N13929

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,909 hrs · 29,596 cycles

GALLEY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,251 hrs · 28,917 cycles

THE CREW REPORTED A BURNING ODOR IN THE CABIN NOTICED BY THE F/A. MX INSPECTED THE ACFT AND WAS UNABLE TO DUPLICATE ANY BURNING ODOR OR SMELL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 28,957 hrs · 27,663 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 1A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L-19L CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L- 19L IAW EMB-145 CPM 51-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 18R-20R IS CORRODED. MAINTENANCE PERFORMED REPAIR ON INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 17R-21L IAW EC5330-02474. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14-15, STRINGERS 20L-15R CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON CIRCUMFERENTIAL SPLICE BETWEEN FRAMES 13-15, STRINGERS 20L-15R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK STRINGER 21L BETWEEN FRAMES 11-12 IS CORRODED. MAINTENANCE REMOVED AND REPLACED STRINGER 21L FRAME 9-13 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET HAS MIGRATING HAT BUSHING. MAINTENANCE PERFORMED REPAIR ON RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET IAW EMB-145 AMM 27-62-05, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R HAS IMPROPERLY PAINTED SKIN AND CORROSION IN UNPAINTED AREAS. MAINTENANCE PERFORMED REPAIR ON SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK CORROSION FOUND ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 57-58, STRINGER 21L-21R. MAINTENANCE PERFORMED REPAIR ON INTERNAL FUSELAGE SKIN, BETWEEN FRAMES 57-58 STRINGER 21L-21R IAW EC5330-02475. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM AT FRAME 20 IAW ETD 2011-145-103674. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK THE RT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 10R-11R, DIRECTLY BELOW THE RT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 27,810 hrs · 26,516 cycles

IAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CAPTAINS YOKE PITCH TRIM SWITCH, AND THE CAPTAINS TRIM DISCONNECT SWITCH. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRIM SWITCH — SHORTED (COCKPIT) · airframe 27,810 hrs · 26,516 cycles

IAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CAPTAINS YOKE PITCH TRIM SWITCH, AND THE CAPTAINS TRIM DISCONNECT SWITCH. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,303 hrs · 26,013 cycles

IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,303 hrs · 26,013 cycles

IAH - FLIGHT 2913, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH AND EXIT ROW SIGN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,301 hrs · 26,011 cycles

IAH - FLIGHT 2093, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,773 hrs · 25,458 cycles

IAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON WHEN THE AIRCRAFT WAS DOWN POWERED WITH ALL SWITCHES IN CORRECT POSITIONS. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,420 hrs · 25,092 cycles

IAH - FLIGHT 2104, THE CREW REPORTED A STRONG ODOR AFTER T/O. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED BOTH ENGINES WITH NO DEFECTS OR ODORS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,993 hrs · 24,655 cycles

IAH - DURING MAINTENANCE INSPECTION THE NR 4 AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHT STRIP ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IAH MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE NUMBER FOUR AISLE PATH LIGHT STRIP ON 06/19/2010, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,788 hrs · 24,451 cycles

IAH - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 25,644 hrs · 24,295 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE BALLAST 2A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (LAVATORY) · airframe 24,374 hrs · 22,947 cycles

FLIGHT 2195, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE LAV. MAINTENANCE INSPECTED THE LAV, AND REMOVED THE LIGHT BULB FROM THE LAV CEILING LIGHT, AND PLACED THE LAV LIGHTING ON NEF-LV-05 CAT "D" CTL NUMBER 176224, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST, OPERATIONALLY TESTED WITRH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED CENTER OMEGA BEAM IAW EMS 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 33. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 23,633 hrs · 22,145 cycles

DURING C-CHECK, TOILET WASTE DRAIN VALVE SUPPORT CORRODED. REPAIRED TOILET WASTE DRAIN SUPPORT IAW SRM 53-31-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ZONE 200) · airframe 23,633 hrs · 22,145 cycles

DURING C-CHECK. FR 75 SHOWS SIGNS OF CORROSION BTW STR 2L-2R. REPAIRED FR 75 IAW EC 5310-01317. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 70-73 STR 19L-19R. REPAIRED SKIN IAW EMB 145 SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 23,633 hrs · 22,145 cycles

