N14902

Part: ACM — FAULTY (NR 2) · airframe 36,218 hrs · 27,886 cycles

THE CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE REPLACED THE NR 2 AIR CYCLE MACHINE. OPS CHECKED GOOD

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,273 hrs · 27,138 cycles

DURING ROUTINE MAINTENANCE THE LT WING FOWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (GALLEY) · airframe 34,707 hrs · 26,682 cycles

THE F/A NOTICED A SLIGHT BURNING ODOR COMING FROM ABOVE THE COFFEEMAKERS. MAINTENANCE INSPECTED AND REPLACED THE NR 1 COFFEEMAKER. OPS CHECKS WERE GOOD.

Part: UNKNOWN — MALFUNCTIONED · airframe 34,025 hrs · 26,112 cycles

THE CREW REPORTED ACFT ROLLED RT SUDDENLY WITH AUTOPILOT ON. ALSO FELT SOME BUFFETING. THE AUTIOPILOT WAS TURNED OFF AND ACFT FLEW WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS . NO FAULTS WERE FOUND. MAINTENANCE REPLACED THE NR 1 IC-600 COMPUTER AND NR 1 AHRS COMPUTER FOR PRECAUTIONARY PURPOSES. OPS CHECKS WERE GOOD. THE ACFT RETURNED TO SERVICE.

Part: BOWL — CORRODED (WASTE DUMP) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK LAV WASTE DUMP BOWL HAS CORROSION, LOCAL LEVEL 2 AND CORRODED HARDWARE. MAINTENANCE PERFORMED REPAIR OF LAV WASTE DUMP BOWL IAW SRM 53-31-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (FRAME 75) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, DRAG ANGLE CRACKED AT FRAME 75 STRINGER 2L. MAINTENANCE R & R THE DRAG ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK LT FUSELAGE SKIN AT FRAME 75, STRINGER 1L-2L CRACKED. MAINTENANCE REPAIRED FUSELAGE SKIN AT FRAME 75, STRINGER 1L-2L IAW EC5330-02944. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, RT INBD PULLEY SUPPORT BRACKET CORRODED, LOCAL LEVEL 2, FRAMES 60 TO 61. MAINTENANCE COMPLETED REPAIR OF RT INBD PULLEY SUPPORT BRACKET BY REINSTALLING REPAIRED BRACKET IAW EC5330-02948. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, RT FUSELAGE SKIN AT FRAME 78-80 CRACKS AROUND RIVET HOLES. MAINTENANCE PERFORMED REPAIR TO RT FUSELAGE SKIN AT FRAME 78-80 IAW EC5330-02945. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAME 20)

DURING C-CHECK RT FUSELAGE SKIN AT FRAME 20 STRINGER 18R-19R, 1, DENT AT RIVETS. MAINTENANCE PERFORMED REPAIR OF OUTERSKIN FUSELAGE FRAME 20 BETWEEN STRINGERS 18R AND 19R IAW SRM 53-21-01 AND INITIATED DMI. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, RT FUSELAGE SKIN AT FRAME 75 STRINGER 1R-2R CRACKED. MAINTENANCE REPAIRED FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R IAW EC5330-02944, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK CARGO DOOR INNER SKIN HAS NUMEROUS TOOLING MARKS. MAINTENANCE R & R CARGO DOOR INNER LOWER SKIN IAW SRM 51-40-02. RESTORED ORIGINAL FINISH IAW CPM 51-21-06. CARGO DOOR INNER UPPER SKIN IS DAMAGE FREE. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, NR 1 ENGINE FORWARD LOWER MOUNT FORWARD LUG IS CRACKED. MAINTENANCE R & R NR 1 ENGINE FORWARD LOWER MOUNT LUG YOKE FITTING IAW EC5450-01117. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK , CARGO DOOR INNER SKIN LOWER FORWARD NUTPLATE HOLE IS CORRODED. MAINTENANCE R & R CARGO DOOR INNER LOWER SKIN IAW SRM 51-40-02. RESTORED ORIGINAL FINISH IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, LT FUSELAGE SKIN AT FRAME 77-80 CRACKS AROUND RIVET HOLES. MAINTENANCE PERFORMED REPAIR TO LT FUSELAGE SKIN CRACK AT FRAME 77-80 IAW EC5330-02945. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK FRAME 10R CRACKED. MAINTENANCE R & R FRAME 10R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, BAGGAGE CENTER SUPPORT FRAME AT FRAME 65-68 CORROSION, LOCAL LEVEL 2. MAINTENANCE R & R BAGGAGE DOOR LOWER SILL IAW SRM 51-40-02, ALODINED, PRIMED, PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (ZONE 200) · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R NEW DRAG ANGLE ON RT FWD VERTICAL TO FUSELAGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK, FUSELAGE SKIN CORRODED, LOCAL LEVEL 2, AT FRAME 61-62, STRINGER 21R-21L. MAINTENANCE COMPLETED REPAIR OF FUSELAGE SKIN AT FRAME 61-62, STRINGERS 21R-21L IAW SRM 53-31-01, FIG 201, TYPE A REPAIR. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,748 hrs · 22,023 cycles

