N16502

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 16,880 hrs · 17,013 cycles

DURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — INACCURATE (HYD SYSTEM) · airframe 16,223 hrs · 16,373 cycles

FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC MODULE (STEERING MANIFOLD) AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 16,222 hrs · 16,372 cycles

FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR IAW EMB 135 AMM 26-15-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. FWD SMOKE DETECTOR: P/N 473597-13 S/N 2907, TOTAL TIME= 9143, TOTAL CYCLES=6652, TIME SINCE INSPECTION=3436 AFT SMOKE DETECTOR: P/N 473597-13 S/N 1054, TOTAL TIME= 16222, TOTAL CYCLES=16372, TIME SINCE INSPECTION=16222

Part: SMOKE DETECTOR — LOOSE (CARGO BAY) · airframe 16,186 hrs · 16,343 cycles

FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — CHAFED (APU) · airframe 16,152 hrs · 16,312 cycles

CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HARNESS. PERFORMED OPERATIONAL CHECKS OF THE SYSTEM.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY) · airframe 16,222 hrs · 16,372 cycles

FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR IAW EMB 135 AMM 26-15-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHOCK ABSORBER — BINDING (RT MLG) · airframe 14,866 hrs · 14,995 cycles

CLE FLIGHT 2514 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR SHOCK ABSORBER. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE HARNESS — FAULTY (NR 1 ENGINE) · airframe 14,714 hrs · 14,835 cycles

CLE FLIGHT 2457 - THE CREW REPORTED A INTERMITTANT ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: SEAL — LEAKING (PAX DOOR) · airframe 13,491 hrs · 13,573 cycles

FLT 3031 - RIC - DURING FLIGHT, RIGHT OVERWING EMERGENCY EXIT DOOR AIR LEAK. RIC MX REMOVED THE DOOR, LUBRICATED DOOR SEAL, AND REINSTALLED IT. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,026 hrs · 13,102 cycles

DURING ROUTINE MAINTENANCE THE FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: SPLICE — DAMAGED (LIGHT WIRE) · airframe 12,833 hrs · 12,882 cycles

CLE - FLIGHT 2828, THE CREW REPORTED THE RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED DAMAGED WIRE SPLICE BEHIND LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 12,755 hrs · 12,799 cycles

SDF - BAGGAGE FIRE DETECTOR INOP. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW EMB 135 AMM 26-15-01. OPS CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 12,433 hrs · 12,434 cycles

SHV - DURING C-CHECK CORROSION DAMAGE WAS DISCOVERED ON STR 20L BETWEEN FRAME 59 AND 60. MAINTENANCE REMOVED CORROSION AND REPAIRED STR 20L BETWEEN FRAME 59 AND 60 IAW EC5310-01388. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,432 hrs · 12,434 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,432 hrs · 12,434 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,432 hrs · 12,434 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 TO 35. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, FIG 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,432 hrs · 12,434 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 TO 32. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,432 hrs · 12,434 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TUBE — LEAKING (NR 1 ENGINE) · airframe 9,407 hrs · 9,254 cycles

ENROUTE, DIVERTED, CREW REPORTED, ENGINE NR 1 LOST OIL INFLIGHT. PERFORMED SHUTDOWN IAW QRH. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED PRESSURE OIL CONTROL TUBE TO ENGINE GEARBOX, OPS AND LEAK CHECKED GOOD REFERENCE MM NR 71-00-01. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — DAMAGED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE SERVICE DOOR FORWARD SILL AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 53-00-04, 51-40-02, 51-30-01 AND CPM 51-21-04, 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (GALLEY FLOOR) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE RT HAND FORWARD DIGITAL UNDER THE GALLEY WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

TYS DUEING A SCHEDULED INSPECTION THE LEFT HAND FORWARD RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM TOP CAP WAS FOUND TO BE CORRODED UNDER SEAT TRACK LF1. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02 AND M.M. 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION 2 DENTS WHERE FOUND AFT OF THE PAX DOOR BETWEEN FRAMES 19 AND 20, ABOVE STR 12L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A FILLER AND DOUBLER, ALIDINED, INSTALLED THE PATCH, PRIMED AND PAINTED. I/A/W-EMB-135/145-SRM-53-21-01, CMP-51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: CAM — CORRODED (NLG) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR STRUT MAIN HOUSING AND LOWER CAM WERE FOUND TO HAVE AREAS OF CORROSION AND PITTING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY IAW EMB MM 32-20-01, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BRACKET — CORRODED (THRESHOLD) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULE INSPECTION THE MAIN PASSENGER DOOR THRESHOLD BRACKETS WERE FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD BRACKETS IAW EMB SRM 51-40/02, 51-30-02 AND CPM 51-21-04,05 AND 06. THE REPAIR WAS FOUND TO SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — DAMAGED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE MAIN DOOR SILL SKIN, MAINTENANCE REMOVED AND REPLACED THE SILL I/A/W-EMB-135-AMM-53-21-00.

