N719AE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,283 hrs · 24,537 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT BULB PER EMB MM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — SHORTED (SPOILER) · airframe 28,183 hrs · 24,464 cycles

ON FLIGHT 4567 THE CREW REPORTED THAT ON CLIMBOUT AT 25,000 FEET THEY RECEIVED A SPOLIER FAIL MESSAGE ON EICAS. THEY NOTICED CIRCUIT BREAKER F22 POPPED AND THE SPOILER WAS VISUALLY VERIFIED CLOSED. THE CREW COMPLETED THE EPC AND CONTACTED MOC AND DISPATCH. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LEFT INNER SPOILER PROXIMITY SENSOR SHORTED OUT. REMOVED AND REPLACED THE PROXIMITY SENSOR IAW EMB 135 AMM 27-63-04. THE OPERATIOAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,576 hrs · 23,998 cycles

ON FLIGHT 4419 THE CREW REPORTED THE EMERGENCY EXIT LIGHT/SIGN OVER F/A JUMPSEAT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD DOOR CLOSET EMERGENCY BATTERY AND BATTERY CHARGER AS PER EMB-135 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FILTER — INOPERATIVE (FUEL SYSTEM) · airframe 26,597 hrs · 23,256 cycles

ON FLIGHT 4521, THE CREW REPORTED AN ENGINE 1-2 FUEL IMPENDING BYPASS ON CLIMBOUT. THE CREW DECLARED AN EMERGENCY AND RETURNED. THE AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AND NR 2 ENGINE FUEL FILTER IAW MM 73-21-10. OPS AND LEAK TESTED GOOD IAW MM 72-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — LOOSE (CABIN) · airframe 26,263 hrs · 23,009 cycles

ON FLIGHT 4565 THE FLIGHT ATTENDANT‘S FLASHLIGHT ABOVE SEAT CHARGES INTERMITTENTLY. THE FLASHLIGHT HOLDER IS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD ENTRANCE FLASHLIGHT & HOLSTER ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 24,618 hrs · 21,685 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE FRAME 55 CHAFED AT STRINGER 8 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGED AERA, FABRICATED, PREPPED AND INSTALLED REPAIR ANGLES IAW EO EM-53MR-1811. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LENS — CRACKED (CABIN) · airframe 24,618 hrs · 21,685 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EXIT EMERGENCY LIGHT LENS TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 23,991 hrs · 21,141 cycles

ON FLIGHT 4423 THE CREW REPORTED THAT ON CLIMBOUT OF JFK AT 240 KNOTS HEARD A DEEP THUMPING NOISE IN THE NOSE WHEEL WELL AREA. THE CREW SLOWED TO 210 KNOTS AND THE NOISE WENT AWAY UNTIL LEVELED OFF AT 28 KNOTS. THE NOISE RETURNED EVEN AT 200 KNOTS. THE HYDRAULIC PRESSURE WAS NORMAL IN BOTH SYSTEMS. THE THUMPING NOISE WENT AWAY ONCE THE GEAR WAS PUT DOWN. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INBOARD BRAKE SHUTOFF VALVE FAILED ON THE CENTRAL MAINTENANCE COMPUTER. REPLACED THE I/B BRAKE SHUTOFF VALVE IAW EMB AMM 32-41-05. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 32-41-00; ALSO BLEED NR 1 AND NR 2 HYDRAULIC SYSTEM IAW EMB AMM 32-40-00. THE LANDING GEAR OPERATIONAL CHECK WAS GOOD IAW EMB AMM 32-30-00. NO FURTHER NOISE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 122,098 hrs · 19,499 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT THE EXIT MARKER SERVICE DOOR AND GALLEY CEILING PANEL SERVICE DOOR LIGHT WOULD NOT COME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR P8530 TO BE LOOSE, INSTALLED CONNECTOR IAW SWRM 20-50-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,023 hrs · 19,440 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT TO BE DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,268 hrs · 18,784 cycles

DURING PREFLIGHT INSPECTION FOR FLIGHT 4445 THE FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN. AIRCRAFT REMOVED FROM SERVICE. PACKS, BALLASTS AND RECIRCULATION FANS WERE ALL CHECKED AND NO SMELL WAS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS)

ON FLIGHT 4771 CREW REPORTED STRONG CHEMICAL FUMES COMING FROM GASPER ABOVE FLIGHT ATTENDANT`S TEMP CONTROL PANEL. ACFT REMOVED FROM SERVICE. INSPECTED AND FOUND 1ST BALLAST OF CEILING LIGHT INOPERATIVE WHICH CREATED CHEMICAL ODOR. REMOVED AND REPLACED BALLAST AND PERFORMED OPERATIONAL CHECK IAW EMB AMM 135 33-21-05. OPERATIONAL CHECKED GOOD. ACFT RETURNED TO SERVICE. (S)

