N13955

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,945 hrs · 26,427 cycles

DURING ROUTINE MX INSPECTION, THE GALLEY AND MAIN DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK STRINGER 21R SPLICE BETWEEN FRAME 13-14 CORRODED (LOCAL LEVEL 2). MX R & R STRINGER SPLICE BETWEEN FRAME 13-14 AT STRINGER 21R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (ZONE 200) · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK FRAME 60 CHAFED STRINGER 4L-5L. MX PERFORMED REPAIR OF FRAME 60 STRINGER 4L-5L IAW EC5320-01728. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK CRACK AT FRAME 10 JUST BELOW RT DV WINDOW (STRINGER 9). MX R & R FRAME 10 UNDER RT DV WINDOW AT STRINGER 9R IAW SRM 51-40-02. ALODINED, PRIMED, AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK CRACK AT FRAME 10 JUST BELOW LT DV WINDOW (STRINGER 9). MX R & R FRAME 10 LT UNDER DV WINDOW IAW SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK INTERNAL SKIN CORRODED FRAMES 13-14 STRINGERS 20L-20R. MX PERFORMED REPAIR OF INTERNAL SKIN AT FRAMES 13-14 STRINGERS 20L-20R IAW EC5330-02651. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,412 hrs · 26,006 cycles

DURING C-CHECK INTERNAL SKIN CORRODED BETWEEN FRAMES 12-13 STRINGERS 20L-20R. MX PERFORMED REPAIR TO INTERNAL SKIN BETWEEN FRAMES 12-13 STRINGER 20L-20R IAW EC5310-01639. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 31,248 hrs · 23,455 cycles

IAH - FLIGHT 2469, DURING POST FLIGHT THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL BALLAST AT SEAT 3A/4A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 31,116 hrs · 23,357 cycles

FLIGHT 2685 MKE-EWR AC N13955 SPOILERS DEPLOYING DURING TAXI WITH ASSOCIATED LOUD BANGING COMING FROM BELOW THE COCKPIT. RETURNED TO BLOCK AT EWR. EWR MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB-145 AMM 27-63-02. OPERATIONAL CHECK GOOD. ALSO, PERFORMED AIRCRAFT TAXI IAW AMM 9-20-00. NO FAULTS NOTED, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 30,780 hrs · 23,103 cycles

DAL - FLIGHT 2544 THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL DURING CLIMB. THE AIRCRAFT RETURNED TO DAL WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT WEIGHT ON WHEELS PROXIMITY SWITCH, AND REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 30,653 hrs · 23,014 cycles

WHEN GEAR HANDLE WAS SELECTED UP GEAR THE HANDLE WOULD NOT MOVE AND MESSAGE LG AIR/GROUND FAIL. REMOVED AND REPLACED LGEU IAW EMB 145 AMM 32-32-01. C/W GEAR SWINGS IAW EMB MM 32-30-00 OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,896 hrs · 22,465 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY FLOOR STRIP LIGHT AT ROW 8A INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (DUMP VALVE) · airframe 29,482 hrs · 22,134 cycles

SHV - DURING C-CHECK TOILET DUMP VALVE SUPPORT HAS CORROSION. REMOVED AND REPLACED TOILED DUMP VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,482 hrs · 22,134 cycles

SHV - DURING C-CHECK FR 75 TO VERT STAB FITTING FRETTING AGAINST FUSELAGE SKIN. REPAIRED IAW EC5310-01317, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,482 hrs · 22,134 cycles

SHV - DURING C-CHECK INDICATION OF CRACKS AROUND RIVET AT FRAME 77-78 JUNCTION STRINGER 8L. MAINTENANCE PERFORMED REPAIR AT FRAME 77-78 JUNCTION STRINGER 8L IAW EC5330-02207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 29,451 hrs · 22,112 cycles

THE CREW REPORTED THE CAPTAINS O2 MASK WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS O2 MASK STOWAGE BOX. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,002 hrs · 21,012 cycles

CLE FLT 2912 THE CREW REPORTED THE EMERGENCY EXIT SIGN BY THE GALLEY DOOR AND THE AISLE PATH EMERGENCY LIGHT STRIP AT SEAT 1A WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 27,980 hrs · 20,995 cycles

BNA - SMOKE COMING FROM AREA OF THE PSU READING LIGHT ABOVE SEAT 1A. REMOVED AND REPLACED BALLAST RT8400. REMOVED AND REPLACED NR 1 PSU CIRCUIT BOARD. OPS CHECK GOOD.

