N13968

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 35,360 hrs · 26,601 cycles

GALLEY SERVICE DOOR EMERGENCY LIGHT REPORTED NOT TO BE ILLUMINATING. MX R & R NR 2 EMERGENCY LIGHT BATTERY AND SIGN WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,331 hrs · 24,206 cycles

PASSENGERS REPORTED ELECTRICAL BURNING ODOR COMING FROM VENTS AROUND ROWS 3,4,5 AND 6. MX PERFORMED SUCCESSFUL OPS CHECK OF BOTH PACKS RUNNING WITH NO EVIDENCE OF BURNING ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,547 hrs · 23,560 cycles

DURING ROUTINE CHECK, MX REPORTED THE EXIT SIGN AT SEAT 12A TO BE INOPERATIVE. MX R & R THE INVERTER FOR AFFECTED EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,984 hrs · 23,135 cycles

DURING SCHEDULED MX INSPECTION, AFT CABIN FLOOR PATHWAY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. R & R THE NR 6 INVERTER IAW AMM 33-50-11 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (COCKPIT) · airframe 29,837 hrs · 22,275 cycles

BNA FLT 5955 THE CREW REPORTED THE NR 1 BLEED VALVE WOULD NOT OPEN DURING FLIGHT. CLOSED INDICATION ON THE EICAS. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE PUSHBUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: RELAY — BROKEN (BLEED AIR SYS) · airframe 29,844 hrs · 22,280 cycles

TYS FOR BNA A/C ON CLIMBOUT HAD A EICIAS WITH A MESSAGE THAT THE NR 1 BLEED VALVE WAS CLOSED IN FLIGHT. THE CREW RETURNED TO BNA AND SWAPPED A/C. MAINTENANCE REMOVED AND REPLACED THE PUSHBUTTON IAW EMB 145 AMM 20-13-04. OPS CHECK GOOD. OPS CHECKED THE NR 1 BLEED SYSTEM IAW EMB 145 AMM 36-11-01, OPS CHECK GOOD AND WAS RELEASED.

Part: ENGINE — VIBRATION (NR 1) · airframe 29,441 hrs · 21,934 cycles

DURING CLIMB THE CREW REPORTED A ENGINE ONE HIGH VIBRATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — CRACKED (SPOILER) · airframe 28,775 hrs · 21,443 cycles

TYS - A/C WAS FERRIED FROM ATL TO TYS FOR A SPOILER FAIL MESSAGE AND CIRCUIT BREAKER POP. MAINTENANCE REMOVED AND REPLACED THE LEFT SPEED BRAKE PROX SENSOR IAW EMB 145 AMM 27-63-04, OPS CHECK WAS GOOD AND A/C RELEASED BACK TO SERVICE.

Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 28,670 hrs · 21,371 cycles

IAH - FLIGHT 2044, THE CREW REPORTED THE NUMBER TWO HYDRAULIC SYSTEM HAD A LOW QUANTITY FOLLOWED BY A NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULIC SYSTEM PRESSURE LINE FROM THE PYLON TO THE HYDRAULIC DAMPER. REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,552 hrs · 21,287 cycles

FLIGHT 3064 - EWR - FLIGHT CREW REPORTED POSSIBLE LIGHTNING STRIKE - CLICKING SOUND IN CEILING AND BURNING SMELL TEMPORARELY. EWR MX PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND NO EVIDENCE OF LIGHTNING DAMAGE NO BURNING SIGNS NOTICED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,004 hrs · 20,076 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,004 hrs · 20,076 cycles

SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 75, STRINGER 2L. MAINTENANCE REMOVED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02199. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,004 hrs · 20,076 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,004 hrs · 20,076 cycles

SHV - DURING C-CHECK THE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 62-63 AND STRINGERS 20-21R. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,004 hrs · 20,076 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 37-38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,906 hrs · 18,534 cycles

IAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL WAS FOUND TO HAVE A 55MM CRACK ON THE LOWER LEG BETWEEN THE CAPTAINS WINDSHIELD AND DV WINDOW. MAINTENANCE REMOVED THE DAMAGED SECTION, AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01988, LEAK CHECKED SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (NOSE GEAR) · airframe 24,761 hrs · 18,422 cycles

CLE - FLT 2861 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS WHEN THE GEAR WAS SELECTED DOWN AND THEN CLEARED ONCE THE GEAR WAS DOWN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: OIL SYSTEM — FLUCTUATES (NR 1 ENGINE)

EWR FLIGHT NR 2142 THE CREW REPORTED DURING TAKEOFF ROLL AND INITIAL CLIMBOUT THE OIL PRESSURE REMAINED ABOVE 115 PSI FOR 2 MIN ON THE NR 1 ENGINE. ALSO BELOW 13000 FT THE NR 1 ENGINE OIL PRESSURE WOULD ENTER THE AMBER RANGE WITH THRUST IN DESCENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE.

