N16963

Part: SKIN — DEFORMED (LT ELEVATOR) · airframe 35,620 hrs · 26,838 cycles

LT ELEVATOR TIP FAIRING UPPER NUT PLATE HOLE IS ELONGATED. CUT-OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A FILLER AND A DOUBLER. PERFORMED BALANCE CHECK OF ELEVATOR.

Part: SKIN — CRACKED (ZONE 200) · airframe 35,572 hrs · 26,799 cycles

DURING 2A INSPECTION, RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR75 BELOW STR 2R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-034022A, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,719 hrs · 25,345 cycles

DURING ROUTINE MX, SEVERAL FORWARD CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,714 hrs · 23,706 cycles

DURING SCHEDULED ROUTINE INSPECTION, BOTH THE LT & RT SIDE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT SYS BATTERY CHARGER TRAY IAW AMM 33-50-04 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (BLEED AIR SYS) · airframe 30,519 hrs · 22,791 cycles

ORD FLT 6062 - THE CREW REPORTED A BLEED 1 AND 2 FAIL MESSAGE IN FLIGHT ALONG WITH A PACK 2 FAIL:ANTI-ICE FAIL AND THE PRESSURIZATION FAILED AS WELL. MAINTENANCE INSPECTED AND FOUND WIRES AT THE HIGH PRESSURE BLEED SWITCH CONNECTOR P 1203 BROKEN. THE WIRES WERE REPAIRED AND OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,500 hrs · 22,773 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 12-19 EMERGENCY LIGHT FLOOR STRIP INTERMITTENT. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,179 hrs · 22,534 cycles

MAINTENANCE REPORTED THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,036 hrs · 22,434 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. MAINTENANCE FUNCTIONALLY TESTED THE PROXIMITY SWITCHES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 29,859 hrs · 22,304 cycles

JAX --- CREW REPORTED, "LANDING GEAR LEVER DISAGREE" EICAS MESSAGE AFTER TAKE OFF THEN TRIED TO RETRACT THE LANDING GEAR. LANDING GEAR WOULD NOT RETRACT. QRH PROCEDURES PERFORMED. LANDED UNDER-WEIGHT. LANDING WAS UNEVENTFUL. MAINTENANCE PERFORMED A GENERAL VISUAL INSPECTION, INSTALLED LANDING GEAR PINS, AND MAINTENANCE FERRIED THE AIRCRAFT TO IAH FOR REPAIR. IAH MAINTENANCE TROUBLESHOT AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IN REFERENCE TO EMB145 AMM 32-32-02-4, SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 29,589 hrs · 22,304 cycles

IAH - FLIGHT 2296, THE CREW REPORTED THAT THE LANDING GEAR INDICATION WAS THREE RED UP, AND LANDING GEAR MASTER DISAGREE WITH THE LEVER IN THE DOWN POSITION, THE CREW SUCCESSFULLY LOWERED THE LANDING GEAR, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 29,859 hrs · 22,304 cycles

CREW REPORTED, "LANDING GEAR LEVER DISAGREE" EICAS MESSAGE AFTER TAKEOFF THEN TRIED TO RETRACT LANDING GEAR. LANDING GEAR WOULD NOT RETRACT. QRH PROCEDURES PERFORMED. LANDED UNDER-WEIGHT. LANDING WAS UNEVENTFUL. MAINTENANCE PERFORMED A GENERAL VISUAL INSPECTION, INSTALLED LANDING GEAR PINS, AND MAINTENANCE FERRIED AIRCRAFT TO IAH FOR REPAIRS. IAH MAINTENANCE TROUBLESHOT AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IN REFERENCE TO EMB145 32-32-04, SYSTEM OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 28,473 hrs · 21,247 cycles

IAH - FLIGHT 3090, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR AIR/GRND PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP · airframe 27,790 hrs · 20,707 cycles

TYS - A/C WAS IN CLT WHEN NR 2 BATTERY SHOWED OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE 3 AT BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK WAS GOOD AND RELEASED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,665 hrs · 19,894 cycles