SHV - DURING C-CHECK CORROSION FOUND ON INTERNAL SKIN AT STR 19L JUST FWD OF FR 61. MAINTENANCE REMOVED CORROSION IAW EMB 135/145 SRM 51-40-02 AND SRM 51-10-03. PREPPED, ALODINED AND PRIMED INTERNAL SKIN IAW EMB 135/145 CPM 51-21-04 AND CPM 51-21-05. INSTALLED NEW SKIN STR 19L-17L FR 61-66 IAW EMB 135/145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 18,289 hrs · 9,643 cycles

SHV - DURING C-CHECK, CRACK IN FR 69 BETWEEN STR 18L-19L. REPAIRED FRAME 69 IAW IC 2009-145/01891. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 23,633 hrs · 22,145 cycles

DURING C-CHECK, STR 21L CORRODED BTW FR 65-66. REPAIRED STR 21L IAW IC 2009-145/01544. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 60-61. REPLACED SKIN IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 44. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 38. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 59. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LONGITUDINAL SPLICE CORRODED BETWEEN FR 61-66 STR 19L-20L. REPAIRED SPLICE IAW EMB 145 SRM 51-14-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 33. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 54. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED OMEGA BEAM AT FR 23 IAW IC 2009-145/01857. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 59. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 9,643 cycles

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

Part: ATTACH FITTING — DAMAGED (SPOILER) · airframe 23,633 hrs · 22,145 cycles

SHV - DURING C-CHECK LT GROUND SPOILER O/B AND I/B ATTACHMENT FITTING BUSHING HOLES ARE OUT OF LIMITS. REMOVED AND REPLACED BRACKETS IAW EMB 145 AMM 57-51-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,633 hrs · 22,145 cycles

SHV - DURING C-CHECK STR 19L HAS AREAS OF CORROSION BETWEEN FRM'S 67-68. MAINTENANCE REMOVED AND REPLACED DAMAGED SECTION OF STR 19L FROM FRM 62-72 IAW EMB-145 SRM 51-40-02 AND SRM 53-00-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,609 hrs · 22,121 cycles

IAH - FLIGHT 2902, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS AFT OF THE EXIT ROW WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LEAKING (CARGO BAY) · airframe 23,507 hrs · 22,013 cycles

FLIGHT 2087, THE CREW REPORTED A BLEED 1 LEAK AT FL180. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R&R THE LT HORIZONTAL BLEED DUCT, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 23,507 hrs · 22,013 cycles

IAH - FLIGHT 2087, THE CREW REPORTED A BLEED ONE LEAK AT FL180. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R&R THE LT SIDE HORIZONTAL BLEED DUCT, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (BLEED DUCT) · airframe 23,507 hrs · 22,013 cycles

IAH - FLIGHT 2042, THE CREW REPORTED A BLEED 1 LEAK INDICATION AT APPROXIMATELY 15,000 FEET ON CLIMBOUT. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND TIGHTENED A CLAMP ON A BLEED LINE IN THE AFT AVIONICS COMPARTMENT. OPS & LEAK CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 23,428 hrs · 21,926 cycles

THE CREW REPORTED AN ENGINE (1) BLEED LEAK ON CLIMB. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R&R RT BLEED DUCT BETWEEN FRAMES 56-60, OPS AND LEAK CHECKED WITH NO DEFECTS, ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 22,919 hrs · 21,412 cycles

LCH DURING MX INSPECTION THE OVERWING CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE NR 6 EMERGENCY LIGHT BALLAST, OPS CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 22,776 hrs · 21,268 cycles

IAH - FLIGHT 2938 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL AT ROW 18. MAINTENANCE INSPECTED THE AIRCRAFT, FOUND A BAD BALLAST AT SEAT 18A. THE BALLAST WAS DISCONNECTED AND THE LIGHT PLACED ON MAL 33-20-00/1 CAT C CONTROL NUMBER 151397 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/03/08 MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST FOR ROW 18, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,168 hrs · 19,664 cycles

SHV - DURING MAINTENANCE ROUTINE CHECK MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR INVERTER (I/B) IAW EMB 145 SWPM 20-50-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — DEFECTIVE (NLG) · airframe 20,104 hrs · 18,548 cycles

CLE FLIGHT 2349 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE GEAR DOOR WAS SLOW TO OPEN. THE NOSE GEAR DOOR ACTUATOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,966 hrs · 18,401 cycles

