N11535

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,095 hrs · 31,837 cycles

MX REPORTED THE EMERGENCY LIGHTS BY WING EMERGENCY EXIT NOT WORKING. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,095 hrs · 31,837 cycles

MX REPORTED THE EMERGENCY FLOOR LIGHT BY WING EMERGENCY EXIT INOP. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 39,620 hrs · 30,667 cycles

DURING CLIMB OUT, WHILE ACTIVATING MAIN PITCH TRIM SWITCH, ICAS WENT TO INOPERATIVE, THE MASTER WARNING WENT TO INOPERATIVE, THE MESSAGE REMAINED AFTER THE TRIM SWITCH WAS RELEASED.. MESSAGE ALSO REMAIN WAS RELEASED. ACFT RETURNED TO BASE AND MAINTENANCE RETRIEVED A CMC MESSAGE FOR THE HSCU FAIL WITH 1 OCCURRENCE ON 5-23. R & R THE HSCU IAW AMM 27-40-01. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,327 hrs · 28,791 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER IAW AMM 33-50-04. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 37,000 hrs · 28,549 cycles

ENGINE NR 1 OUT IN FLIGHT. REMOVED AND REPLACED NR 1 ENG. OPS AND LEAK CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 36,919 hrs · 28,488 cycles

DURING ROUTINE MAINTENANCE THE EXTERNAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY CHARGER AND BATTERY PACK. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCYLIGHTS) · airframe 35,362 hrs · 27,289 cycles

DURING SCHEDULED MAINTENANCE INSPECTION THE AFT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BURNED (YOKE) · airframe 35,354 hrs · 27,282 cycles

THE CREW REPORTED CLIMBING OUT THROUGH 6000 FT, THEY SMELLED A FOUL ODOR AND RECEIVED A PITCH TRIM MAIN FAIL MESSAGE. NONE OF THE TRIM SWITCHES WOULD WORK. PITCH TRIM BREAKER POPPED AND SMELL WENT AWAY. MAINTENANCE INSPECTED AND REPAIRED BURNED PITCH TRIM WIRES ON THE CAPTAINS YOKE AND REPLACED THE PITCH TRIM SWITCH.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,286 hrs · 27,228 cycles

DURING ROUTINE MAINTENANCE THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,122 hrs · 27,092 cycles

DURING MAINTENANCE INSPECTION, MAINTENANCE DISCOVERED AN OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT CHARGER ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,931 hrs · 26,938 cycles

DURING ROUTINE MAINTENANCE THE CABIN FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 18 TO ROW 24. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,880 hrs · 36,894 cycles

DURING MAINTENANCE INSPECTION THE ALL OF THE EMERGENCY LIGHTS THAT OPERATE OFF OF BATTERY NR 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,827 hrs · 26,849 cycles

DURING ROUTINE MAINTENANCE, THE AFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,631 hrs · 26,699 cycles

DURING ROUTINE MAINTENANCE, THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: SKIN — CRACKED (FRAMES 75) · airframe 32,586 hrs · 25,087 cycles

DURING C-CHECK, RT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 75. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 32,586 hrs · 25,087 cycles

DURING C-CK. CENTER OMEGA BEAM CORRODED AT FR 59. REPAIRED CENTER OMEGA BEAM IAW EC5320-02020. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 32,586 hrs · 25,087 cycles

DURING C-CK. RT FUSELAGE SKIN CRACKED AROUND RIVET FR 79. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAMES 77-78) · airframe 32,586 hrs · 25,087 cycles

DURING C-CHECK, LEFT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 77-78. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,285 hrs · 22,521 cycles

CREW REPORTED EMERGENCY LIGHT ON MAIN CABIN DOOR CEILING PANEL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 28,650 hrs · 22,034 cycles

