N13997

Part: MOUNT — CRACKED (LT ENGINE) · airframe 36,378 hrs · 27,896 cycles

DURING C-CHECK, THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01162. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 36,378 hrs · 27,896 cycles

DURING C-CHECK, THE MAIN CABIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION, PERFORMED A DOUBLER REPAIR IAW EC5210-01356. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (RUDDER) · airframe 36,378 hrs · 27,896 cycles

DURING C-CHECK, THE RUDDER I CENTER LOWER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 35,045 hrs · 26,859 cycles

LEFT FORWARD FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R NR 1 BATTERY FUSE. OPS CHECKED GOOD.

Part: COFFEEMAKER — SHORTED (GALLEY) · airframe 34,598 hrs · 26,495 cycles

F/A REPORTED, SPARKS SHOT OUT BETWEEN THE COFFEE POTS, IN FLIGHT. THE F/A TURNED OFF THE COFFEE POTS AND THE SPARKS STOPPED. R & R THE NR 2 COFFEE BREWER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 34,386 hrs · 26,321 cycles

THE CREW REPORTED THAT THE WINDSHIELD 2 HEAT FAILED SEVERAL TIMES ON GROUND AND IN FLIGHT WITH RELAY CLICKING AND A FAINT BURNING ODOR WHEN IT STARTED. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND R & R THE NR 2 WINDSHIELD HEAT CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 2 ENGINE) · airframe 34,203 hrs · 26,169 cycles

DURING ROUTINE MAINTENANCE CHECK, THE NR 2 ENGINE LOWER FORWARD YOKE FITTING WAS FOUND CRACKED APPROXIMATELY 9MM LONG. MAINTENANCE REPLACED THE FORWARD LOWER YOKE FITTING IAW SB145-54-0013 AND ETD2014-145-069032.

Part: START VALVE — FAULTY (APU) · airframe 34,021 hrs · 26,021 cycles

THE CREW REPORTED ON CLIMB OUT OF STL, AFTER SWITCHING TO ENGINE BLEEDS THEY NOTICED A STRONG ODOR SIMILAR TO "BURNED FIREWORKS". MX PERFORMED A GENERAL VISUAL INSPECTION OF NR 1 PACK SYS, PERFORMED HIGH POWER RUNS, AND PERFORMED A VISUAL INSPECTION OF THE RECIRCULATED FANS AND AIR CONDITIONING DUCTS IN CABIN. NO DEFECTS NOTED. R & R THE APU ANTI-SURGE VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — UNKNOWN (GALLEY) · airframe 33,931 hrs · 25,944 cycles

THE CREW REPORTED LT COFFEEMAKER CAUGHT FIRE. MAINTENANCE INSPECTED COFFEEMAKER AND SURROUNDING AREAS. NO EVIDENCE OF FIRE WAS NOTED.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 32,953 hrs · 25,200 cycles

DURING MX CHECK THE RT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT POWER SUPPLY FUSE WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 32,461 hrs · 24,822 cycles

THE CREW REPORTED THE EMERGENCY LIGHT AND CABIN LIGHT BUTTONS WOULD NOT EXTINGUISH. THE CREW RESET SYS AND OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,456 hrs · 24,819 cycles

THE CREW REPORTED LT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,285 hrs · 24,679 cycles

DURING MX INSPECTION, THE FWD LT WING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER WITH OPSL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 31,870 hrs · 24,361 cycles

THE CREW REPORTED BURNING ODOR IN CABIN BY LT SIDE CEILING LIGHT. MX INSPECTED AND REPLACED THE CEILING LIGHT BALLAST OVER SEAT 2A. OPS CHECKED GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,572 hrs · 24,136 cycles

THE CREW REPORTED ENROUTE, THE CAPTAINS WINDSHIELD CRACKED/SHATTERED. THE ACFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE CAPTAINS WINDSHIELD. OPS CHECKS WERE GOOD AND THE ACFT WAS RELEASED FOR SERVICE.

