N22971

Part: BALLAST — FAULTY (GALLEY) · airframe 36,931 hrs · 27,848 cycles

THE CREW REPORTED AN ELECTRICAL ODOR NEAR SEAT 2B. MAINTENANCE INSPECTED AND REPLACED GALLEY LIGHT BALLAST. OPS CHECKS WERE GOOD.

Part: DUCT — LOOSE (CABIN AIR) · airframe 35,900 hrs · 27,047 cycles

PILOT REPORTED AN UNUSUAL ODOR IN COCKPIT WITH BLEED 1 LEAK MESSAGE. F/A REPORTED UNUSUAL NOISE IN CABIN. MX FOUND LOOSE DUCT AND SECURED THE DUCT TO HEAT EXCHANGER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GENERATOR — INOPERATIVE (NR 4) · airframe 35,895 hrs · 27,042 cycles

FLT DIVERSION, GEN 4 OFF BUSS. R & R NR 4 GENERATOR IAW AM 24-31-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 35,633 hrs · 26,850 cycles

THE CREW REPORTED AN ELECTRICAL ODOR IN THE BACK OF THE CABIN. MAINTENANCE INSPECTED THE ACFT AND R & R THE LIGHT BALLAST AT ROW 28 ON THE RT SIDE. OPS CHECKS PERFORMED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (ZONE 200) · airframe 35,632 hrs · 26,848 cycles

DURING C CHECK. STRINGER 6R FOUND CRACKED AT FRAME 13. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 35,632 hrs · 26,848 cycles

DURING C-CHECK NR 1 ENGINE FWD LOWER ENGINE MOUNT YOKE CRACKED.

Part: FRAME — DENTED (ZONE 100) · airframe 35,632 hrs · 26,848 cycles

DURING C-CHECK FRM 74 IS DENTED AT STR 14L-15L. MAINTENANCE PERFORMED REPAIR OF FRAME 74 AT STR 14L-15L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,514 hrs · 26,767 cycles

THE CREW REPORTED EMERGENCY EXIT LIGHT WAS INOPERATIVE ON BULKHEAD. MAINTEANCE REPLACED THE EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,832 hrs · 26,264 cycles

DURING A-CK INSPECTION, THE PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 34,483 hrs · 25,991 cycles

CREW REPORTED EMERGENCY LIGHTS NOT ARMED MESSAGE ON EICAS WITH LIGHTS ON. MX R & R THE CABIN LIGHT PANEL ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — FAILED (CABIN LIGHTS) · airframe 34,301 hrs · 25,831 cycles

PILOT REPORTED A BURNING ODOR IN THE CABIN APPEARING TO BE COMING FROM THE AIR CONDITIONING PACKS. MX PERFORMED AN OPS CHECK OF THE AIR CONDITIONING PACKS SUCCESSFULLY WITH NO ABNORMAL ODORS COMING FROM THE PACKS. UPON FURTHER INVESTIGATION MX DID DISCOVER A BURNING ODOR COMING FROM CABIN LIGHT 5A AND 6A. REPLACED LAMPS OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,247 hrs · 25,002 cycles

THE CREW REPORTED A STRONG EXHAUST ODOR IN FLIGHT WITH POWER IN CRUISE. WHEN IN DESCENT THE ODOR SEEMS TO GO AWAY UNTIL POWER IS APPLIED. MX INSPECTED AND PERFORMED TROUBLESHOOTING IAW FIM TASK 72-00-00-810-814. NO DEFECTS WERE FOUND UNABLE TO DUPLICATE. THE ACFT WAS RELEASED FOR SERVICE.

Part: LAMP — BURNED (CABIN) · airframe 30,344 hrs · 22,637 cycles

DURING POST FLIGHT THE CREW NOTED AN ELECTRICAL SMELL AROUND ROW 4 OF THE CABIN. READING LIGHTS WERE DETERMINED TO BE THE SOURCE OF THE ODOR. MX REPLACED THE READING LIGHT LAMPS AT ROW 4, OPS CHECKED THE SYS AND NO ODOR DETECTED.

