N18556

Part: INVERTER — INOPERATIVE (CABIN) · airframe 41,674 hrs · 36,860 cycles

DURING ROUTINE MAINTENANCE LEFT AND RIGHT OVERWING FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DENTED (FRAME 22) · airframe 41,411 hrs · 31,993 cycles

DAMAGE TO FUSELAGE AT FRAME 22, STRINGER 15L-16L. REPAIRED AREA BY CUTTING OUT DAMAGE, FABRICATING AND INSTALLING FILLER & DOUBLER.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,037 hrs · 31,700 cycles

DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT ROW 3CD WAS INOP. MX REMOVED AND REPLACED THE EXIT SIGN WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 38,563 hrs · 29,680 cycles

IAH - FLIGHT 4432 THE CREW REPORTED A BURNING SMELL NEAR ROW 21 IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CEILING LIGHT ASSEMBLY AT ROW 21A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 38,288 hrs · 29,456 cycles

WHEN PASSING FROM 9000 FT DURING DESCENT, CABIN RATE WENT TO -1800 AND CABIN DELTA P WENT TO ZERO. MX FOUND THE GROUND CONNECTION VALVE STUCK OPEN AND GROUND CONNECTOR VALVE DUCT BLOWN. SECURED THE DUCT, ADJUSTED VALVE AND REMOVED AND REPLACED THE AUTO PRESSURE CONTROLLER, OPS CHECKED GOOD. ACCT WAS APPROVED FOR RETURN TO SERVICE.

Part: TUBE — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 37,983 hrs · 29,217 cycles

RIGHT ELEVATOR MASS BALANCE TUBE CORRODED. CLEANED AND TREATED THE CORROSION ON THE MASS BALANCE TUBE IAW ETD2018-145-033009.

Part: SKIN — CRACKED (FRAMES 37-38) · airframe 37,983 hrs · 29,217 cycles

DURING A C CHECK, FOUND SURFACE CORROSION ON THE SKIN AT FRAMES 37 - 38 STRINGER 21L AND 22R. MAINTENANCE CUTOUT THE DAMAGE SKIN AND INSTALL A FILLER AND PATCH IAW SRM 53-23-01.

Part: RIB — CRACKED (LT WING) · airframe 37,983 hrs · 29,217 cycles

DURING A C CHECK, FOUND A CRACK AROUND THE FUEL SHUTOFF VALVE INSIDE FUEL PANELS 531CB AND 531DB. MAINTENANCE INSTALLED A REPAIR TO RIB 7, LEFT WING IAW ETD 2018-145-027438.

Part: MOUNT — CRACKED (ZONE 200) · airframe 37,983 hrs · 29,217 cycles

DURING A C CHECK, FOUND A CRACK TO THE FO SIDE LATERAL UPPER MOUNTING BRACKET AT WINDSHIELD POST SIDE. MAINTENANCE CUTOUT AND REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS FOR THE FO LATERAL UPPER FRAME. REPAIRED IAW ETD 2018-145-027627.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 37,983 hrs · 29,217 cycles

HORIZONTAL STAB RT SIDE SPHERICAL BEARING WORN. REMOVED, REAMED BEARING HOUSING TO 1ST OVERSIZE AND INSTALLED A NEW BEARING. BACKLASH AND OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 37,983 hrs · 29,217 cycles

HORIZONTAL STAB LEFT SIDE SPHERICAL BEARING WORN. REMOVED, REAMED BEARING HOUSING TO 1ST OVERSIZE AND INSTALLED A NEW BEARING. BACKLASHE AND OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,983 hrs · 29,217 cycles

LEFT REAR FUSELAGE SKIN AT FRAME 75, STRINGER 1L AND 2L HAS A CRACK. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-31-01.

Part: STRINGER — CRACKED · airframe 37,983 hrs · 29,217 cycles

STRINGER 2L CRACKED AT FRAME 75. CUT OUT CRACKED PORTION OF STRINGER INSTALLED FILLER AND DOUBLER IAW SRM 53-00-03. AIRCRAFT STILL IN C CHECK.

