N10575

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,074 hrs · 22,760 cycles

DURING C-CHECK THE SERVICE DOOR BOTTOM FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5340-01100. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 28,074 hrs · 22,760 cycles

DURING C-CHECK THE CARGO DOOR BOTTOM FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01371. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 28,074 hrs · 22,760 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: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 28,074 hrs · 22,760 cycles

DURING C-CHECK, THE SHEAR CLIP AT FRAME 65 CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04, FIG. 213. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FCU — LEAKING (APU) · airframe 22,499 hrs · 18,429 cycles

THE CREW REPORTED A STRONG FUEL ODOR IN COCKPIT DURING TAXI AND ROTATION. MX REPLACED THE APU FUEL CONTROL ASSY THAT WAS LEAKING. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (WARNING SYSTEM) · airframe 18,280 hrs · 15,040 cycles

ORD FLT 6159 THE CREW REPORTED A RUDDER II INOP MESSAGE IN FLIGHT AND THE RUDDER I C/B WAS POPPED. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND COULD NOT DUPLICATE THE PROBLEM. THE WIRING FROM CONNECTOR PO827 TO PO055 WAS CHECKED AND NO DEFECTS WERE FOUND.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 17,989 hrs · 14,818 cycles

AIRCRAFT N10575 A-CHECK RIC. FLOOR EXIT LIGHT STRIP INOP 12A UPPER AND LOWER EXIT SIGN INOP, 12BC UPPER AND LOWER EXIT SIGN INOP, 12A CEILING LIGHT, 12BC CEILING LIGHT AND CENTER EXIT SIGN AFT INOP. MAINTENANCE REMOVED INOP POWER SUPPLY AND DEAD BATTERY AND INSTALLED REPAIRED POWER SUPPLY AND REPAIRED BATTERY IAW EMB-145 AMMII 33-50-04, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,177 hrs · 14,162 cycles

ORD - THE CREW REPORTED A STRONG FUEL SMELL ON APU START-UP ON GROUND. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TESTS OF APU. NO FUEL SMELL WAS NOTED.

Part: UNKNOWN — ODOR · airframe 16,631 hrs · 13,709 cycles

ORD FLT 5918 THE CREW REPORTED A RAW FUEL SMELL AFTER LANDING WITHIN 60 SECONDS. THE APU WAS OFF AND BLEEDS AND PACKS WERE ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON BLEED SYSTEM. NO FUEL SMELL WAS NOTED AND NO FUEL LEAKS WERE FOUND. NO DEFECTS NOTED AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: SENSOR — FAULTY (LAVATORY) · airframe 15,100 hrs · 12,278 cycles

LNK FLT 5754 THE CREW REPORTED A LAV SMOKE INDICATION ON THE EICAS DURING APPROACH. THE INDICATION WENT AWAY AND THEN RETURNED SECONDS LATER. NO FLAMES OR SMOKE WERE SEEN/SMELLED.

Part: ECU — FAULTY (TE FLAP) · airframe 14,462 hrs · 11,737 cycles

CLE FLIGHT 995 THE CREW REPORTED A FLAP FAIL MESSAGE ON THE EICAS DURING APPROACH INTO CLE. ALSO REPORTED A FLAP LOW SPEED AND SPS ADVANCE MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE FECU. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,462 hrs · 11,737 cycles

CLE FLIGHT 600 THE CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY AND OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,400 hrs · 11,683 cycles

DURING ROUTINE MAINTENANCE THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND DISCHARGED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: TURBINE WHEEL — CRACKED (NR 2) · airframe 14,399 hrs · 11,679 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.

