N13964

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,191 hrs · 26,775 cycles

DURING C-CHECK, INSPECTION FOUND CORROSION AT STRINGER 21R AND 21L FRAMES 13 TO 14. MX R & R STRINGER SPLICES IAW SRM 51-40-02.

Part: LAMP — ARCED (ZONE 900) · airframe 34,330 hrs · 26,058 cycles

F/A REPORTED A BURNING ODOR COMING FROM CEILING LIGHT IN GALLEY ONCE TURNED OFF, THE ODOR DISSAPATED. MX R & R THE GALLEY CEILING LIGHT LAMP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SLEEVE — LEAKING (ANTI ICE SYS) · airframe 32,670 hrs · 24,762 cycles

CREW REPORTED ICE COND- ANTI ICE SYS INOPERATIVE WITH WING ANTI/ICE FAIL. AN ODOR THAT SMELLED LIKE BURNED CRAYONS ENTERED THE CABIN. ANTI-ICE WAS OBSERVED TO WORK INTERMITTENTLY. MX R & R DUAL TEMP CONTROL VALVE SLEEVES THAT WERE FOUND LEAKING. OPS CHECKS WERE SUCCESSFUL AND NO ODOR'S NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,169 hrs · 22,075 cycles

RT SIDE OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW EMB 145 AMM 33-50-07. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 9,949 hrs · 7,334 cycles

IAH - FLIGHT 2674, THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 27,422 hrs · 20,728 cycles

FLIGHT 2549 - EWR - FLIGHT CREW REPORTED GALLEY SMOKE DETECTOR PANEL STAYS ON WHEN BUTTON IS PUSHED. EWR MX REMOVED AND REPLACED SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 25,988 hrs · 19,659 cycles

IAH - FLIGHT 2139, THE CREW REPORTED THAT THE LEFT LANDING GEAR UP INDICATIONS ARE INDICATING RED IN THE UPLOCK POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPLOCK PROXIMITY SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (LT MLG) · airframe 25,988 hrs · 19,659 cycles

IAH - FLIGHT 2139, THE CREW REPORTED THAT THE LEFT LANDING GEAR UP INDICATIONS ARE INDICATING RED IN THE UPLOCK POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPLOCK PROXIMITY SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK FR 65 HAS CORROSION BETWEEN STR 16L AND 17L. REPAIRED FR 65 IAW EC5310-01505. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK RT EXTERNAL NOSE FUSELAGE SKIN HAS LIGHTNING STRIKES. MAINTENANCE REPAIRED RT EXTERNAL NOSE FUSELAGE SKIN IAW EC5330-02070. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FLOOR SKIN FR 17-19 STR 21L-21R. MAINTENANCE PERFORMED REPAIR OF FLOOR SKIN FR 17-19 STR 21L-21R STR 21L-21R IAW EC5330-02069. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,436 hrs · 10,254 cycles

SHV - DURING C-CHECK AFT FLOOR PROX LIGHT INOP. MAINTENANCE REMOVED AND REPLACED PROXIMITY LIGHT IAW EMB-145 AMM 3-50-12. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK DENT ON FUSELAGE FWD OF FRM 3 AT 11 O'CLOCK POSITION. MAINTENANCE PERFORMED REPAIR OF DENT ON FUSELAGE FWD OF FRM 3 AT 11 O'CLOCK POSITION IAW EC5330-02073. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV DURING C-CHECK RT OMEGA BEAM CORRODED BETWEEN FR 18-19. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV DURING C-CHECK SKIN HAS CORROSION FR 17-19 STR 21L- 21R. REPAIRED SKIN IAW EC5330-02069. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,936 hrs · 19,617 cycles

SHV DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION FR 65-68. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 24. REPAIRED LT OMEGA BEAM IAW EC 5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,936 hrs · 19,617 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 43. REPAIRED LT OMEGA BEAM IAW EC 5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAULTY (CABIN) · airframe 25,251 hrs · 19,095 cycles

CLE - FLT 2150 - THE CREW REPORTED A ELECTRICAL SMELL BY THE OVERWING EXIT DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LIGHTING BALLAST AT ROW 12A. OPERATIONAL CHECKS WERE GOOD.