Part: ENGINE — LEAKING (NR 2) · airframe 36,103 hrs · 27,739 cycles

PILOT REPORTED LAV SMOKE WARNING AFTER TAKEOFF WITH NO SMOKE. ACFT PERFORMED UNEVENTFUL AIR RETURN. MX RAN ENGINES AND APU NOTICING ODOR DURING PACK 2 OPERATION. MX REMOVED AND REPLACED THE NR 2 ENGINE, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 36,102 hrs · 27,739 cycles

LAV SMOKE WARNING AFTER TAKEOFF WITH NO SMOKE. REMOVED AND REPLACED NR 2 ENGINE. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — DENTED (FRAME 2) · airframe 34,159 hrs · 2,622 cycles

SKIN DENTED AT FRAME 2 STRINGER 2R. CUTOUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER, INSTALLED , PRIMED AND PAINTED. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 34,089 hrs · 26,152 cycles

ACFT WAS ON TAKEOFF AND THE MLG WOULDN'T RETRACT, SO PILOT RETURNED TO BASE WHERE MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH IAW AMM 32-63-02. REMOVED AND REPLACED NLG WOW CONNECTOR IAW SWPM 20-50-00. PERFORMED OPS CHECKS IAW AMM 32-63-00, OPS CHECKED.

Part: BALLAST — FAILED (LAVATORY LIGHT) · airframe 32,249 hrs · 24,704 cycles

THE CREW REPORTED AN "ABNORMAL ODOR IN LAVATORY". "ODOR SIMILAR TO SINGED ELECTRICAL WIRING". THE ACFT WAS FERRIED, WHERE MAINTENANCE R & R THE LAVATORY LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BURNED (SEAT 2A) · airframe 30,426 hrs · 23,283 cycles

THE CREW REPORTED A BURNING ODOR COMING FROM THE COFFEEMAKERS. MAINTENANCE INSPECTED AND FOUND NO DEFECT WITH COFFEEMAKERS. FOUND CEILING LIGHT SOCKET BURNED AT SEAT 2A.

Part: LIGHT — BURNED (CABIN) · airframe 30,386 hrs · 23,253 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FRONT OF THE CABIN AND FLIGHT DECK DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND PLACED CABIN LIGHTING ON MEL33-20-00-1, CAT C, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 11-23-14 MAINTENANCE R & R THE LIGHT ASSEMBLY AT ROW 2A, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,716 hrs · 22,725 cycles

DURING ROUTINE MAINTENANCE THE AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. 2ND MOST AFT. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD.

Part: PANEL — CORRODED (FRAME 68) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

FRAME 68 DOOR CLOSE OUT PANEL CORRODED BEYOND LIMITS AROUND NUT PLATE. R & R PANEL.

Part: PROFILE — CORRODED (FRAME 62) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

MULTIPLE AREAS OF CORROSION BEYOND LIMITS AFTER BLEND-OUT ON RT OTBD LATERAL FLOOR SUPPORT. R & R SUPPORT.

Part: FITTING — CORRODED (FRAME 65) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

FRAME 65 DOOR CUTOUT FITTING CORRODED BEYOND LIMITS. R & R DOOR CUTOUT FITTING.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-65) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

RT FLOOR SUPPORT HAS CORROSION BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: BEAM — CORRODED (FRAME 65) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

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

Part: FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 28,390 hrs · 21,719 cycles

FRAME 68 DOOR CUTOUT FITTING CORRODED BEYOND LIMITS. R & R CUTOUT FITTING.

Part: FITTING — BROKEN (ENGING FUEL) · airframe 27,507 hrs · 21,071 cycles

NR 1 ENGINE SHUTDOWN INFLIGHT AND DIVERTED. MX INSPECTED NR 1 ENGINE AND FOUND MAIN FUEL LINE ADAPTER FITTING BROKEN. MX R & R FUEL LINE FITTING, LEAK AND OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 21,865 hrs · 16,684 cycles

FLIGHT 2078 EWR - APU DRAIN LEAKING FUEL. EWR MAINTENANCE REMOVED AND REPLACED APU FUEL CONTROL UNIT IAW EMB-145 AMM 49-32-01, OPERATIONAL CHECK AND LEAK CHECK IS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HANDLE — FAULTY (COCKPIT) · airframe 20,978 hrs · 16,013 cycles

PIT FLT 3146 - THE CREW REPORTED A UNCOMMANDED SWERVING ON THE GROUND. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE STEERING HANDLE. OPERATIONAL CHECKS WERE GOOD.

