N14952

Part: UNKNOWN — ODOR (COCKPIT) · airframe 36,054 hrs · 27,230 cycles

PILOT REPORTED A STRONG EXHAUST/FUEL ODOR IN FLIGHT DECK AND CABIN THROUGHOUT FLIGHT. MX RAN THE ENGINES AND APU WITH NO FUEL OR EXHAUST ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,261 hrs · 26,607 cycles

ACFT WAS IN FOR A LINE CHECK WHEN INSPECTION FOUND A FLOOR PROXIMITY LIGHT STRIP INOPERATIVE BETWEEN ROLL 2 THRU5. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD AND WAS RELEASED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK SHEAR TIE AT FRAME 68 CORRODED. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT FRAME 68 BY INSTALLING DOUBLER AND FILLER IAW EC 5320-01494. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK, STRINGER 20L CORRODED, AROUND RIVETS (2 EA) BETWEEN FRAMES 65-66. MAINTENANCE COMPLETED STRINGER REPAIR AT FRAMES 65-66 STRINGER 20L IAW SRM 53-00-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK, FRAME 65 CORRODED, IN UPPER RADIUS AT STRINGER 17L AND AT NUT PLATES FOR GUIDE. MAINTENANCE COMPLETED REPAIR AT FRAME 65 STRINGER 17L IAW EC5330-02661. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK LT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED UNDER TEFLON GUIDE. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT LT OVERWING EMERGENCY EXIT LOWER FRAME IAW EC 5220-01043. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK, CARGO DOOR SILL CORRODED, FROM FRAME 65 TO 68. MAINTENANCE R & R CARGO DOOR SILL AT FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,277 hrs · 25,861 cycles

DURING C-CHECK, SHEAR TIE CORRODED, FRAME 65, STRINGER 17L. MAINTENANCE COMPLETED SHEAR TIE SPLICE REPAIR AT FRAME 65, STRINGER 17L IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 33,791 hrs · 25,467 cycles

THE CREW REPORTED A STRONG ELECTRICAL ODOR IN CABIN. 17A CEILING LIGHT WAS INOPERATIVE. MX REPLACED ROW 17A CEILING LIGHT ELECTRICAL HARNESS ASSY. OPS CHECKS WERE GOOD.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 32,848 hrs · 24,695 cycles

DURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: CONDITIONER — FAULTY (NR 1 ENGINE) · airframe 31,717 hrs · 23,888 cycles

AFTER TAKEOFF, IN CLIMB CREW REPORTED FUEL QTY NR1 WENT TO DASHES AND FUEL QUANITY NR 2 READ 0 LBS. CREW PERFORMED AIR RETURN WITHOUT ISSUE. MX R & R FUEL CONDITIONING UNIT IAW AMM 28-41-01 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 31,510 hrs · 23,748 cycles

MCI - THE LAV SMOKE DETECTOR WAS REPORTED AS MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — FAILED (LT MLG) · airframe 31,276 hrs · 23,579 cycles

THE CREW REPORTED IMMEDIATELY AFTER TAKEOFF FROM CLE A LOUD REPETITIVE THUMPING NOISE FROM UNDER THE AIRCRAFT. MOMENTARILY THE LEFT MAIN GEAR INDICATED AMBER CROSS-HATCHES WITH A MISCOMPARE INDICATION ON THE COCKPIT EICAS. CREW PERFORMED AN AIR RETURN TO CLE WITHOUT FURTHER INCIDENT. MX TESTED WIRING AND REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX. ALL OPERATIONAL CHECKS WERE GOOD.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 31,103 hrs · 23,421 cycles

IAH - FLIGHT 4586, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND VERIFIED NORMAL OPERATION OF THE CAPTAINS DV WINDOW, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BLOWN (CABIN) · airframe 31,017 hrs · 23,357 cycles

TYS - A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE EMERGENCY LIGHT BLOWN ON THE RIGHT OVERHEAD WING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD AND WAS RELEASED.