Part: UPLOCK — INOPERATIVE (NLG) · airframe 22,988 hrs · 17,385 cycles

BTR FLIGHT 2789. THE CREW REPORTED A LG LEVER DISAGREE MSG IN FLIGHT AND THE NOSE GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO BTR WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE MX R&R THE NLG UPLOCK BOX. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 22,815 hrs · 17,276 cycles

FLIGHT 3053 - EWR - FLIGHT CREW REPORTED A STRONG ELECTRICAL/HOT PLASTIC SMELL NEAR SEAT 1A ASSOCIATED WITH OVERHEAD PANEL. EWR MX REMOVED AND REPLACED BALLAST AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,444 hrs · 17,008 cycles

EWR MX DURING ROUTINE MX EWR MX FOUND LT OVER WING EMERGENCY LIGHT INOPERATIVE. MX R&R LIGHT BULB AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UPLOCK — FAILED (RT MLG) · airframe 21,507 hrs · 16,366 cycles

TYS FLT 2926 - AIR RETURN BACK TO TYS FOR LANDING GEAR AIR GROUND FAIL AND LANDING GEAR LEVER DISAGREE ON EICAS. THE RT MLG UPLOCK BOX WAS REMOVED AND REPLACED AND OPS CHECKED GOOD IAW EMB AMM 32-33-10. A/C WAS RETURNED TO SERVICE.

Part: INLET — OBSTRUCTED (APU) · airframe 21,376 hrs · 16,277 cycles

CLE FLIGHT 2423 - THE CREW REPORTED AN APU FIRE WARNING DURING TAXI WITH APU AUTOSHUT DOWN. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REMOVED EXCESSIVE BUILD UP OF ICE AND SNOW FROM THE APU INLET. OPERATIONAL CHECKS OF APU WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,565 hrs · 15,677 cycles

FLT 2882 - EWR - CREW REPORTED EMERGENCY FLOOR STRIPS INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO BAY) · airframe 20,527 hrs · 15,645 cycles

CXO - FLIGHT 4945, THE CREW REPORTED THAT THE BAGGAGE EXT LIGHT ILLUMINATES IN FLIGHT. THE AIRCRAFT LANDED IN CXO WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE SMOKE DETECTORS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 20,525 hrs · 15,643 cycles

EMERGENCY PROX LIGHT INOP. RERACKED EMERGENCY LIGHT BATTERY NR 2 & 3 IAW EMB 145 SWPM 20-21-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,289 hrs · 15,470 cycles

FLT 2355 EWR - EMERGENCY FLOOR PROXIMITY RIGHT STRIP INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY STRIP IAW EMB 145 AMM 33-50-12. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: CONNECTOR — BROKEN (CABIN) · airframe 20,285 hrs · 15,466 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND NR 3 EMERGENCY FLOOR PROXIMITY LIGHT STRIP HAD THE CONNECTOR BROKEN. MX REMOVED AND REPLACED CONNECTOR PIN IAW EMB 145 AMM 20-13-12 AND WM 33-50-50. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,832 hrs · 15,136 cycles

CREW REPORTED OVERWING EMERGENCY LIGHT INOP. MX MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,223 hrs · 13,898 cycles

STL - DURING MAINTENANCE INSPECTION, THE NR 2 AND 3 EMERGENCY FLOOR LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 17,754 hrs · 13,521 cycles

DURING ROUTINE MAINTENANCE, THE AFT CABIN AISLE PATH EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACE THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — FAULTY (FUSELAGE) · airframe 16,541 hrs · 12,551 cycles

DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ON RIGHT SIDEWALL AFT OF THE EMERGENCY EXIT HATCH NOT WORKING. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM NR 33-50-00. OPS CHECKED GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYSTEM) · airframe 16,394 hrs · 12,440 cycles

DURING FLIGHT, PILOT REPORT LOW HYDRAULIC QUANTITY INDICATION ON NR 1 ENGINE AND DECLARED EMERGENCY LANDING. MX FOUND NR 1 ENGINE PUMP LEAKING. REMOVED AND REPLACED NR 1 ENGINE HYD PUMP IAW AMM 29-10-03 LEAK AND OPS CHECK GOOD. SERVICED NR 1 HYD SYSTEM IAW EMB 145 AMM 12-13-01. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,174 hrs · 12,271 cycles

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY CHASSIS ASSY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,151 hrs · 12,250 cycles

SDF - OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY SUPPLY NR 4 TRAY IAW EMB 145 VCMM 25-60-03. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · airframe 15,590 hrs · 11,800 cycles

DURING A SCHEDULED INSPECTION THE CENTER OMEGA BEAM IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM. IAW SRM-51-40-02.