Part: JACK — INOPERATIVE (COCKPIT) · airframe 20,393 hrs · 15,574 cycles

IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS BOOM MIC JACK, HAND MIC JACK, RECONNECTED THE F/O'S HAND MIC JACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DEFECTIVE (BLEED AIR SYS) · airframe 19,710 hrs · 15,030 cycles

FLIGHT 2260 - EWR - FLIGHT CREW REPORTED BLEED LEAK WARNING ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED O-RINGS AND TIE WRAPS ON BLEED TUBE CONNECTIONS. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,594 hrs · 14,936 cycles

THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING AT SEAT 3A THRU SEAT 7A WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD. NO FURTHER DEFECTS WERE FOUND.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,519 hrs · 14,880 cycles

FLIGHT 18556 - EWR - FLIGHT CREW REPORTED SMELL COMING FROM PACK NR 1. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,825 hrs · 14,355 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 20 CARBON CROSSBEAM AREA HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM RAMP ANGLE AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,825 hrs · 14,355 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 CARBON CROSSBEAM AREA HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CROSSBEAM AREA AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,825 hrs · 14,355 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 29 CARBON CROSSBEAM AREA HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,825 hrs · 14,355 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 24-25 CARBON CROSSBEAM AREA HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 24-25 CARBON CROSSBEAM SUPPORT IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (ZONE 600) · airframe 18,823 hrs · 14,353 cycles

CVG - FLIGHT 3135, ATC NOTIFIED THE CREW THAT FUEL WAS LEAKING FROM THE RIGHT WING, AND FUEL GAUGES CONFIRMED. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A LEAKING CHECK (FLAPPER) VALVE ON THE RIGHT WING AT RIB 19, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,293 hrs · 13,965 cycles

FLIGHT 2504 - EWR - FLIGHT CREW REPORTED CABIN RATE WOULD NOT CLIMB/DESCEND FROM 200 TO 1500 FT PER MIN IN CRUISE. CABIN ALTITUDE CLIMBED UP TO 8500 FT IN CRUISE. EWR MX PERFORMED VISUAL INSPECTION OF STATIC PORTS AND PERFORMED PRESSURIZATION TEST OF THE ACFT SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,293 hrs · 13,965 cycles

FLIGHT 2504 - EWR - FLIGHT CREW REPORTED CABIN RATE WOULD NOT CLIMB/DESCEND FROM 200 TO 1500 FT PER MIN IN CRUISE. CABIN ALTITUDE CLIMBED UP TO 8500 FT IN CRUISE. EWR MX PERFORMED VISUAL INSPECTION OF STATIC PORTS AND PERFORMED PRESSURIZATION TEST OF THE ACFT SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — ERRATIC (CABIN PRESSURE) · airframe 18,096 hrs · 13,822 cycles

EWR FLT 2741 THE CREW REPORTED AN EXCESSIVE CABIN ALTITUDE AND RATE ON CLIMBOUT. UNABLE TO CONTROL PRESSURIZATION MANUALLY. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD. ALSO CLEANED AND LUBED THE MAIN CABIN DOOR SEAL.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 18,070 hrs · 13,802 cycles

DURING ROUTINE INSPECTION THE AFT FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AFT FLASHLIGHT LAMP. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — FAULTY (MAIN BATTERY) · airframe 17,932 hrs · 13,698 cycles

CLE FLT 3073 THE CREW REPORTED A ELECTRICAL EMERGENCY ABNORMAL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AND NR 2 BATTERY SWITCHES (S7125,S7126) AND THE ESS POWER PUSH BUTTON SWITCH AND RELAY KO097. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG DOOR) · airframe 17,740 hrs · 13,547 cycles

IAH - FLIGHT 2561, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOOR OPENED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 14,077 hrs · 10,802 cycles

FLT 444 - SAN - WHILE PERFORMING SERVICE CHECK MX PERSONNEL FOUND AISLE 1 EMERGENCY LIGHTING AND LT FWD EXTERNAL EMERGENCY LIGHTING INOP. MX PERSONNEL REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY ASSY, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: O-RING — WORN (FUEL SYSTEM) · airframe 13,971 hrs · 10,711 cycles

FLT 0060 - TUS - FLIGHT CREW REPORTED E2 FUEL IMPENDING BYPASS MSG ON EICAS/ E2 FUEL LEAK. MX PERSONNEL FROM IAH REMOVED AND REPLACED O-RINGS FOR THE ELECTRICAL IMPENDING BYPASS SWITCH OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,534 hrs · 10,412 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APRROVED TO RETURN FOR SERVICE.

Part: DOOR FRAME — CORRODED (MAIN DOOR) · airframe 13,534 hrs · 10,412 cycles

SHV - DURING C-CHECK BOTTOM OF MAIN DOOR FRAME HAS CORROSION AROUND NUT PLATES. MX INSTALLED DOUBLER ON FWD DOOR HALF IAW EC 5212-01159. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 90,532 hrs · 11,540 cycles

TYS - MAINTENANCE FOUND A CRACK IN THE FUSELAGE AT FR 77, FR 78 AND FR 79 AT STRINGER 6L. MAINTENANCE REMOVED THE DAMAGED SKIN, FAB A DOUBLER, ALODINED AND REINSTALLED. ALL WORK WAS ACCOMPLISHED IAW EC5330-01680. AIRCRAFT RELEASED BACK TO SERVICE.