Part: BEARING CAP — CRACKED (RT MLG) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE FLOORBEAM AT FRAME 22 RT, WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 22 IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PLATE — CORRODED (GALLEY FLOOR) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE GALLEY RIGHT HAND AFT CROSS BEAM PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CROSS BEAM PLATE IAW EMB SRM 51-10-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CAP — CRACKED (LEFT MLG) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE LT MLG BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (GALLEY FLOOR) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: AXLE — DAMAGED (RT MLG) · airframe 7,745 hrs · 7,598 cycles

DURING A SCHEDULED INSPECTION THE RIGHT MLG RETRACTION AXLE CHROME PLATED AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG RETRACTION AXLE I/A/W-EMB-135-AMM-32-10-03. OPS AND LEAK CHECKED GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,745 hrs · 7,598 cycles

TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,739 hrs · 7,594 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL BUTTSTRAP WAS CORRODED. MAINT REMOVED THE FWD DIGITAL, FAB A DOUBLER AND INSTALL A NEW FWD DOUBLER, ALLODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: PLATE — CORRODED (FUSELAGE) · airframe 7,739 hrs · 7,594 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE RT AFT CROSS BEAM PLATE WAS CORRODED. MAINT R&R THE AFT CROSS BEAM PLATE IAW EMB 135/145 SRM 51-10-02 ALLODINED, PRIMED AND PAINTED REWORK AREA IAW EMB 135/145 CPM 51-21-04'05'06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,739 hrs · 7,594 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE FLOORBEAM AT FR 22 RT SIDE WAS FOUND CORRODED IN SEVERAL AREAS. MAINT R&R THE FLOOR BEAM AT FR 22 IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 7,739 hrs · 7,594 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND WITH SEVERAL AREAS THAT WAS CORRODED. MAINT R&R THE AFT GUSSET IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: BEARING — SEIZED · airframe 6,937 hrs · 6,821 cycles

EWR ACFT PULLS RIGHT ON T/O. ABORTED T/O AND TAXI BACK TO GATE. ACFT CONTINUED TO PULL RIGHT DURING TAXI. REMOVED AND REPLACED NOSE TIRE/WHEEL ASSYS. FOUND SEIZED BEARING. ALL IAW EMB MM 32-49-05. OPS CHECK GOOD.

Part: RECEPTACLE — BURNED (GALLEY)

CLE FLIGHT 3180 THE CREW REPORTED ELECTRICAL SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED BOTH LEFT AND RIGHT COFFEE WARMER RECEPTACLES. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE MAINTENANCE FOUND THE CABIN EMERGENCY AISLE LIGHT INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE EMERGENCY AISLE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (TAIL)

MSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR AND THE HORIZONTAL STABILIZER CONTROL UNIT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.HORIZONTAL STAB CONTROL UNIT P/N 362100-1007 S/N 1207 TOTAL TIME:4724 CSN:4448

Part: BRACKET — CHAFED (PAX DOOR) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE MAIN CABIN DOOR, HANDLE BRACKET WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB-GST-1405/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PLATE — CORRODED (CABIN) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE JUST AFT OF FLIGHT DECK WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SLICE REPAIR IAW EMB-GST-1266/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AFT OF FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EMB-135 SRM-53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: MOUNT — CHAFED (LT PYLON) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AFT RAMP ANGLE FORWARD OF FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-30-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-GST-3120/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FITTING — GOUGED (HORIZ STAB) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1340/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA RAMP ANGLE WAS FOUND CORRODED AT FRAME 20. 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: BRACKET — GOUGED (LT WING) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT AILERON ACTUATOR ATTACH BRACKET WAS FOUND GOUGED ON THE SECOND FROM INBOARD FITTINGS. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST-1299/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE EXTERIOR HANDLE. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1314/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM TOP CAP BETWEEN FRAMES 18 AND 22 WAS FOUND GOUGED AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM TOP CAP IAW EMB-135 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 3,632 hrs · 3,337 cycles

TYS DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN WAS FOUND CORRODED AT FRAME 67 ON STRINGER 17R. MAINTENANCE REPAIRED THE DAMAGE AREA IAW EMB-135 SRM 53-31-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DUCT — CRACKED (E/E BAY)

CLE: CREW REPORTED NR 1 BLEED LEAK INDICATION AFTER TAKEOFF IN CLEVELAND. A/C RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE BLEED DUCT CRACKED ON LEFT SIDE IN THE AFT AVIONICS COMPARTMENT. DUCT WAS REPLACED IAW 36-12-02 & 36-11-09. OPERATIONAL CHECKS WERE GOOD IAW 36-00-00.

Part: ENGINE — FAILED (NR 1)

CLT - FLT 3909 - CREW REPORTED ON TAKEOFF ROLL, JUST AFTER SETTING THRUST TO TAKEOFF POSITION, THE NR 1 ENGINE OIL PRESSURE SPIKED TO 119 PSI. THE CREW REDUCED THRUST SETTINGS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW EMB135 TASK CARD 7271001. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)