IAH - FLIGHT 2347, DURING POST FLIGHT INSPECTION THE AISLE PATH LIGHT STRIP AT THE EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, LT FUSELAGE SKIN HAS CRACKS BETWEEN FR 75-78. REPAIRED SKIN IAW EC 5330-02009. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 39. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, RT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 75-80. REPAIRED SKIN IAW EC 5330-02009. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 39. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK SHEAR CLIP AT FRAME 65 STRINGER 19L-17L HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP AND SPLICE AT FRAME 65 STRINGER 19L-17L IAW EMB-145 EC5320-01494 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLANGE — CRACKED (LAV PAN) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LAV WASTE DRAIN PAN FLANGE IS MISDRILLED AND CRACKED. MAINTENANCE PERFORMED REPAIR OF LAV WASTE DRAIN PAN FLANGE IAW EMB-145 ETD 2009-145/08910. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LT OMEGA BEAM FRAME 29 AT CROSSBEAM ATTACHMENT FLANGE CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED LT OMEGA BEAM FRAME 29 AT CROSSBEAM ATTACHMENT FLANGE IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BOWL — CORRODED (WASTE DUMP) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LAV PAN CORRODED (LEVEL 2 LOCAL) FWD WASTE DRAIN VALVE. MAINTENANCE REMOVED AND REPLACED WASTE DRAIN DUMP BOWL ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT CARBON CROSSBEAM MEMBER MATING SURFACE HAS CORROSION (LEVEL 2 LOCAL) FRAME 32-33. MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM AT CARBON CROSS MEMBER MATING SURFACE AT FRAME 32-33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 300) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK RT SPRING TAB OTBD PANEL ATTACH BRACKET INBD HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT SPRING TAB OTBD PANEL ATTACH BRACKET IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK CARGO DOOR THRESHOLD CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR THRESHOLD IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL) AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAMES 15-21. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 51-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (LAV WASTE) · airframe 25,927 hrs · 19,347 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED LT OMEGA BEAM IAW EC5310-01466 AND EMB 145 SRM 53-00-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK, SERVICE DOOR CUTOUT HAS CORROSION UNDER AFT LWR TEFLON GUIDE. REPAIRED SERVICE DOOR CUTOUT IAW ETD2009-145/09007A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,927 hrs · 19,347 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: FRAME — CRACKED (FUSELAGE) · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LT FRM 10 UNDER DV WINDOW CUTOUT IS CRACKED. MAINTENANCE REMOVED AND REPLACED FUSELAGE FRAME 10 LT SIDE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CORRODED (LT ENGINE) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING CHECK LT ENG FRONT MOUNTING FLANGE HAS 24 CORRODED (LEVEL 2 LOCAL) BOLT HOLES. MAINTENANCE CLEANED, REAMED AND POLISHED UP TO 0.306 CORRODED HOLES AT 24 LT ENG MOUNTING FLANGE BOLT HOLES IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AROUND CARBON CROSSBEAM FR 54. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM AT FR 54 IAW EMB-145 SRM 53-00-10 FIG 202 DET A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 58-59. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM BETWEEN FRAMES 58-59 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 39 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 39 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CORRODED (RT ENGINE) · corrosion level 2 · airframe 25,927 hrs · 19,347 cycles

SHV - DURING C-CHECK RT ENGINE FRONT MOUNTING FLANGE HAS ON CORRODED (LEVEL 2 LOCAL) BOLT HOLE. MAINTENANCE CLEANED, REAMED AND POLISHED ONE CORRODED HOLE AT RT ENGINE FRONT MOUNTING FLANGE IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 25,274 hrs · 18,829 cycles

FLIGHT 2319 - EWR - FLIGHT CREW REPORTED "AIR GROUND FAIL" MESSAGE ON EICAS WITH ASSOCIATED MESSAGES: AIR GROUND SENSOR FAIL, GROUND IDLE STOP FAIL, AND AOA INOP. EWR MX REMOVED AND REPLACED NOSE WOW A/G PROX SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,047 hrs · 18,662 cycles

CLE FLIGHT 2972 - CREW REPORTED CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND RESET SYSTEM. OPERATIONAL CHECK PERFORMED. CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 25,009 hrs · 18,627 cycles

FLIGHT CREW REPORTED CABIN/CABIN EMERGENCY BUTTON ON ICU PANEL ILLUMINATED AND WILL NOT RESET. MX CONTROL INSTRUCTED FLIGHT CREW HOW TO PERFORM SYSTEM RESET. RESET SUCCESSFULL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

THE CREW REPORTED SMOKE OR ELECTRICAL, ODOR IN THE CABIN AND FLIGHTDECK DURING TAXI. THE AC RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINT INSPECTED CONTACTORS, RELAYS AND ELECTRICAL CONNECTIONS IN THE COCKPIT. CHECKED OPERATION FO THE LAV AND CABIN LIGHTS, BALLASTS AND SOCKETS. INSPECTED ENG NR 1 AND NR 2 AND APU FOR LEAKS AND BLEED VALVE OPERATION. NO DEFECTS FOUND. PERFORMED ENGINE RUNS AND APU OPERATION AND NO FAULTS OR EVIDENCE OF SMOKE OR ELECTRICAL FAILURES WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (K)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,578 hrs · 16,372 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND EXIT ROW LIGHT AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED NR 5 INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 21,569 hrs · 16,254 cycles

