N14105

Part: ENGINE — LEAKING (RIGHT) · airframe 38,989 hrs · 22,634 cycles

GPT- THE CREW REPORTED SUSPECTED OIL LEAK NR 1 & 2 ENGINES AND A STRONG BURNT OIL DOOR IN THE COCKPIT. THE AIRCRAFT LANDED IN GPT WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND APPROVED A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER 2 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,375 hrs · 21,489 cycles

DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT BATTERY AND BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 36,459 hrs · 20,818 cycles

THE CREW REPORTED CAPTAIN`S EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE CAPTAIN`S EMERGENCY FLASHLIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: HOSE — LOOSE (RECIRCULATION) · airframe 34,804 hrs · 19,702 cycles

CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. ACFT AIR RETURN BACK TO DEPARTURE. MAINTENANCE INSPECTED AND FOUND HOSE TO NR 1 RECIRCULATION FAN MUFFLER CAUSING CONDENSATION TO POUR IN THE CABIN THROUGH THE LOWER VENTS AT THE CENTER AISLE. MAINTENANCE RESECURED HOSE AND PERFORMED A SUCCESSFUL OPS CHECK. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,787 hrs · 19,689 cycles

DURING MAINTENANCE INSPECTION, THE AFT CABIN EMERGENCY EXIT SIGN AND LT AND RT OVERWING EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SCREW — BACKED OUT (EMERGENCY EXIT) · airframe 32,848 hrs · 18,452 cycles

DURING "A" CHECK, FOUND LT OVERWING EXIT JAMMED. WILL NOT OPEN MAINTANCE FOUND SCREW BACKED OUT ON TRIM. REPLACED SCREW AND PREFORMED OPS CHECK. OPS CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,246 hrs · 18,058 cycles

DURING A MAINTENANCE INSPECTION, EMERGENCY EXIT LIGHTS ON THE INTERIOR EXIT HATCH WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 31,696 hrs · 17,701 cycles

THE CREW REPORTED A CARGO FIRE LIGHT IN FLIGHT. THE CREW DISCHARGED THE CARGO FIRE EXTINGUISHERS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT FOUND NO EVIDENCE OF FIRE AND R & R THE CARGO SMOKE TEST RELAY K0629, CARGO FAN RELAY K0630, BOTH THE FORWARD AND AFT CARGO SMOKE DETECTORS, CARGO FAN, AND BOTH CARGO BAY FIRE EXTINGUISHERS. OPS CHECK PERFORMED WITHOUT DEFECT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 31,696 hrs · 17,701 cycles

THE CREW REPORTED A BAGGAGE FIRE LIGHT IN FLIGHT. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT FOUND NO EVIDENCE OF FIRE AND R & R THE BAGGAGE SMOKE TEST RELAY K0629, BAGGAGE FAN RELAY K0630, BOTH THE FORWARD AND AFT BAGGAGE SMOKE DETECTORS, THE CARGO FAN, AND BOTH BAGGAGE COMPARTMENT FIRE EXTINGUISHERS. OPS CHECKS WERE PERFORMED WITHOUT DEFECT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (AFT CARGO) · airframe 31,692 hrs · 17,698 cycles

CREW REPORTED THE BAGGAGE FIRE EXTINGUISHER LIGHT ILLUMINATED INFLIGHT. NO SIGN OF FIRE, BLEW BOTTLES. MAINTENANCE R & R THE BAGGAGE FIRE BOTTLES. AGAIN REPORTED THE BAGGAGE FIRE LIGHT ILLUMINATED INFLIGHT. MAINTENANCE R & R THE BAGGAGE SMOKE DETECTORS AND RELAYS ALONG WITH THE FIRE BOTTLES AND COMPARTMENT FAN. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 27,805 hrs · 15,272 cycles

CORROSION OUT OF LIMITS AFTER BLEND-OUT, AT NUT PLATE HOLES ON BOTTOM OF PAX DOOR STRUCTURE. REMOVED CORROSION AND INSTALLED NUT PLATE DOUBLERS.

