N13914

Part: A/C PACK — ODOR (NR 2) · airframe 33,958 hrs · 25,903 cycles

THE CREW REPORTED THAT THE PACK SYS HAD A STANGE ODOR. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND PACK 2 TO BE CAUSING THE ODOR. PACK 2 WAS PLACED ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE OPERATIONALLY TESTED THE NR 2 PACK, FOUND NO ODORS PRESENT IN PACK 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 32,239 hrs · 24,571 cycles

DURING A-CHECK INSPECTION, THE LT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAMES 75 - 76 AT ONE RIVET. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 31,825 hrs · 24,233 cycles

DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 31,825 hrs · 24,233 cycles

DURING C-CHECK THE WASTE DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED AT FRAMES 60-61, STRINGERS 18-20R. MAINTENANCE R & R THE SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 31,825 hrs · 24,233 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 31,488 hrs · 23,968 cycles

ACFT WAS IN FLIGHT WHEN CREW RECEIVED AN EICIAS MESSAGE FOR LANDING GEAR AIR-GROUND FAIL. ACFT WAS FERRIED, WHERE MAINTENANCE REPAIRED THE NLG WOW PROXIMITY SWITCH IAW AMM 32-63-01, IPC 32-50-06; FIGURE 1, ITEM 1. OPS CHECK GOOD AND WAS RELEASED BACK TO NORMAL CONFIGURATION.

Part: TRANSDUCER — FAULTY (MLG) · airframe 29,276 hrs · 22,299 cycles

CREW REPORTED BRAKES DIDN'T WORK PROPERLY ON LANDING AND TOOK ENTIRE RUNWAY TO SLOW. MX FOUND NR 1 WHEEL SPEED TRANSDUCER FAILED. MX R & R NR 1 WHEEL SPEED TRANSDUCER WITH OPS AND TAXI CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,590 hrs · 21,748 cycles

DURING MX INSPECTION, THE MAIN DOOR EMERGENCY LIGHT WAS FOUND NOT TO ILLUMINATE. MX R & R THE NR 1 EMERGENCY LIGHT INVERTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,239 hrs · 21,486 cycles

FOUR DENTS LOCATED BETWEEN FR22/FR23 AND STRINGER 12L/14L. MX REPARIED FUSELAGE SKIN IAW ETD2013-145-000362-C AND SRM 53-21-01, TYPE A1. (1 DOUBLER) FIG 202 USING 3 RIVET ROWS. ACFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,263 hrs · 20,689 cycles

CREW REPORTED ELECTRICAL SMOKE ODOR IN FLIGHT. MX INSPECTED THE ACFT AND FOUND LT AVIONICS EXHAUST FAN INOPERATIVE WITH NO OTHER DEFECTS AFTER GROUND RUNS. APPROVED FOR RETURN TO SERVICE. OPS CHECK OF THE ELECTRONIC COMPARTMENT VENTILATION SUCCESSFUL AND NO FAULTS NOTED.

Part: STARTER GEN — INOPERATIVE (APU) · airframe 27,262 hrs · 20,688 cycles

THE CREW REPORTED APU GENERATOR OFF BUS INDICATION AND A BURNING ODOR IN COCKPIT. MX REPLACED APU STARTER GENERATOR. PERFORMED OPS CHECKS GOOD AND NO BURNING ODOR WAS NOTED.

Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 23,467 hrs · 17,753 cycles

CLE FLT 2019 - THE CREW REPORTED AN ENGINE NR 1 FIRE DETECT FAIL MESSAGE DURING PREFIGHT CHECKS. MAINTENANCE INSPECTED AND REPLACED THE ENGINE NR 1 FIRE DETECTOR LOOP. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,487 hrs · 17,016 cycles

FLIGHT 2685 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 21,070 hrs · 15,951 cycles

CLE FLT 2180 THE CREW REPORTED A RUDDER SYSTEM 1 INOP MESSAGE DURING TAXI. RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 RUDDER PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 20,436 hrs · 15,478 cycles

IAH - FLIGHT 2363 THE CREW REPORTED THAT THE NUMBER ONE HYDRAULIC SYSTEM FAILED ON TAXI. THE AIRCRAFT WAS SHUTDOWN AND TOWED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP, SERVICED HYDRAULICS, OPERATIONALLY / LEAK TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 17,402 hrs · 13,196 cycles

FLIGHT 2874 - CHS - FLIGHT CREW REPORTED AUTO PRESS FAIL IN FLIGHT. MX REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A)

Part: CONNECTOR — DIRTY (MLG) · airframe 17,043 hrs · 12,937 cycles

IAH - FLIGHT 2331, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS ON INITIAL TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED, CLEANED, AND REINSTALLED THE CONNECTORS ON THE RIGHT MAIN LANDING GEAR FORWARD PROXIMITY SENSORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (LANDING GEAR) · airframe 17,043 hrs · 12,937 cycles

