N13118

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,477 hrs · 23,638 cycles

MX REPORTED EMERGENCY LIGHT OUT AT ROW 18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK NR 3 AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,751 hrs · 19,641 cycles

DURING C-CHECK, CARGO DOOR LOWER MAIN BEAM CORRODED, LOCAL LEVEL 2, FRAMES 65-68. MAINTENANCE R & R CARGO DOOR LOWER MAIN BEAM AT FRAMES 65-68 IAW EMB-145 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CRACKED (ZONE 100) · airframe 34,751 hrs · 19,641 cycles

DURING C-CHECK LT OVERWING STRAP AT FRAME 46 CRACKED, 195 PANEL FAIRING UPPER. MAINTENANCE R & R LT OVERWING STRAP AT FRAME 46-51 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ZONE 400) · airframe 34,751 hrs · 19,641 cycles

DURING C-CK. NR 2 ENGINE FWD LOWER YOKE CRACKED. R & R NR 2 ENG FWD LOWER YOKE IAW EC5450-01070. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · airframe 34,751 hrs · 19,641 cycles

DURING C-CK. CARGO DOOR LOWER BEAM CORRODED BETWEEN FR 65-68. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,341 hrs · 18,747 cycles

PILOT REPORTED THE FWD CABIN OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. SECURED THE FWD OVERHEAD EMERGENCY EXIT CONNECTOR PLUG WITH PERFORMED OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,841 hrs · 17,161 cycles

CREW REPORTED EMERGENCY SIGN IN CENTER CABIN FOUND TO BE INOPERATIVE. MX R & R EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,426 hrs · 16,261 cycles

DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. R & R SILL IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,426 hrs · 16,261 cycles

DURING C-CHECK THE PAX DOOR LOWER FRAME WAS FOUND TO BE CORRODED AROUND NUT PLATE HOLES. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,426 hrs · 16,261 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,426 hrs · 16,261 cycles

DURING C-CHECK THE SKIN SPLICE BETWEEN FRAMES 14-15 AND STRINGERS 21R-21L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 900) · corrosion level 2 · airframe 29,426 hrs · 16,261 cycles

DURING C-CHECK THE CENTER SERVICE DOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 20-22 AND STRINGERS 15R-16R. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 24,099 hrs · 12,907 cycles

EMERGENCY LIGHT ON THE SERVICE DOOR SWING ARM INOP. REMOVED AND REPLACED WIRE SPLICE CONNECTOR IAW EMB 145 SWPM 20-50-00. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FCU — DEFECTIVE (APU) · airframe 23,276 hrs · 12,514 cycles

FLIGHT 2762 - EWR - FLIGHT CREW REPORTED STRONG SMELL OF OIL AND FUEL WITH APU RUNNING. MX REMOVED AND REPLACED APU FCU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,738 hrs · 12,166 cycles

TYS - EMERGENCY LIGHT IN CEILING AT 12B INOP. REMOVED AND REPLACED EMERGENCY CEILING LIGHT AT SEAT 12B, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,564 hrs · 12,073 cycles

FLIGHT 2107 - EWR - FLIGHT CREW REPORTED BURNING SMELL FROM PACK NR 1 WITH ENGINE BLEED ON. EWR MX PERFORMED OPERATIONAL CHECK OF PACK NR 1 WITH APU RUNNING AND QITH ENGINE RUNNING BUT COULD NOT DUPLICATE THE BURNING SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,547 hrs · 12,063 cycles

PVD - FLT 2742 THE CREW REPORTED A BURNING SMELL FROM THE NR 1 PACK WITH THE NR 1 BLEED VALVE OPEN. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE THE BURNING SMELL WITH THE NR 1 ENGINE AND APU RUNNING.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,463 hrs · 11,454 cycles

IAH - DURING PRE-FLIGHT INSPECTION THE EMERGENCY LIGHTS OVER ROW 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,365 hrs · 10,318 cycles

SHV - DURING C-CHECK LT OMEGA BEAM FACE AT FRAME 20 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE COMPLETED REPAIR ON LT OMEGA BEAM CROSS BEAM AT FRAME 20 IAW EMB-145XR SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,365 hrs · 10,318 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM BETWEEN FRAMES 59-60 AT NUT PLATE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM BETWEEN FRAMES 59-60 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 19,365 hrs · 10,318 cycles