Part: ENGINE — SMOKE (RIGHT) · airframe 27,805 hrs · 15,272 cycles

LAV SMOKE WARNING ON CLIMB-OUT WITH ELECTRICAL BURNING ODOR. ACFT WAS FERRIED TO FOR NR 2 ENGINE CHANGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,231 hrs · 13,554 cycles

DURING SCHEDULED MX INSPECTION ROW 12BC OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. RIC MX REMOVED AND REPLACED ROW 12BC OVERHEAD EMERGENCY EXIT LIGHT BULB WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (SMOKE WARNING) · airframe 13,227 hrs · 24,658 cycles

DEN - FLIGHT 6158, THE CREW REPORTED AN INTERMITTENT BAGGAGE SMOKE INDICATION ON EICAS. MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY TESTED THE BAGGAGE SMOKE DETECTION, PERFORMED ENGINE RUNS AND TAXIED THE AIRCRAFT ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 23,597 hrs · 12,570 cycles

THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON TAKEOFF. MX INSPECTED AND REPLACED THE LT GEAR WOW PROXIMITY SWITCH. ADJUSTED ALL MAIN GEAR WOW PROXIMITY SWITCHES. OPS CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (ZONE 100) · airframe 23,331 hrs · 12,430 cycles

IAH - FLIGHT 2025 THE CREW REPORTED A LANDING GEAR AIR / GRND FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 23,292 hrs · 12,410 cycles

IAH - FLIGHT 2405, DURING CRUISE FLIGHT, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — OPEN (RT COWLING) · airframe 23,150 hrs · 12,334 cycles

FLIGHT 3157, AC N14105, IAH TO SLC TWO PANELS OPENED IN FLIGHT ON RT LOWER ENGINE COWLING. SLC MAINTENANCE ADJUSTED OIL SERVICE DOOR HINGE TO ALLOW CLOSURE OF DOOR WITH LATCHES/APPLIED THREE LAYERS OF SPEED TAPE TO THE DOOR PER FERRY. ALSO, APPLIED THREE LAYERS OF SPEED TAPE TO THE PUNCTURED AREA OF COWLING DOOR. AC N14105 WAS THEN FERRIED TO SHV FOR MAINTENANCE DUE TO THE RT LOWER ENGINE COWLING PANEL DAMAGE FROM TWO PANELS OPENING IN FLIGHT. SHV MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE LOWER COWLING IAW EMB-145 AMM 71-12-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 22,285 hrs · 11,845 cycles

FLIGHT 2985 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX ADJUSTED AND LUBED THE MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,073 hrs · 11,726 cycles

AIRCRAFT HIT A FLOCK OF SEAGULLS AT 11000 FT. AIRCRAFT SUFFERED A BIRD STRIKE TO THE FWD FUSELAGE DAMAGING THE UPPER SKINS AND SUPPORTING STRUCTURE BETWEEN FRM 1 AND THE AFT PRESSURE BULKHEAD BETWEEN STR 15L & 11R. REPAIRED AC IAW EC5300-01018 ALONG WITH ASSOCIATED M-602'S DOCUMENTING ALL DAMAGE AND REPAIRS.

Part: SKIN — DENTED (FUSELAGE) · airframe 20,533 hrs · 10,910 cycles

DENT ON FUSELAGE UNDER STR 11L BETWEEN FRM 19-20. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW ETD2010-145/01128.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 20,384 hrs · 10,825 cycles

MSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK- SMELL THEN DISSIPATED BUT RETURNED ON DESCENT FROM MID 20'S TO APPROX 17000. A/C FERRIED FROM EWR TO TYS. TYS MX REMOVED AND REPLACED THE NR 1 ENGINE ASSY AND OPS AND LEAK CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 20,384 hrs · 10,825 cycles

MSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK - SMELL THEN DISSIPATED BUT RETURNED ON DESCENT FROM MID 20'S TO APPROX 17000. A/C FERRIED FROM EWR TO TYS. TYS MX REMOVED AND REPLACED THE NR 1 ENGINE ASSY AND OPS AND LEAK CHECKED GOOD. DUPLICATE OF CONTROL NUMBER C2XATY -- CORRECTED THE CONTROL NUMBER

Part: LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 19,020 hrs · 10,104 cycles

FLIGHT 2557 - EWR - FLIGHT CREW REPORTED CAPT / F/O AIRSPEED /ALT INDICATOR MISCOMPARE. FLIGHT CREW DIVERTED TO CMH AND LANDED ACFT UNEVENTFULLY. MX DRAINED PITOT STATIC SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,791 hrs · 9,978 cycles

LT EMERGENCY ESCAPE HATCH EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.