ON DESCENT, CREW REPORTED A VERY STRONG ODOR OF BURNING IN FLIGHT DECK. F/A REPORTED BURNING ODOR ALSO AROUND ROW 11. SMOKE WAS NOT VISIBLE ONLY STRONG ODOR. MX INSPECTED AND FOUND EVIDENCE OF INGESTED BIRD IN NR 1 ENGINE. PERFORMED BORESCOPE AND BIRD STRIKE INSPECTION, NO DEFECTS NOTED. MX COULD NOT DUPLICATE OIL/ELECTRICAL ODOR ANYWHRE IN CABIN. PERFORMED GROUND POWER RUNS OF NR 1 AND NR 2 ENGINES WITH NO FURTHER ODOR. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (ZONE 600) · airframe 28,342 hrs · 21,817 cycles

LIQUID VAPOR WAS REPORTED TO BE TRAILING OFF THROUGH RT WING AFTER TAKEOFF BY FLIGHT ATTENDANT. MX R & R THE RT WING OTBD FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CHAFED (ZONE 200) · airframe 27,592 hrs · 21,228 cycles

STRINGER 2L IS CHAFED AT FRAME 20. BLENDED OUT DAMAGE IAW SRM 51-10-03, NDT PERFORMED, NO DEFECTS NOTED, ALODINED DAMAGED AREA, FABRICATED REPAIR, ALODINED AND PRIMED FABRICATED PARTS, INSTALLED NEW FABRICATED REPAIR, DOUBLER. CLASSIFIED AS A MAJOR.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,592 hrs · 21,228 cycles

RT HAT BEAM AT FRAME 60 IS CORRODED. R & R RT HAT BEAM AT FRAME 60 IAW SRM 51-40-02, 53-24-10,51-20-03, 51-20-01, AND CPM 51-21-06,51-21-05,51-21-04, AND AMM 25-40-01.

Part: SILL — CORRODED (ZONE 100) · airframe 27,592 hrs · 21,228 cycles

LT SILL AT FRAME 58 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME 58 IAW SRM 51-10-03, 51-40-02,51-40-06, 53-31-10, AND CPM 51-21-06.

Part: SILL — CORRODED (ZONE 100) · airframe 27,592 hrs · 21,228 cycles

RT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R SILL IAW SRM 51-10-03,51-40-02, 51-40-06, 53-31-10, AND CPM 51-21-06.

Part: SILL — CORRODED (ZONE 100) · airframe 27,592 hrs · 21,228 cycles

LT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME 61 IAW SRM 51-10-03,51-40-02,51-40-06,53-31-10, AND CPM 51-21-06.

Part: SILL — CORRODED (ZONE 200) · airframe 27,592 hrs · 21,228 cycles

CORROSION ON AFT CARGO DOOR SILL AROUND 2 FASTENER HOLES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R AFT CARGO LOWER DOOR SILL IAW SRM 51-10-03, 53-31-15, 51-20-03, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: GUSSET — CORRODED (ZONE 100) · airframe 27,592 hrs · 21,228 cycles

GUSSET ON CENTER HAT LT BEAM AT FRAME 60 CORRODED. R & R CENTER HAT GUSSET AT FRAME 60 IAW SRM 51-40-02, 53-24-10, 51-20-03,51-20-01, AND CPM 51-21-04,51-21-05.

Part: ANGLE — CORRODED (ZONE 800) · airframe 27,592 hrs · 21,228 cycles

CARGO DOOR TOP FRAME HAS CORROSION AROUND FORWARD FASTENER HOLE. INSTALLED NEW TOP CARGO DOOR ANGLE TO CARGO DOOR. PN 145-31544-001 IAW SRM 51-40-02, 51-20-03, AND 52-30-01.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 27,238 hrs · 20,949 cycles

THE CREW REPORTED LT EXTERNAL FORWARD EMERGENCY LIGHT INOPERATIVE. MX INSPECTED AND REPLACED THE LT WING FORWARD EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,020 hrs · 20,787 cycles

CREW REPORTED A FUEL ODOR IN COCKPIT DURING POWER CHANGES. MX PERFORMED ENGINE RUNS AT HIGH POWER AND VARIABLE SETTINGS WITH BOTH PACKS ON AND COULD NOT DUPLICATE ANY FUEL ODOR IN COCKPIT OF CABIN. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,623 hrs · 18,127 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND CEILING EXIT LIGHT NOT WORING DURING TEST. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,568 hrs · 18,091 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 7 FLOOR PROXIMITY STRIP INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRANSPONDER — INOPERATIVE (INTEGRATED COMM) · airframe 22,736 hrs · 17,437 cycles

