N14171

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,048 hrs · 20,623 cycles

FWD CABIN OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R THE BULB, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,002 hrs · 20,577 cycles

MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND THE BATTERY LOW. CHARGED THE BATTERY. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,991 hrs · 20,565 cycles

CABIN EMERGENCY LIGHTS AT 18A INOPERATIVE. REMOVED AND RESEATED SIDWALL EMERGENCY LIGHT CONNECTOR OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,675 hrs · 20,264 cycles

CENTER CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 32,587 hrs · 20,179 cycles

NOTICEABLE ELECTRICAL SMELL/SMOKE WHEN TURNING ON SIDEWALL LIGHTS. R&R PASSENGER SIDEWALL LIGHT ASSY AT SEAT 3A. OPS CHECK SAT. NO OTHER DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,559 hrs · 20,152 cycles

FWD EMERGENCY LIGHTS INOPERATIVE BY THE MAIN CABIN DOOR. R & R THE BATTERY. OPS CHECKED GOOD.

Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT) · airframe 32,536 hrs · 20,128 cycles

CAPTAIN`S AND FIRST OFFICER WINDOW WILL NOT OPEN. CLEANED AND LUBRICATED CAPTAIN`S AND FO`S WINDOWS. OPS CHECKED SAT.

Part: WIRE HARNESS — FAILED (CABIN LIGHT) · airframe 32,187 hrs · 19,826 cycles

SMOKE COMING FROM OVERHEAD LIGHT AT 4A. R & R THE ELECTRICAL HARNESS, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,488 hrs · 19,138 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 & NR 4 EMERGENCY BATTERIES, PN 2013-1A, SN 96788, TAH 21091.25, TAC 15137.

Part: UNKNOWN — SMOKE (CABIN) · airframe 30,648 hrs · 18,518 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT ON DEPARTURE. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS AND PRESSURIZATION CHECKS. COULD NOT DUPLICATE ANY DEFECTS. NO SMOKE OR ODOR IN THE COCKPIT WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: BRACKET — CORRODED (FRAMES 65-68) · airframe 30,237 hrs · 18,240 cycles

DURING C-CHECK, FOUND CARGO DOOR UPPER ANGLE BRACKET IS CORRODED AROUND NUTPLATE HOLES. R & R CARGO DOOR UPPER ANGLE BRACKET IAW SRM 51-20-03. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (ZONE 200) · airframe 26,295 hrs · 15,571 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. THE ACFT DIVERTED, AND LANDED WITHOUT INCIDENT. MAINTENACE R & R THE EXHAUST FAN, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER FITTING) · airframe 24,565 hrs · 14,506 cycles

DURING C-CHECK, LT SPEED BRAKE UPPER ACTUATOR FITTING INBD HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE UPPER ACTUATOR FITTING INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 24,565 hrs · 14,506 cycles

DURING C-CHECK, FWD CARGO DOOR TORSION BAR BRACKET CRACKED FRM 61, STR 4R-5R. MX R & R FWD CARGO DOOR TORSION BAR BRACKET AT FRAME 61, STRINGER 4R-5R IAW IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER FITTING) · airframe 24,565 hrs · 14,506 cycles

DURING C-CHECK LT GROUND SPOILER UPPER ACTUATOR FITTING OTBD LUG OTBD HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER UPPER ACTUATOR FITTING OB LUG OTBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPORVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER FITTING) · airframe 24,565 hrs · 14,506 cycles

DURING C-CHECK, LT GROUND SPOILER INBD ATTACHMENT FITTING OTBD HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER INBD ATTACHMENT FITTING OTBD HAT BUSHING IAW EMB-145XR EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL TRANFER) · airframe 19,876 hrs · 10,970 cycles

FLT 4359, DURING CRUISE CREW REPORTED A FUEL TRANSFER INOPERATIVE MESSAGE. AIRCRAFT RETURNED. PLACED VENTRAL TANK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE OPS TESTED FUEL TRANSFER WITH NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE.

Part: BOLT — MISSING (TE FLAPS) · airframe 17,272 hrs · 9,698 cycles

FLIGHT 2163, DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE RIGHT OUTBOARD FLAP HAD LEADING EDGE DAMAGE. UPON INSPECTION IT WAS DETERMINED THAT THE OUTBOARD FLAP SHROUD DRIVER FORWARD BOLT CAME LOOSE ALLOWING THE FLAP TO RETRACT INTO THE LOWER FLAP SHROUD. MAINTENANCE REPLACED THE FLAP ASSEMBLY, FLAP JACKSCREW ACTUATORS, FLAP FLEX SHAFT AND LOWER FLAP SHROUD THEN CLEARED THE DISCREPANCY.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 17,244 hrs · 9,683 cycles

IAH - FLIGHT 2268, DURING TAKEOFF THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION. THE CREW DISCHARGED BOTH BOTTLES AS A PRECAUTION AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED AND REPLACED BOTH FIRE BOTTLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 17,244 hrs · 9,683 cycles