Part: FCU — LEAKING (APU) · airframe 30,647 hrs · 23,414 cycles

THE CREW REPORTED A VERY STRONG FUEL ODOR RT AFTER TAKEOFF AND LASTED 2-03 MINUTES. MX INSPECTED AND REPLACED THE APU FUEL CONTROL UNIT. OPS CHECKED GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 30,054 hrs · 22,947 cycles

ACFT WAS IN FOR A 3A CHECK WHEN INSPECTION FOUND THE LT FRONT EXTERNAL EMERGENCY LIGHT INOPERATIVE. MX R & R THE FUSE IN THE EMERGENCY LIGHT BATTERY TRAY IAW VCMM 25-60-03, OPS CHECK GOOD AND WAS RELEASED.

Part: FADEC — FAULTY (AFT AVIONICS BAY) · airframe 29,703 hrs · 22,667 cycles

CREW SQUAWKED E1 POWER LOSS IN CRUISE FLIGHT AND DECENT. N1 82 PERCENT DOWN TO 70 PERCENT THEN SURGE BACK UP. THREE TIMES IN CRUISE AND THREE TIMES IN DESCENT. E1-2 NO DISPATCH MESSAGE ON TOUCHDOWN WITH RUD HDOV PROT FAIL ON EICAS. MX R & R FADEC 1A WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONDENSER — FAULTY (NR 2 A/C PACK) · airframe 28,503 hrs · 21,646 cycles

CREW REPORTED STRONG BURNING ODOR WHILE IN FLIGHT WITH PACK NR 1 DESELECTED AND WHEN THE F/O TURNED BOTH PACK TEMP KNOBS TO FULL COLD. MX REPLACED THE NR 2 PACK CONDENSOR/MIXER. OPS CHECKED GOOD. .

Part: ELT — FALSE ACTIVATION (CABIN) · airframe 27,302 hrs · 20,740 cycles

ELT WENT OFF DURING FLIGHT. R & R ELT REMOTE SWITCH PANEL AND REPLACED ELT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,688 hrs · 20,268 cycles

SHV - DURING C-CHECK RT INTERCOSTAL BETWEEN FRAMES 12-13 STRINGER 20R CORRODED. MAINTENANCE REMOVED AND REPLACED RT INTERCOSTAL BETWEEN FRAMES 12-13 STRINGER 20R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,688 hrs · 20,268 cycles

SHV - DURING C-CHECK STRINGER 21R CORRODED BETWEEN FRAMES 13-14. MAINTENANCE REMOVED AND REPLACED STRINGER 21R BETWEEN FRAMES 10-14 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,688 hrs · 20,268 cycles

SHV-DURING C-CHECK INTERNAL FUSELAGE SKIN HAS CORROSION BETWEEN FRAMES 7-8 STRINGER 20L-21L. MAINTENANCE PERFORMED REPAIR TO DAMAGED AREA OF FUSELAGE SKIN BETWEEN FRAMES 7-8 STRINGER 20L-21L IAW EMB-145 SRM 53-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 26,613 hrs · 20,210 cycles

MCI - FLIGHT 2493, THE CREW REPORTED A LOSS OF THE NUMBER ONE HYDRAULIC SYSTEM DURING FLIGHT. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED THE NUMBER ONE HYDRAULIC SYSTEM RETURN LINE IN THE BELLY AT FRAME 55, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,063 hrs · 19,791 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND RT SIDE FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY BATTERY CHARGER NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRANSDUCER — INOPERATIVE (BRAKE SYS) · airframe 25,673 hrs · 19,486 cycles

FLIGHT 2036 - EWR - FLIGHT CREW REPORTED BRAKE DEGRADE ON EICAS. AFTER SECOND EXTENSION/RETRACTION ATTEMPT IT WENT AWAY, CREW DECLARED EMERGENCY AND LANDED UNEVENTFULLY. ON LANDING, ACFT JERKED TO THE LEFT. EWR MX REMOVED AND REPLACED NR 2 BRAKE PEDAL TRANSDUCER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (RT WING) · airframe 23,147 hrs · 17,516 cycles