IAH - FLIGHT 2331, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS ON INITIAL TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED, CLEANED, AND REINSTALLED THE CONNECTORS ON THE LEFT MAIN LANDING GEAR FORWARD PROXIMITY SENSORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (STABILIZER) · airframe 16,782 hrs · 12,754 cycles

CLE FLIGHT 2898 THE CREW REPORTED A YAW TRIM RUNAWAY IN FLIGHT. QRH WAS FOLLOWED AND FOUND BOTH SYSTEMS TO BE INOPERATIVE. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE YAW TRIM SWITCH AND ACTUATOR. OPERATIONAL CHECKS WERE GOOD. SWITCH P/N 79-2257.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 14,760 hrs · 11,310 cycles

BNA FLIGHT 2634 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM BNA. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,284 hrs · 10,976 cycles

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,028 hrs · 9,985 cycles

EWR LOG SQUAWK EMERGENCY OVERWING EXIT LIGHT INOP RIGHT SIDE. REMOVED AND REPLACED NR 5 INVERTER. OPS CHECK GOOD IAW EMB145 AMM 33-50-50.

Part: LIGHT — FAULTY (CABIN)

EWR---CO2996, CREW REPORTED EMERGENCY EXIT ROW SIGN AT ROW 12 IS NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT ROW LIGHT PANEL IAW EMB145 AMM NR 33-50-13, OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,527 hrs · 9,576 cycles

SHV - DURING C-CHECK THE AFT SERVICE DOOR FRAME WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15 & 16R. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 12,443 hrs · 9,513 cycles

DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPING. MAINTENANCE INSPECTED THE AIRCRAFT, REPAIRED WIRING AT THE NR 4 EMERGENCY LIGHT BATTERY PACK, AND REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE PERFORMED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,921 hrs · 9,113 cycles

CLE FLIGHT 2118 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT IN REAR WAS NOT WORKING. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 11,710 hrs · 8,945 cycles

STL - DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 11,710 hrs · 8,945 cycles

STL - DURING MAINTENANCE INSPECTION, THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECK WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: REINFORCEMENT — GOUGED (FUSELAGE) · airframe 7,789 hrs · 5,874 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,789 hrs · 5,874 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 20 IAW EMB 145 SRM 53-21-10. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 7,789 hrs · 5,874 cycles

SHV - DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,789 hrs · 5,874 cycles

SHV - DURING C-CHECK, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (HORIZ STAB)

IAH - FLT 2546 - CREW REPORTED THAT THE PITCH TRIM 1 AND 2 FAIL MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU). THE AIRCRAFT WAS OPERATIONALLY TESTED AND APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — LEAKING (SPEED BRAKE)

IAH- FLIGHT 2751, THE CREW DECLARED EMERGENCY INTO IAH DUE TO NR 2 HYDRAULIC LOW QUANTITY AND LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 2 SPEED BRAKE ACTUATOR, SERVICED THE HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — LEAKING (SPOILER)

IAH- FLIGHT 2751, THE CREW DECLARED EMERGENCY DUE TO NR 2 HYDRAULIC LOW QUANTITY AND LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 2 GROUND SPOILER ACTUATOR, SERVICED THE HYDRAULIC SYSTEM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (CABIN) · airframe 3,749 hrs · 2,730 cycles

DURING C CHECK EMERGENCY LIGHT ON PANEL 191 HL WAS FOUND INOPERATIVE. MAINTENANCE REMOVED ANT REPLACED BULB OF AFFECTED LIGHT. OPERATIONAL CHECKED GOOD IAW EMB 145 AMM 33-50-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU FIREWALL) · airframe 3,749 hrs · 2,730 cycles

SHV- DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT TOP 2 RIVETS OF R/H VERTICAL REINFORCEMENT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED · airframe 3,749 hrs · 2,730 cycles

SHV-DURING C CHECK 19L STRINGER'S T REINFORCEMENT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED T REINFORCEMENT IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 3,749 hrs · 2,730 cycles

DURING C CHECK CENTER STRAP BETWEEN FRAMES 18 AND 13 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED · airframe 3,749 hrs · 2,730 cycles

SHV-DURING C CHECK TWO DENTS WHERE FOUND AFT OF PAX DOOR BETWEEN FRAMES 20 AND 21 AT STRINGERS 13L AND 14L. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: MODULE — FAULTY (COCKPIT)

CLE FLIGHT 4094 THE CREW REPORTED A APU FIRE EICAS MESSAGE INFLIGHT WITH THE APU RUNNING. THE CREW SHUT DOWN THE APU AND CLOSED THE FUEL SOLENOID VALVE FOR THE APU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF A FIRE. REPLACED THE APU CONTROL MODULE AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.