Part: RELAY — INOPERATIVE (COCKPIT) · airframe 18,279 hrs · 9,701 cycles

IAH - FLIGHT 3137, THE CREW REPORTED THAT AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR AIR/GROUND RELAY KO024, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 17,950 hrs · 9,527 cycles

PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE NR 0 CARBON SEAL ASSEMBLY IAW RR AE3007A SERIES MM 72-25-25. ALSO, SHUFFLED ENGINE NR 1 FAN BLADES IAW EOTM WORKSHEET CTRL NR 1105022709, (OPS AND VIBE CHECK GOOD AT THIS TIME). THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 17,950 hrs · 9,527 cycles

PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE NR 0 CARBON SEAL ASSEMBLY IAW RR AE3007A SERIES MM 72-25-25. ALSO, SHUFFLED ENGINE NR 1 FAN BLADES IAW EOTM WORKSHEET CTRL NR 1105022709, (OPS AND VIBE CHECK GOOD AT THIS TIME). THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 17,950 hrs · 9,527 cycles

PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE NR 0 CARBON SEAL ASSEMBLY IAW RR AE3007A SERIES MM 72-25-25. ALSO, SHUFFLED ENGINE NR 1 FAN BLADES IAW EOTM WORKSHEET CTRL NR 1105022709, (OPS AND VIBE CHECK GOOD AT THIS TIME). THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 17,941 hrs · 9,519 cycles

FLIGHT 2165 - EWR - FLIGHT CREW REPORTED LAV SMOKE WARNING ON EICAS DURING FLIGHT. EWR MX PERFORMED OPERATIONAL CHECK IN THE SYSTEM AND NO FAULTS WERE FOUND. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,677 hrs · 9,369 cycles

FLIGHT 2393 - EWR - FLIGHT CREW REPORTED THAT DURING CLIMB OUT, "LAV SMOKE" INDICATION SHOWED ON EICAS AND FLIGHT ATTENDANT SAID SHE COULD SMELL SMOKE IN CABIN/LAV. CREW PERFORMED AIR RETURN AND LANDED WITHOUT INCIDENT. EWR MX RAN BOTH ENGINES WITH BLEEDS ON AND COULD NOT DUPLICATE THE PROBLEM. MX R&R LAV SMOKE DETECTOR AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 17,679 hrs · 9,371 cycles

WHILE CLIMBING OUT OF EWR, THE FLIGHT ATTENDANT SMELLED FUMES AND SMOKE IN THE CABIN AND LAV. CREW RETURNED TO EWR AND MX RAN BOTH ENGINES AND FOUND TO BE GLYCOL IN THE BLEED SYSTEM. MX R&R THE LAV SMOKE DETECTOR IAW EMB 145XR MM 26-14-01 AND MM 30-21-00. ACFT WAS RELEASED TO SERVICE.

Part: SWITCH — OUT OF POSITION (REFUEL PANEL) · airframe 17,217 hrs · 9,134 cycles

FLIGHT 2539 - RIC - FLIGHT CREW REPORTED FUEL XFER CRITICAL MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. RIC MX FOUND POWER SELECTION SWITCH ON REFUEL PANEL IN BATT POSITION. MX REPOSITION SWITCH TO NORMAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (COCKPIT) · airframe 14,730 hrs · 7,816 cycles

IAH - FLIGHT 2555, THE CREW REPORTED BRAKE INBOARD INOP ON EICAS DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED WOW RELAY K0200 IAW EMB 145 AMM 32-63-00, OPS CHECK GOOD. TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,611 hrs · 7,754 cycles

IAH - FLIGHT 2901 THE CREW REPORTED SMOKE SMELL FROM THE RECIRC FANS. THE AIRCRAFT LANDED AT IAH UNEVENTFULLY WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPS CHECKED THE RECIRC FANS ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (RT AILERON) · airframe 13,995 hrs · 7,421 cycles

TYS DURING A CURRENT C-CHECK INSPECTION THE RIGHT AILERON PCA BRACKET WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE PCA BRACKET IAW EMB 145XR AMM 27-10-00 AND EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. OPS CHECKS WERE GOOD.

