N718AE

Part: CHARGER — FAILED (EMERGENCY LIGHT)

FLOOR STRIP EMERGENCY EXIT LIGHT ROW 7-8 VERY DIM. RAI NR 3 BATTERY POWER SUPPLY, IAW EMB 135, AMM 33-50-04 AND RAI NR 3 EMERGENCY LIGHT CHARGER, IAW EMB 135, AMM 33-50-04. OPS CHECK GOOD, RETURNED TO SERVICE. (M)

Part: CHANNEL — CORRODED (GALLEY)

THE RIGHT HAT BEAM IN THE GALLEY WAS FOUND TO BE CORRODED. REMOVED THE CORRODED HAT BEAM. INSTALLED NEW SERVICEABLE HAT BEAM IAW EMB SRM, SRM 145/1142 REV 30 CHAPTERS 51-20-03, 51-40-02 AND EMB CPM, CPM-145/1132 REV 12, CHAPTERS 51-21-04. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FS 24-25)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-00-10 FIG 201 SHEET AND 51-40-02. (M)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-20-01, 41, 51-40-06 AND 51-40-09. (M)

Part: SMOKE — DETECTED (CABIN)

BOS - FLT 4596 - DURING TAXI CREW REPORTED SMOKE IN COCKPIT BUT NOT IN CABIN. AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLCIATE DISCREPANCY. A GOUND ENGINE RUN WITH BOTH ENGINES AND BOTH PACKS OPERATING WAS SATISFACTORY WITH NO SMOKE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY FLOOR LIGHT EXIT LOCATOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR NOT CORRECTLY CONNECTED. THE CANNON PLUG WAS RESECURED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 10,448 hrs · 9,671 cycles

CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AFT OF ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: CONTROLLER — MALFUNCTIONED (CABIN)

CAPTAIN REPORTED STRONG ODOR OF BURNED PLASTIC FROM FLIGHT ATTENDANT GASPER AND FROM CABIN LIGHTS CONTROL MODULE. ALSO, LIGHTS FLICKERING THROUGHOUT THE CABIN. REPLACED CABIN LIGHT CONTROLLER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INVERTER — INOPERATIVE (NR 2)

LGA - FOUND MAINTENANCE REPORTED THE SERVICE DOOR AREA LIGHT AND EMERGENCY LIGHTS GO DIM WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (UFSELAGE)

ABI - DURING AN IMBV INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT FUSELAGE SKIN BETWEEN FRAMES 48 AND 49 AT THE OVERWING PANEL AFT UPPER ATTACH POIT. PERFORMED CUT OUT OF THE DAMAGE AREA. FABRICATED A FILLER, REPAIR DOUBELR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-23-12, 51-40-04 AND 51-40-06. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED CUT OUT OF THE DAMAGED AREA. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 53-21-10 PARA 5 FIG 204 SHEET 2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON FORWARD DIGITAL STATION 163 AND BL 0.0 THAT WAS BEYOND SRM LIMITS. FABRICATED REPAIR DOUBLER, WORK DONE IAW EMB GST-0508/02, EMB145 SRM 145/1142, REV 17, STANDARD PRACTICES AND CPM 51-21-04, 51-21-05. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20 WHICH EXCEEDED SRM LIMITS. FABRICATED DOUBLER ANGLE, A FILLER, AND PLATE. WORK DONE IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 17 53-21-10 PARA 2 AND STANDARD SRM PRACTICES. (M)

Part: BATTERY — DISCONNECTED (CABIN)

CLE - FLT 4462 - FIRST HALF OF FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. MAINTENANCE INSPECTED EMERGENCY LIGHTING SYSTEM AND FOUND BATTERY NR 2 IN GALLEY NOT CONNECTED, BATTERY WAS RECONNECTED. OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00 AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — FAILED (STABILIZER)

ORD - FLT 4433 - CREW REPORTED AFTER TAKEOFF PRIMARY TRIM CONTROL TO BE INOPERATIVE, FOLLOWED LATER BY AUTO TRIM FAIL. BACKUP TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED PITCH TRIM ACTUATOR IAW AMM. OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (E/E BAY DOOR)

CMH - FLT 4985 - THE FLIGHT CREW REPORTED THE AVIONICS BAY DOOR OPEN LIGHT ILLUMINATED IN CLIMB ON CONFIGURATION. PUT ON MEL AT THIS TIME. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - FLT 3477 - CABIN FLOOR EMERGENCY LIGHTS ILLUMINATED WHEN NO COMMANDED. MAINTENANCE REMOVED AND REPLACED BATTERY PACK BY SERVICE DOOR. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (POWER SUPPLY)

DFW - FLT 3476 - HALF OF EMERGENCY LIGHTS ILLUMINATED ON LANDING. RESET AIRCRAFT POWER THEN PROPERLY SEATED CONNECTOR AT NR 2 EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD. (M)