Part: PRINTED CKT BOARD — BURNED (CABIN) · airframe 27,979 hrs · 20,994 cycles

SMOKE COMING FROM AREA OF THE PSU READING LIGHT ABOVE SEAT 1A. REMOVED AND REPLACED BALLAST RT8400 IAW EMB 145AMM 33-21-03 AND REPLACED NR 1 PSU CIRCUIT BOARD IAW EMB 145 VCMM 25-28-23. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROLS) · airframe 27,676 hrs · 20,764 cycles

IAH - FLIGHT 2257, DURING TAKEOFF THE CREW REPORTED THAT THE FLIGHT CONTROLS FELT AS THOUGH THEY WERE POPPING AND CATCHING WHEN MOVED LEFT OR RIGHT OF CENTER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE FLIGHT CONTROLS ALL WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,118 hrs · 20,377 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT STRIPS BETWEEN SEATS 2A AND 3A INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,155 hrs · 18,896 cycles

MCI - DURING MX INSPECTION THE NR 2 AND NR 3 AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (RUDDER) · airframe 24,785 hrs · 18,631 cycles

SHV - DURING C-CHECK RUDDER 1 UPPER ACTUATOR ATTACHMENT LOWER HINGE UPPER HAT BUSHING MIGRATED.

Part: BALLAST — FAULTY (CABIN)

IAH - FLT 2001, DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG SMELL OF ELECTRICAL COMPONENTS COMING FROM THE CABIN. MX REMOVED AND REPLACED BALLAST FROM SEAT 12BC. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,392 hrs · 17,656 cycles

DURING ROUTINE MAINT THE AISLE PATH EMERGENCY LIGHT STRIP NR 6 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 6 AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 22,909 hrs · 17,355 cycles

BNA - FLIGHT 3025M THE CREW REPORTED A SMOKE SMELL COMING FROM THE LAV WHEN FLUSHED. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE LAV ON MEL 38-30-00 CAT C CONTROL NUMBER 140961, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST ABOVE THE SINK, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,657 hrs · 17,184 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BELLCRANK — BROKEN (PAX DOOR) · airframe 22,502 hrs · 17,076 cycles

YQM FLIGHT 2230 - THE CREW REPORTED THE MAIN CABIN DOOR WILL NOT CLOSE OR OPEN FROM INSIDE THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE INTERNAL HANDLE BELLCRANK ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 21,013 hrs · 15,975 cycles

FLT 2796 - SDF - CREW REPORTED ELECTRICAL FIRE OVERHEAD BETWEEN SEATS 1A AND 2A. VISUAL CONFIRMATION OF SMOKE (NOT CONDENSATION) BY FLIGHT ATTENDANT AND PAX ACCOMPANIED BY ACRID ELECTRICAL SMELL. MX PERFORMED INSPECTION AND FOUND NO EVIDENCE OF FIRE. FOUND BULB LOOSE FROM CONNECTORS. MX REINSTALLED BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LOCK — DEFECTIVE (PAX DOOR) · airframe 20,376 hrs · 15,495 cycles

IAH - THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT CLOSE NORMALLY. MAINTENANCE REMOVED AND REPLACED THE FORWARD PAX DOOR LOCK BOX ASSEMBLY, RIGGED AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,418 hrs · 14,748 cycles

IAH - FLIGHT 3080, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT MAIN CABIN DOOR EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 19,055 hrs · 14,471 cycles

FLT 2512 - RIC - AFTER TAKEOFF, BAG DOOR OPEN ILLUMINATED. AC RETURNED. MX RELEASED AC IAW MEL 52-70-00/C. ON 08/26/2006, MX CHECKED DOOR ADJUSTMENT, CLEANED UP DOOR SWITCHES. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. MEL WAS CLEARED AND AC WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 17,992 hrs · 13,619 cycles

DURING SERVICE AND ROUTINE CHECK ON RON MAINTENANCE, FOUND THE EMERGENCY LIGHTS FAILED OPERATIONAL CHECK. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM NR 33-50-04. OPS. CHECKED GOOD.

Part: SCREW — LOOSE (CABIN DOOR) · airframe 17,472 hrs · 13,218 cycles

CLE FLIGHT NR 2498, THE CREW REPORTED THE CABIN DOOR WAS HARD TO CLOSE. MAINTENANCE INSPECTED AND TIGHTENED THE BOTTOM DOOR STOP SCREW. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 17,432 hrs · 13,189 cycles

PILOT REPORT; LANDING GEAR WOULD NOT RETRACT. AC RETUNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK PROXIMITY SWITCHES (2 EA). LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,609 hrs · 12,523 cycles

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

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 16,352 hrs · 12,324 cycles

BTV---CO2874, DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE FLOOR EMERGENCY AISLE PATH STRIP HAD A BROKEN WIRE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW EMB145 AMM NR 33-50-12, OPS CHECKED GOOD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 16,352 hrs · 12,324 cycles

BTV---CO2874, DURING SERVICE AND ROUTINE CHECK MAINTENANCE, FOUND THE SERVICE DOOR EMERGENCY LIGHT TO NOT BE WORKING. REMOVED AND REPLACED NR 2 BATTERY CHARGER IAW EMB145 AMM NR 33-50-05, OPS CHECK GOOD.