Part: RELAY — FAILED (SPOILER SYS)

ON FLIGHT 4870 - CREW REPORTED AFTER TAKEOFF THAT THEY GOT A SPOILER FAIL EICAS MSG. THE CREW DECLARED AN EMERGENCY AND RETURN TO THE FIELD. MESSAGE EXTINGUISHED AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT IAW EMB FIM 27-63-00-820-807. REMOVED AND REPLACED RELAYS K0479, K0482, K1202, K0030, K0031 QLWO. OPERATION CHECK GOOD IAW EMB MM 27-03-00. REFORMED CHECK FLIGHT CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: UNKNOWN — ODOR (CABIN) · airframe 16,005 hrs · 14,338 cycles

OIL ODOR ON FLIGHT DECK AT A=CRUISE ALTITUDE. PERFORMED EMB FIM TASK 21-20-00-810-801, STEP 51 AND RR FIM TASK 72-00-00-810-814 WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

RIGHT SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

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

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

SERVICE DOOR SILL CORRODED BETWEEN FRAMES 19 AND 22. REPAIRED DOOR SILL IAW EMB IC 2007-145/03094. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

RIGHT SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

FLOOR PANEL RISER AT FRAME 22 CORRODED. REMOVED AND REPLACED RISER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

FOWARD DIGITAL CORRODED BETWEEN FRAMES 15 AND 18. REPAIRED DIGITAL IAW EMB IC 2007-15/03083. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 TO 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE

Part: ATTACH BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

PASSENGER DOOR THRESHOLD BRACKETS CORRODED BETWEEN FRAME 17 AND 18. REMOVED AND REPLACED BRACKETS IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

LEFT SEAT TRACK CORRODED BETWEEN FRAMES 18 AND 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,875 hrs · 14,224 cycles

LEFT SEAT TRACK CORRODED BETWEEN FRAMES 23 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE)

A PREVIOUS REPAIR OF STRINGER 19R WAS FOUND TO BE CHAFED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-24-02 AND EMB IC2005-145/4506 DATED AUGUST 19, 2005. (M)

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE)

CREW REPORTED A LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10,000 FT DURING DESCENT. MAINTENANCE REMOVED AND REPLACED THE E1 HIGH STAGE AND PRESSURE OUTFLOW VALVE IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT DID A FUNCIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (K)

Part: CONTROL SYSTEM — MALFUNCTIONED (CABIN PRESSURE)

BNA - LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10,000 DURING DESCENT. OXYGEN MASKS DEPLOYED. (M)

Part: VALVE — FAILED (CABIN PRESSURE)

CREW REPORTED A LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10000 FT DURING DESCENT. MAINTENANCE REMOVED AND REPLACED THE E1 HIGH STAGE AND PRESS OUTFLOW VALVE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT DID A FUNCTIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (SW21200505705) (K)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFE BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ONE REPAIR ANGLE, TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2633, IC2003-145/2718A AND STANDARD EMB SRM PRACTICES. (M)

Part: FRAME — DENTED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE LOWER RIGHT SECTION OF FRAME 72 WAS FOUND TO BE CREASED AND DENTED. REMOVED THE DAMAGED LOWER SECTION OF FRAME 72. INSTALLED NEW FRAME IAW EMB SRM, SRM 145/1142 REV 22, 51-40-02 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (CARGO DOOR)

ABI - DURING AN 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 135 SRM, SRM 145/1142 REV 22, 51-40-02, 06, 51-20-03 EMB 145 CPM 51-21-04, 51-21-05. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED ARAE. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-22-10, 51-40-02, 51-40-04 AND 51-40-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER, FORWARD SHIMS, AFT SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-20 PAGE 201 ITEM 2 FIG 201. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER HAT BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING HAT BEAM AND INSTALLED NEW HAT BEAM IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M)

Part: SILL — CORRODED (FUSELAGE)

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

Part: LIGHT — INOPERATIVE (CABIN)

BOS - FLT 9300 - CREW REPORTED AN EMERGENCY FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 LIGHT STRIP IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MBV - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT FLOOR SUPPORT IN CARGO BAY AT FRAME 71. MAINTENANCE REMOVED CORROSION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0331/02. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED CORROSION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0332/02. (M)

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

DURING MBV INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB SRM 51-40-02. (M)

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

CMH - FLT 4544 - DURING TAKEOFF ROLL, CREW NOTED E1 N1 LOW SPEED INDICATION. CREW RETURN TO GATE SAFELY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. INDICATION WENT AWAY WHEN AIRCRAFT RETURNED TO GATE. RESET FADECS. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ORF - FLT 4522 - AFT OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE RECONNECTED CANNON PLUG FOR LIGHT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)