DURING CLIMB THE CREW REPORTED THE NR 2 TRANSPONDER. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE INTEGRATED COMM /TRANSPONDER UNIT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,595 hrs · 17,332 cycles

SHV - DURING C-CHECK EXTERNAL SKIN CRACKED AT FRAME 50 STRINGER 15R. MAINTENANCE PERFORMED REPAIR ON EXTERNAL SKIN AT FRAME 50 STRINGER 15R IAW EMB-145 EC5330-02393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTY (GWPS) · airframe 20,377 hrs · 15,659 cycles

FLIGHT 2985 - EWR - FLIGHT CREW REPORTED BURNING SMELL IN COCKPIT, GPWS/WINDSHEAR/TCAS INOP, THEN MESSAGE CLEAR. CREW RETURNED TO GATE UNEVENTFULLY. EWR MX REMOVED AND REPLACED GPWS COMPUTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 18,723 hrs · 14,406 cycles

FLIGHT 2767 - EWR - FLIGHT CREW DIVERTED TO EWR DUE TO LANDING GEAR NOT RETRACTING (ORIGINAL FLIGHT WAS ALB TO CLE). EWR MX VERIFIED GAP IN ALL WOW SWITCHES, SERVICED NOSE LANDING GEAR STRUT AND PERFORMED LANDING GEAR OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — CORRODED (NLG) · airframe 18,656 hrs · 14,348 cycles

FLIGHT 2007 - RIC - AFTER TAKING OFF OF DCA TO CLE, FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFULLY. RIC MX FOUND CORROSION ON NOSE DOWN PROX SWITCH. MX CLEANED CORROSION AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: COUPLING — BLOWN (AC PACK) · airframe 18,170 hrs · 13,965 cycles

CLE FLIGHT 2351 - CREW REPORTED BOTH ENGINE BLEEDS CLOSED ADVISORY MESSAGE AND BOTH PACKS CLOSED, ADVISORY MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED TWO PACK COUPLINGS FOR PACK NR 1 AND ONE COUPLING FOR PACK NR 2. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 18,150 hrs · 13,951 cycles

THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON CLIMB. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE NLG WOW PROX SWITCH, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED RT HORIZONTAL STAB LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED CORROSION AND INSTALLED REPAIR DOUBLER AT FRAME 20 ON LT OMEGA BEAM IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 29. MAINTENANCE REMOVED CORROSION IAW EMB-145 SRM 53-22-10 AND INSTALLED FABRICATED REPAIR AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND CPM 51-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED LT HORIZONTAL STABILIZER LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK RT OMEGA BEAM BETWEEN FRMS 40 AND 52 HAS CORROSION. MAINTENANCE REMOVED CORROSION AND FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW IC2009-145/03242B AT FRAME 41, NO CORROSION DAMAGE NOTED AT OTHER FRAMES. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (PAX DOOR) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK PAX DOOR BOTTOM FOUR NUT PLATE HOLES FOR MAIN LINER PANEL CORRODED. MAINTENANCE REPAIRED PAX DOOR LOWER FOUR NUT PLATE ATTACHMENT HOLES FOR MAIN LINER PANEL IAW EC5210-01154 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 38. MAINTENANCE REMOVED CORROSION AT FR 38 IAW EMB-145 SRM 53-23-10 AND REPAIRED LT OMEGA BEAM AT FR 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (AILERON) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B ATTACHMENT POINT HAS TOOLING MARKS. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK NR 4 AND NR 5 FLOOR PROXIMITY LIGHT STRIPS INOP (EMERGENCY LIGHTS). MAINTENANCE REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY HOLDER ASSY IAW EMB-145 AMM 33-50-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (AILERON) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND IAW EC 5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK FRAME 10 JUST ABOVE STR 10L CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND INSTALLED NEW FRAME 10 CHANNEL AT FRAME 10 STRINGER 10L BELOW DV WINDOW CUTOUT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK SKIN DENT JUST FWD OF FWD PRESSURE BULKHEAD AT RT UPPER REINFORCEMENT FOR EA5310-01069. MAINTENANCE REMOVED DAMAGE AND FABRICATED NEW REPAIR DOUBLER AND FILLER IAW IC2009-145/03155, EMB-145 SRM 51-75-04 AND COMPLETED ALL OTHER WORK IAW EC5330-01915. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,954 hrs · 13,791 cycles