Part: LIGHT — FAULTY (FUSELAGE) · airframe 15,965 hrs · 12,015 cycles

EWR-CO2455, CREW REPORTED, "EMERGENCY LIGHT BELOW COCKPIT DOOR DOESN'T WORK." MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BELOW THE COCKPIT DOOR IAW EMB145 AMM NR 33-50-05, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,782 hrs · 11,874 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LAST 8 INCHES OF EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHTING ON MEL 33-50-12 CAT-C CONTROL NUMBER 056545, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT BNA ON FLIGHT 3374 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH EMERGENCY LIGHT STRIP, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE.

Part: CONTROL LEVER — DEFECTIVE (MLG) · airframe 14,645 hrs · 11,001 cycles

DURING CLIMBOUT OF BNA GEAR SELECTED UP AND DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECKED GOOD.

Part: CONTROL LEVER — DEFECTIVE (MLG) · airframe 14,645 hrs · 11,001 cycles

DURING CLIMBOUT OF BNA GEAR SELECT UP AND GEAR DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 14,616 hrs · 10,982 cycles

DURING FINAL APPROACH CREW REPORTED FLAP FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED AT JAX WITH INCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT, OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 14,241 hrs · 10,696 cycles

IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS ALL IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CIRCUIT BOARD — BURNED (EMERGENCY LIGHT)

BUF FLIGHT 2167, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR NEAR THE GALLEY AND ALONG ROW 3 SEAT B&C. MAINTENANCE FOUND THE ELECTRICAL ODOR COMING FROM THE PSU AT ROW 3 B&C. THE CIRCUIT BOARD WAS REMOVED AND THE AIRCRAFT WAS RELEASED IAW MEL 25-60-02/4 AND 25-60-02/11. ON 6/25/04 THE CIRCUIT BOARD WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (UPLOCK BOX)

PILOT REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ELECTRICAL CONNECTIONS TO BE LOOSE ON THE LT MAIN GEAR UPLOCK BOX. THE AFFECTED CONNECTORS WERE CLEANED AND RECONNECTED, THE LANDING GEAR SYSTEM OPERATIONALLY TESTED, AND THE AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (APU COWLING) · airframe 11,870 hrs · 8,812 cycles

SHV DURING C CHECK THE APU COWLING FRAME CRACKED AND SKIN BENT AT 11 O'CLOCK. MAINTENANCE REPAIRED AFFECTED SECTION IAW EMB 145 IC2003-145/2629 AND EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE CARGO DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 65 AND 68 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: RAMP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

SHV- DURING C-CHECK, THE SUPPORT RAMP BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

SHV- DURING C-CHECK, THE FORWARD SERVICE DOOR SILL BETWEEN FRAMES 18 AND 19 WAS FOUND TO BE CORRODED. 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: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 FROM FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE LT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 16 AND 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: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,870 hrs · 8,812 cycles

SHV- DURING C CHECK THE CENTER OMEGA BEAM IN GALLEY WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (RT WING COWL) · airframe 11,870 hrs · 8,812 cycles

SHV DURING C-CHECK, THE RIGHT HAND LOWER COWLING AFT EDGE MEMBER WAS FOUND TO HAVE CHAFING MARKS. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,870 hrs · 8,812 cycles

SHV- DURING C-CHECK, THE T-REINFORCEMENT ON STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NACELLE) · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE NUMBER 1 UPPER ENGINE COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,870 hrs · 8,812 cycles

DURING C-CHECK, THE T-REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2)

STL FLIGHT 2462 CREW REPORTED NUMBER TWO ENGINE LOW OIL PRESSURE AND QUANTITY IN FLIGHT. IN FLIGHT COMMANDED SHUTDOWN OF NUMBER TWO ENGINE. CREW DIVERTED TO CLE. MAINTENANCE FOUND ENGINE TO BE LEAKING INTERNALLY. NUMBER 2 ENGINE WAS REMOVED AND REPLACED. GROUND RUNS AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — FAULTY

BTV---CO3180, MAINTENANCE FOUND "AFT EMERGENCY LIGHT STRIP INOPERATIVE, REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP IAW EMB145 MM 33-50-12. OPS.CHECKED GOOD.