Part: FIRE DETECTOR — DEFECTIVE (NR 1 ENGINE) · airframe 29,038 hrs · 21,660 cycles

FLIGHT 3153 - EWR - FLIGHT CREW REPORTED E1 FIRE DETECTOR FAIL EN ROUTE - ENGINE OPERATING NORMALLY. EWR MX REMOVED AND REPLACED ENGINE 1 FIRE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 28,591 hrs · 21,324 cycles

CREW REPORTED A STAB ANTI-ICE FAIL MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND PERFORMED OPS CHECKS. NO DEFECTS OR FAULTS WERE FOUND. THE ACFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,113 hrs · 19,389 cycles

LAST THREE CABIN EMERGENCY LIGHT FLOOR STRIPS INOP. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145 AMM 33-50-11 OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: SHUTTLE VALVE — LEAKING (NR 1 BRAKE) · airframe 25,950 hrs · 19,274 cycles

FLIGHT 2571 - YQB - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 2 LOW QTY IND IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX FOUND NR 1 HYD RESERVOIR TO BE LEAKING THROUGH RELIEF VALVE. MX REMOVED AND REPLACED NR 1 RESERVOIR AND PERFORMED OPERATIONAL CHECK HYD RESERVOIR NR 1 SUCCESSFULLY. DURING LEAK CHECK, IT WAS FOUND HYD SYSTEM NR 1 TO BE BLEEDING OVER TO HYD SYSTEM NR 2. MX INSPECTED AND FOUND NR 1 BRAKE SHUTTLE VALVE TO BE BAD. MX REMOVED AND REPLACED NR 1 BRAKE ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA10RI039=> RESERVOIR INFO. SDR C2XA10RI040=> BRAKE INFO.

Part: RESERVOIR — LEAKING (HYDRAULIC SYS) · airframe 25,950 hrs · 19,274 cycles

FLIGHT 2571 - YQB - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 2 LOW QTY IND IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX FOUND NR 1 HYD RESERVOIR TO BE LEAKING THROUGH RELIEF VALVE. MX REMOVED AND REPLACED NR 1 RESERVOIR AND PERFORMED OPERATIONAL CHECK HYD RESERVOIR NR 1 SUCCESSFULLY. DURING LEAK CHECK, IT WAS FOUND HYD SYSTEM NR 1 TO BE BLEEDING OVER TO HYD SYSTEM NR 2. MX INSPECTED AND FOUND NR 1 BRAKE SHUTTLE VALVE TO BE BAD. MX REMOVED AND REPLACED NR 1 BRAKE ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA10RI039=> RESERVOIR INFO. SDR C2XA10RI040=> BRAKE INFO.

Part: SOLENOID VALVE — FAULTY (NLG) · airframe 25,771 hrs · 19,146 cycles

CLE FLT 2915 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS TEMPORARILY AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED BETWEEN FR 59-61. REPAIRED CENTER OMEGA BEAM IAW EC5310-01473. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK LT FUSELAGE SKIN CRACKED AROUND RIVETS FR 77-79 BETWEEN STR 1L AND 7L. REPAIRED SKIN IAW EC 5330-02065. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK LEFT FR 10 CRACKED BETWEEN STR 11L AND 14L. REMOVED AND REPLACED FR 10 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION 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 25,692 hrs · 19,092 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED CENTER OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,514 hrs · 18,968 cycles

LAST THREE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 POSITION BATTERY IAW EMB 145AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,763 hrs · 18,382 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW FOUND THE AFT EMERGENCY LIGHTS WERE NOT ILLUMINATING. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE EMERGENCY LIGHT SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,806 hrs · 17,660 cycles

TYS - DURING ROUTINE MX THE EMERGENCY LIGHT IN THE CEILING PANEL ABOVE ROW 17 WAS FOUND INOP. THE LIGHT BULB WAS REPLACED IAW EMB 145 AMM 33-50-08 AND OPS CHECKED GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: FAIRING — LOOSE (PAX DOOR) · airframe 23,650 hrs · 17,552 cycles

FLIGHT 2788 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX RE-SECURED DOOR FAIRING, LUBRICATED MAIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — SMOKE (CABIN)

FLIGHT 2528 - EWR - FLIGHT CREW REPORTED THAT MULTIPLE PASSENGERS COMPLAINED OF ELECTRICAL SMOKE SMELL IN CABIN BY ROW 15. EWR MAINTENANCE REMOVED AND REPLACED SEAT 15 A CEILING LIGHT ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 21,244 hrs · 15,873 cycles

CLE FLIGHT 2890 - THE CREW REPORTED ENGINE NR 2 CAUSING SMOKE SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW.