CLE FLIGHT 2934 - THE CREW REPORTED THE FORWARD EMERGENCY AISLE LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 19,497 hrs · 17,906 cycles

IAH - DURING PRE-FLIGHT FOR FLIGHT 2406, THE CREW REPORTED THAT THE F/O'S WINDSHIELD WAS SMOKING FROM THE TERMINAL. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — FAILED (MLG) · airframe 19,100 hrs · 17,465 cycles

CLE FLT NR 2308, CREW REPORTED LANDING GEAR/LEVER DISAGREE WITH RED NOSE WHEEL INDICATION AND GEAR HANDLE IN THE UP POSITION. MAINTENANCE INSPECTED AND FOUND THE NOSE LANDING GEAR UPLOCK BOX FAILED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX. LANDING GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — OUT OF ADJUST (TE FLAPS) · airframe 18,797 hrs · 17,117 cycles

SHV - DURING DESCENT OF FLIGHT 2869, THE EICAS DISPLAYED A FLAP FAIL WARNING. THE CREW DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. MAINTENANCE ZERO RIGGED THE INBOARD FLAPS IAW EMB 145 AMM 27-53-04 AND OPERATIONALLY CHECKED THE FLAPS. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 18,550 hrs · 16,821 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE GALLEY, MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND NO EVIDENCE OF BURNING SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LOOSE (A/C PACK) · airframe 18,505 hrs · 16,768 cycles

IAH FLIGHT 2684 - PILOT REPORTED A SMELL OF SMOKE IN COCKPIT AND CABIN ASSOCIATED WITH A LARGE THUD. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. A DUCT WAS FOUND DISLODGED ON THE RIGHT AIR CONDITIONING PACK. THE DUCT WAS RESECURED, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE DISCREPANCY WAS CLEARED.

Part: ROD — OUT OF ADJUST (DOOR) · airframe 16,958 hrs · 14,992 cycles

CLE - THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE AND LATCH. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR FOLDING FLAP RODS. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 15,817 hrs · 13,723 cycles

CRP - CREW REPORTED THAT THE LEFT WING EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPS CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO TIMES ARE AVAILABLE ON THIS PART.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,681 hrs · 2,841 cycles

CRP - DURING MAINTENANCE INSPECTION THE NUMBER THREE EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,380 hrs · 13,164 cycles

SHV - DURING C-CHECK THE LT HAND OMEGA BEAM ASSEMBLY WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,380 hrs · 13,164 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT STRIP AT SEAT 1A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: STRUT — STICKS (NLG) · airframe 13,552 hrs · 10,925 cycles

EWR---CO2049, CREW REPORTED, "ON LIFT OFF, RECEIVED AIR/ GROUND FAIL MESSAGE ON EICAS. GEAR WOULD NOT RETRACT. MESSAGE DID NOT GO AWAY. RETURNED TO NEWARK." MAINTENANCE TROUBLESHOT AND FOUND NOSE LANDING GEAR STRUT STICKING. SERVICED STRUT IAW EMB145 MM 32-20-01, OPS. CHECKED GOOD ON GROUND, REQUESTED TEST FLIGHT TO VERIFY REPAIR. AIRCRAFT TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 13,547 hrs · 10,919 cycles

EWR---CO2024, CREW REPORTED, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. EMERGENCY LIGHT BATTERY PACK S/N REMOVED: [1]72619 [2]68594 [3] 68911 [4] 68902). AIRCRAFT RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LANDING GEAR)

CLE FLIGHT NR 2227 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER RETRACTION UNTIL ABOUT 300AGL. THE GEAR DID NOT RETRACT. MAINTENANCE INSPECTED AND COULD NOT FIND ANY DEFECTS. ALL 5 WEIGHT ON WHELLS PROXIMITY SWITCHES WERE REPLACED FOR PRECAUTIONARY REASONS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FRAME — BENT (FUSELAGE) · airframe 13,452 hrs · 10,833 cycles

ON GROUND WITH GUSTLOCK ENGAGED, AIRCRAFT EXPERIENCED WINDS GUSTING 54+KTS. GUSTLOCK DISENGAGED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE FRAME JUST FORWARD OF THE GUSTLOCK ASSY IN THE FORWARD FUSELAGE UNDER THE COCKPIT CENTER PEDESTAL BENT. MAINTENANCE REMOVED AND REPLACED THE FRAME IAW EMB-135/145 SRM 51-40-02. TEST FLIGHTED GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: SKIN — SPLIT (ELEVATOR) · airframe 13,452 hrs · 10,833 cycles