Part: YOKE — MALFUNCTIONED (COCKPIT)

THE CREW REPORTED DURING TAKEOFF ROLL, THE YOKE MOVED TO FULL PITCH UP POSITION AND FROZE THERE. THE SYSTEM RELAXED AFTER ABORTED TAKEOFF. MAINTENANCE INSPECTED THE FLIGHT CONTROL SYSTEMS AND PERFORMED A HIGH SPEED TAXI. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — LEAKING (APU BAY)

CLE- THE CREW NOTED THAT A STRONG FUEL ODOR OCCURRED WHEN STARTING THE APU. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU. PERFORMED A OPERATIONAL CHECK OF THE APU, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT)

CLE FLIGHT 3260 THE CREW REPORTED A STRONG FUEL SMELL IN COCKPIT AFTER STARTING THE APU. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NOZZLE — DIRTY (APU)

IAH- FLIGHT 3794, STRONG FUEL SMELL IN CABIN AND COCKPIT WHEN APU STARTED ON APPROACH. MAINTENANCE CLEANED APU START FUEL NOZZLES, PERFORMED A OPERATIONAL CHECK OF THE APU, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — STICKS (APU)

CLE FLIGHT 3218 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND FORWARD CABIN WHEN THE APU IS STARTED. THE APU WAS PLACED ON MEL. MAINTENANCE REMOVED AND REPLACED THE APU FUEL DRAIN CHECK VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: ODOR — DETECTED (COCKPIT)

EWR - DURING APPROACH ON FLIGHT 3359, THE CREW REPORTED THAT THERE WAS A STRONG FUEL ODOR IN THE COCKPIT WHEN THE APU WAS STARTED. THE AIRCRAFT LANDED SAFELY AT EWR, WHERE MAINTENANCE RELEASED THE AIRCRAFT UNDER MEL 49-00-00. MAINTENANCE IN CLE PERFORMED OPERATIONAL TESTS OF THE APU AND IT'S ASSOCIATED SYSTEMS. NO FUEL ODOR OR DEFECTS WERE NOTED.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT 3189 THE CREW REPORTED A FUEL ODOR WHEN SELECTING THE PACKS ON WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND RAN PACKS OFF THE APU BLEED AND FOUND NO DEFECTS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING ROUTINE OVERNIGHT MAINTENANCE THE RIGHT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY CHARGER AND REPAIRED WIRING IN SERVICE DOOR FOR THE LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT NR 4247 THE CREW REPORTED A STRONG FUEL SMELL EACH TIME THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF APU WITH THE BLEED SYSTEM ON AND NO FUEL SMELL WAS NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT 3928 - CREW REPORTED THAT A STRONG ODOR OF FUEL WAS PRESENT AFTER THE APU WAS STARTED. THE APU WAS PLACED ON MEL AND THE AIRCRAFT DISPATCHED FOR SERVICE. ON 10/23/2001 IN BNA, MAINTENANCE PERFORMED GROUND RUNS OF THE APU WITH THE LEFT AND RIGHT ENVIROMENTAL SYSTEMS OPERATING AND COULD NOT DETECT ANY FUEL SMELL. THE APU WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,605 hrs · 5,562 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

BNA-DURING POST FLIGHT INSPECTION THE CREW THE OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY, PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARTRIDGE — DISCHARGED (FIRE EXTINGUISHER)

IAH - REFERENCE CONTINENTAL EXPRESS SERVICE DIFFICULTY REPORT CONTROL NR C2XA00IA054. THE H2O FIRE EXTINGUISHER WAS INSPECTED FOR WEAR ON THE FACE OF THE C-O2 CARTRIDGE DUE TO DEFECTS LISTED ON THE AFOREMENTIONED SDR. AN INDENTATION WAS FOUND ON THE C-O2 CARTRIDGE FACE WITHOUT ANY VISUAL HOLE BEING NOTED. THE CARTRIDGE WAS THEN TEST FIRED AND THE DISCHARGE TIME AND PRESSURE WERE FOUND TO BE LESS THAN THAT OF A NEW CARTRIDGE SAMPLED AT THE SAME TIME. A NEW H2O CARTRIDGE WAS INSTALLED IN THE FIRE BOTTLE AND RETURNED TO THE AIRCRAFT FOR RE-INSTALLATION. (X)

Part: VENT LINE — LOOSE (LT ENGINE)

TYS - FLT 3942 - CREW DIVERTED AIRCRAFT INTO TYS AFTER THE LEFT ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE FORWARD CENTER SUMP VENT TUBE ASSEMBLE TO BE LOOSE AT THE SERVICE MANIFOLD. THE VENT TUBE ASSEMBLE WAS TIGHTENED REFERENCE ALLISON ENGINE MM 79-27-30, LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE RIGHT EXTERIRO EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DAMAGED (NR 2 NACELLE)

BTV - DURING 5A INSPECTION, FOUND FUSELAGE DAMAGE ON RIGHT SIDE UNDER NR 2 ENGINE AS MARKED. MAINTENANCE REPAIRED SKIN AS PER EMB145 SRM NR 53-31-01. PRESSURE CHECKED AIRCRAFT GOOD. (M)

Part: BULB — FAILED (EMERGENCY EXIT)

IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)