CVG - FLIGHT 3135, THE CREW REPORTED A FUEL LEAK FROM THE RIGHT WING DURING CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER CHECK VALVE AT RIB 19 ON THE RIGHT WING. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,834 hrs · 17,280 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 22,621 hrs · 17,128 cycles

IAH - FLIGHT 2573, THE CREW REPORTED A NR 1 BLEED OVERTEMP INDICATION WITH WING ANTI-ICE ON. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR SENSOR, AND NR 1 PRE-COOLER. OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — LEAKING (BLEED AIR SYS) · airframe 22,621 hrs · 17,128 cycles

IAH - FLIGHT 2573, THE CREW REPORTED A NR 1 BLEED OVERTEMP INDICATION WITH WING ANTI-ICE ON. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR SENSOR, AND NR 1 PRE-COOLER. OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 22,620 hrs · 17,127 cycles

IAH - FLIGHT 2992 THE CREW REPORTED A BLD 1 OVERTEMP MESSAGE ON EICAS AT 1000FT ON T/O IN ICING CONDITIONS. THE MESSAGE CLEARED IN LESS THAN ONE MINUTE, THE QRH WAS ACCOMPLISHED WITH NORMAL OPS AFTER THAT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR VALVE FILTER, LEAK AND OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (APU) · airframe 22,290 hrs · 16,891 cycles

IAH - DURING MX TROUBLESHOOTING ON MEL 49-00-00 FOR FUEL SMELL COMING FROM PACKS WHEN USING APU, MAINTENANCE REMOVED AND REPLACED THE APU FUEL PRESSURE SWITCH, OPERATIONALLY, AND LEAK CHECKED WITH NO DEFECTS NOTED. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,280 hrs · 16,886 cycles

IAH - FLIGHT 2560, THE CREW REPORTED A FUEL SMELL IN THE CABIN WHEN OPERATING ON APU. MAINTENANCE OPERATIONALLY CHECKED THE APU & PACKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — FAULTY (APU) · airframe 22,256 hrs · 16,866 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG FUEL SMELL WHEN OPERATING PACKS OFF OF APU. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/26/09, MAINTENANCE REMOVED AND REPLACED THE APU FUEL SOLENOID VALVE, OPERATIONALLY TESTED WITH THE FUEL SMELL STILL REMAINING IN THE COCKPIT. ON 11-27-09, MAINTENANCE OPERATIONALLY TESTED THE PACKS WITH THE APU MULTIPLE TIMES WITH NO FUEL SMELL NOTED. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 21,726 hrs · 16,455 cycles

SHV - DURING C-CHECK FRAME 10 CRACKED AT LT DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED CHANNEL SPLICE FOR FRAME 10 BELOW LT DV WINDOW CUTOUT IAW EMB-145 SRM 51-40-02 AND CPM 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (SPEED BRAKE) · airframe 21,726 hrs · 16,455 cycles

SHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE POINT I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER FITTING IAW EMB145 SRM 51-40-02 AND LT SPEED BRAKE ACTUATOR IAW EMB145 AMM 27-62-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,726 hrs · 16,455 cycles

SHV - DURING C-CHECK BAGGAGE DOOR LOWER CENTER CUTOUT HAS SEVERAL AREAS CORRODED (LEVEL 2). MAINTENANCE REMOVED AND REPLACED BAGGAGE DOOR LOWER CENTER BEAM IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,726 hrs · 16,455 cycles

SHV - DURING C-CHECK BAGGAGE DOOR FWD LWR CUTOUT CORNER HAS CORROSION (LEVEL 2). MAINTENANCE REPAIRED FRAME 65 SHEAR CLIP AT BAGGAGE DOOR FWD LWR CUTOUT CORNER IAW EC5320-01475 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 21,728 hrs · 16,457 cycles