ON GROUND WITH GUSTLOCK ENGAGED, AIRCRAFT EXPERIENCED WINDS GUSTING 54+KTS. GUSTLOCK DISENGAGED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LEFT ELEVATORS UPPER SKIN DAMAGED. MAINTENANCE REPAIRED THE DAMAGE AND BALANCED ELEVATORS IAW EC5520-0026 AND AMM-51-60-00. TEST FLIGHTED GOOD.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 13,452 hrs · 10,833 cycles

THE LEFT AND RIGHT HORIZ STAB SPHERICAL BEARINGS FAILED WEAR CHECK. MAINTENANCE REPAIRED THE LEFT AND RIGHT VERTICAL STAB SPHERICAL BEARING HOUSINGS AND INSTALLED BOTH SPHERICAL BEARINGS IAW EC5510-01059 AND EMB-IC2003-145/2529. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: FIRE DETECTOR — FAULTY (NR 1 ENGINE) · airframe 13,388 hrs · 10,770 cycles

GRR/EWR---CO2355, CREW REPORTED, ( NR 1 ENGINE FIRE INDICATION IN CRUISE FLIGHT, DIVERTED)....MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL MODULE (PN: 902061 SN: 236) IAW EMB145 AMM NR 26-11-03. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR (PN: 3601-133-500/230C-9.0M SN: 228082) IAW EMB145 AMM NR 26-11-01. OPERATIONAL TEST OF NR 1 ENGINE FIRE DETECTION SYSTEM GOOD IAW EMB145 AMM NR 26-10-00. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 12,740 hrs · 10,125 cycles

EWR "BRK OUTBOARD FAIL" DURING ROLLOUT. REMOVED AND REPLACED BRAKE CONTROL UNIT OPS CHECK IAW EMB145MM 32-41-02 GOOD.

Part: DUCT — SEPARATED (APU SHUTOFF VALV)

CLE FLIGHT 2032 THE CREW REPORTED ON TAXI RECEIVED A APU BLEED LEAK INDICATION THEN A SMOKE ODOR WAS NOTICED. THE APU WAS SHUTDOWN. MAINTENANCE INSPECTED AND FOUND THE APU BLEED DUCT SEPARATED DOWN STREAM OF THE APU SHUT-OFF VALVE. THE BLEED DUCT ASSEMBLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE LIGHT STRIP HAD BROKEN WIRES. THE LIGHT STRIP WAS REPLACED.OPERATIONAL CHECKS WERE GOOD.

Part: UPLOCK — FAULTY

EWR---CO3540, CREW REPORTED "LANDING GEAR DISAGREEMENT ON MAIN GEAR. AIRCRAFT AIR RETURNED" (TO NEWARK WITHOUT INCIDENT).....MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED RIGHTHAND MAIN LANDING GEAR UPLOCK IAW EMB145 AMM #32-33-10. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CORRODED · airframe 1,101 hrs · 8,486 cycles

TYS, During a scheduled inspection the ramp angle on center omega beam has corrosion. Maintenance removed and replaced the ramp angle. I/A/W-EMB135/14SRM-51-40-02, 51-20-03, 51-40-06 and 51-40-02. Repair procedures where satisfactory and the aircraft will be released upon complection of inspection.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 1,101 hrs · 8,486 cycles

TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL, AFT OF THE COCKPIT DOOR WAS FOUND CORRODED.

Part: BEAM — CORRODED · airframe 1,101 hrs · 8,486 cycles

TYS, During a scheduled inspection the center omega beam between FR18 and FR24 was found corroded. Maintenance removed and replaced the omega beam. I/A/W-EMB-SRM-51-40-02 and 51-21-02. Repair procedures where satisfactory and the aircraft will be released upon complection of inspection.

