N705AE

Part: SENSOR — MALFUNCTIONED (RUDDER) · airframe 17,283 hrs · 15,599 cycles

RUDDER SYSTEM 1/2 INOP MESSAGE A/C RETURNED TO DFW REMOVED AND REPLACED RUDDER SYSTEM 2 SENSOR IAW EMB MAINTENANCE MANUAL.

Part: SENSOR — MALFUNCTIONED (RUDDER) · airframe 17,283 hrs · 15,599 cycles

RUDDER SYSTEM 1/2 INOP MESSAGE A/C RETURNED TO DFW REMOVED AND REPLACED RUDDER SYSTEM 2 SENSOR IAM EMB MAINTENANCE MANUAL. AIRCRAFT RETURN TO SERVICE.

Part: FCU — FAILED (ZONE 100) · airframe 16,313 hrs · 14,770 cycles

NR 1 FUEL QUANITY WENT ZERO ON EICAS, DIVERTED TO RIC. REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND RIGHT FORWARD INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHINCAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND CENTER SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND LEFT INBOARD SEAT TRACK FROM FRAME 34 TO 43 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND LEFT INBOARD SEAT TRACK AT FRAME 19 TO 25 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 15,855 hrs · 14,409 cycles

FOUND RIGHT SIDE ELEVATOR CABLE WORN AT PRESSURE SEALS JUST AFT OF VERTICAL LEADING EDGE. REMOVED AND REPLACED ELEVATOR CABLE IAW EMB AMM 27-31-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND SEAT TRACK BETWEEN FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 15,855 hrs · 14,409 cycles

FOUND RIGHT RUDDER CABLE WORN AFT OF FRAME 50 PRESSURE SEAL. REMOVED AND REPLACED CABLE IAW EMB AMM 27-21-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,855 hrs · 14,409 cycles

FOUND FORWARD SERVICE DOOR SILL CORRODED AT FRAME 20. REPAIRED FORWARD SILL IAW EMB SRM 53-21-10, FIGURE 204. RETURNED AIRCRAFT TO SERVICE.

Part: CABLE — WORN (RUDDER) · airframe 15,855 hrs · 14,409 cycles

FOUND OUTBOARD RUDDER CABLE WORN AT FRAME 50 PRESSURE SEAL. REMOVED AND REPLACED CABLE IAW EMB AMM 27-21-01. OPERATIONAL CHECK GOOD, RETURN AIRCRAFT TO SERVICE.

Part: ACM — SMOKE (NR 1)

CREW REPORTED BURNING ODOR IN BOTH COCKPIT AND CABIN. REAR OF ACFT HAD SMALL AMOUNT OF SMOKE VISIBLE. MEL WAS ISSUED AND ACFT RETURNED TO SERVICE. MX REMOVED AND REPLACED NR 1 ACM IAW EMB MM. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION FOUND, CENTER OMEGA HAS CORROSION UNDER CROSS BEAM AT FRAME 29. REMOVED AND REPLACED OMEGA BEAM, IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM HAS CORROSION UNDER CROSS BEAM AT FRAME 25. REMOVED AND REPLACED LEFT OMEGA BEAM AT FRAME 25 IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION FOUND, LEFT OMEGA HAS CORROSION UNDER CROSSBEAM AT FRAME 29. REMOVED AND REPLACED LEFT OMEGA BEAM AT FRAME 29 IAW EMB135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND CENTER OMEGA BEAM HAS CORROSION UNDER CROSS BEAM AT FRAME 25. REMOVED AND REPLACED OMEGA BEAM IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RAMP — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND SUPPORT RAMP IN CENTER HAT SECTION IS CORRODED AT FRAME 20. INSTALLED NEW RAMP IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BUSHING — WORN (HORIZ STAB)

SAW - BUSHING AT HORIZONTAL STABILIZER HINGE POINTS HAVE PLAY. COMPLIED WITH EMB 135 SRM 55-10-02 FOR HORIZONTAL STABILIZER BUSHING RAI. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND Z-ANGLE AT FRAME 22A CORRODED. RAI'D ANGLE AT FRAME 22A IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 HAS CORRODED REPAIR DOUBLER. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW EMB SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND DIGITAL FORWARD OF FRAME 15 IS CORRODED. RAI'D DIGITAL FORWARD OF FRAME 15 IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR FORWARD HAS AREAS OF CORROSION. RAI'D SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: A/C PACK — ODOR (NR 1)