SHV - DURING C-CHECK ALL (4) PAX DOOR BROKEN NUT PLATE HOLES FOR LINER CORRODED (LEVEL 2 LOCAL). MAINTENANCE COMPLETED REPAIR OF ALL (4) PAX DOOR NUT PLATE HOLES FOR LINER IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STATIC LINE — LEAKING (PITOT/STATIC SYS) · airframe 18,224 hrs · 9,703 cycles

OKC - FLIGHT 2962, THE CREW REPORTED AN IAS FLAG ON FLIGHT. THE AIRCRAFT DIVERTED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NR 2 SYSTEM STATIC HOSE FROM THE ADC TO THE STATIC PORT. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 17,431 hrs · 9,282 cycles

COS - FLIGHT 2116, THE CREW REPORTED A RAPID DEPRESSURIZATION AT FL360. THE CREW PERFORMED AN EMERGENCY DESCENT AND LANDED AT COS WITHOUT INCIDENT. MX INSPECTED THE ACFT, OPS CHECKED THE MANUAL AND AUTO PRESSURIZATION SYSTEMS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (ZONE 400) · airframe 17,319 hrs · 9,225 cycles

IAH- FLIGHT 2632, THE CREW REPORTED A LOSS OF PRESSURIZATION AT THE TOP OF DESCENT. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MX R&R THE HIGH STAGE BLEED VALVE. OPS TESTED WITH NO DEFECTS FOUND, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE AFT GALLEY WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY AND INVERTER. OPERATIONAL CHECKS WERE GOOD. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY LIGHT AT ROW 7A WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RELAMPED THE OVERHEAD LIGHT AT SEAT 7A. OPERATIONAL CHECKS WERE GOOD. (S)

Part: SHUTOFF VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 15,652 hrs · 8,348 cycles

IAH - FLT 2187 - THE CREW REPORTED A VENTRAL TANK TRANSFER FAIL MESSAGE ON THE EICAS. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND RELEASED IAW MEL 28-45-14. SUPPLEMENT TO FOLLOW: MAINTENANCE REPLACED THE VENTRAL TANK TRANSFER SHUT-OFF VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: STRUT — LOW (NLG) · airframe 15,133 hrs · 8,072 cycles

FLIGHT 2076 - EWR - CREW REPORTED GEAR WOULD NOT RETRACT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX SERVICE THE NOSE LANDING GEAR STRUT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,477 hrs · 7,757 cycles

EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT AT 12C SEAT INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PLATE — CORRODED (AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK PANEL 197BB HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197BB IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (LT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK LT AILERON LOWER SHROUD HAS CORROSION ON BONDING PLATE. MX REPAIRED LT AILERON LOWER SHROUD BONDING PLATES IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK PANEL 197CL HAS BAD BONDING PLATE. MX REPAIRED 197CL PANEL IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (RT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK RT LOWER AILERON SHROUDS HAS CORRODED BONDING PLATE. MX REMOVED AND REPLACED RT LOWER AILERON BONDING PLATE IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK PANEL 197DR HAS BAD BONDING PLATES. MX REPAIRED PANEL 197 DR BONDING PLATES IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK PANEL 197AB HAS CORRODED BONDING PLATES. MX REPAIRED PANEL 197AB BONDING PLATES IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (LT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK LT AILERON UPPER SHROUD HAS CORROSION ON BONDING PLATES. MX REPAIRS LT AILERON UPPER SHROUD BONDING PLATES IAW EMB EC 5750-0315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (RT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK RT UPPER AILERON SHROUDS HAS CORRODED BONDING PLATES. MX REPAIRED RT UPPER AILERON SHROUDS BONDING PLATES IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SHROUD — CORRODED (RT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK, MAINTENANCE FOUND RT AILERON UPPER SHROUD BONDING STRIP WITH CORROSION. MAINTENANCE REPAIRED RT AILERON UPPER SHROUD IAW EC 5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK, MAINTENANCE FOUND AT FRAME 65 SHEAR CLIP WITH CORROSION AT CARGO DOOR CUT OUT LOWER BEAM. MAINTENANCE REPAIRED FRAME 65 SHEAR CLIP AT CARGO DOOR CUTOUT LOWER BEAM IAW EC5330-01458. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHROUD — CORRODED (RT AILERON) · airframe 14,322 hrs · 7,683 cycles

SHV - DURING C-CHECK, MAINTENANCE FOUND RT AILERON LOWER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT LOWER AILERON SHROUD IAW EC 5750-01315 REV. E. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,287 hrs · 7,665 cycles

