N702AE

Part: BUSHING — WORN (YOKE) · airframe 16,316 hrs · 14,934 cycles

CAPTAIN YOKE HAS APPROXIMATELY QUARTER INCH OF DEAD SPACE WHEN MOVING ELEVATOR. REMOVED AND REPLACED BUSHING ON ELEVATOR BELL CRANK IAW EMB AMM. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,957 hrs · 14,612 cycles

FOUND OMEGA BEAM CORRODED AT FRAME 32. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,957 hrs · 14,612 cycles

FOUND LEFT OMEGA BEAM CORRODED AT FRAME 44. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,957 hrs · 14,612 cycles

FOUND OMEGA BEAM CORRODED AT FRAME 38. PERFORMED CUTOUT OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 15,360 hrs · 14,340 cycles

BURNED RUBBER SMELL IN COCKPIT. INSPECTED LEFT AND RIGHT COCKPIT PANELS, OPERATED APU AND AIR CONDITIONING PACKS WITH NO ODORS NOTED. ODOR DUPLICATED WHEN RECONNECTED GROUND HEATER. RETURNED AIRCRAFT TO SERVICE.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 15,594 hrs · 14,308 cycles

ABORTED TAKEOFF FOR TEMPORARY LOSS OF NOSEWHEEL STEERING, AIRCRAFT VEERED LEFT WITH FULL RIGHT RUDDER APPLIED. LOUD NOISE FROM NOSE AREA ENCOUNTERED DURING EVENT. REMOVED AND REPLACED STEERING MANIFOLD IAW EMB AMM 32-50-04. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (ELECT ALERT SYS)

DURING TAXI TO ROLL AFTER APU SHUTDOWN GOT AN ELECTRIC EMERGENCY ABNORMAL/ EMERGENCY LIGHTS NOT ARMED. CREW DID AN ABORTED TAKEOFF, HOWEVER, IT DOES NOT REFLECT IT IN THE LOG BOOK WRITE-UP. PERFORMED ALL CHECKS IAW THE FIM AND COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24-25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K)

Part: PITOT SYSTEM — CONTAMINATED (BOTH)

DUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT SYSTEMS. DRAINED PITOT STATIC SYSTEM. ENGINE OPERATIONAL CHECKS GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CORRODED (COCKPIT)

DURING AN IMBV INSPECTION, THE RIGHT WINDSHIELD LOWER BEAM OUTBOARD 8 SCREW HOLES WERE FOUND TO BE CORRODED. HOLES WERE REAMED TO REMOVED CORROSION. FIVE HOLES REQUIRED FURTHER REAMING AND REQUIRED BUSHINGS TO BE FABRICATED AND INSTALLED. ALL WORK WAS DONE IAW REPAIR STATEMENT IC2003-145/0899, GST-1578/02-B AND ETN EB-53-035. (M)

Part: WINDOW FRAME — CORRODED (COCKPIT)

ABI - DURING AN IMBV INSPECTION, THE LEFT WINDSHIELD LOWER OUTBOARD 14 SCREW HOLES WERE FOUND TO BE CORRODED. THE SCREW HOLES WERE REAMED TO REMOVE CORROSION. THREE HOLES REQUIRED REAMING A SECOND TIME. THREE BUSHINGS WERE FABRICATED AND INSTALLED. REPAIRED IAW EMB STATEMENT IC2003-145/0899, GST-1578/02-B AND ETN EB-53-035. (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 SERVIVCE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03, AND 51-40-06. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DUIRNG AN IMBV INSPECTION, FORWARD PASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW EMB135 SRM 51-40-02 ND ETN EB 53-032R1. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, CORROSION ON THE CENTER OMEGA BEAM AT FRAME 20. REMOVED CORRODED AREA BY CUTOUT. FABRICATED AN EXTERNAL U-SHAPE DOUBLER. REPAIRE DONE IAW EMB 145 SRM (145/1142, REV 20) 53-21-10 PARA 5, FIG 204 SHEET 2 AND STANDARD SRM PRACTICES. (M)

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

THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, RIGHT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-20-03, 51-40-02, 51-40-06. (M)

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

THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR FORWARD FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW EMB 135/145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR AFT FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED NEW SUPPORT IAW EMB135 SRM 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 AFT SILL PLATE CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DOOR SILL IAW EMB 135 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

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

Part: SUPPORT — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION FLOOR BOARD RAMPS SUPPORT CORRODED. REMOVED AND INSTALLED NEW RAMP SUPPORTS IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04. (M)

Part: CROSSBEAM — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION CROSSBEAM CORRODED AT FRAME 22. REMOVED AND INSTALLED NEW CROSSBEAM SUPPORT IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M)

Part: GUSSET — CORRODED (GALLEY)

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

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. BEAM WAS REPAIRED IAW EMB SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (THRUST REVERSER)

BOS - FLT 4980 - ON TAKEOFF ROLL, TR1 DISAGREE CAME ON THE EICAS, ABORTED TAKEOFF AND RETURNED TO GATE FOR MAINTENANCE. MEL''D TR1 SYSTEM. MAINTENANCE TIGHTENED CANNON PLUG ON T/R STOW SWITCH. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — STUCK (NR 2 ENGINE) · airframe 1,944 hrs · 1,860 cycles

RIC - FLT 4940 - DURING TAKEOFF, CREW NOTED E2 THRUST REVERSER DISAGREE MESSAGE ON EICAS. TAKEOFF ABORTED, AIRCRAFT RETURNED TO GATE. PUT ON MEL AT THIS TIME. MAINTENANCE FOUND RIGHT ENGINE THRUST REVERSER LOWER STOW SWITCH STUCK. REMOVED SWITCH, LUBED, AND REINSTALLED IAW EMB MM. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: DUCT — DEFECTIVE (NR 2 ENGINE)

FLT 4035 - ORD - CREW REPORTED UNUSUAL ODOR IN AIRCRAFT ACCOMPANIED BY EYE IRRITATION AND THROAT IRRITATION AFTER DEPARTURE. MAINTENANCE INSPECTED AIRCRAFT AND ALL FLUID SYSTEMS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR FCF. FCF WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. ON 3/13/2001 DISCREPANCY WAS WRITTEN UP AGAIN. AT THIS TIME MAINTENANCE REMOVED AND REPLACED ALL FUEL NOZZLES FOR THE NR 2 ENGINE AND THE PRECOOLER DUCT ASSEMBLY IN THE NR 2 PYLON. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)