Part: BRACKET — DAMAGED (LT AILERON) · airframe 13,995 hrs · 7,421 cycles

TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON PCA BRACKET HAD A BUSHION THAT WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE PCA BRACKET AND REINSTALL THE AILERON IAW EMB 145XR AMM 27-10-00 AND EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND OPS CHECK GOOD. A/C WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,819 hrs · 6,826 cycles

IAH - FLIGHT 2739, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 12,616 hrs · 6,714 cycles

IAH - FLIGHT 2110, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 11,798 hrs · 6,279 cycles

BFL - FLIGHT 2608, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE GALLEY AND RIGHT WING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — CONTAMINATED · airframe 11,761 hrs · 6,260 cycles

FLT 2279 - ORF - DURING CRUISE, CREW DETECTED SMOKE IN COCKPIT WHEN RECIRC FAN WAS ON. MX FOUND PIECE OF INSULATION ON FWD AVIONICS FAN. MX REMOVED INSULATION AND PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,532 hrs · 6,140 cycles

EWR LOG SQUAWK EMERGENCY LIGHT ABOVE GALLEY DOOR INOP. REMOVED AND REPLACED INVERTER ABOVE GALLEY DOOR IAW EMB145 AMM 33-50-11. OPS CHECK GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,360 hrs · 6,044 cycles

SDF - FIRST FWD RT PHOTOLUMINESCENT FLOOR LIGHTING SECTION MISSING. INSTALLED FWD RT PHOTOLUMINESCENT FLOOR STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,360 hrs · 6,044 cycles

SDF - FIRST FWD LT PHOTOLUMINESCENT FLOOR LIGHTING SECTION MISSING. INSTALLED FIRST FWD LT PHOTOLUMINESCENT FLOOR LIGHT IAW EMB 145 AMM 33-50-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,237 hrs · 5,982 cycles

IAH - FLIGHT 2265, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EXIT SIGN ON THE FORWARD RIGHT BULKHEAD TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,563 hrs · 5,596 cycles

SHV - DURING ROUTINE INSPECTION THE CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 XR AMM 33-50-08. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,233 hrs · 5,413 cycles

IAH - FLIGHT 2183, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE CABIN BULKHEAD EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 9,052 hrs · 4,788 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 49. MAINTENANCE REMOVED THE CORROSION AND REPROTECTED THE AREA IAW EC5310-01371. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,044 hrs · 4,783 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,202 hrs · 3,309 cycles

CLE - FLIGHT 3393, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING BY THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED AND TIMES ARE NOT AVAILABLE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 4,736 hrs · 2,544 cycles

DURING A SCHEDULED C CHECK INSPECTION, THE FWD CROSS MEMBER AT FRAME 20 WAS FOUND TO HAVE CORROSION AT BOTH ENDS. MANTENANCE REMOVED CORRODED AREAS, INSTALLED FILLER, SHIMS AND DOUBLER IAW THE MFG SRM. ACFT PENDING RELEASE UPON COMPLETION OF C-CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,736 hrs · 2,544 cycles

DURING A SCHEDULED 1C INSPECTION CORROSION WAS FOUND BETWEEN FR 24 AND FR 25 ON THE LT OMEGA BEAM. MAINTENANCE CUTOUT THE CORRODED AREA, FAB A DOUBLER AND SHIMS AND REINSTALL IAW SRM 53-21-01. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL C-CHECK WORK.

Part: RELAY — FAILED (FIRE BOTTLE) · airframe 2,191 hrs · 1,158 cycles

BAG EXTINGUISHER NOT ILLUMINATED DURING FIRE DETECT TEST. REMOVED AND REPLACED RELAY NR I01. OPS CHECK GOOD IAW EMB145 MM 26-23-00.