE — DENTED (APU BAY) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE APU FIRE EXTINGUISHER DISCHARGE TUBE WAS FOUND DENTED NEXT TO THE FITTING AT APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE APU DISCHARGE TUBE IAW EMB 135AMM 20-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION.

Part: BRACE — GOUGED (LT MLG) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT MLG SIDE BRACE WING ATTACHMENT WAS FOUND SCRATCHED AND REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION.

Part: ATTACH FITTING — GOUGED (AILERON) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION, NOTED THAT THE LEFT AILERON FITTING WAS GOUGED. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK INSPECTION.

Part: BUSHING · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION,THE BOTTOM BUSHING ON THE PAX-DOOR HOLD OPEN ROD WAS FOUND TO BE MIGRATING. MAINTENANCE R/R THE BUSHING IAW GST-1682/01. THE GST STATED THAT THE BUSHION TO BE INSTALL FROM THE BOTTOM WITH A CORROSION INHIBITOR AND SEAL THE GAP WITH PR1440 B2. ALL THIS WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE RIGHT SILL AT FRM17 AROUND A NUT PLATE. MAINTENANCE REMOVED THE CORROSION IAW 135/145 CPM 51-14-02. THIS WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND AT THE LEFT OMEGA BEAM. MAINTENANCE CLEAN INSPECTED AND OVERSIZE ONE RIVET IAW EMB 135/145 SRM 51-10-02 AND 51-40-02. WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION.

Part: BRACE — GOUGED (LT MLG) · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT MLG SIDE BRACE WING ATTACHMENT WAS FOUND SCRATCHED AND GOUGED WHICH REQUIRED A GST. WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION.

Part: DOUBLER · airframe 3,057 hrs · 2,639 cycles

TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON DOUBLER AT FRM. 20 ON THE RIGHT SIDE.MAINTENANCE REMOVED THE CORROSION IAW 135/145 CPM 51-14-02 APPLIED ALLODINE ,PRIME AND PAINTED IAW EMB. 135/145 CPM 51-21-04,05,06. THE WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF 1-C INSPECTION.

Part: GUSSET — CORRODED · airframe 3,057 hrs · 2,639 cycles

TYS, During a scheduled 1C inspection, corrosion was found in several areas of the gusset, aft of the forward digital. Maintenance removed and replaced the gusset I.A.W.-EMB-135/145-SRM-51-40-02, The repair procedures where satisfactory and the aircraft will be released upon complection of inspection.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,057 hrs · 2,639 cycles

TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE CENTER TOP CAP AFT OF GUSSET. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-135/145-SRM-51-40-02. THE REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: MODULE — DEFECTIVE (CABIN)

CLE FLIGHT# 3574 THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON IN FLIGHT.THEY COULD ONLY BE TURNED OFF WITH THE COCKPIT SWITCH.CABIN SWITCH HAD NO CONTROL.MAINTENANCE REPLACED THE CABIN LIGHT CONTROL MODULE.OPERATIONAL CHECKS WERE GOOD.

Part: SEAL — LEAKING (LEFT ENGINE)

ICT FLT#4151 - CREW REPORTED A "PACK 2 FAIL" MESSAGE AFTER TAKEOFF AND RETURNED TO ICT. THE #2 PACK WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED. UPON THE NEXT TAKEOFF WITH THE #2 PACK MEL, A LAV SMOKE INDICATION WAS DISPLAYED AND THE AIRCRAFT RETURNED AGAIN TO ICT WHERE MAINTENANCE PLACED THE NUMBER ONE BLEED SYSTEM ON MEL. THE AIRCRAFT WAS RETURNED TO SERVICE. AT IAH, DURING FURTHER TROUBLESHOOTING OF THE #1 BLEED SYSTEM MEL, MAINETANNCE FOUND THE #1 ENGINE FAN SEAL TO BE LEAKING OIL. THE AFFECTED SEAL WAS REMOVED AND REPLACED, THE AIRCRAFT WAS OPERATIONALLY AND LEAK CHECKED, AND THEN RETURNED TO SERVICE.

Part: ODOR — DETECTED (COCKPIT)

CLE FLIGHT 4169 THE CREW REPORTED A MODERATE SMOKE SMELL AFTER TAKEOFF WHEN THE ENGINE BLEEDS WERE SELECTED. MAINTENANCE INSPECTED AND PERFORMED ENGINE GROUND RUNS AND FOUND NO DEFECTS WITH THE ENGINE BLEED SYSTEM OR THE AIR CONDITIONING SYSTEM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE — DETECTED (CABIN)

CLL - FLIGHT 4134 THE CREW REPORTED A LAV SMOKE WARNING AND AND VISIBLE SMOKE PRESENT ON APPROACH TO IAH. THE AIRCRAFT WAS DIVERTED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN BOTH PACKS FROM ENGINE BLEED AND APU BLEED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: APU — FAILED (APU BAY)

CLE FLIGHT 3683 THE CREW REPORTED THE APU FAILED IN FLIGHT. ATTEMPTED RESTART BUT IT WOULD NOT CONTINUE TO RUN. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON APU AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.