N16501

Part: RMU — SMOKE (COCKPIT) · airframe 12,620 hrs · 12,578 cycles

CLE FLIGHT NR 2786, CREW REPORTED SMOKE COMING FROM THE CO-PILOTS RMU WHILE TAXIING TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE CO-PILOTS RMU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,521 hrs · 12,462 cycles

SHV - DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED AT FRAME 51. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,521 hrs · 12,462 cycles

DURING C-CHECK LT OMEGA BEAM FROM FR 20 TO 24 HAS CORROSION. MAINTENANCE SPLICED IN NEW LT OMEGA BEAM AT FR 18 TO 24 IAW EC5320-01229.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 12,521 hrs · 12,462 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 24. MAINTENANCE REMOVED THE DAMAGED AREA AND SPLICED IN A NEW BEAM SECTION IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 12,521 hrs · 12,462 cycles

SHV - DURING C-CHECK CENTER FUSELAGE 3 EXTERNAL SKIN HAS AREA OF CORROSION AT STR 19R FR 50 HYDRAULIC LINE PASS THROUGH. MAINTENANCE REPAIRED CENTER 3 EXTERNAL SKIN AT STR R19 FR 50 IAW EC5330-01624. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PDU — FAILED (TE FLAPS) · airframe 11,424 hrs · 11,265 cycles

CLE FLIGHT 2056 - THE CREW REPORTED A -FLAP FAIL- MESSAGE ON THE EICAS UPON SELECTING FLAPS -22- DEGREES. FLAPS WERE STUCK AT THE -18- DEGREE POSITION. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLAP POWER DRIVE UNIT. PERFORMED -O- DEGREEE RIGGING AND OPERATIONAL CHECKS WERE GOOD.

Part: HEATER — BURNED (WINDSHIELD) · airframe 10,090 hrs · 9,886 cycles

CLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,066 hrs · 7,822 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ATTACH FITTING — GOUGED (VERTICAL STAB) · airframe 8,066 hrs · 7,822 cycles

DURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SOLENOID VALVE — FAILED (NLG)

CLE FLIGHT 3960 AFTER LANDING GEAR RETRACTION CREW REPORTED LOUD AIR NOISE COMING FROM NOSE LANDING GEAR AREA. NOISE INCREASED WITH AIRSPEED. AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITH OUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SOLENOID VALVE. PERFORMED OPERATIONAL CHECKS AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW — LEAKING (COCKPIT)

CLE FLIGHT 3971 AFTER DEICING OF AIRCRAFT THE CREW REPORTED A HISS AND POP SOUND FOLLOWED BY SMOKE COMING FROM FIRST OFFICER''S SIDE PANEL. THE ENGINES WERE SHUT DOWN AND ALL ELECTRICAL POWER WAS TURN OFF. MAINTENANCE INSPECTED AND FOUND DEICE FLUID HAD LEAKED THRU THE RIGHT SIDE WINDOW AND DOWN INTO THE TAT 2 SENSOR RELAY (KO494) AND THE PITOT STATIC SENSOR RELAY (KO054). THESE RELAY''S ARE BEHIND PANEL 224 ERW AND WERE FOUND TO BE BURNT. THE RELAYS WERE REPLACED ALONG WITH THERE SOCKETS. MAINTENANCE ALSO COMPLIED WITH EA 2510-01030 SIDE CONSOLE PANEL AND STORM WINDOW SEALING IMPROVEMENT. ALL DEICE FLUID WAS REMOVED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE - FLT 3949 - THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE AT ROWS 3 THROUGH 6. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY NR 3. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: CHARGER — INOPERATIVE (CABIN)

CLE - FLT 4135 - THE CREW REPORTED THAT THE 2ND AND 3RD SEAT OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE DURING THERE PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW EMB135 MM 33-50-04. MAINTENANCE ALSO REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW 33-50-04. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: UNKNOWN — ODOR (CABIN)

CREW REPORTED A STRONG SMELL OF JET FUMES WHEN THE APU RUNS PACK NR 1. MX RAN APU AND CHECKED FOR LEAKS, NO LEAKS FOUND ALSO RAN PACK AND NO FUMES WERE NOTED. A/C WAS RELEASED FOR SERVICE.

Part: STARTER — FAILED (LT ENGINE)

ROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE INFLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVETFULLY. MAINTNANCE DISPATCHED TO TROUBLESHOOT AND FOUND LEAKING NR 1 ENGINE AIR STARTER SHAFT, BROKEN. MAINTENANCE REMOVED AND REPLACED AIR START GENERATOR IAW EMB135 MM 80-10-01. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: STARTER GEN — LEAKING (LT ENGINE)

ROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE IN FLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVENTFULLY. MAINTENANCE DISPATCHED TO T/S AND FOUND LEAKING NR 1 ENGINE AIR STARTER. MAINTENANCE REMOVED AND REPLACED AIR START GENERATOR. (M)

Part: STARTER — FAILED (LT ENGINE)

RDU-CLE - FLT 4009 - THE CREW REPORTED THE NR 1 ENGINE OIL QUANTITY DROPPED TO 2 QUARTS INDICATED. THE CREW PERFORMED AN INFLIGHT SHUTDOWN AND DIVERTED INTO ROA. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE AIR TURBINE STARTER SHAFT HAD BROKEN. THE STARTER WAS REPLACED IAW EMB135 MM 80-10-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

TYS - DURING A SCHEUDLED INSPECTION, THE LEFT ENGINE WAS FOUND TO BE PRODUCING METAL THAT WAS BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-135 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)