N27512

Part: SWITCH — FAULTY (NLG DOOR) · airframe 10,273 hrs · 10,358 cycles

CLE FLIGHT 2501 THE CREW REPORTED A VERY LOUD NOISE FROM THE FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTION. THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: SELECTOR — DEFECTIVE (TE FLAPS) · airframe 7,458 hrs · 7,421 cycles

CLE - UPON GEAR RETRACTION OF FLIGHT 2127 THE LANDING GEAR AURAL WARNING INDICATION CAME ON. REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB 135/145 AMM 27-51-03. OPS CHECKS WERE GOOD OF THE FLAPS AND LANDING WARNING SYSTEM IAW EMB AMM 27-50-00 AND 32-60-00. A/C WAS RELEASED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 9BC (IN PSU) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.

Part: LINER — MISALIGNED (EMERGENCY DOOR)

DURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE LT OVERWING INNER DOOR LINER TO BE MISALIGNED. MAINTENANCE REALIGNED LINER AND OPERATIONAL CHECKS WERE GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE AFT DIGITAL STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE RIGHT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AFT OF FRAME 23 AND FORWARD OF FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAME 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 14 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV - DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE PASSENGER DOOR FORWARD THRESHOLD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (STRINGER) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE STRINGER REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 7,039 hrs · 6,992 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 18 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG STRUT — SEIZED (NLG)

CLE FLIGHT 2127 THE CREW REPORTED ON APPROACH THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. THE CREW FOLLOWED THE QRH AND ACCOMPLISHED LANDING GEAR EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR MAIN DRAG STRUT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: ACCESS DOOR — STICKING (COCKPIT)

CLE FLIGHT 2438 THE CREW REPORTED, COULD NOT OPEN THE LANDING GEAR EMERGENCY EXTENSION ACCESS DOOR LOCATED IN THE COCKPIT. MAINTENANCE INSPECTED AND LUBED AND UNSTUCK THE ACCESS DOOR. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 6,313 hrs · 6,255 cycles

AIRCRAFT AIR-RETURNED TO CLE, EMERGENCY DECLARED, THE LEFT ENGINE FAILED IN FLIGHT, ITT SPIKED AT 1100 DEG C, WITH A LOUD BANG. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE, OPS AND LEAK CHECKED GOOD IAW EMB135-MM-71-00-00 AND TASK CARD 6271001. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CREW (DURING WALKAROUND) NOTICED THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AND OPS CHECKED SYSTEM GOOD.

Part: CONNECTOR — LOOSE (EXTINGUISHER)

CLE FLIGHT 2083 THE CREW REPORTED A EXTINGUISHING BOTTLE -B- ENGINE 1/2 MESSAGE INTERMITTENTLY IN FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED CANNON PLUG ON EXTINGUISHING BOTTLE -B- AND SECURED LOOSE BACKSHELL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

THE CREW REPORTED A FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — BURNED (CABIN)

CMH FLIGHT 3961 THE CREW REPORTED A BURNED PLASTIC ODOR COMING FROM THE REAR OF THE CABIN. THEY REPORTED THE ODOR SEEMED TO BE ASSOCIATED WITH THE APU AND THE NR 2 PACK.THE AIRCRAFT WAS RELEASED IAW MEL 21-51-00/1. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU AND NR 2 PACK. NO DEFECTS WERE FOUND. MAINTENANCE FOUND THE AFT EMERGENCY FLASHLIGHT CHARGER ASSEMBLY BURNED. THE CHARGER ASSEMBLY WAS REPLACED.