Part: MANIFOLD — CHAFED (APU) · airframe 1,101 hrs · 8,486 cycles

TYS, DURING A SCHEDULED INSPECTION THE APU FIRE EXTINGUISHER HEAD MANIFOLD WAS FOUND CHAFED AT B-NUT. MAINTENANCE REMOVED AND REPLACED THE MANIFOLD IAW-EMB135/145MM-20-10-03 AND 26-23-05. REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: TUBE — KINKED · airframe 1,101 hrs · 8,486 cycles

TYS, During a scheduled inspection the right APU fire extinguisher tube was found damaged. Maintenance removed and replaced the tube. I/A/W-EMB145MM-20-10-03 and 26-23-05. Repair procedures where satisfactory and the aircraft will be released upon complection of inspection.

Part: GUSSET — CORRODED · airframe 1,101 hrs · 8,486 cycles

TYS, During a scheduled inspection the aft gusset was found corroded. Maintenance removed and replaced the aft gusset. I/A/W-EMB-SRM-51-40-02 and CMP-51-04-00. Repair procedures where satisfactory and the aircraft will be released upon complection of inspection.

Part: ATTACH FITTING — CHAFED (RUDDER) · airframe 11,017 hrs · 8,486 cycles

DURING A SCHEDULED 1-C INSPECTION THE LOWER RUDDER 1 STABILIZER ATTACH POINT HAS DISPLACED METAL ON RT SIDE NEAR BUSHING.

Part: FITTING — CORRODED · airframe 1,101 hrs · 8,486 cycles

TYS, During a scheduled inspection the aft galley inboard floor fitting was found corroded, Maintance removed and replaced the fitting. I/A/W-C & D Aerospace VCMM-25-31-45. The replacement was satisfactory and the aircraft will be released upon complection of the inspection.

Part: LIGHT — INOPERATIVE (FUSELAGE)

IAH - DURING A-CHECK INSPECTION, THE LEFT AND RIGHT HAND AFT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLIES IN ACCORDANCE WITH EMB145 M/M 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — BROKEN (CARGO BAY)

IAH - FLIGHT 4211, THE CREW REPORTED THAT ON CLIMB THE CARGO BAY FILLED WITH SMOKE AND PRESSURIZATION WAS LOST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE ENGINE PNEUMATIC DUCT CLAMP IN THE CARGO BAY TO HAVE COME APART. MAINTENANCE REPLACED THE AFFECTED CLAMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GCU — FAULTY (APU)

EWR-CREW REPORTED SMELL OF BURNING PLASTIC NOTED IN COCKPIT & CABIN DURING TAXIOUT. APU GEN. DROPPED OFF LINE & SMELL GOT WORSE SIMULTANEOUSLY. MX REMOVED & REPLACED APU GEN.(P/N23080013A) & APU GEN. CONTROL UNIT (P/N51525014A) GEN. STILL INOPERATIVE. A/C RELEASED MEL 49-00-00 CATEGORY C PLACARD 002649 ABD RETURNED TO SERVICE. NO BURNING SMELL NOTED. MX REMOVED/REPLACED GEN. CONTROL UNIT ON 10-25-00 & OPERATIONALLY CHECKED SYSTEM GOOD. (P/N51525014A) MEL CLEARED & A/C RETURNED TO SERVICEABLE CONDITION. SDR REF. C2XAOOBT083 CLOSED

Part: WINDSHIELD — CRACKED (COCKPIT)

CREW REPORTED WHILE IN FLIGHT THE FIRST OFFICERS WINDSHIELD CRACKED. A/C LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMBRAER MM 56-10-01. A/C WAS RELEASED TO SERVICE.

Part: GENERATOR — INOPERATIVE (APU)

EWR-CREW REPORTED SMELL OF BURNING PLASTIC NOTED IN COCKPIT & CABIN DURING TAXIOUT. APU GENRTR. DROPPED OFF LINE & SMELL GOT WORSE SIMULTANEOUSLY. MAIN. REMOVED AND REPLACED APU GENERATOR (P/N23080-013A) AND APU GEN CONTROL UNIT (P/N51525-014A) GENERATOR STILL INOPERATIVE. A/C RELEASED IAW MEL #49-00-00 CATEGORY C PLACARD 002649 AND RETURNED TO SERVICE. NO BURNING SMELL NOTED. SDR OPEN.

