N707EB

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 17,457 hrs · 15,618 cycles

DURING TAKEOFF ROLL AIRCRAFT HAD A TRIPLE CHIME FOLLOWED BY FLAPS AURAL WARNING MESSAGE. AIRCRAFT ABORTED TAKEOFF AT 110KTS WITH NO OTHER DISCREPANCIES. FLAP CHANNEL 1 CURRENTLY UNDER MEL 27-9. CMC DOWNLOAD SHOWED FAULTS FLAP SHORT CIRCUIT AND FLAP RT MOTOR BRAKE FAIL CHECKED RESISTANCE OF LT/RT MOTORS AND FLAP POWER TRANSITION UNIT ALL GOOD RAR FLAP ELECTRONIC CONTROL UNIT IAW EMB MM 27-53-02. OPS CHECK GOOD IAW EMB MM 27-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,680 hrs · 14,950 cycles

CREW NOTICED BURNING ODOR ON IN THE FLIGHT DECK AFTER LANDING, FLIGHT ATTENDANT NOTICE ODOR IN FRONT PORTION OF CABIN. PERFORMED ENGINE RUNS WITH PACKS ON WITH NO DEFECTS. INSPECTED ELECTRICAL SYSTEMS AND COMPONENTS FINDING NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 16,030 hrs · 14,414 cycles

FOUND EMERGENCY LIGHTS STAY ON ALL THE TIME. REPAIRED BROKEN GROUND WIRE AT GS8008 IAW EMB AMM 20-13-21. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,844 hrs · 14,269 cycles

FOUND PREVIOUS LEFT OMEGA BEAM REPAIR CORRODED AT FRAME 20. REMOVED EXISTING REPAIR. CLEANED AND TREATED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHT)

LGA - FLT 4866 - STRONG MELTING/BURNING SMELL OF ELECTRICAL WIRING FROM ROW 5 TO BACK OF AIRCRAFT. RAI LIGHT BALLAST. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FAN — OBSTRUCTED (E/E BAY)

DURING DESCENT ELECTRICAL ODOR IN COCKPIT AND CABIN FOR A DURATION OF 10 MINUTES. IN PRECIPITATION, WINDSHIELD HEAT ON AND WORKING. REMOVED THERMOCOUPLE INSULATION OUT OF BOTH FWD ELECTRONIC COMPARTMENT INTERNAL RECIRC FANS. FCF PASSED. AIRCRAFT RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THE GALLEY FORWARD DIGITAL WAS FOUND CORRODED. REMOVED EXISTING DIGITAL AND INSTALLED SERVICEABLE DIGITAL IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTER 51-40-02. (M)

Part: ACM — SEIZED (NR 1)

DURING CRUISE FLIGHT, THE CREW REPORTED VISABLE SMOKE AND BLACK SOOT COMING FROM AIR VENTS IN FLIGHT DECK ALSO, FLIGHT ATTENDANT ALSO NOTED SMOKE IN CABIN AND CRACKLING NOISE FROM UNDER CABIN FLOOR. CREW DIVERTED TO ROA, EMERGENCY WAS DECLARED AND CFR FOLLOWED A/C TO GATE WITH NO FURTHER INCIDENT REPORTED. REPLACED NR 1 ACM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPUTER — FAILED (EICAS)

IN CRUISE AT FL 290 CAPTAIN MULITFUNCTIONAL DISPLAY AND EICAS FAILED WITH BURNING ODOR. DIVERTED, OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200407047)

Part: ENGINE — MALFUNCTIONED (NR 1)

PWM - FLT 4645 - A/C LEVEL AT 21K FT JUST ABOUT TO SET CRUISE MODE FELT YAW AND HEARD LOUD BANG NOISE. NR 1 ENGINE UNCOMMANDED SHUTDOWN. AIRCRAFT DECLARED EMERGENCY AND LANDED IN PWM. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

DURING PREFLIGHT CREW REPORTED THE LEFT WING EXIT SIGN DID NOT WORK. AIRCRAFT WAS INSPECTED AND FERRIED TO LGA FOR CORRECTIVE ACTION. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