IAH - FLIGHT 2268, DURING TAKEOFF THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION. THE CREW DISCHARGED BOTH BOTTLES AS A PRECAUTION AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED AND REPLACED BOTH FIRE BOTTLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,243 hrs · 9,682 cycles

IAH - FLIGHT 3048, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON FINAL. THE CREW DISCHARGED BOTH FIRE BOTTLES AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, REMOVED AND REPLACED BOTH FIRE BOTTLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 15,942 hrs · 8,947 cycles

CLE FLT 2730 THE CREW REPORTED A FLAP LOW SPEED MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: A/C PACK — ODOR (NR 1) · airframe 14,525 hrs · 8,176 cycles

FLIGHT 2010, DURING TAXI THE CREW REPORTED A STRANGE ODOR COMING FROM A/C PACK ONE, AND THAT IT WOULD NOT COOL OFF WHEN ACTIVATED. THE ACFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE ACFT AND PLACED THE ACFT ON MEL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ACFT WAS INSPECT IN IAH, OPERATIONALLY TESTED WITH NO DEFECTS, THE MEL CLEARED, AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

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

Part: SUPPORT — CORRODED (WATER WASTE) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK FRAME 65 RAMP ANGLE CUTOUT CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR BY INSTALLING REPAIR DOUBLER AT FRAME 65 RAMP ANGLE CUTOUT IAW EMB-145 EC5320-01479 REPAIR 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK TWO (2) CRACKS ON FUSELAGE SKIN JUST BELOW VERTICAL STAB LT SIDE. MAINTENANCE COMPLETED REPAIR ON LT REAR FUSELAGE SKIN AT FRAME 79 STR 4L AND 6L IAW EC5330-02008. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK FRAME 65 RAMP ANGLE CUTOUT CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF FRAME 65 RAMP ANGLE CUTOUT BY INSTALLING A REPAIR DOUBLER IAW EMB-145 EC5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK SHEAR CLIP DOUBLER AT FRM 65 LOWER CARGO DOOR CUTOUT SILL CORRODED (LEVEL 2 LOCAL) ABOVE AND BELOW SILL. MAINTENANCE PERFORMED REPAIR OF SHEAR CLIP DOUBLER AT FRM 65 LOWER CARGO DOOR CUTOUT SILL IAW EMB-145 EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT SILL CORRODED (LEVEL 2 LOCAL) BETWEEN FRMS 65 AND 68. MAINTENANCE PERFORMED REPAIR OF CARGO DOOR LOWER CUTOUT SILL AT FRMS 65-68 BY INSTALLING NEW LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (MAIN DOOR) · corrosion level 2 · airframe 13,855 hrs · 7,798 cycles

SHV - DURING C-CHECK MAIN DOOR MOST LOWER NUT PLATE HOLES HAVE SURFACE CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF MAIN DOOR MOST LWR NUT PLATE HOLES IAW EMB-145 EC 5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 4 ENGINE) · airframe 8,842 hrs · 4,832 cycles

FLT 7827 - LAX TO SFO - FLIGHT CREW REPORTED SMOKE IN CABIN. AIRCRAFT WAS FERRY FLIGHT TO ONT MX HANGER WHERE MX PERSONNEL REMOVED AND REPLACED NR 1 ENG, OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. NR 4 ENGINE CARBON SEAL EXHIBITED SIGNS OF HEAVY LEAKAGE(SEGMENTS FULLY WETTED WITH OIL AND COCKING ON THE EXTERIOR OF HOUSING). NR 4 CARBON SEAL WAS REPLACED WITH POST SB72-348 STANDARD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 8,358 hrs · 4,543 cycles

FLT 7743 - LAS TO LAX - FLIGHT CREW ABORTED TAKEOFF DUE TO SMOKE IN COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT, MX PERSONNEL PERFORMED ENG RUNS WITH FLIGHT CREW; OPERATIONALLY CHECKED PACKS AND AIR BLEED SYSTEMS WITH NO DEFECTS OR ODORS WERE DETECTED AND THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,130 hrs · 3,269 cycles

DURING MAINTENANCE INSPECTION, THE FORWARD GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 2,282 hrs · 4,338 cycles

TYS, DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN AT FRAME 19, STRINGER 12L WAS FOUND DENTED. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER, ALODINED, PRIMED, PAINTED AND INSTALLED IAW EC5330-01574.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 3,388 hrs · 1,777 cycles

DEN - FLIGHT 2187, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL AFTER TAKEOFF. THE AIRCRAFT DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEIGHT ON WHEELS PROX SWITCH ON THE NLG, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 134 hrs · 70 cycles

IAH - FLIGHT 2916, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON IN THE ARM POSITION. MAINTENANCE CYCLED THE EMERGENCY LIGHT SWITCH AND THE LIGHTS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. DURING PREFLIGHT INSPECTION FOR FLIGHT 3460, THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CABIN LIGHTS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE UNDER THE BULKHEAD, OPERATIONALLY CHECKED LIGHTS WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.