EWR FLIGHT 2756 - THE CREW REPORTED FUEL FUMES IN THE COCKPIT WHEN THE APU WAS STARTED AND SHUT DOWN. THE APU WAS MEL'ED CONTROL NR 137605. ON 1/18/08 CLE MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL ASSEMBLY P/N 4504616A, S/N 04-02-63, AND THE APU FUEL FLOW DIVIDER P/N 4951486, S/N 0494 AND THE APU ANTI SURGE VALVE P/N 4950899, S/N 1206. OPERATIONAL CHECKS WERE GOOD.

Part: SOLENOID VALVE — FAULTY (APU) · airframe 21,555 hrs · 16,243 cycles

EWR FLIGHT 2947 - THE CREW REPORTED A FUEL SMELL AFTER APU START ON THE GROUND. THE AIRCRAFT WAS RELEASED IAW MEL CONTROL 137419. ON 1/16/08 CLE MAINTENANCE REMOVED AND REPLACED THE MAIN FUEL SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (APU) · airframe 21,529 hrs · 16,223 cycles

IAH - FLIGHT 2481, THE CREW REPORTED A FUEL SMELL ON T/O WITH THE APU RUNNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CAT C, CTL NUMBER 137330, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/12/08 THE AIRCRAFT RON'D IN IAH WHERE MAINTENANCE REMOVED AND REPLACED THE FUEL SOLENOID VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,089 hrs · 15,189 cycles

FLIGHT 2431 - THE FLIGHT CREW NOTED A STRONG FUEL SMELL DURING THE LATE STAGES OF TAKEOFF. MAINTENANCE PERFORMED INSPECTIONS OF THE ENGINES AND AUXILIARY POWER UNIT. HIGH POWER ENGINE RUNS AND OPERATIONAL TESTS OF THE BLEED AIR SYSTEM WERE PERFORMED AND THE DISCREPANCY COULD NOT BE DUPLICATED. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 18,210 hrs · 13,692 cycles

IAH - FLIGHT 2287, THE CREW REPORTED AN ELECTRICAL SMELL ABOVE SEAT 5A. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHTING BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,345 hrs · 11,433 cycles

RIC - DURING ACFT ROUTINE INSPECTION, LT FWD EMERGENCY LIGHT OVER THE WING DID NOT ILLUMINATE. SYSTEM WAS MEL'D. ACFT WAS RELEASED FOR FLT. (OPEN)

Part: CONTROL LEVER — INOPERATIVE (MLG) · airframe 13,851 hrs · 10,276 cycles

CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 13,851 hrs · 10,276 cycles

CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR PROXIMITY SWITCH. AIRCRAFT RETURNED TO SERVICE.

Part: BUSS — BURNED (WINDSHEILD)

DURING CRUISE THE PILOT REPORTED A SMOKE ODOR IN THE COCKPIT. THE AIRCRAFT DIVERTED TO MGM WHERE MAINTENANCE COULD NOT DUPLICATE THE SMOKE ODOR. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE MAINTENANCE FOUND THE CAPTAINS WINDSHIELD BUSS BLOCK TO HAVE EVIDENCE OF OVERHEATING. THE CAPTAINS WINDSHIELD WAS REPLACED AND THE DISCREPANCY CLEARED.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION, THE FORWARD PARTITION ON LEFT SIDE UNDER THE CABIN FIBER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB-135/145 SRM 51-40-02/03 AND CMP51-21-04.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-135/145 SRM-51-20-03, 51-40-02 AND CMP-51-21-04/05/06.

Part: SILL — GOUGED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT AT FRAME 68 WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB-135/145-SRM-51-40-02 / CMP-51-21-04/06.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION THE PAX DOOR LOWER ENTRANCE SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL IAW EMB-135/145 SRM-51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION THE CENTER TOP CAP IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE CLEANED AND BLENDED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-IC2004-145/0302.

Part: SILL — GOUGED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 61 AND 64 WAS FOUND DAMAGED. MAINTENANCE REMOVED THE FLOOR SUPPORT, FABRICATED NEW PARTS, ALODINED, PRIMED AND INSTALLED IAW EMB-135/145 SRM 51-40-02/03 AND CMP-51-21-04.