Part: SWITCH — FAULTY (COCKPIT) · airframe 30,796 hrs · 23,162 cycles

CLE FLT 2431 THE CREW REPORTED A BLEED 2 VALVE CLOSED MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED 2 ON/OFF PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 30,739 hrs · 23,118 cycles

ORD FLT 6187 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE REPLACED THE BLEED LINE O-RINGS AT JOINT 5, 9, 11, 13, 15, 19 AND 23. ALSO REPLACED THE NR 1 BLEED VALVE Y DUCT ASSEMBLY AND AFT CLAMP. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERTEMP (NR 1) · airframe 30,735 hrs · 23,111 cycles

ORD FLT 5854 THE CREW REPORTED A BATTERY NR 1 OVERTEMP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,307 hrs · 22,777 cycles

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHT STRIPS NR 3 AND NR 4 WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,083 hrs · 22,612 cycles

FLOOR PROX LIGHTS NR 1 2 & 3 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ACM — INOPERATIVE (AC BAY) · airframe 30,002 hrs · 22,556 cycles

MTY - FLIGHT 2127, THE CREW REPORTED THAT THE NUMBER ONE PACK WAS SURGING AND THE CABIN FILLS WITH SMOKE. PACK ONE WAS PLACED ON MEL, AND THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,885 hrs · 22,467 cycles

TYS - A/C HAD A DENT IN A PRIEVIOUS REPAIR AND TO MAY IN 1 AREA BETWEEN FR19 AND FR 20 AND STR 15L AND WAS PLACED ON 750 FLIGHT CYLE DMI. MAINTENANCE REMOVED AND REPLACED THE CENTER FUSELAGE 1 LEFT DOOR SURROUND SKIN PANEL IAW EC5330-02372. PERFORMED A RVSM MAPPING OF AREA AND RVSM PASSED IAW TASKCARD 34-13-04 AND RECEIVED A CERTIFICATE OF CONFORMITY. ALL WORK ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE.

Part: PROBE — INOPERATIVE (NR 2 FUEL) · airframe 29,776 hrs · 22,381 cycles

HOU - FLIGHT 2636 THE CREW REPORTED THAT THE NR 2 FUEL QUANTITY INDICATION DASHED OUT. THE AIRCRAFT DIVERTED TO HOU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR LEAKS WITH NO DEFECTS NOTED, AND PLACED THE NR 2 FUEL QUANTITY ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE RIGHT TANK NR 2 FUEL PROBE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BURNED (CABIN) · airframe 29,383 hrs · 22,084 cycles

MTY - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT SIDEWALL LIGHT AT 9A TO BE SMOKING. MAINTENANCE PLACED THE SIDEWALL LIGHT IN MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/25/10 IAH MAINTENANCE REPAIRED A WIRE ON THE AFFECTED SIDEWALL LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,350 hrs · 22,058 cycles

TYS - EMERGENCY FLOOR LIGHTS AT ROWS 6 AND 12 INOP. REMOVED AND REPLACED ROW 6 AND ROW 12 EMERGENCY LIGHT STRIPS, OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,350 hrs · 22,058 cycles

TYS - DENT ON PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20 STRINGER 15L. REPAIRED DENTS IAW EC5330-02287.

Part: FAIRING — DAMAGED (HORIZ STAB) · airframe 29,351 hrs · 22,059 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT SIDE HORIZIONTAL STAB TIP FAIRING WITH MULTIBLE SPOTS OF DAMAGE COMPOSITE. MAINTENANCE REPAIRED THE HORIZ STAB TIP IAW EC5750-01183 REV B AND EMB 145 SRM 51-70-06 PARAGRAPH 4, STEPS A, B AND D. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BRACKET — WORN (AILERON) · airframe 29,351 hrs · 22,059 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT AILERON PCA BRACKET OUTBOARD HAT BUSHION HOLE OUT OF LIMITS. MAINTENACE REMOVED AND REPLACED THE RIGHT AILERON PCA BRACKET IAW EC5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 29,351 hrs · 22,059 cycles

TYS - A/C IS CURRENTLY IN A C-CHECK STATUS WHEN THE INSPECTION DEPARTMENT FOUND CORROSION UNDER THE LOWER AFT SERVICE DOOR TEFLON GUIDE. MAINTENANCE REPAIRED THE CORROSION UNDER THE TEFLON GUIDE AT THE SERVICE DOOR IAW EC5310-01532, REFER TO M6023 (0554421 2-339) FOR THE DMI. WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,350 hrs · 22,058 cycles