IAH - FLIGHT 2380, THE CREW REPORTED A BLEED 2 LEAK IN CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND TIGHTENED A CLAMP ON NUMBER TWO PACK DUCT. OPERATION AND LEAK CHECKS WERE PERFORMED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,816 hrs · 15,772 cycles

IAH FLIGHT 2629 THE CREW REPORTED A STRONG SMELL OF FUEL ON TAKEOFF. THE APU WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. CLE MAINTENANCE PERFORMED ON OPERATIONAL CHECK OF THE APU WITH BOTH PACKS SELECTED AND NO FUEL SMELL WAS NOTED. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 19,632 hrs · 14,909 cycles

FLIGHT 2064 - EWR - FLIGHT CREW REPORTED EMERGENCY EXIT ROW 12 B/C AFTERWARD SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: OUTFLOW VALVE — DIRTY (CABIN PRESSURE) · airframe 19,341 hrs · 14,711 cycles

FLIGHT 3114 - RIC- AIR CREW REPORTED THAT DURING CRUISE, CABIN PRESSURE WAS AT 12,000 FT AT ALTITUDE OF 32,000 FT. FLIGHT WAS DIVERTED TO RIC. CREW LANDED ACFT UNEVENTFULLY. RIC MAINTENANCE CLEANED RT OUTFLOW VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: OUTFLOW VALVE — DIRTY (CABIN PRESSURE) · airframe 19,341 hrs · 14,711 cycles

FLIGHT 3114 - RIC-AIR CREW REPORTED THAT DURING CRUISE, CABIN PRESSURE WAS AT 12,000 FT AT ALTITUDE OF 32,000 FT. FLIGHT WAS DIVERTED TO RIC. CREW LANDED ACFT UNEVENTFULLY. RIC MAINTENANCE CLEANED LT OUTFLOW VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,301 hrs · 14,024 cycles

MCI- DURING MAINTENANCE INSPECTION THE LOWER GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 17,899 hrs · 13,739 cycles

FLIGHT 2491 - EWR - CREW REPORTED STRONG SMELL IN CABIN AND FLIGHT DECK. CREW PERFORMED AN AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PERFORMED VISUAL INSPECTION OF BOTH ENGINE INLET ZERO BEARING AND NO OIL LEAK WAS FOUND. MX ALSO RUN APU, AND BOTH ENGINES AND BOTH PACKS, BUT COULD NOT DUPLICATE THE SMELL. PERFORMED ICE TEST, BUT COULD NOT DUPLICATE THE SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,784 hrs · 12,930 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 29. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM AT FRAME 29 IAW EMB 145 SRM 53-00-10 FIG 202. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PLATE — CORRODED (LT AILERON) · airframe 16,784 hrs · 12,930 cycles

SHV - DURING C-CHECK LEFT LOWER AILERON SHROUD HAS CORRODED BONDING PLATE. MAINTENANCE REPAIRED LEFT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,784 hrs · 12,930 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 19 & 23. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PLATE — CORRODED (RT AILERON) · airframe 16,784 hrs · 12,930 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LOWER AILERON SHROUD WITH CORRODED BONDING PLATE. MAINTENANCE REPAIRED RIGHT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PLATE — CORRODED (RT AILERON) · airframe 16,784 hrs · 12,930 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT UPPER SHROUD WITH CORRODED BONDING PLATE. MAINTENANCE REPAIRED RIGHT UPPER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,249 hrs · 12,534 cycles

RIC - DURING SCHEDULED ROUTINE INSPECTION, MX FOUND LEFT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 16,192 hrs · 12,491 cycles

CLE FLIGHT 2519 - THE CREW REPORTED A ELECTRICAL BURNING SMELL WHEN THE COFFEE POTS WERE TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT. OPERATIONAL CHECKS WERE GOOD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 16,175 hrs · 12,477 cycles