BGR - FOUND EMERGENCY EXIT SIGN FOR LEFT OVERWING EXIT WOULD NOT ILLUMINATE. MAINTENANCE INSTALLED NEW INVERTER, OPS CHECK GOOD AND RETURNED A/C TO SERVICE. (M)

Part: SIGN — INOPERATIVE (OVERWING)

MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT SIGN TO BE INOPERATIVE. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC2003-145/0818. (M)

Part: FLOORBEAM — CORRODED (FS 20)

ABI - DURING A IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION OF THE LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM (SRM EMB 145/1142 REV 20) CHAPTERS 53-21-10, FIG 201. (M)

Part: BEAM — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM RAMP SUPPORT CORRODED. REMOVED AND INSTALLED NEW GALLEY CENTER BEAM RAMP SUPPORT IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04. (M)

Part: SILL — CORRODED (CARGO DOOR)

ABI - DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED NEW SILL IAW EMB-145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-40-06, 51-40-02, 51-20-03, EMB 145 CPM 51-21-04, THROUGHT 51-21-06. (M)

Part: SILL — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR FORWRAD SILL IAW EMB 135 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2

THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION PASSENGER DOOR FORWARD FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED PASSENGER DOOR FORWARD FLOOR SUPPORT IAW EMB 135 51-40-02 AND 51-20-03. (M)

Part: SILL — CORRODED (GALLEY) · corrosion level 2

THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR AFT SILL CORRODED. REMOVED SERVICE DOOR AFT SILL AND INSTALLED NEW SERVICEABLE SILL IAW EMB 135 SRM 51-40-02, 51-40-06, 51-40-04 AND 51-20-03. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, RIGHT BEAM FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE RIGHT BEAM FORWARD GUSSET IAW EMB 135 SRM 51-40-02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION CENTER BEAM GUSSET CORRODED IN GALLEY. INSTALLED NEW GALLEY CENTER BEAM GUSSET IAW EMB 135 51-20-03, 51-20-01, 51-40-02, 51-40-04 AND 51-40-06. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, PASSENGER DOOR AFT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE PASSENGER DOOR AFT FLOOR SUPPORT IAW EMB 35 SRM 51-40-02, 51-20-03. (M)

Part: DOUBLER — CORRODED (CARGO FLOOR) · corrosion level 2

THIS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, LEFT DOUBLER CORRODED BETWEEN FRAME 65 AND 68. REMOVD AND INSTALLED NEW LEFT DOUBLER BETWEEN FRAMES 65 AND 68 IAW EMB135/145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06 AND CPM 51-21-04. (M)

Part: BEAM — CORRODED

THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM GUSSET IAW EMB 135/145 SRM 51-40-02, 51-40-04, 51-40-06 AND CPM 51-21-04. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOS - FLT 4644 - CREW REPORTED LEFT ESCAPE HATCH EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ANTI-ICE SYSTEM — ODOR (COCKPIT)

ORF - FLT 4973 - CREW REPORTED THAT DURING FLIGHT WHEN ANTI-ICE SYSTEM TURNED ON THEY NOTICED A BURN SMELL IN THE COCKPIT. WHEN THE ANTI-ICE SYSTEM WENT OFF THE SMELL WNT AWAY. (M)

Part: UNKNOWN — ODOR (COCKPIT)

BOS - FLT 4745 - CREW REPORTED THAT DURING FLIGHT WHEN ANTI-ICE SYSTEM TURN ON THEY NOTICED A BURN ODOR IN THE COCKPIT. WHEN THE ANTI-ICE SYSTEM WENT OFF THE ODOR WENT AWAY. BOS MAINTENANCE RAN ENGINES IAW AMM AND COULD NOT DUPLICATE THE ODOR. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (HORIZ STAB)

BOS - FLT 4746 - PITCH TRIM 1 FAILED IN FLIGHT, WARNING ON EICAS. RETURNED TO BOS FOR MAINTENANCE. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW AMM. OPS CHECK GOOD. (M)