DURING ROUTINE MX, THE EMERGENCY LIGHT AT ROW 8 WOULD NOT ILLUMINATE. MX INSPECTED AND REPLACED THE EMERGENCY LIGHT AT ROW 8. OPS CHECKED GOOD.

Part: BATTERY PACK — WEAK (FLASHLIGHT) · airframe 27,937 hrs · 21,387 cycles

DURING MX INSPECTION, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE DIM AND WOULD NOT TAKE A CHARGE. MX R & R THE CAPTAIN'S FLASHLIGHT BATTERY PACK WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

LATERAL "L" SHAPE CORRODED BEYOND LIMITS. R & R CORRODED SECTION OF SHEAR FOOT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,483 hrs · 21,029 cycles

CRACK IN CARGO DOOR FWD SILL REST. CUT-OUT DAMAGE SECTION, INSTALLED DOUBLER AND FILLER.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

DIGITAL AT Y=0.0 FRM 46 CORRODED BEYOND LIMITS. R & R DIGITAL

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

CARGO DOOR CUTOUT LOWER THRESHOLD BEAM CORRODED BEYOND LIMITS. R & R THRESHOLD.

Part: PLATE — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

LOWER REST PLATE FOR CARGO DOOR CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR IAW ETD2012-145-016826 & EC5320-01723.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

DIGITAL LT Y-479 CORRODED BEYOND LIMITS. R & R DIGITAL. ACFT IN C-CHECK.

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

DIGITAL AT Y=0 CORRODED BEYOND LIMITS. R & R DIGITAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

LEFT WALL SUPPORT/DOUBLER WEB AT FLOOR SUPPORT AND FRM 61 CORRODED BEYOND LIMITS. R & R SUPPORT/DOUBLER.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 27,483 hrs · 21,029 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,933 hrs · 20,560 cycles

DURING MX INSPECTION THE LT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX RELAMPED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,123 hrs · 18,361 cycles

FLIGHT 2201 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT OVER RIGHT WING INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 23,627 hrs · 17,887 cycles

FLIGHT 6023 - IAD - FLIGHT CREW REPORTED ERROR ON AUTO PRESS CONTROL UNIT. IAD MX REMOVED AND REPLACED DIGITAL CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 22,619 hrs · 17,111 cycles

FUEL QUANTITY DASHED OUT ON CLIMB. RESET ALL SWITCHES TO NORMAL AND COULD NOT DUPLICATE FAULT. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK SERVICE DOOR CUTOUT FWD STRUCTURE HAS CORROSION AT NUT PLATE HOLE BETWEEN STRINGER 15R & 16R. MAINTENANCE PERFORMED REPAIR ON SERVICE DOOR CUTOUT FWD STRUCTURE BETWEEN STRINGER 15R & 16R IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 2 ENGINE) · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK NR 2 ENGINE LOWER FWD YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE LOWER FWD YOKE IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK CENTER SILL FOR SERVICE DOOR IS CORRODED BETWEEN FRAMES 19A-22A. MAINTENANCE REMOVED AND REPLACED CENTER SILL FOR SERVICE DOOR IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CENTER SERVICE DOOR SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (SPOILER) · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK RT GROUND SPOILER CENTER HINGE I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT GROUND SPOILER CENTER HINGE IAW EMB-145 AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,568 hrs · 17,073 cycles

SHV - DURING C-CHECK LT FRAME 10 CLIP IS CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 CLIP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CIRCUIT CARD — INOPERATIVE (NR 1) · airframe 19,454 hrs · 14,711 cycles