Part: WIRE HARNESS — DEFECTIVE (NLG)

CLE FLIGHT NR 2320 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE IN FLIGHT. THE GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NOSE GEAR WOW HARNESS AND PROXIMITY SWITCH. OPS CHECKS WERE GOOD.

Part: SOLENOID VALVE — DEFECTIVE (NLG)

FLIGHT 3001 - EWR - FLIGHT CREW REPORTED THAT IT SOUNDED LIKE LANDING GEAR DOORS OPEN IN FLIGHT. EWR MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SOLENOID VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: SUPPORT — CRACKED (DOOR HANDLE) · airframe 21,591 hrs · 16,065 cycles

SHV - DURING C-CHECK PAX DOOR INTERNAL HANDLE SUPPORT CRACKED. MX REMOVED AND REPLACED PAX DOOR INTERNAL HANDLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 21,591 hrs · 16,065 cycles

SHV - DURING C-CHECK WASTE DRAIN SUPPORT CORRODED INSIDE AIRCRAFT. MX REMOVED AND REPLACED WASTE DRAIN DUMP VALVE SUPPORT ASSY IAW EMB 145SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 21,591 hrs · 16,065 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM REPAIR AT FR 20 IS CORRODED. MX REMOVED AND REPLACED PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,960 hrs · 15,625 cycles

DURING ROUTINE MAINTENANCE, THE EXIT MARKER LIGHT AT ROW 3 BC WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,273 hrs · 15,113 cycles

IAH - FLIGHT 2618, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE CENTER AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 19,866 hrs · 14,792 cycles

ATL - FLIGHT 3067, THE CREW REPORTED LAV SMOKE WARNING & HAZE IN CABIN DURING FLIGHT. DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPS CHECK NR 1/ NR 2 PACKS IAW EMB 145 MM AMM 21-51-00. ALL OPS & INDICATIONS NORMAL. VISUALLY INSPECTED, NO DEFECTS NOTED. PLACED LAV SMOKE DETECTOR ON MEL CAT C CONTROL 128344 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 3067 FROM ATL THE CREW REPORTED LAV SMOKE WARNING AND SMOKE FROM UPPER DUCTS IN CABIN AFTER T/O, THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RAN NR 1/ NR 2 ENGINES. FOUND NR 2 ENG BLEED SYSTEM TO BE CAUSING SMOKE IN CABIN. PLACED ON MEL IAW 36-11-05, CAT C CONTROL 128351. THE AIRCRAFT WAS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,677 hrs · 13,924 cycles

IAH FLIGHT 2305, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE LAST ROW OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAST SECTION OF AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (NR 1) · airframe 18,597 hrs · 13,862 cycles

IAH - FLIGHT 2082, DURING TAKEOFF ROLL, THE CREW REPORTED A STRONG SMOKE ODOR INVADED THE CABIN AND FLIGHT DECK. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 16,969 hrs · 12,575 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT AND MOISTURE IN THE LINES. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED (CABIN) · airframe 16,701 hrs · 12,370 cycles

CLT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, ELECTRICAL ODOR, CREW DID AN AIR RETURN, OVERWEIGHT LANDING, NORMAL LANDING AND ROLL OUT. MAINTENANCE FOUND SOURCE OF SMOKE AND ELECTRICAL ODOR TO BE COMING FROM THE READING LIGHTS AT SEATS 6A AND 7A, MAINTENANCE REPLACED THE LIGHTS IAW-EMB-145AMM-33-25-02, OPS CHECKED GOOD, AND C/W EC0550-01004, NO OVERWEIGHT LANDING INSPECTION REQUIRED. LOG PAGE 2054906, FLIGHT 3281

Part: SIGN — FAULTY (EMERGENCY EXIT) · airframe 14,865 hrs · 10,911 cycles

DURING 5A INSPECTION, MAINTENANCE FOUND THE AFT GALLEY EMERGENCY EXIT SIGN FAULTY. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-14. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE 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 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOVED AND REPLACED THE RIGHT TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BRACKET — CORRODED (SINK DRAIN) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED AND INSTALL THE NEW BRACKET IAW EMB 13/145 SRM 51-40-02; 51-30-03; 51-21-03; 04; 05 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-21-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FRAME — GOUGED (APU FIREWALL) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLENDED DYE PEEN GOUGE AREA, REMOVED RIVETS, FAB DOUBLER AND INSTALL IAW EC 5330-01352. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE EFFECTED AREA AND INSTALL NEW REPAIR PART IAW EMB 135/145 SRM 53-21-10; 53-21-03 AND 51-40-06 ALSO CPM 51-21-04; 05; 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BUSHING — CORRODED (RUDDER) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 20-10-08. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 12,058 hrs · 8,772 cycles

DURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. THEN INSTALL FAB PART IAW EMB 135/145 SRM 51-30-03; SRM 51-40-02; 03; 04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (GALLEY FLOOR) · airframe 12,057 hrs · 8,772 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 12,057 hrs · 8,772 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (GALLEY FLOOR) · airframe 12,057 hrs · 8,772 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW EMB SRM 51-40-02 AND 57-20-03. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FAN — SEIZED (A/C BAY)

CLE FLIGHT NR 2123) THE CREW REPORTED A VERY STRONG SMELL OF SMOKE FROM CABIN ON APPROACH. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND THE NR 2 RECIRCULATION FAN WAS SEIZED. MAINTENANCE REPLACED THE NR 2 RECIRCULATION FAN. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE — DETECTED (COCKPIT)

CLE) FLIGHT NR 3230, THE CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE ON DESCENT INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 BLEED AIR SYSTEM,THE NR 1 AND NR 2 ENGINES AND APU. NO DEFECTS WERE FOUND. MAINTENANCE SUSPECT GLYCOL ODOR.

Part: ENGINE — FAILED (NR 1)

STL FLIGHT NR 2368 THE CREW REPORTED THE NR 1 ENGINE UNCOMMANDED SHUT DOWN ON APPROACH INTO STL.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 9,204 hrs · 6,548 cycles

DURING CLIMB RECEIVED A ICAS MESSAGE OF LDG AIR/GND FAIL AT ROTATION. LANDING GEAR WOULDN'T RETRACT. AIR RETURN AND MAINT FOUND PROX SWITCHES OUT OF ADJUSTMENT. DID A RE-ADJUSTMENT OF THE SWITCHES AND DID THE GEAR SWINGS AS REQUIRED. A/C WAS PUT BACK INTO SERVICE. ALL WORK WAS IAW EMB 135/145 AMM32-34-00 GEAR SWINGS AND 32-62-00 ADJUSTMENT OF SWITCHES.

Part: APU — SEIZED (TAIL CONE) · airframe 9,157 hrs · 6,504 cycles

EWR FLT2578 CREW REPORTED DURING APU START APU FAILED INDICATION WAS INSTRUCTED I HAD A FIRE BLEW EXTINGUISHER BOTTLE. MX FOUND APU SIEZED INSPECTED AND PLACED ON MEL. #49-00-00. ACFT RELEASED FOR SERVICE. SDR REMAINS OPEN.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,027 hrs · 5,619 cycles

SHV- DURING C-CHECK INSPECTION, FRAME 18-19 RIGHT HAND OUTBOARD SILL FORWARD OF SERVICE DOOR HAD THREE AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OUTBOARD SILL BETWEEN FRAMES 18 AND 19 IAW EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,027 hrs · 5,619 cycles

SHV- DURING C-CHECK INSPECTION, FRAME 22 RIGHT HAND OUTBOARD SILL AFT OF SERVICE DOOR WAS FOUND TO HAVE FOUR AREAS OF CORROSION. MAINTENANCE OUT OF LIMITS RIGHT HAND OUTBOARD SILL IAW EMB 145-SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

DURING 3A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND TIGHTENED THE CONNECTOR ON THE EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (COCKPIT)

BTV DURING OPERATIONAL CHECK OF LANDING GEAR WARNING SYSTEM THE RIGHT DOWN INDICATOR DID NOT SHOW DOWN AND LOCKED. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

SDF FLIGHT 4077 THE CREW REPORTED THE LAST THREE ROWS OF EMERGENCY FLOOR AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

TYS. DURING HEAVY CHECK INSPECTION CORROSION WAS FOUND ON THE CENTER FLOOR BEAM AT FRAME 19A BETWEEN STRINGERS 21L AND 21R. MX REMOVED/REPLACED THE FLOOR BEAM IAW EMB-145 SRM 51-40-02.

Part: ENGINE — ODOR (RIGHT)

IAH-FLIGHT 3876 FROM OKC TO IAH, THE CREW REPORTED AN EXTREMELY STRONG EXHAUST SMELL WHEN ANTI-ICE WAS ON IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (CABIN)

IAH - DURING FLIGHT 3941 - THE CREW REPORTED A PUNGENT ODOR IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 RECIRCULATION FAN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RECIRCULATION FAN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

TYS - FLT 4301 - CREW REPORTED THAT AFTER TAKEOFF THEY OBSERVED SMOKE IN THE LAVATORY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED SEVERAL ENGINE RUN OPERATIONAL CHECKS WITH NO DISCREPANCIES NOTED. AIRCRAFT RELEASED FOR SERVICE. (M)