Part: LIGHT — FAULTY (FUSELAGE) · airframe 14,645 hrs · 11,051 cycles

BTV-CO2366, DURING 1A INSPECTION, MAINTENANCE FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT TO BE NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW EMB145 AMM NR 33-50-10, OPS CHECKED GOOD.

Part: ENGINE — DAMAGED (LEFT) · airframe 13,932 hrs · 10,473 cycles

IAH - FLIGHT 2720, THE CREW REPORTED THAT DURING FLIGHT THEY SMELLED A BURNED PACK SMELL WITH NO INDICATION OF SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,774 hrs · 10,351 cycles

DURING MAINTENANCE INSPECTION, ONE AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED.

Part: DUAL VALVE — INOPERATIVE (NR 1 A/C PACK) · airframe 13,783 hrs · 10,357 cycles

EWR - CREW REPORTED THAT THE NR 1 PACK WAS BLOWING ONLY WARM AIR IN AUTO & MANUAL MODES WITH MINIMAL AIRFLOW, AND A BURNING SMELL AT LOW POWER SETTINGS. THE AIRCRAFT WAS RELEASED ON MEL 21-51-00-1 CONTROL NR 048227. FLIGHT 3138 IAH MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK DUAL VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 13,540 hrs · 10,171 cycles

IAH - FLIGHT 2964, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY TESTED THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM SEVERAL TIMES WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (READING LIGHT) · airframe 5,164 hrs · 4,153 cycles

CREW REPORTED, SMOKE CAME FROM FIRST OFFICERS YOKE READING LIGHT AFTER LANDING. MAINTENANCE IN MSN DEACTIVATED FIRST OFFICER'S CHARTHOLDER LIGHT AND RELEASED THE AIRCRAFT IAW MEL 33-10-00 CAT-C CONTROL 046503. UPON ARRIVAL INTO EWR MAINTENANCE SECURED CHARTHOLDER WIRES AND OPS CHECKED LIGHTS, OPS CHECKED GOOD IAW EMB145 MM 33-11-01. NO SMOKE NOTED. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (APU)

IAH - FLIGHT 2197, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED AFTER LANDING. MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ADC — BURNED OUT (COCKPIT)

DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AIR DATA COMPUTER TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COMPUTER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 11,718 hrs · 8,738 cycles

CREW REPORTED, STRONG ODOR OF FUEL/OIL IN COCKPIT AND CABIN AFTER EVERY APU START. MAINTENANCE INSPECTED, PERFORMED SEVERAL APU STARTS IAW EMB145 AMM 49-00-00. OPS AND LEAKED CHECKED GOOD. NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE THE FORWARD EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTS AND CLEARED THE DISCREPANCY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED THE LIGHT AND CLEARED THE DISCREPANCY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,531 hrs · 8,592 cycles

RT SIDE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED ON MEL 33-50-00/1, PLACARD NR 038565 FOR FURTHER TROUBLESHOOTING. MAINTENANCE RELAMPED THE EMERGENCY EXIT LIGHT, OPERATIONAL CHECKED GOOD.

Part: CLIP — CORRODED (FUSELAGE) · airframe 11,394 hrs · 8,483 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SHEAR CLIP AT FR59 BETWEEN STR 20L AND 21L. MAINTENANCE REMOVED AND REPLACED THE SHEAR CLIP IAW EMB 135/145 SRM 51-40-02.

Part: CLIP — CORRODED (FUSELAGE) · airframe 11,394 hrs · 8,483 cycles

TYS, DURING A SCHEDULED INSPECTION THE SHEAR CLIP AT FR61 BETWEEN ST20L AND 21L WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CLIP IAW EMB-135/145 SRM 51-40-02.

Part: SUPPORT — CORRODED (LAVATORY) · airframe 11,394 hrs · 8,483 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT FLOOR SUPPORT BETWEEN FR60 AND 61, STR 161 AND 181. MAINTENANCE CUT OUT THE CORRODED AREA, FABRICATED A NEW FLOOR SUPPORT, ALODINED, PRIMED, PAINTED AND INSTALLED IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-06, CMP-51-40-02/03/06.