FLT 2465 - EWR - CREW REPORTED BURNING ODOR FROM COFFEEMAKER WHEN POWER DOWN. EWR MX PERFORMED VISUAL INSPECTION OF BOTH COFFEEMAKERS AND NO FAULTS WERE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE. COFFEEMAKER NR 1 P/N 500-0640-01 S/N 03-1-32803 TT:9809, TC:7818, TSI:3584. COFFEEMAKER NR 2 P/N 500-0640-01 S/N 02-2-30703 TT:10797, TC:7108, TSI:5143.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 12,419 hrs · 9,497 cycles

DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY CEILING LIGHT NOT WORKING EXIT ROW 12. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BULB IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FR 23) · airframe 12,073 hrs · 9,213 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED AROUND NUT PLATE AT FR 23. MAINTENANCE REPAIRED RT OMEGA BEAM NUT PLATE AREA AT FR 23 BY INSTALLING DOUBLER IAW EMB 145 SRM 53-21-10 FIG 205 & EC 5320-01137. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DELAMINATED (AILERON) · airframe 12,073 hrs · 9,213 cycles

SHV - DURING C-CHECK THE LT AILERON HAS TWO AREAS OF DELAMINATION AND CRACKS ON LOWER INNER SKIN AT HINGE POINT. MAINTENANCE REPAIRED THE TWO AREAS OF DELAMINATION AND CRACK ON LOWER INNER SKIN AT HINGE POINT IN THE LT AILERON IAW EC5750-01260. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 11,006 hrs · 8,377 cycles

CREW REPORTED, BAGGAGE SMOKE WARNING, USED EXTINGUISHER BOTTLES. MAINTENANCE TROUBLESHOT SYSTEM REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLES P/N 33700027-1, S/N 3454D1, BOTTLE P/N 34600073-1, S/N 18200F1 FOR BAGGAGE COMPARTMENT IAW EMB145 MM 26-23-01; REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTOR FOR BAGGAGE COMPARTMENT IAW EMB145 MM 26-15-01 P/N 473597-13, S/N'S 1511 AND 1662]; REMOVED AND REPLACED BAGGAGE COMPARTMENT FIRE DETECTION TEST SWITCH IN MAINTENANCE PANEL IAW EMB145 MM 20-30-00 P/N M83731/10-27. OPS CHECKED SYSTEM GOOD.

Part: CONNECTOR — LOOSE (APU)

IN CRUISE CREW REPORTED APU FIRE MESSAGE DURING APU START. MESSAGE WENT AWAY AFTER APU GOT TO FULL SPEED. CREW SHUT DOWN APU AND CONTINUED FLIGHT. INSPECTED APU, NO SIGN OF FIRE AND CLEANED THE APU FIRE LOOP CONNECTOR AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTY (FIRE CONTROL) · airframe 9,871 hrs · 7,469 cycles

EWR - CREW REPORTED, APU FIRE (WARNING) INFLIGHT. MAINTENANCE INSPECTED APU COMPARTMENT AND APU FOR EVIDENCE OF FIRE. NO SIGNS OF FIRE WERE FOUND, PERFORMED OPS CHECK OF SYSTEM. OPS CHECKED GOOD. REMOVED AND REPLACED FIRE CONTROL MODULE IAW EMB 145 26-12-02. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — STUCK (APU)

CLE FLIGHT 2044, THE CREW REPORTED A STRONG FUEL ODOR FROM THE APU. MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — FAULTY (MLG) · airframe 8,022 hrs · 6,029 cycles