Part: SILL — CORRODED (DOOR FRAME) · airframe 11,803 hrs · 8,688 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB SRM 57-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FAIRING — GOUGED (RT AILERON) · airframe 11,803 hrs · 8,688 cycles

TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND AILERON TO PCA INBOARD FITTING. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EC5750-01177 AND CPM 51-21-05AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,803 hrs · 8,688 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAME 71. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — DENTED (FUSELAGE) · airframe 10,995 hrs · 8,022 cycles

TYS AIRCRAFT FERRIED FROM BNA, A LARGE DENT WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF THE SERVICE DOOR WITH A DEEP SCRATCH, MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, ALLIDINED, INSTALLED PATCH, PRIMED AND PAINTED I/A/W-EMB-135/145-SRM-51-60-02, 53-21-01 AND CMP-51-21-06, PRESSURIZED GOOD I/A/W-EMB-145-AMM-21-31-00

Part: LEVER — FAULTY (COCKPIT AREA) · airframe 9,004 hrs · 6,427 cycles

EWR---CO3543, CREW REPORTED "AIR RETURN TO EWR: LANDING GEAR WOULD NOT RETRACT QRH UNSUCCESSFUL." MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM #32-32-02. REMOVED AND REPLACED LGEU IAW EMB145 AMM #32-32-01. LANDING GEAR SWING OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: FUEL LINE — LOOSE (APU)

IAH FLIGHT NR 3922 THE CREW REPORTED A STRONG FUEL SMELL IN CABIN AND COCKPIT WHEN STARTING THE APU. MAINTENANCE INSPECTED AND RESECURED FUEL LINE AT THE APU FUEL ACCELERATION CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: APU — FAILED (TAILCONE) · airframe 8,495 hrs · 6,020 cycles

EWR/BTV---CO3526, ON TAXI, CREW REPORTED APU FAIL AND SMOKE ENTERED COCKPIT.....AIRCRAFT RETURNED TO GATE UNEVENTFULLY. MAINTENANCE INSPECTED AIRCRAFT/APU AND FOUND APU SHAFT TURBINE NOT TO SPIN. RAN BOTH ENGINES #1 AND #2. NO SMOKE IN COCKPIT. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RELEASED IAW MEL 49-00-00 CONTROL NUMBER 023128 APU INOPERATIVE. AIRCRAFT RETURNED TO SERVICE.....BTV CO3387, MAINTENANCE REMOVED AND REPLACED APU IAW EMB145 AMM #49-10-01. OPS. AND LEAK CHECKED GOOD. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — FAILED (NLG)

IAH- FLIGHT 3815, THE CREW NOTED THAT THE NOSE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX. PERFORMED A OPERATIONAL CHECK, AND A LEAK CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING ROUTINE MAINTENANCE THE LEFT UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — BURNED OUT (LEFT FUSELAGE)

AGU - During scheduled maintenance the left overwing emergency light was found to be inoperative. Maintenance relamped the light assembly, performed an operational check, and approved the aircraft for return to service.

Part: UPLOCK — FAILED (RT MLG)

IAH- ON CLIMBOUT THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE/UP POSITION/RIGHT MAIN NOT FULLY RETRACTED (AIRBORNE). THE CREW DECLARED EMERGENCY AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPLOCK BOX IN THE RIGHT MAIN LANDING GEAR WHEEL WELL, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT HEAVE CORROSION ON THE LEFT HAND INBOARD FLOORBEAM AT FRAME 20 AT THE COMPOSITE FLOOR SUPPORT ATTACHMENT AREA. MAINTENANCE REPAIRED THE AREA, IAW EMB145 SRM 53-21-10, STEP NR 2 AND PAGE 204, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE UPON RELEASE FROM C-CHECK.

Part: CHARGER — INOPERATIVE

BNA MAINTENANCE DURING A SERVICE CHECK DISCOVERED LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERTIVE.MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY CHARGING UNIT. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: A/C PACK — SMOKE (NR 1)

IAH - FLT 3865 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE COCKPIT. THE CREW PERFORMED AN AIR RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE NR 1 AIRCONDITIONING PACK ON MEL 21-51-00, CAT C CONTROL NR 001233. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE NR 2 AIRCONDITIONING PACK. NO SMOKE OR OTHER DISCREPANCIES WERE NOTED. THE AIR CONDITIONING PACK WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — LACK OF LUBE (RIGHT)