Part: BRACKET — CORRODED (STAB PULLEY) · airframe 11,394 hrs · 8,483 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT SUPPORT PULLY CMD STAB BRACKET BETWEEN FR60 AND 61, STR 21L AND 20L. MAINTENANCE REMOVED AND REPLACED THE PULLY SUPPORT BRACKET IAW EMB 135/145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE LEFT OMEGA BEAM WAS CORRODED AT THE BOTTOM OF THE GALLEY RAMP ANGLE. MAINT REMOVED THE OMEGA BEAM, FAB SPLICE DOUBLER, ALODINED, PRIMED AND INSTALL SPLICE DOUBLER AND INSTALL THE NEW OMEGA BEAM IAW EMB 135/145 SRM 51-40-02; 53-21-10; CPM 51-21-04-05 AND SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE LEFT SILL AT STR 16L AND FR 59 AND 61. MAINT REMOVED AND REPLACED THE LEFT FLOOR SILL AT THE DAMAGE AREA IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE LT OMEGA BEAM WAS CORRODED AT BOLT HOLES BETWEEN FR 20 AND FR 25. MAINT REMOVED AND REPLACED THE OMEGA BEAM AT DAMAGE AREA AND REINSTALL THE TOPCAP IAW EMB 135/145 AMM 20-10-01 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE FORWARD SERVICE DOOR SILL WAS FOUND CORRODED. MAINT CLEANED UP THE CORROSION, REPAIRED, ALODINED, PRIMED AND PAINTED IAW EMB 135/145 EC 2003-145/1158; SRM 53-21-10; CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE Z-PROFILE BEHIND SERVICE DOOR AT GALLEY WAS CORRODED. MAINT REMOVED AND REPLACED THE Z-PROFILE IN GALLEY IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE MAIN DOOR SILL WAS CORRODED AT THE NUT PLATES. MAINT REMOVED AND REPLACED THE MAIN DOOR SILL AND NUT PLATES. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,395 hrs · 8,483 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE CENTER TOP CAP IN LAV WAS CORRODED. MAINT REMOVED AND REPLACED THE CENTER TOP-CAP IN THE LAV, ALL WORK WAS IAW SRM 51-40-02 AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED MAINTENANCE THE AFT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT#2099 THE CREW REPORTED 2 EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST.MAINTENANCE INSPECTED AND REPLACED THE #2 INVERTER.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE NR 1 EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH FLIGHT 3650, THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE AT THE MAIN CABIN DOOR. MAINTENANCE INSPECTED AND REPLACED THE AISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY AISLE PATH LIGHTS FORWARD STRIP FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY AISLE PATH LIGHT STRIP. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RECEPTACLE — DIRTY (CABIN)

IAH- DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY AISLE PATH LIGHTS FORWARD STRIP WAS INTERMITTENT. IAH- MAINTENANCE CLEANED AND RESECURED THE LIGHT STRIP CONNECTOR, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

IAH- THE CREW NOTED THAT THE FORWARD EXIT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE SECURED A LOOSE CONNECTOR ON THE EMERGENCY EXIT LIGHT ASSY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3175, THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 4040 THE CREW REPORTED THE CABIN EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — CRACKED

ORF Flt#3483-Crew reported Air/Ground circiut breaker A29 popped. Maintenance found the # 2 Wieght on Wheels proximity sensor cracked.Maintenance removed and replaced the # 2 Weight on Wheels proximity sensor and performed a satisfactory system operational test. The aircraft was approved for return to service.

Part: SILL — CORRODED (FUSELAGE)

IAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACES OF FLOORBEAMS FROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 19 TO FRAME 20 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM C-CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE REMOVED THE CORRODED AREA, FABRICATED A FILLER, REINFORCEMENT AND INSTALLED IT ON THE OMEGA BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM C-CHECK.

Part: SILL — CORRODED (FUSELAGE)

IAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON THE UPPER SURFACES OR THE FLOORBEAMS FROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 22 TO FRAME 23 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM C-CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN)

IAH- DURING "C" CHECK IT WAS NOTED THAT THE FLOOR BEAM CROSS STRUCTURE ABOVE FUSELAGE FRAME 23 WAS CORRODED AT THE INBOARD FORWARD CORNER. IAH- MAINTENANCE REMOVED THE DAMAGED AREA,AND, INSTALLED A DOUBLER WITH A FILLER,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WHEN RELEASED FROM "C" CHECK.