Part: WARNING SYSTEM — FALSE ACTIVATION (SMOKE DETECTION) · airframe 21,232 hrs · 15,863 cycles

IAH - FLIGHT 4917, THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT WITH NO EVIDENCE OF SMOKE. CIRCUIT BREAKERS E11 AND E12 WERE PULLED IAW EMERGENCY / ABNORMAL PROCEDURES AND THE WARNING WENT AWAY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND RESET THE CIRCUIT BREAKERS, INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — INTERMITTENT (SMOKE WARNING) · airframe 21,175 hrs · 15,828 cycles

CLE FLIGHT 2905 - THE CREW REPORTED A FALSE LAV SMOKE WARNING DURING CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE TEST PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 21,151 hrs · 15,812 cycles

FLIGHT 3128 - EWR - CREW REPORTED LAVATORY SMOKE DETECTOR WARNING DURING DESCENT. EWR MX REMOVED AND REPLACED SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,155 hrs · 15,815 cycles

FLIGHT 2794 - EWR - CREW REPORTED LAVATORY SMOKE MASTER WARNING. CREW PERFORMED SYSTEM RESET SUCCESSFULLY. NO MAINTENANCE ACTION WAS NECESSARY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RESISTOR — LOOSE (LT ENGINE TRIM) · airframe 20,408 hrs · 15,285 cycles

IAH - FLT 2185 - DURING CLIMB THE CREW REPORTED THAT ENGINE 1 WAS SURGING ON TAKEOFF AND LOST 5% ON N1. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE TRIM RESISTOR IN THE ENGINE 1 -A- HARNESS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,140 hrs · 14,350 cycles

EWR - DURING SCHEDULE MAINTENANCE, MX FOUND AFT CEILING EMERGENCY ROW EXIT IDENTIFIER INOP. MX REMOVED AND REPLACED FWD CEILING EXIT INVERTER IAW EMB-145 AMM 33-50-11 AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,772 hrs · 13,281 cycles

IAH - FLIGHT 2812, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE RESET THE AIRCRAFT ELECTRICAL SYSTEM, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (CABIN)

IAH FLT 2711 - PILOT REPORTED THAT THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. THE EMERGENCY LIGHTING SYSTEM WAS INSPECTED AND A LOOSE WIRE WAS FOUND AT FLOOR PROXIMITY LIGHT NR 4, SPLICE SP9102. THE WIRE WAS RESECURED, THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECKED, AND THE DISCREPANCY CLEARED.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 15,997 hrs · 11,905 cycles

DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10, SECTION 3, FIG 202, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 15,997 hrs · 11,905 cycles

DURING C-CHECK THE AFT SERVICE DOOR FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (CABIN) · airframe 11,829 hrs · 8,667 cycles

DURING C-CHECK FRAME 22 WAS FOUND TO BE CRACKED BETWEEN STRINGER 21 LT AND 21 RT. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04, PG. 205, FIG. 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (ENGINE NACELLE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE RIGHT ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 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: ANGLE — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

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

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED IN TWO PLACES AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FIREWALL IAW EMB 145 SRM 51-40-02 AND EA 5340-01016 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (LT COWLING) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE LEFT UPPER ENGINE COWLING AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE LEFT HAND AFT CARGO FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 68 TO FRAME 71. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSLEAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED JUST UNDER THE COCKPIT STEP PANEL. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01115. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE CARGO DOOR LOWER 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: SILL — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE RIGHT HAND FORWARD SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 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: SILL — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE LEFT HAND FORWARD CARGO FLOOR 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: SILL — CORRODED (FUSELAGE) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE RIGHT HAND CENTER CARGO FLOOR 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: SWITCH — DIRTY (EMERGENCY EXIT) · airframe 11,829 hrs · 8,667 cycles

SHV-DURING C CHECK THE LEFT EMERGENCY EXIT FAILED THE WARNING MESSAGE OPERATIONAL CHECK. MAINTENANCE CLEANED DIRT AND DEBRIS FROM THE EMERGENCY EXIT MICRO SWITCH. MAINTENANCE PERFORMED THE OPERATIONAL CHECK IAW EMB 145 AMM 52-21-00-700-801-A AGAIN. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 10,902 hrs · 7,926 cycles

DURING A SCHEDULED INSPECTION BOTH HORIZONTAL STABILIZER SPHERICAL BEARING WERE FOUND TO BE WORN BEYOND SERVICE LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPHERICAL BEARINGS IAW EMB MM 55-37-00 AND EC 5510-01070. AIRCRAFT RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