IAH - FLIGHT 2308, THE CREW REPORTED A LOSS OF N1, ITT DATA, A DAU FAIL MESSAGE, AND A FUEL IMBALANCE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE IC600, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — INOPERATIVE (NR 1) · airframe 19,454 hrs · 14,711 cycles

IAH - FLIGHT 2308, THE CREW REPORTED A LOSS OF N1, ITT DATA, A DAU FAIL MESSAGE, AND A FUEL IMBALANCE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ON DAU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,359 hrs · 14,641 cycles

EMERGENCY CABIN LIGHTING DOES NOT STAY ILLUMINATED. REMOVED AND REPLACED EMERGENCY BATTERIES IAW EMB 145 AMM 33-50-04. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — THERMAL RUNAWAY (NR 2) · airframe 19,359 hrs · 14,641 cycles

BATTERY NR 2 THERMAL RUNAWAY DURING FLIGHT. REMOVED AND REPLACED NR 1 AND NR 2 MAIN BATTERIES IAW EMB 145 AMM 24-36-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (LAVATORY) · airframe 18,483 hrs · 13,973 cycles

FLIGHT 2925 - EWR - FLIGHT CREW REPORTED BURNING SMELL FROM LAVATORY. EWR MX REMOVED AND REPLACED BALLAST ABOVE SINK IN THE LAVATORY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: COVER — LEAKING (CABIN PRESSURE) · airframe 18,251 hrs · 13,810 cycles

BNA - FLIGHT 2458 - THE CREW REPORTED THAT THE PRESSURIZATION WAS UNCONTROLLABLE ON MANUAL OR AUTO. THE AIRCRAFT RETURNED TO BNA WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND THE PRESSURIZATION WAS PLACED ON MEL 21-30-00/3 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT FLEW TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REINSTALLED THE GROUND AIR CONNECTION VALVE COVER, OPERATIONALLY TESTED THE PRESSURIZATION WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,837 hrs · 13,497 cycles

SHV DURING C-CHECK RT HORIZONTAL STAB LEADING EDGE CORRODED AROUND ALL EXTERNAL SKIN RIVET HEADS. MX REPAIRED RT HORIZONTAL STAB LEADING EDGE SKIN AROUND ALL EXTERNAL SKIN RIVET HEADS IAW IC 2008-145/09800. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,837 hrs · 13,497 cycles

SHV DURING C-CHECK LT HORIZONTAL STAB LEADING EDGE CORRODED AROUND ALL EXTERNAL SKIN RIVET HEADS. MX REPAIRED LT HORIZONTAL STAB LEADING EDGE SKIN IAW IC2008-145/09800. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — OUT OF LIMITS (RT AILERON) · airframe 17,837 hrs · 13,497 cycles

SHV DURING C-CHECK RT AILERON DAMPER BRACKET O/B FITTING OUT OF LIMITS IAW EC5740-01152B. MX R&R RT AILERON BRACKET O/B FITTING IAW EMB-145 SRM 51-40-02 AND EMB-145 CPM 51-21-07. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PUMP — LEAKING (NR 1) · airframe 17,539 hrs · 13,276 cycles

FLIGHT 2554 - RIC - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 1 LOW QTY INDICATION IN FLIGHT, SYSTEM INDICATION IN AMBER AND DECREASING. CREW DECIDED TO DIVERT FLIGHT TO RIC AND LANDED AIRCRAFT UNEVENTFULLY. RIC MX REMOVED AND REPLACED HYDRAULIC PUMP NR 1 AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (PITOT/STATIC SYS) · airframe 15,414 hrs · 11,863 cycles

MCI - FLIGHT 2212, THE CREW REPORTED A PITOT2 INOP MESSAGE APPEARED DURING APPROACH WITH A BURNING SMELL. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY FOR PITOT TWO, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — LEAKING (NLG) · airframe 13,415 hrs · 10,405 cycles

CLE FLIGHT 3094 THE CREW REPORTED A LOUD CONTINOUS BANGING SOUND FROM NOSE GEAR AFTER LANDING. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 13,395 hrs · 10,387 cycles

SHV - DURING C-CHECK LIGHTNING STRIKE ON RIGHT ELEVATOR UPPER O/B TRAILING EDGE SURFACE. MX REPAIRED DAMAGE ON RIGHT ELEVATOR UPPER O/B TRAILING EDGE SURFACE IAW EC 5330-01692. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 13,395 hrs · 10,387 cycles