BURNING ELECTRIC ODOR IN COCKPIT AND FRONT OF GALLEY AREA IN FRONT OF SEAT 1A. DETECTED ODOR AFTER LANDING AND INCREASED ON THE WAY TO THE GATE. MX INSPECTED AREA AND RELAYS. NO DEFECTS FOUND. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 13,786 hrs · 7,428 cycles

IAH - FLIGHT 2170, THE CREW REPORTED THAT THE COCKPIT HAD A TOXIC ODOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FLIGHT GUIDANCE CONTROLLER TO BE BURNT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (MLG) · airframe 12,934 hrs · 6,981 cycles

DURING CLIMB, CREW REPORTED LOUD NOISE AND VIBRATION FROM NOSE AREA AND UNABLE TO CYCLE NOSE GEAR IN AIR. AFTER AIR RETURN, MX MAINTENANCE DISCOVERED THE NOSE LANDING GEAR DOOR SOLENOID VALVE TO BE THE CAUSE. MX REMOVED AND REPLACED NLG DOOR SOLENOID VALVE WITH OPERATIONAL AND LEAK CHECKS GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,285 hrs · 6,094 cycles

IAH - FLT 2509, THE CREW REPORTED THE EMERGENCY LIGHT ON BULKHEAD TO BE BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — BLOWN (CABIN) · airframe 9,483 hrs · 5,124 cycles

IAH - FLIGHT 3096, DURING TAKEOFF THE CREW REPORTED SMOKE IN THE CABIN FOLLOWED BY BLEED 1 LEAK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 BLEED DUCT BETWEEN FR 56 & 60 TO BE BLOWN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLEED DUCT, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — WORN (NR 2 ENGINE) · airframe 9,442 hrs · 5,093 cycles

TYS, DURING A SCHEDULED TEST FLIGHT FOR POST C-CHECK EVALUATION, LAV SMOKE EICAS MESSAGE CAME ON IN FLIGHT AT 10000 MSL, DECLARED EMERGENCY LANDING, ORDER NOTED IN AFT CABIN. MAINTENANCE REMOVED AND REPLACED THE O-RING ON THE ZERO CARBIN SEAL ON NR 2 ENGINE, OPS AND LEAK CHECKED GOOD IAW AE3007A SERIES MM 72-25-25, COMPLIED WITH ANOTHER TEST FLIGHT, TEST FLIGHT SATISFACTORY.

Part: BUSHING — MIGRATED (HORIZONTAL STAB) · airframe 9,440 hrs · 5,090 cycles

TYS, DURING A SCHEDULED INSPECTION THE LEFT HORIZONTAL STAB HINGE PIN BUSHING WAS FOUND MIGRATED. MAINTENANCE REMOVED THE BUSHING, REAMED THE HOLE TO THE FIRST OVERSIZE, ALODINED, APPLIED SEALANT AND INSTALLED THE NEW BUSHING IAW EMB-145XR SRM 55-10-02.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 7,265 hrs · 3,992 cycles

STL---CO3279, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED INVERTER, OPS CHECKED AND RETURNED TO SERVICE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 6,454 hrs · 3,466 cycles

EWR - CO2641, DURING ROUTINE CHECK MAINTENANCE FOUND EMERGENCY EXIT LIGHT SIGN ABOVE FLIGHT ATTENDANTS FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT MARKING SIGN ASSEMBLY ABOVE FLIGHT ATTENDANTS FORWARD JUMPSEAT IAW EMB AMM NR 33-50-14, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,964 hrs · 2,688 cycles

DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10.

Part: SUPPORT — DAMAGED (MLG) · airframe 4,964 hrs · 2,668 cycles

DURING C-CHECK THE LEFT MAIN GEAR FORWARD BEARING CAP WAS FOUND TO HAVE ELONGATED BOLT HOLES. REPLACED THE BEARING CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — ODOR (COCKPIT AREA) · airframe 336 hrs · 178 cycles

EWR---CO2006, CREW REPORTED "PLASTIC/RUBBER SMELL CONTINUING INFLIGHT ON FLIGHT DECK. NO SMOKE DETECTED." MAINTENANCE FOUND EICAS CAUSING SMOKE SMELL. REMOVED AND REPLACED EICAS DISPLAY UNIT IAW EMB145XR AMM 34-22-01. OPS.CHECKED GOOD.