Part: FIRE DETECTOR — FAILED (NR 2 ENGINE) · airframe 10,765 hrs · 8,454 cycles

CAE FLIGHT 2097 - THE CREW REPORTED A NR 2 ENGINE FIRE DETECT FAIL ECIAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 9,938 hrs · 7,794 cycles

IAH - FLIGHT 2426, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT ELECTRICAL COMPONENTS, RAN THE PACKS FOR EXTENDED PERIOD WITH NO ODOR NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: RELAY — BURNED (COCKPIT) · airframe 8,739 hrs · 6,862 cycles

IAH - FLIGHT 2433, THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND RELAY K0054 TO BE DISCOLORED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RELAY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — BURNED (COCKPIT) · airframe 8,739 hrs · 6,862 cycles

IAH - FLIGHT 2433, THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE THE NUMBER TWO PITOT STATIC CURRENT SENSOR TO BE DISCOLORED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DR CUTOUT) · corrosion level 2 · airframe 8,738 hrs · 6,860 cycles

SHV - DURING C-CHECK THE BAGGAGE DOOR LOWER CUTOUT BEAM 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: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 7,234 hrs · 5,681 cycles

CREW REPORTED, "THAT THE OVERWING EMERGENCY EXIT ROW LIGHT DID NOT WORK." MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY EXIT LIGHT BATTERY PACK IAW EMB145 AMM 33-50-04. OPS.CHECKED GOOD.

Part: CHARGER — FAULTY (CABIN) · airframe 7,239 hrs · 5,687 cycles

THE CREW REPORTED A MID CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 7,183 hrs · 5,636 cycles

AFT EMERGENCY LIGHT STRIP NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY PACK IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 7,167 hrs · 5,623 cycles

RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHTS ON THE FLOOR AT EMERGENCY EXIT AND REAR INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POSITION 4. OPERATIONAL TEST WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHT) · airframe 7,130 hrs · 5,593 cycles

TYS MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY AND OPS CHECKS WERE GOOD.

Part: DUCT — LEAKING (APU)

CLE FLIGHT 2899 THE CREW REPORTED A APU FIRE WARNING ON DESCENT AFTER APU START UP. WARNING WENT AWAY AFTER A FEW SECONDS AND APU STARTED NORMALLY. MAINTENANCE INSPECTED AND FOUND A BLEED LEAK OF THE APU BLEED DUCT AT THE FLEX JOINT. THE BLEED DUCT WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — DAMAGED (NR 1) · airframe 4,438 hrs · 3,507 cycles

SHV - FLIGHT 2806 FROM IAH TO MEM CREW REPORTED LOW OIL QUANTITY AND HIGH OIL TEMPERATURE 25 MINUTES AFTER TAKEOFF AT CRUISE ALTITUDE. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE IAW CONTINENTAL EXPRESS TASK CARD 6271001. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK WHILE PERFORMING A FUNCTIONAL OF THE EMERGENCY LIGHTING SYSTEM, THE FLOOR PROXIMITY LIGHT STRIP AT THE OVERWING EMERGENCY EXITS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AND OPERATIONALLY CHECKED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,383 hrs · 3,455 cycles

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

Part: COWLING — GOUGED (LT ENGINE) · airframe 4,383 hrs · 3,455 cycles

DURING C-CHECK THE LT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED ON THE INNER SKIN AT STATION XN1485.0. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 54-10-01 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. 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) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE 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 (FLOORBEAM) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22 TO FRAME 23. 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) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01265. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (CABIN) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 17 TO 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (RT ENGINE) · airframe 4,383 hrs · 3,455 cycles

DURING C-CHECK THE RIGHT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (LT ENGINE) · airframe 4,383 hrs · 3,455 cycles

SHV- DURING C-CHECK THE LEFT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT)

AFTER DEPARTURE THE CREW NOTED THAT THE LANDING GEAR DID NOT RETRACT, AND, RETURNED TO DAL, AND, LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE PINNED LANDING GEAR,AND, SIGNED FERRY FLIGHT RELEASE. THE AIRCRAFT FLEW FROM DAL TO IAH FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER REF. EMB 145 MM 32-32-02, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.