SHV DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM AT FR 65-68 HAS CORROSION. MX REMOVED AND REPLACED CARGO DOOR CUT OUT LOWER BEAM AT FR 65-68 IAW 145 SRM 51-40-02 AND CPM 51-21-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (E&E BAY) · airframe 12,699 hrs · 9,861 cycles

FLT 2820 - EWR - DURING CLIMB LANDING GEAR WILL NOT RETRACT - AIR/GROUND FAIL. FLIGHT CREW PERFORMED AN AIR RETURN AND LANDED UNEVENTFULLY. MX PERFORMED TROUBLESHOOTING AND FOUND LGEU FAIL. MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 12,579 hrs · 9,766 cycles

BTV DURING 3A CHECK FOUND EMERGENCY LIGHT ON CEILING ROW 17 INOP. REPLACED BULB IAW AMM 33-50-08. OPS CHECK GOOD.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 12,547 hrs · 9,739 cycles

CLE FLIGHT 3032 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER, THE NOSE GEAR WOW PROXIMITY SWITCH AND THE NOSE WOW HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 12,547 hrs · 9,739 cycles

CLE FLIGHT 3032 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER, THE NOSE GEAR WOW PROXIMITY SWITCH AND THE NOSE WOW HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,565 hrs · 6,611 cycles

TYS - DURING A INSPECTION CORROSION WAS FOUND AT THE LEFT OMEGA BEAM AT FRAME 25. MAINTENANCE BLENDED AND REMOVED CORROSION AND FINISHED THE REPAIR AT FRAME 25 IAW EMB 145 SRM 53-22-10.

Part: HOUSING — WORN (VERTICAL STAB) · airframe 8,565 hrs · 6,611 cycles

TYS - DURING A SCHEDULED INSPECTION THE RIGHT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116.

Part: HOUSING — WORN (VERTICAL STAB) · airframe 8,565 hrs · 6,611 cycles

TYS - DURING A SCHEDULED INSPECTION THE LEFT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,897 hrs · 5,343 cycles

DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE BACK HALF OF THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR (4) EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING 4A INSPECTION MAINTENANCE FOUND ROW 3 OVERHEAD CENTER AISLE EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LAMP IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1)

DAY FLIGHT NR 2239 THE CREW REPORTED NR 1 OIL PRESSURE IN AMBER IN CLIMB MODE FOR 3-4 MINUTES. ALSO FUEL SMELL NOTED AFTER LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — INOPERATIVE (APU)

WHILE TRYING TO START THE APU THE CREW NOTED A STRONG FUEL ODOR AFTER TGE APU WAS STARTED. NOTE: IT IS DIFFICULT TO START THE APU, HAVE TO HOLD SWITCH UNTIL APU IS AT 100 PERCENT. MAINTENANCE REMOVED AND REPLACED THE APU EXTINGUISHER SWITCH, PERFORMED A OPERATIONAL CHECK, NO FUMES NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INTERMITTENT (CABIN)

CLE FLIGHT#2865 THE CREW REPORTED THE EMERGENCY LIGHTS IN THE CABIN WOULD INTERMITTENTLY ILLUMINATE IN THE ARM POSITION.MAINTENANCE INSPECTED AND REPLACED RELAY KO275 AND THE OVERHEAD LIGHT CONTROL MODULE.OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL MODULE — INOPERATIVE (CABIN)

IAH - DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT NOT ARMED CAUTION, AND EXIT LIGHTS CAME ON EVERY TWO (2) MINUTES FOLLOWING RESET FROM OFF TO ARMED. IAH - MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (CABIN)

IAH- DURING POST FLIGHT THE CREW NOTED THAT THE "EMERGENCY LIGHT NOT ARMED" CAUTION, AND, EXIT LIGHTS CAME ON EVERY TWO (2) MINUTES FOLLOWING RESET FROM OFF TO ARMED. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: REGULATOR — STICKING (ELEVATOR SYS)

CLE FLIGHT 3083 THE CREW REPORTED VIBRATION IN THE CONTROL COLUMN/YOKE IN ALL PHASES OF FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AND LEFT ELEVATOR CABLE TENSION REGULATORS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY)

CLE FLIGHT 3057 THE CREW REPORTED THE LEFT HOT JUG HAD BURNT ELECTRICAL SMELL EMITTED WHEN POWER WAS ON. MAINTENANCE PLACED THE ITEM ON MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HOT JUG. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.