SHV - DURING C-CHECK FRAME 10 JUST ABOVE STR 10R CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND INSTALLED NEW FRAME 10 CHANNEL AT FRAME 10 JUST BELOW DV WINDOW CUTOUT AND JUST ABOVE STR 10R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: HEATER — INOPERATIVE (TAT PROBE) · airframe 17,559 hrs · 13,524 cycles

FLIGHT 2915 - FLIGHT CREW REPORTED NR 1 TAT SENSOR HEAT FAIL ON EICAS ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX R&R TAT PROBE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 15,345 hrs · 11,955 cycles

IAH - FLIGHT 2156, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, TEST FLEW WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (ENGINE) · airframe 14,316 hrs · 11,273 cycles

FLT 3158 - EWR - CREW REPORTED THAT ENGINE NR 1 WOULD NOT SHUT-DOWN, E1 NO DISPATCH ON EICS. CREW USED T-HANDLE TO SHUT DOWN THE ENGINE. EWR MX REMOVED AND REPLACED POWER PLANT CONTROL MODULE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — DAMAGED (FIRE DETECTION) · airframe 13,457 hrs · 10,661 cycles

ON CLIMB, 5 MINUTES AFTER T/O, CREW RECEIVED A STEADY E2 FIRE DETECTION FAIL MSG AND THEN IT WENT INTERMITTENT. AIR-RETURNED. MAINTENANCE REPAIRED WIRES W407-14-20 AND W407-13-20 IAW EMB 145 SPWM 20-21-00 WITH REF TO EMB 145 MM 36-11-51. OPERATIONAL CHECK GOOD 26-10-00. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — OUT OF LIMITS (VERTICAL STAB) · airframe 13,422 hrs · 10,637 cycles

TYS - DURING A CURRENT C-CHECK INSPECTION THE VERTICAL STAB HINGE FITTING SPHERICAL BEARING HOUSING ON THE LT AND RT WERE OUT OF LIMITS. MAINTENANCE REAMED BOTH SIDES OF VERTICAL STAB AND REPLACED NEW BUSHINGS IAW EMB 145 SRM 55-30-02. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK.

Part: STRINGER — DENTED (FUSELAGE) · airframe 13,422 hrs · 10,637 cycles

DENT ON FUSELAGE AT FRAME 15 AND STRINGER 20L. CUT OUT DAMAGED SECTION OF STRINGER, DRILLED AND INSTALLED REPAIR IAW EMB SRM 53-00-03 AND 51-40-02. AIRCRAFT STILL IN C-CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,752 hrs · 6,969 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION I/B SIDE AT FR 23-24. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 23-24 IAW EC 5320-01256. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 8,752 hrs · 6,969 cycles

SHV - DURING C-CHECK APU FIREWALL CRACKED AROUND FASTENER 2 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-01483. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

DURING CLIMB THROUGH 15,000 FT, THE CREW REPORTED THE ODOR OF SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. ENGINE RUNS WERE PERFORMED OPERATING THE PRESSURIZATION, AIR CONDITIONING, AND BLEED SYSTEMS AND THE ODOR COULD NOT BE DUPLICATED. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY WITH NO ODOR OF SMOKE IN THE CABIN OR FLIGHT DECK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING ROUTINE INSPECTION ON OVERNIGHT, MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LAMP AT SERVICE DOOR EMERGENCY LIGHT IAW EMB145 MM 33-50-10. OPS.CHECKED GOOD.

Part: LAMP — INOPERATIVE (CABIN)

CLE FLIGHT 2863 THE CREW REPORTED THE AFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE AFT EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

THE CREW REPORTED THE EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT UPPER EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.MAINTENANCE REPLACED THE #4 BATTERY POWER SUPPLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.