Part: BATTERY — DISCHARGED

CLE FLT. #3369 THE CREW REPORTED 2 FLOOR EMERGENCY LIGHT STRIPS INOPERTIVE.MAINTENANCE REPLACED #3 EMERGENCY FLOOR LIGHTING BATTERY PACK AND CHARGER BASE. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING AT SEATS 8A THRU 12A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

SLW - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING AT ROW 11-12 WAS INOPERATIVE. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING 1A INSPECTION IT WAS NOTED THAT THE EMERGENCY FLOOR LIGHTING MIDDLE SECTION DID NOT ILLUMINATE WHEN SELECTED. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY, OPERATIONAL CHECKED. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE FLIGHT 4075 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 12. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK NR 3. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT 4058 THE CREW REPORTED EMERGENCY LIGHTS OUT ON AISLE PATH LIGHTING. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING 4-A INSPECTION, THE NUMBER FIVE AND SIX FLOOR EMERGENCY LIGHTS, AND THE LEFT HAND DOOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EWR--CO4095, CREW REPORTED EMERGENCY BATTERY PACKS INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM AND FOUND BATTERY POWER PACKS DEFECTIVE. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER PACKS. OPS CHECKED SYSTEM GOOD.

Part: NOZZLE — ODOR (NR 2 ENGINE)

AMA - FLIGHT 4022, THE CREW REPORTED A FUEL SMELL IN THE COCKPIT AND CABIN, THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 4 THROUGH NR 13 FUEL NOZZLES ON THE NUMBER TWO ENGINE IN ACCORDANCE WITH R/R MM 73-11-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE PROBLEM REOCCURED ON 03/02/01 ON FLIGHT 3997 FROM LBB TO IAH. THE AIRCRAFT RETURNED TO LBB WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1, 2, 3, 14, 15 AND 16 FUEL NOZZLES ON THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WITH NO FURTHER INCIDENTS TO DATE.

Part: FAN — INOPERATIVE (CABIN)

EWR - FLIGHT 4148, THE CREW REPORTED THAT DURING THE IN-FLIGHT PORTION OF THE ICE TEST THE CABIN BEGAN TO FILL WITH SMOKE AND A STRONG ODOR. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NUMBER TWO RECIRCULATION FAN ON MEL 21-24-01 CONTROL NR 007600, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON 03/03/01 WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RECIRCULATION FAN, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (CABIN)

CAE - FLIGHT 4205, THE CREW REPORTED SMOKE IN THE CABIN, THE AIRCRAFT DIVERTED TO CAE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE AIR CONDITIONING SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

IAH - FLIGHT 4205, THE CREW REPORTED A STRONG ODOR IN THE COCKPIT AND CABIN. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE AIR CONDITIONING SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (RT EXTERIOR)

BNA - DURING MAINTENANCE INSPECTION, THE TOP RT EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

CLE - FLT 3965 - THE CREW REPORTED A SECTION OF EMERGENCY LIGHTING INOPERATIVE NEAR THE EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD IAW 33-50-04 AND 33-50-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT FLOOR PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK IN ACCORDANCE WITH EMB145 M/M 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND ONE AISLE PATH LIGHT STRIP WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CENTER CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT CENTER FLOOR CABIN EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOOR EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: HOSE — CUT (ENGINE)

PVD REPORTED LOSS OF SYSTEM ONE HYDRAULIC QUANTITY IN CRUISE FLIGHT, DECLARED EMERGENCY AND DIVERTED INTO EWR.. A/C LANDED UNEVENTFULLY. MX FOUND A CUT HYDRAULIC HOSE ON LEFT ENGINE DRIVEN PUMP..REMOVED/REPLACED HYDRAULIC HOSE ON LT. EDP IAW EM145 MM29-20-04. OPS. AND LEAK CHECKED GOOD.

Part: STRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHTS AT 11 ABC, 12 ABC, AND 14 ABC WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK IAW EMB145-LR MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — LOOSE (CABIN)

TYS - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE FORWARD SECTION OF EMERGENCY AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE RESECURED THE BATTERY PACK ON THE AFFECTED POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, CREW REPORTED THE LEFT AFT EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 MM 33-50-04 AND 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)