CREW REPORTED A HEAVY OIL SMELL COMING FROM THE NR 1 AIR CONDITIONING PACK. NR 1 PACK WAS PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERTATIONAL CHECK OF BOTH PACKS WAS COMPLIED WITH , NO SMELL NOTED. AIRCARFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

RDU - FLT 4572 - CREW REPORTED THE FORWARD OVERHEAD EMREGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR ON LIGHT. MAINTENANCE RECONNECTED THE CANNON PLUG. AN OPERATIONAL CHECK WAS COMLIED WITH AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — LACK OF LUBE (COCKPIT)

RDU - FLT 4852 - PILOT REPORTED AN UNCOMMANDED SEAT MOVEMENT. MAINTENANCE CLEANED AND LUBRICATED THE SEAT TRACK AND RAILS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CARGO)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-40-02, 51-20-03, EMB 145 CPM 51-21-04 THROUGH 51-21-06 AND AEAI ETN NR EB53-021R1. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS AROUND THE NUTPLATES. CUT OUT CORRODED AREAS THAT WREE BELOW .040 INCH, OTHER CORRODED AREAS WERE BLENDED. FABRICATED A FORWARD UPPER NUTPLTAE DOUBLER AND LOWER NUT PLATE AND DOUBLER FOR MID AND AFT NUTPLATE. REPAIR DONE IAW EMB IC2003-145/0496 DATED FEB 7, 2003 AND EMB SRM (SRM EMB-145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-04, 51-40-06 AND 53-21-02. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION. PASSENGER DOOR ENTRY FLOOR SUPPORTS HAVE CORROSION. REMOVED SUPPORTS AND INSTALLED SERVICEABLE SUPPORTS IAW EMB 135 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL HAS CORROSION ON PREVIOUS REPAIR. REMOVED CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE DOOR SILL IAW EMB 135 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, CENTER BEAM GUSSET IN GALLEY AREA HAS CORROSION. REMOVED CORRODED CENTER BEAM GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02. (M)

Part: PLATE — CORRODED (CARGO DOOR)

ABI - THIS IS A LEVEL, TWO FINDING FOUND DURNG AN IMBV INSPECTION, LOWER CARGO DOOR CUTOUT SILL PLATE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW LOWER SILL PLATE IAW EMB 135 SRM 51-40-02, 51-20-03, ETN EB-53-021R1. (M)

Part: FLOORBOARD — CORRODED (GALLEY)

ABI - A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION GALLEY FLOORBOARD EXTENSION CORRODED. REMOVED AND INSTALLED SERVICEABLE EXTENSION IAW EMB 134 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE REPORTED THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. AFTER REMOVAL OF CORROSION IT WAS FOUND TO BE OUT OF LIMITS. OMEGA BEAM WAS REPAIRED IAW EMB SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FIRE BOTTLE — FAILED (CARGO BAY)

ORF - FLT 4968 - EICAS MESSAGE INOPERATIVE. REMOVED AND REPLACED CARGO FIRE BOTTLE IAW AMM. OPS CHECK GOOD. (M)

Part: SEAL — TORN (NR 1 ENGINE)

RIC - FLT 4537 - ON DESCENT, CREW NOTED E1 WARNING FOR LOW OIL PRESSURE. COMPLETED CHECKLIST AND SHUT ENGINE DOWN AND CONTINUED LANDING WITH NO OTHER PROBLEMS. REMOVED AND REPLACED NR 1 ENGINE MAGNECTIC STARTER CARBON SEAL IAW AMM. OPS CHECK GOOD. (M)

Part: ACTUATOR — WEAK (RT NLG DOOR)

ORD - FLT 4035 - FOUND NOSE GEAR DOOR DOES NOT CLOSE. REMOVED AND REPLACED NLG DOOR ACTUATOR. OPS CHECK GOOD. (M)