Part: SWITCH — SHORTED (COCKPIT)

CLE FLIGHT 3605-THE CREW REPORTED THE FIRST OFFICERS PITCH TRIM SWITCH BEGAN TO SMOKE ON APPROACH TO CLEVELAND. THE A/C LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S PITCH TRIM SWITCH I/A/W EMBRAER MAINTENANCE MANUAL 27-40-03. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT)

DAL - FLT 4208 - CREW ABORTED TAKEOFF DUE TO THE RIGHT ENGINE EXCEEDING ITT LIMITS. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED GROUND RUN OPERATIONAL CHECKS. THE ENGINE PARAMETERS ALL CHECKED WITHIN MANUFACTURES LIMITS. THE AIRCRAFT WAS REPOSITIONED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES. ALL WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS TAST CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SKIN — DELAMINATED (RT WING AILERON)

IAH - DURING C-CHECK INSPECTION, THE RIGHT AILERON WAS FOUND TO HAVE LIGHTNING STRIKE DAMAGE OUTBOARD OF THE OUTBOARD STATIC WICK. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AILERON, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EWR - FLT 3811 - MAINTENANCE FOUND EMERGENCY FLOOR PATH STRIP LIGHTING INOPERATIVE. RESECURED THE CANNON PLUG ON THE EMERGENCY AISLE PATH LIGHTS AND OPS CHECKED SYSTEM GOOD. (M)

Part: DOOR SEAL — RUPTURED (PAX DOOR)

CLE - FLT 4049 - THE CREW REPORTED THAT THE CABIN DOOR SEAL RUPTURED IN FLIGHT. THE AIRCRAFT HAD A PRESSURIZATION LOSS AND A EMERGENCY LANDING WAS MADE IN SBN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPAIRED THE CABIN DOOR SEAL IAW EMBRAER MM 52-00-04. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

BTV - FLT 4201 - CREW REPORTED AISLE PATH LIGHTING INOPERATIVE ON HEADSTART. MAINTENANCE REPAIRED A BROKEN WIRE ON AISLE PATH LIGHTS AND OPS CHECKED SYSTEM GOOD. (M)

Part: CLAMP — LOOSE (CABIN)

CLE - FLT 4041 - THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PACK SYSTEM AND FOUND THE LEFT NOISE ATTENUATOR AND CLAMP HAD COME LOOSE. MAINTENANCE RESECURED THE NOISE ATTENUATOR AND CLAMP AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED IAW EMB145 MM 21-20-04 AND 21-20-00. REFERENCE EMB145 IPC 21-24-01 FOR LOCATION OF PARTS. (M)

Part: NOISE ATTENUATOR — LOOSE (CABIN)

CLE - FLT 4041 - THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PACK SYSTEM AND FOUND THE LEFT NOISE ATTENUATOR AND CLAMP HAD COME LOOSE. MAINTENANCE RESECURED THE NOISE ATTENUATOR AND CLAMP AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED IAW EMB145 MM 21-20-04 AND 21-20-00. REFERENCE EMB145 IPC 21-24-01 FOR LOCATION OF PARTS. (M)

Part: OVERTEMP IND — ACTIVATED (BLEED AIRSYSTEM)

FLT 4115 - THE PILOT REPORTED, GOT A DAUL BLEED OVERTEMP DURING ICING CONDITIONS DURING CLIMB. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE BLEED SYSTEM IAW EMB145 MM 36-20-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SOCKET — BURNED (ROW 4A)

EWR - FLT C04235 - CREW REPORTED SEAT 4A LIGHT SOCKET BURNED AND ELECTRICAL SMOKE MESSAGE REPORTED ON EICAS PERFORMED GATE RETURN. REMOVED AND REPLACED LIGHT SOCKET AND OPS CHECKED GOOD. (M)

Part: ENGINE — CONTAMINATED (LEFT)

CLE - DURING A SCHEDULED INSPECTION, A OIL DEBRIS MESSAGE WAS FOUND ON THE EICAS FOR THE LEFT ENGINE. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE OIL DEBRIS TO BE BEYOND MANUFACTURES LIMITS. THE LEFT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FIREWALL — CRACKED (AFT FUSELAGE)

CLE - DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 20 INCHES ACROSS THE CENTER LINE OF THE WALL. MAINTENANCE ACCOMPLISHED A TEMPORARY REPAIR IAW CONT EXPRESS EC5310-01082. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: CONTROL HANDLE — FAULTY (COCKPIT)

CLE - FLT 4234 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE NOSE GEAR DOORS WOULD NOT CLOSE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT THEN REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW EMB-145 MM 32-33-00. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. (X)