THE CREW REPORTED ON APPROACH AFTER STARTING THE APU HAD A BURNING ODOR IN THE COCKPIT AND CABIN. ALSO REPORTED THE BURNING ODOR AT THE GATE WITH THE APU OFF. MAINTENANCE INSPECTED THE CABIN AND COCKPIT LIGHTING SYSTEM, THE RADIO EQUIPMENT FANS AND AVIONICS BAY AREA. ALSO INSPECTED THE CABIN/COCKPIT COOLING FANS WITH NO DEFECTS FOUND. THE APU WAS OPERATIONAL CHECKED AS WAS THE COOLING/HEATING SYSTEM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTING WAS FOUND INOPERATIVE AT ROW 8. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (NLG PROX SENSOR)

CLE FLIGHT 2144 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED THE BACKSHELL AND CLEANED THE CONNECTOR PLUG TO THE NOSE GEAR WEIGHT ON WHEELS PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: ODOR — DETECTED (CABIN)

ATL FLIGHT 3268 THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT AND GALLEY DURING TAXI. THE AIRCRAFT WAS RELEASED IAW 21-26-00. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS WITH BLEEDS AND PACKS ON. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,393 hrs · 5,104 cycles

DURING A ROUTINE CHECK THE AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AND OPS CHECK WAS GOOD IAW AMM-33-50-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED 1C/2C INSPECTION, THERE WAS EVIDENCE OF CORROSION IN THE LEFT AND RIGHT SIDES OF THE CARGO COMPARTMENT FLOORBEAMS AT THE BULKHEAD AREA. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FORWARD FLOORBEAMS IAW 135/145 SRM 51-40-02-03 AND 51-40-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED 1C/2C INSPECTION THE LEFT OMEGA BEAM HAS CORROSION IN THE GALLEY AREA. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW EMB135/145 SRM 53-21-10.

Part: SKIN — GOUGED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED 1C/2C INSPECTION A GOUGE WAS FOUND IN THE CARGO DOOR CUTOUT SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM UNDER THE LAVATORY WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB-SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: STRAP — CORRODED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE BELLY DRAIN GUSSET STRAP AT FRAME 53 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE GUSSET STRAP IAW EMB-145 SRM 51-40-02 AND EMB-145 CPM 51-21-04 AND 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD CENTER OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-20-03, 51-40-06 AND 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CAP — GOUGED (NLG) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR FORWARD UPPER BEARING CAP WAS FOUND TO BE DAMAGED ON THE MATING SURFACE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-1126/02. THE DYE PENETRANT INSPECTION WAS SATISFACTORY AFTER THE REPAIR. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: HOUSING — GOUGED (RT MLG) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND MAIN LANDING GEAR FORWARD SIDE-BRACE BEARING HOUSING WAS FOUND GOUGED ON THE INNER SURFACE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-113/02. THE DYE PENETRANT INSPECTION WAS SATISFACTORY AFTER REPAIR. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: STOP FITTING — GOUGED (FUSELAGE) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT UPPER STOP WAS FOUND GOUGED BEYOND MANUFACTURERS LIMITS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT UPPER STOP IAW EMB-145 MM 20-10-01.

Part: BRACKET — CHAFED (RUDDER) · airframe 7,393 hrs · 5,104 cycles

TYS DURING A SCHEDULED INSPECTION THE RUDDER II MID-BEARING BRACKET WAS FOUND TO BE CHAFED AT THE CONNECTING ROD ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB-145 SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PROXIMITY SWITCH — FAULTY (NOSE GEAR)

TYS - FLIGHT 9379 - AFTER DEPARTURE, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE, ALONG WITH A ENGINE 1/2 REV DISAGREE MESSAGE. THE AIRCRAFT RETURNED TO TYS AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS APPREOVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 5,907 hrs · 4,101 cycles

AVL FLIGHT 3664. CREW REPORTED THAT THEY RECEIVED ENGINE NR 2 ATTCS NO MARGIN MESSAGE ON TAKE-OFF ROLL. MAINTENANCE INSPECTED THE ENGINE AND AFTER SEVERAL ATTEMPTS TO CORRECT THE DISCREPANCY THE AIRCRAFT WAS FERRIED TO TYS. THE RIGHT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPRESSOR — CONTAMINATED (ENGINE)

IAH - FLIGHT 375, THE CREW REPORTED A STRONG ODOR COMING FROM THE NR 1 PACK WHEN SUPPLIED BY ENGINE BLEED AIR. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ODOR WAS CAUSED BY RESIDUAL FLUID FROM THE PREVIOUS NIGHT COMPRESSOR WASH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE)

DURING C CHECK INSPECTION THE CENTER FLOORBEAM GUSSET STRAP UNDER THE LAV MODULE, FRAME 57 TO 60, WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE DAMAGED GUSSET IAW EMB145 SRM 51-40-02. A/C APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE)

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