TYS - LOWER SKIN CORRODED AT FR14 BETWEEN STR 19L AND 19R. REMOVED AND REPLACED SKIN IAW EC5330-02280.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 29,351 hrs · 22,059 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE STRINGER SPLICE CORRODED AT STRINGER 20R AND FRAMES 13-14. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW EMB 145SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 29,055 hrs · 21,823 cycles

FLIGHT 2348 - EWR - FLIGHT CREW REPORTED LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX PERFORMED OPERATIONAL CHECK AND FOUND NO DEFECTS. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,550 hrs · 21,458 cycles

IAH - FLIGHT 2973 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WHEN ANTI-ICE CAME ON AND ON DESCENT. IT WAS NOTED THAT THE SMELL DISSIPATED QUICKLY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE RUNS ON NUMBER ONE AND NUMBER TWO ENGINES WITH NO SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN DOOR) · airframe 27,736 hrs · 20,847 cycles

FLIGHT 2892 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR VERY DIFFICULT TO OPEN. EWR MX LUBRICATED MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 25,773 hrs · 19,394 cycles

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

Part: TUBE — LEAKING (FUEL SYSTEM) · airframe 19,154 hrs · 25,452 cycles

DURING ROUTINE MAINTENANCE THE PRESSURE REFUEL/DEFUEL LINE WAS FOUND LEAKING. MAINTENANCE INSPECTED AND FOUND THE TUBE ASSEMBLY TO BE CORRODED. THE TUBE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: CLAMP — DEFORMED (BLEED AIR SYS) · airframe 24,751 hrs · 18,620 cycles

FLIGHT 2775 - EWR - FLIGHT CREW REPORTED ENG NR 1 BLEED LEAK INDICATION ON EICAS IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX R&R BLEED V-CLAMP AND PERFORMED OPX CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (BLEED VALVE) · airframe 24,734 hrs · 18,607 cycles

FLIGHT 2306 - EWR - DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX R&R NR 2 BLEED VALVE PUSH BUTTON SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BLEED VALVE — INOPERATIVE (NR 2) · airframe 24,734 hrs · 18,607 cycles

FLIGHT 2306 EWR DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX R&R NR 2 BLEED VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 203, STEP 4. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (RUDDER) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK THE RUDDER UPPER CENTER ATTACHMENT BRACKET WAS FOUND TO BE WORN AND THE HAT BUSHINGS MIGRATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU) · airframe 24,544 hrs · 18,464 cycles

DURING C-CHECK APU FIREWALL HAS CHAFING DAMAGE A 6 O`CLOCK POSITION. MX REPAIRED APU FIREWALL AT FR 81 IAW EC 5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK CORRODED NUT PLATE HOLE ON OMEGA BEAM LAV AREA BETWEEN FRAME 60 AND 61 LT SIDE. REPAIRED LT OMEGA BEAM BETWEEN FR 60-61 AT NUT PLATE ARE IAW EC 5320-01430. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM JUST ABOVE FR 20 CARBON CROSS BEAM. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIG 201. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SUPPORT — CORRODED (CABIN) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT HAS CORROSION AROUND RIVETS AT FR 45,46 AND 50. MX REPAIRED LT UPPER SEAT TRACK SUPPORT AT FR 45, 46 AND 50 IAW EC 5320-01429. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SUPPORT — CORRODED (CABIN) · airframe 24,544 hrs · 18,464 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT HAS CORROSION AROUND RIVETS AT FR 45, 46 AND 50. MX REPAIRED LT UPPER SEAT TRACK SUPPORT AT FR 45, 46 AND 50 IAW EC 5320-01429. THE AIRCRAFT WAS APPROVED TO RETURN FOR MAINTENANCE.

Part: RIVET — CORRODED (HORIZ STAB) · airframe 24,544 hrs · 18,464 cycles

DURING C-CK LT HORIZONTAL STAB L/E HAS NUMEROUS RIVETS WITH CORROSION UPPER AND LOWER SURFACE. MX REMOVED AND REPLACED AFFECTED RIVETS ON LT HORIZONTAL STAB L/E UPPER AND LOWER SURFACE IAW EC5510-01192. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: INVERTER — BLOWN (EMERGENCY LIGHT)

ACFT WAS IN FOR A SERVICE ROUTINE AND MX FOUND THE LT OVERWING EMERGENCY EXIT MARKER INOP. MX R&R THE EMERGENCY LIGHT INVERTER AT THE NR 4 POSITION. IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,373 hrs · 18,327 cycles