Part: NOZZLE — COKED (NR 2 ENGINE)

CLE FLIGHT 3085 THE CREW REPORTED A STRONG BURNING ODOR DURING ICE TEST AND WHEN NR 2 PACK IS ON. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — INOPERATIVE (A/C BAY)

CLE FLIGHT 4141 THE CREW REPORTED A SMOKE SMELL WHEN IN ICE CONDITIONS AND WHEN THE ICE TEST WAS DONE. MAINTENANCE INSPECTED AND REPLACED NR 2 PACK SETDOWN SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT 3193 THE CREW REPORTED NR 2 PACK HAD A BURNING SMELL. THE SMELL WENT AWAY AFTER THE PACK WAS TURNED OFF. MAINTENANCE INSPECTED NR 2 PACK AND PERFORMED SYSTEM CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: GENERATOR — CONTAMINATED (LEFT/RIGHT ENGIN)

CLE FLIGHT# 3194 THE CREW REPORTED ALL 4 GENERATORS FELL OFF LINE AFTER GEAR RETRACTION.THE #4 GENERATOR DID COME BACK ONLINE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND ALL FOUR GENERATORS TO BE CONTAMINATED WITH GLYCOL AND SAND.ALL FOUR GENERATORS WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULE INSPECTION THE FUSELAGE WAS DAMAGED BEHIND FRAME 31 BETWEEN STRINGER 12 AND 13R. REMOVED DAMAGED AREA. FABRICATED A DOUBLER, ALODINED AND INSTALLED, SEALED, PRIMED AND PAINTED IAW EMB 135 SRM 51-40-02 AND 51-22-01 AND CPM 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL INSPECTIONS.

Part: BYPASS JACKET — CORRODED (ENGINE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCHUP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MAGNESIUM AND PAINTED WITH A CORROSION PAINT IAW AE3007EC7220-01009, AESPM70-32-03 AND AE3007ASMM70-00-00 WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BYPASS JACKET — CORRODED (NR 1 ENGINE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCH UP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MAGNESIUM AND PAINTED WITH A CORROSION PAINT IAW AE3007EC7220-01009, AESPM70-32-03 AND AE3007ASMM70-00-00 WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE FLOOR SUPPORT ANGLES LOCATED BELOW THE THRESHOLD STRIP AT THE MAIN ENTRY DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-135 SRM 51-20-03, 51-40-02 AND CPM 51-21-04,05,06. THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ATTACH FITTING — DAMAGED (CABIN) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND COCKPIT PARTITION WALL ATTACHMENT POINTS WERE FOUND TO BE DAMAGED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST 3877/01, EMB-135 CPM 51-21-04, 51-21-05 AND 51-21-06. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: INLET — DAMAGED (RT ENGINE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE AIR INLET WAS FOUND TO HAVE TWO NICKS ON THE ACOUSTIC PERFORATED INNER SKIN. MAINTENANCE REWORKED THE NICKS (BLEND-OUT) IAW EMB-135 SRM 54-20-01 AND EMBRAER GST 3879/01, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LIMITER — GOUGED (ELEVATOR) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND ELEVATOR INBOARD LIMITER TUBE WAS FOUND TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST-3934/01, THE REPAIR AND INSPECTION WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BELOW THE FLOORING AND JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE SUBFLOOR GUSSET LOCATED JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE GUSSET IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE RAMP ANGLE ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE TOP CAP ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED THE CORRODED AREA AND ACCOMPLISHED A DOUBLER REPAIR IAW EMB-135 SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LINE — CORRODED · airframe 3,097 hrs · 2,942 cycles

TYS During a scheduled inspection the pottable water line was found corroded at the fuselage to tube fitting. Maintenance removed and replaced the potable water overflow line I.A.W.-EMB-135-AMM-38-10-07. Repairs where satisfactory and the aircraft will be released upon complection of the inspection.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 3,097 hrs · 2,942 cycles

TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER ACTUATOR FAILED A FUNCTIONAL CHECK. THE ACTUATOR INNER PISTON HAS PLAY AND NONE WAS ALLOWED IAW CONTINENTAL EXPRESS TASK CARD 27-40-02-220-001-A00. MAINTENANCE REMOVED AND REPLACED THE ACTUATOR IAW EMB-135 MM 27-40-02, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ACTUATOR — LEAKING (NOSE GEAR)

CLE FLIGHT#3128 THE CREW REPORTED INFLIGHT WITH GEAR UP INDICATION.THERE WAS A LOUD NOISE AND VIBRATION COMING FROM THE NOSE AREA.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND NOSE LANDING GEAR DOOR ACTUATOR LEAKING.THEY REPLACED THE ACTUATOR AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT TEST FLIGHT WAS GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.