Part: BUTTSTRAP — CRACKED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO COMPRATMENT CENTER BUTTSTRAP WAS CRACKED AT FRAME 71. MAINTENANCE FABRICATED AND INSTALLED A REPAIR PIECE IAW CONTINENTAL EXPRESS EC5320-01412. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER OMEGA BEAM WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: SUPPORT — CORRODED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE TOILET EXTERNAL WASTE VALVE SUPPORT WAS CORRODED AT FRAME 60. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB145 SRM 53-31-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FITTING — WORN (RT AILERON)

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA FITTING HAD MIGRATED HAT BUSHINGS. THE HOLES WERE FOUND TO BE WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: MANIFOLD — INOPERATIVE (NR 2 AILERON) · airframe 13,073 hrs · 10,623 cycles

FLT 7822 - LAX - DURING PREFLIGHT CHECK CREW REPORTED NOT GETTING AILERON 2 INOP MSG ON EICAS WHILE AIRCRAFT WAS POWER UP WITH HYD SYSTEM OFF. MX PERSONNEL REMOVED AND REPLACED NR 2 AILERON HYD MANIFOLD OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: ALTIMETER — INOPERATIVE (COCKPIT) · airframe 12,586 hrs · 10,197 cycles

FLT 7803 - SLC TO EUG - FLIGHT CREW REPORTED RA 1 INOP IN FLIGHT. MX PERSONNEL REMOVED AND REPLACED RA 1, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,391 hrs · 8,199 cycles

FLIGHT 2362 DESENDING INTO ATL, THE NUMBER ONE WINDSHIELD SHATTERED. A/C LANDED SAFELY AND MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE WINDSHIELD IAW EMB 145 AMM TWO 56-10-01. PRESSURIZATION CHECKS AND LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,742 hrs · 6,912 cycles

SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM FRAME 18-23. MAINTENANCE REPAIRED LT OMEGA BEAM FROM FRAME 18-23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 8,000 hrs · 6,314 cycles

DURING ROUTINE MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,946 hrs · 6,277 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT AND RT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — DAMAGED (BLEED SYSTEM) · airframe 5,416 hrs · 4,269 cycles

SHV - DURING CLIMB, ENG NR 2 HAS FIRE WARNING INDICATION. MAINTENANCE INSPECT AND FOUND UPPER BLEED DUCT DAMAGE NO FIRE WAS EVIDENT. REPLACE BOTH UPPER BLEED DUCTS PER EMB 145AMM 36-11-09. PERFORMS GROUND OPPERATIONAL CHECK AND LEAK CHECK PER AMM 72-00-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: BLADE — FRACTURED (STAGE 1 HPC) · airframe 4,514 hrs · 3,561 cycles

1ST STAGE HPC BLADE FOR NR 2 ENGINE FRACTURED DURING OPERATION, RESULTING IN UNCOMMANDED IN-FLIGHT SHUTDOWN. ONCE ENGINE DISASSEMBLED, BLADE REMNANT RETURNED TO ROLLS-ROYCE FOR ANALYSIS.

Part: BLADE — FAILED (COMPRESSOR)

DURING DESCENT INTO RDU, RIGHT ENGINE HAD A UNCOMMANDED SHUTDOWN AFTER A LOUD NOISE WAS HEARD. MAINTENANCE REMOVED AND REPLACED THE ENGINE. THE TEAR DOWN REPORT SHOWS THE CAUSE OF THE FAILURE TO BE A COMPRESSOR BLADE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,092 hrs · 3,242 cycles

TYS - DURING A SCHEDULED 1C INSPECTION THE RT OMEGA BEAM FOR THE AISLE CROSS BEAM WAS FOUND CORRODED AT FR 25. MAINTENANCE REMOVED THE CORRODED AREA, FORMED, BENT A DOUBLER AND FILLER, PLUS SHIMS, ALODINED, PRIMED AND PAINTED. FAB PARTS WERE INSTALL IAW EMB 135/145 SRM 51-21-10; EMB 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,092 hrs · 3,242 cycles

TYS - DURING A SCHEDULED 1C INSPECTION THE CENTER FLOORBEAM AT FR 25 WAS FOUND CORRODED. MAINT BLENDED AREAS OF CORROSION FORWARD OF CROSSBEAM AT FR 25. ALODINED BLENDED AREA. PRIMED AND PAINTED AREA IAW EMB 135/145 CPM 51-21-04, 05, 06 AND SRM 51-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BLEED VALVE — FAULTY (APU)

EWR FLIGHT 2060, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00. ON 3/31/04 MAINTENANCE REPLACED THE APU BLEED AIR VALVE. OPERATIONAL CHECKS WERE GOOD.