N715AE

Part: O-RING — WORN (FUEL CAP) · airframe 2,157 hrs

STRONG FUEL SMELL NOTED DURING FLIGHT. UPON MAINTENANCE INSPECTION, FOUND FUEL FILLER CAP O-RING WORN, WHICH ALLOWED THE CAP TO LEAK FUEL.

Part: CONTROLLER — ODOR (WINDSHIELD HEAT) · airframe 18,250 hrs · 16,187 cycles

ON FLIGHT 4684, CREW REPORTED A ACRID SMELL IN COCKPIT ON APPROACH TURNED OFF WINDSHIELD HEAT 1 AND 2 SMELL DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FO'S WINDSHIELD TEMP CONTROLLER IAW EMB 135 AMM 30-42-01. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 17,947 hrs · 15,936 cycles

ON FLIGHT 4557, CREW REPORTED THAT AFTER TAKEOFF LANDING GEAR AIR/GND FAIL CAUTION MESSAGE ILLUMINATED. RETURNED FOR NORMAL LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LGEU IAW EMB 135 32-32-01. PERFORMED OPERATIONAL CHECK NO DEFECTS OR MESSAGES NOTED. PERFORMED FCF, NO DEFECTS OR MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (MLG) · airframe 17,079 hrs · 15,227 cycles

AIRCRAFT DIVERTED TO JFK, ON TAKEOFF FROM DCA HEADING TO BOS RECEIVED LANDING GEAR AIR/GROUND FAIL MSG AND GEAR HANDLE WOULD NOT GO TO THE UP POSITION. FLEW WITH GEAR DOWN INTO JFK FOR REPAIR. DID DECLARE EMERGENCY. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK PROX SWITCH, BOTH LT MLG PROX SWITCH, AND LANDING GEAR MODULE. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL SYSTEM — FAILED (NWW)

ON LANDING, THE AIRCRAFT SWERVED RIGHT UNCONTROLLABLY, NOSE WHEEL STEERING DISCONNECTED. AIRCRAFT DEPARTED THE SIDE OF THE RUNWAY AND THEN RETURNED BACK ON TO THE RUNWAY. REPLACED FEED BACK POTENTIOMETER, P0054 PLUG, STEERING MANIFOLD AND ALL 6 TIRES. PERFORMED GEAR SWINGS FOR CENTERING CHECK. PASSED HIGH-SPEED TAXI CHECK. NLG TIRES P/N OFF RT 31551, S/N 2847, LT 31551, S/N 0940, CONNECTOR P0054 P/N 03899/26FA35PN, POTENTIOMETER P/N 1170A3500-01, S/N 01012, MANIFOLD P/N 308570-1003 S/N 0296. (M)

Part: FLOOR SUPPORT — CORRODED (FR 14)

SAW - FOUND DURING CPCP INSPECTION, DIGITAL CORRODED AT FRAME 14 COCKPIT ENTRY. REMOVED CORROSION AND FOUND DIGITAL TO BE CRACKED. REPLACED DIGITAL IAW SRM 51-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ROD — DAMAGED (RUDDER)

FOUND DURING MBV, FORWARD END OF LOWER NR 2 RUDDER ROD HAS PLAY WHERE FORWARD FITTING SCREWS INTO ROD. REPLACED LOWER NR 2 RUDDER ROD IAW EMB AMM 27-21-08. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (RUDDER)

FOUND DURING MBV, RUDDER NR 2 SKIN CRACKED ON RIGHT LOWER TRAILING EDGE. REPAIRED DAMAGED SKIN ON RUDDER NR 2 IAW IC2005-145/4198A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FR 20)

SAW - FOUND DURING CPCP INSPECTION, INBOARD RAMP AT FRAME 20 CORRODED. REPLACED INBOARD RAMP AT FRAME 20 IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 22)

FOUND DURING CPCP INSPECTION, GALLEY FLOOR SUPPORT CORRODED AT FRAME 22. INSTALLED NEW GALLEY FLOOR SUPPORT AT FRAME 22 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10 FIG 202. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142, REV 22, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. APPLIED TREATMENT TO THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW EMB REPAIR STATEMENT IC 2003-145/2467A DATED JULY 22, 2003. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, CORROSION FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CREATIN A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND A PLATE. REPAIR DONE IAW EMB 145 SRM, 145-1142 REV 22, 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - DURING AN IMBV INSPECTOIN, SEVEN GOUGES WERE FOUND JUST AFT OF FRAME 24 AND BELOW STRINGER 18L. COMPLETELY REMOVED DAMATE BY PERFORMING A CUTOUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMBL 145 SRM, SRM 145/1142 REV 22, 53-22-01, CPM 51-21-05 AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS LEVEL TWO ITEM FOUND DURING AN IMBV INSPECTION, THE CENTER BEAM WEB EXTENSION CORRODED AT FRAMES 22-23. REMOVED CORRODED CENTER BEAM WEB EXTENSION AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-20-03, 51-40-06, 51-40-02. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. FABRICATED A DOUBLER, FILLER, PLATE, AND TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1172 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: SWITCH — OUT OF ADJ (THRUST REVERSER) · airframe 957 hrs · 794 cycles

CLE - FLT 4384 - DURING TAKEOFF CREW NOTED E2 THRUST/REVERSER DISAGREE MESSAGE. RETURNED TO CLE WITH NO FURTHER INCIDENTS REPORTED. PUT ON MEL AT THIS TIME. MAINTENANCE PERFORMED STOW/TRANSIT MICROSWITCH ADJUSTMENT IAW EMB MM 78-34-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)