IAH FLIGHT 2026. DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FORWARD AREA OF THE CABIN. MX INSPECTED THE ACFT WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 24,372 hrs · 18,325 cycles

IAH FLIGHT 2331 THE CREW REPORTED A ODOR OF HOT WIRES COMING FROM TOP OF BULKHEAD IN FRONT OF SEAT 1A WITH NO SMOKE VISIBLE. THE ACFT LANDED AT IAW WITHOUT INCIDENT WHERE MX PLACED THE CABIN LIGHTING ON MEL 33-20-00/1 CAT C CONTROL NR 154736 AFTER DISCONNECTING THE BALLAST AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 09/23/08. MX R&R THE BALLAST AT SEAT 2A. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 24,357 hrs · 18,213 cycles

FLIGHT 2897 - EWR - FLIGHT CREW REPORTED ELECTRIC SMELL IN GALLEY. EWR MX REMOVED AND REPLACED BALLAST AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 21,830 hrs · 16,551 cycles

FLT 2416 - EWR - CREW REPORTED HYDRAULIC SYSTEM 1 LOW QTY MESSAGE ON TAXI AND HYDRAULIC SYSTEM 1 FAIL MESSAGE ON DURING GATE RETURN. DURING TAXI BACK TO GATE, LOSS OF TILLER COMMAND. EWR MX FOUND HYDRAULIC SYSTEM 1 PRESSURE SWITCH LOOSE. MX RESECURED PRESSURE SWITCH AND PERFORMED OPERATIONAL CHECKS FOR HYDRAULIC SYSTEM AND TILLER SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BULB — BURNED (EMERGENCY LIGHTS) · airframe 20,869 hrs · 15,839 cycles

RIC - DURING SCHEDULE INSPECTION, MX FOUND RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,224 hrs · 15,336 cycles

602 NR 110291- AIRCRAFT IN FOR C-CHECK. CORROSION ON LT OMEGA BEAM AT FRM 20. SPLICED IN NEW SECTION OF BEAM, ALODINED, PRIMED AND PAINTED. REPAIRS MADE IAW EC5320-01229 AND EMB145 CPM 51-21-07.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,224 hrs · 15,336 cycles

TYS DURING A CURRENT 1C INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FR 20. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM IAW EMB 145 SRM 51-40-02. DRILL, COUNTERSUNK, ALLODINED, PRIMED AND PAINTED NEW PART IAW EMB 145 51-21-03 AND CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,681 hrs · 13,335 cycles

STL - DURING MAINTENANCE INSPECTION, THE FORWARD AND AFT CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 AND NUMBER 6 INVERTERS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (MLG) · airframe 16,450 hrs · 12,358 cycles

CLE FLIGHT NR 2496 - THE CREW REPORTED, THE LANDING GEAR WOULD NOT RETRACT ON CLIMB-OUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: MOUNT — WORN (NR 2 ENGINE) · airframe 15,405 hrs · 11,532 cycles

TYS DURING A SCHEDULED 4C INSPECTION THE NR 2 ENGINE MOUNT FORWARD UPPER WAS FOUND MIGRATED. MAINT REMOVED, CLEANED AND MEASURED THE DEFECT, FAB A NEW BUSHING AND INSTALL, TORQUE AND SAFTIED MOUNT BOLTS IAW AMM71-20-00. AIRCRAFT RETURNED TO SERVICE.

Part: HOUSING — CORRODED (RT MLG) · airframe 15,405 hrs · 11,532 cycles

TYS DURING A 4C INSPECTION THE RIGHT MLG FWD HOLLOW PIN HOUSING WAS FOUND WITH AREAS OF PITTING. AFTER MAINTENANCE REMOVED THE PITTING IT WAS BEYOND LIMITS AND A EC WAS CUT FOR THE REPAIR (EC5750-01239). THE HOLLOW PIN HOUSING WAS REPLACED IAW EC5750-01239. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — WORN (VERTICAL STAB) · airframe 15,405 hrs · 11,532 cycles

DURING A 4C INSPECTION THE HORIZONTAL TO VERTICAL STAB RT SPHERICAL BEARING HOUSING IN THE VERTICAL STABILIZER FITTING WAS FOUND WORN. MAINTENANCE REAMED THE RT SPHERICAL HOUSING, INSTALLED NEW INTERNAL AND EXTERNAL BUSHINGS, AND COMPLIED WITH A DIEHEDRAL AND INCIDENCE CHECK. AIRCRAFT TO BE RELEASED UPON COMPLETION OF SCHEDULED CHECK.