CREW REPORTED, AFTER TAKEOFF RECEIVED LANDING GEAR AIR/GROUND FAILURE WARNING, UNABLE TO RETRACT LANDING GEAR. AIR RETURNED, AND LANDED UNEVENTFULLY. AIRCRAFT MAINTENANCE FERRIED TO RIC. MAINTENANCE TIGHTENED NR 2 (RIGHTHAND) MAIN LANDING GEAR WOW PROXIMITY SWITCH IAW EMB145 AMM 32-61-02. OPS CHECKED GOOD (SEE M-602 677475), AIRCRAFT RELEASED FOR TEST FLIGHT, AIRCRAFT TEST FLOWN SATISFACTORILY, AIRCRAFT RETURNED TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 7,833 hrs · 5,871 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01015 AND EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

SHV- DURING C-CHECK THE RAMP ANGLE AT FRAME 20 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: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

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

Part: LONGERON — GOUGED (FUSELAGE) · airframe 7,833 hrs · 5,871 cycles

DURING C-CHECK THE LEFT LOWER ENGINE COWLING AFT STRINGER THIRD FROM INBOARD WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

SHV- DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

DURING C-CHECK THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER CARGO DOOR CUTOUT BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

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

Part: BEARING — LOOSE (ELEVATOR)

THE CREW NOTED THAT THERE WAS A VIBRATION IN THE CONTROL YOKE. VIBRATION BEGAN IN THE LOW 30,000'S AND CONTINUED IN CLIMB TO 35,000. VIBRATION SEEMED MORE PRONOUNCED AS AIRCRAFT ACCELERATED, VIBRATION DECREASED MARKABLY BELOW 30,000 FT, COULD ALSO FEEL VIBRATION ON FLOOR. A/C RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ELEVATOR HINGE POINTS AND FOUND THAT LT ELEVATOR BEARING TIP TORQUE TUBE HOUSING LOOSE. MAINTENANCE REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE TIP BEARING HOUSING, PERFORMED ELEVATOR DEFLECTION CHECKS, NO DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR TEST FLIGHT PURPOSES ONLY. TEST FLIGHT WAS SATISFACTORY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (COCKPIT)

IAH- FLIGHT 3844, THE CREW NOTED THAT RUDDER SYSTEM #2 INOPERATIVE DURING INITIAL CLIMBOUT, THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED RELAY K0378, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (TAIL)

IAH- THE CREW NOTED THAT RUDDER SYSTEM #2 FAIL ON EICAS IN FLIGHT, THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 RUDDER PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (TAIL)

IAH- THE CREW NOTED THAT RUDDER SYSTEM #2 FAIL ON EICAS IN FLIGHT, THE AIRCRAFT RETURNED TO IAH AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 RUDDER PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK , NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (COCKPIT)

EWR---CO3541, AIRCRAFT AIR RETURN TO EWR. CREW REPORTED, WHEN LANDING GEAR BROUGHT TO RETRACT, RECEIVED ON EICAS LG/LEVER DISAGREE MESSAGE, ALSO LEFT MAIN ON EICAS WAS RED CROSS HATCHED(INDICATION), NOSE AND RIGHT MAIN RED DOWN INDICATION. MAINTENANCE TROUBLESHOT PROBLEM AND REMOVED AND REPLACED LGEU IAW REFERENCE EMB 145 MM 32-32-01. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — FAULTY (FUSELAGE) · airframe 3,804 hrs · 2,617 cycles

EWR---CO3395, CREW REPORTED, "CAPTAINS WINDSHIELD CRACKED IN FLIGHT" DECLARED EMERGENCY; AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD I/A/W EMB145 MM 56-10-01. OPS. CHECKED AND HEAT CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE EMERGENCY LIGHT ABOVE SEAT 12BC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

BNA- DURING PREFLIGHT THE CREW NOTED THE EMERGENCY FLOOR PATH LIGHTING AT SEATS 7 AND 8A DID NOT ILLUMINATE. BNA- MAINTENANCE PLACED THE EMERGENCY LIGHTING SYSTEM ON MEL. LFT- MAINTENANCE REMOVED AND REPLACED THE FLOOR PATH LIGHT STRIP AT SEATS 7 AND 8A. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. CLEARED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.