CRP - FLT 3865 - IAH-HRL - DURING CRUISE, THE CREW REPORTED A LOSS OF OIL QUANTITY AND PRESSURE IN THE NR 2 ENGINE. THE CREW PERFORMED AN INFLIGHT SHUTDOWN OF THE AFFECTED ENGINE DECLARED AN EMERGENCY, AND DIVERTED TO CRP WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: EXTINGUISHER — MALFUNCTIONED (CARGO BAY)

EWR - FLT 3677 - CREW REPORTED, CARGO COMPARTMENT FIRE EXT LIGHT ILLUMINATED ON PREFLIGHT. MAINTENANCE PERFORMED VISUAL INSPECTION AND FUNCTIONAL CHECK OF CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPRESSOR — CONTAMINATED (ENGINE)

TYS - CREW REPORTED LAV AND SMOKE BAGGAGE FIRE INDICATIONS IMMEDIATELY AFTER TAKEOFF. AIR RETURNED TO TYS. UPON INSPECTION MAINTENANCE FOUND SMOKE TO BE RESIDUAL COMPRESSOR WASH SOLUTION RAN AIRCRAFT AT HIGH POWER SETTINGS TO BURN OFF EXISTING SOLUTION AIRCRAFT SAFE FOR FURTHER FLIGHT. RELEASED IAW MEL 26-23-00 CATEGORY C PLACARD NR 264513. (M)

Part: A/C PACK — ODOR (NR 1)

EWR - FLT 3899 - CREW REPORTED NR 1 PACK FAULT AND BURNING ODOR IN COCKPIT. MAINTENANCE FOUND RAM AIR DOOR INLET AND PRECOOLER AREA FROZEN AND FILLED WITH ICE. CLEARED ICE AND OPERATIONALLY CHECKED SYSTEM GOOD. (M)

Part: CONTROLLER — INOPERATIVE (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE STUCK ON. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHTING CONTROL MODULE, AND THE ARICRAFT WAS APPROVED FOR RETURN TO SERVICE (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR - FLT 4202 - DURING ROUTINE INSPECTION, FOUND BOTH LEFT AND RIGHT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 3 BATTERY PACK AND OPS CHECKED SYSTEM GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EWR - FLT 4145 - REAR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWR SUPPLY AND OPS CHECKED THE SYSTEM GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EWR - MAINTENANCE REPORTED LAST STRIP OF EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED AFT EMEREGNCY LIGHT BATTERY POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR - FLT 4184 - CREW REPORTED REAR EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY PACK AND OPS CHECKED THE SYSTEM GOOD. (M)

Part: LINE — CLOGGED (FUEL DRAIN)

EWR - FLT 8081 - CREW REPORTED AFTER TAKEOFF IN CLIMB AT 3000 FEET, SMELL IN AIRCRAFT SMOKE OR FUEL, AIR RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SMELL DOWN TO FAULTY APU. APU PLACED ON MEL AND RETURNED TO SERVICE. FOUND APU FUEL DRAIN LINE CLOGGED.. MAINTENANCE UNCLOGGED DRAIN LINE OPERATIONALLY CHECKED APU GOOD. NO FUEL SMELL OR SMOKE NOTED. AIRCRAFT REMOVED FROM MEL AND RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR - FLT 4264 - CREW REPORTED THAT THE AFT EMERGENCY EXIT LIGHT FLOOR STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY PACK AND OPS CHECKED THE SYSTEM GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR - FLT 4145 - DURING SERVICE CHECK, FOUND REAR PORTION OF EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK. OPS CHECKED SYSTEM GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (LT/RT EMER EXIT)

BTV - DURING 4A INSPECTION MAINTENANCE, FOUND LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE AND TWO AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ACM — INOPERATIVE (NR 2)

FLT 4205 - GSP-IAH - THE CREW REPORTED A SMOKE SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR CYCLE MACHINE IAW EMB145 MM 21-51-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 1 FOUR EMERGENCY EXIT LIGHT BATTERY PACK WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (ROW 12)

IAH - DURING PREFLIGHT INSPECTION AT EWR, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB145MM 33-50-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERNAL)

MAINTENANCE REPORTED THAT THE AFT EXTERNAL EMERGENCY LIGHTS ARE NOT WORKING. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 33-50-00 CAT 'C' CONTROL NUMER 184927. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (RT EMER EXIT)

BTV - CO4218 - DURING ROUTINE INSPECTION, FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT, OPS CHECKED SYSTEM GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 3 EMERGENCY BATTERY PACK WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 3-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (LT EMER EXIT)

IAH - DURING A-CHECK INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - FLT 4215 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)