Part: CONNECTOR — FAULTY (EMERGENCY LIGHT)

CREW REPORTED, DURING TAXI-OUT, EMERGENCY LIGHTS NOT ARMED, AND ELECTRICAL EMERGENCY ABNORMAL MESSAGES ON EICAS, EMERGENCY LIGHTS CAME ON IN CABIN. EVERYTHING BACK TO NORMAL AFTER 10-15 SECONDS. RETURN TO GATE IN NEWARK. MAINTENANCE FOUND PIN 62 ON CONNECTOR JO838 NOT STAYING SECURE. REMOVED AND REPLACED CANNON PLUG JO838, OPS CHECKED SYSTEM GOOD IAW EMB 145 AMM 24-61-55 (CHAPTER 20-4-0-01). AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BURNED (FUSELAGE)

THE CREW REPORTED A HEAVY ELECTRICAL ODOR IN THE AFT CABIN AREA WITH PITCH TRIM 2 AND RUDDER 2 INOP MESSAGES, STICK SHAKER 1 AND CABIN INTERPHONE CIRCUIT BREAKERS POPPED ON FINAL APPROACH. THE AIRCRAFT LANDED AT HRL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CONNECTOR P0838 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CONNECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — FAULTY (COCKPIT)

CREW REPORTED, ELECTRICAL EMERGENCY ABNORNAL WITH EMERGENCY LIGHTS NOT ARMED AFTER SHUTTING DOWN APU ON AFTER TAKEOFF CHECKLIST. AIRCRAFT DIVERTED BACK TO EWR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE NR 1 DAU IAW EMB145 MM 31-41-01. OPS CHECKED SYSTEM GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 12,927 hrs · 9,615 cycles

CREW REPORTED, BURNING ODOR AROUND ROW 3 AND 4 IN CABIN AFTER POWERED UP. MAINTENANCE REMOVED ROW 3 AND 4 OVERHEAD PANELS, INSPECTED CEILING LIGHTS AND SIDE WALL LIGHTS, NO ODOR NOTED NOR DEFECTS FOUND IAW EMB145 AMM 05-25-05. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE AT ROW 17. MAINTENANCE REPLACED EMERGENCY CEILING LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE FORWARD PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV- DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE FORWARD PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV-DURING C-CHECK THE DOUBLER AT FRAME 17 STRINGER 17R WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,556 hrs · 8,481 cycles

SHV-DURING C-CHECK THE APU FIREWALL LOWER FRAME 81 WAS FOUND TO HAVE A CRACK. MAINTENANCE PERFORMED A DOUBLER REPAIR AT FRAME 81 IAW EC 5310-01238. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

DURING C-CHECK THE BAGGAGE DOOR THRESHOLD LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK THE BUTTSTRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (LT NACELLE) · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK LEFT HAND ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE RUB MARKS. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK LEFT HAND LOWER LINING CARGO SUPPORT AT FRAME 61 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK, THE RIGHT HAND LOWER ENGINE COWLING HAS RUB MARKS ON THE MOST AFT INBOARD STIFFENER. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STIFFENER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK LEFT HAND CROSSBEAM AT FRAME 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK THE RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED RAMP ANGLE IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 11,556 hrs · 8,481 cycles

SHV DURING C-CHECK LEFT HAND LOWER LINING CARGO SUPPORT AT FRAME 61 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED

YYZ---CO3350, CREW REPORTED, "AFT OF ROW SIX EMERGENCY LIGHTS COME ON THEN GO OUT (DURING TEST)"....MAINTENANCE REMOVED AND REPLACED #3 AND #4 EMERGENCY BATTERY PACKS IAW EMB145 MM #33-50-04. OPS.CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SERVICE/ROUTINE CHECK ON OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB ON PASSENGER DOOR IAW EMB145 AMM #33-50-06. OPS. CHECKED GOOD.

Part: CONTROL UNIT — INTERMITTENT (COCKPIT)

CLE FLIGHT 3296 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON THE EICAS AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — CRACKED (FUSELAGE)

CLE FLIGHT#3232 THE CREW REPORTED #1 HYDRAULIC SYSTEM FAILED IN FLIGHT.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE #1 HYDRAULIC SYSTEM PRESSURE SWITCH HAD CRACKED.THE SWITCH WAS REPLACED.OPOERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (COCKPIT)

CLE FLIGHT 3243 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IMMEDIATELY AFTER TAKEOFF. THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT AND THE NOSE GEAR AIR/GROUND PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3742 THE CREW REPORTED THE EMERGENCY AISLE LIGHTING STRIP WAS OUT AT ROW 7/8. MAINTENANCE REPLACED THE LIGHTING STRIP AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE - FLIGHT 3742, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS AT ROWS EIGHT AND NINE WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FAILED (NR 1 ENGINE)

LGA - FLT 4161 - CREW REPORTED ''E1 FIRE DETECTOR FAIL'', LGA MAINTENANCE REMVOED AND REPLACED NR 1 ENGINE FIRE LOOP IAW EMB145 MM 26-11-01, OPS CHECKED GOOD. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

RIC - FLT 3669 - CREW REPORTED ''RIGHT AFTER V1 ON GROUND ON TAKEOFF, RECEIVED MASTER WARNING (NO EICAS MESSAGES) PITCH TRIM HAD RUN FROM 7 UNITS UP TO 2 UNITS UP WITHIN 2 SECONDS. AIRCRAFT COULD NOT BE TRIMMED AGAIN UNTIL APPROXIMATELY 500 FEET, 160 KNOTS. NO OTHER IRREGULARITIES NOTED. MAINTENANCE IN RIC, REPORTED OPS CHECKED GOOD IAW EMB145 MM 27-40-00. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

BTV - FLT 3944 - DURING 1A INSPECTION MAINTENANCE, FOUND LEFT REAR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT EMERGENCY LIGHT ASSY P/N 3025101, AND NR 4 BATTERY CHARGER P/N 110049. OPS CHECKED SYSTEM GOOD. (M)

Part: WINDSHIELD — MELTED (COCKPIT)

EWR - FLT 4105 - DURING FLIGHT TO MILWAUKEE CREW NOTICED THE CAPTAINS WINDSHIELD HEATING ELEMENT WAS MALFUNCTIONING. IT APPEARED THAT THE GLASS WAS MELTING. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB MM 145 56-10-01. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE 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 EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT BRACKET — CORRODED (CABIN) · airframe 3,831 hrs · 2,811 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR BOARD SUPPORT AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REPAIR ON THE AFFECTED FLOOR BOARD SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE SKIN WAS FOUND TO BE DENTED JUST AFT OF THE PASSENGER DOOR. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A REPAIR DOUBLER IAW EMB145 MM 53-22-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ACTUATOR — FAILED (TE FLAP)

CLE - FLT 3973 - THE CREW REPORTED THAT AFTER TAKEOFF, THE FLAPS GOT STUCK AT THE 4 DEGREE POSITION. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB145 MM 27-51-09. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)

EWR - FLT 3984 - CREW REPORTED NR 1 ENGINE SHUTDOWN UPON LANDING GOING INTO REVERSE. MAINTENANCE FOUND NR 1 ENGINE HP VIBRATION TO BE OFF THE SCALE, BOROSCOPED 9TH STAGE COMPRESSOR AND FOUND DAMGE WITH METAL IN INNER BYPASS DUCT. REMOVED AND REPLACED THE ENGINE PERFORMED OPS CHECKS, ALL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING SERVICE CHECK INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING ROUTINE INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (FUSELAGE)

IAH - DURING PRE-FLIGHT INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULBS IN THE AFFECTED LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: UNKNOWN — SMOKE (COCKPIT)

IAH - FLT 4121 - DURING FLIGHT ON APPROACH TO IAH, CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE VERIFIED OPERATION OF AFFECTED SYSTEMS AND PERFORMED A VISUAL INSPECTION OF EQUIPMENT AND WIRING IN THE COCKPIT. NO DEFECTS WERE FOUND AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTHER INCIDENTS HAVE BEEN REPORTED TO-DATE.