N738NR

Part: FLAPPER VALVE — MALFUNCTIONED (LT WING) · airframe 25,213 hrs · 22,136 cycles

ON FLIGHT 2981 DEPARTURE CONTROL CONTACTED THE CREW AND REPORTED A POSSIBLE FUEL LEAK FROM THE LEFT WING. THEY OBSERVED A WHITE VAPOR/SMOKE COMING FROM LEFT WING. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING FLAP VALVE IAW EMB 135 AMM 28-11-04. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 24,753 hrs · 21,661 cycles

ON FLIGHT 3322 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT OVER THE JUMP SEAT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT IAW EMB 135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,333 hrs · 21,282 cycles

FLIGHT 4505, FLIGHT ATTENDANT CAME ONBOARD AND FOUND THE EMERGENCY LIGHTS ON. THE BACK HALF OF THE FLOOR STRIP AND OVERWING EXITS DID NOT LIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH NR 3 AND 4 EMERGENCY BATTERY POWER SUPPLY. OPS CHECKED GOOD AS PER AMM 33-50-04. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PANEL — LOOSE (LT WING) · airframe 24,201 hrs · 21,182 cycles

ON FLIGHT 4500 THE CREW REPORTED THAT DURING ROTATION A PASSENGER ON THE LEFT SIDE OF AIRCRAFT NOTICED FLUID COMING OFF THE TRAILING EDGE OF THE LEFT WING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. POST FLIGHT INSPECTION REVEALED A STRONG ODOR OF JET FUEL AND FRESH FUEL STREAKS UNDERNEATH LEFT WING. RE-TORQUED LEFT WING NACA AIR INLET PANEL IAW AMM 28-11-01. PERFORMED LEAK CHECK IAW AMM 28-11-00. NO LEAKS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,095 hrs · 21,108 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTING BATTERY AND POWER CHARGER NR 4 INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY AND CHARGER AS PER MAINTENANCE WORK CARD NR 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 23,587 hrs · 20,724 cycles

ON FLIGHT 4468 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN/ CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED MAIN CABIN DOOR ROLLERS IAW EMB 135 AMM # 52-00-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 23,560 hrs · 20,701 cycles

DURING MAINTENANCE INSPECTION FOUND THE PROXIMITY LIGHT POSITIONS 3 AT ROW 6 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROXIMITY LIGHT POSITION 3 AT ROW 6 IAW EMB 135 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,510 hrs · 20,664 cycles

DURING B-INSPECTION FOUND THE NR 3 EMERGENCY STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY STRIP IAW EMB135 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 23,459 hrs · 20,626 cycles

ON FLIGHT 4553 THE CREW REPORTED THAT ONE MINUTE AFTER TAKEOFF THEY RECEIVED A BAGGAGE SMOKE WARNING MESSAGE. THE CREW BLEW BOTTLES AFTER WARNING ILLUMINATED. THE CREW DECLARED AN EMERGECNY AND RETURNED TO LGA WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BOTH FWD AND AFT SMOKE DETECTORS PER AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. PART NUMBERS: FWD SMOKE DET P/N 473597-13 S/N 1669 AFT SMOKE DET P/N 473597-13 S/N 3159. REMOVED AND REPLACED BOTH UPPER & LOWER FIRE BOTTLES IAW EMB-26-23-01. PART NUMBERS: FIREX BOTTLE-630 CU.IN.346000731 S/N 20784F1. FIREX BOTTLE-224 CU IN 337000271. S/N 34197D. CARTRIDGE M30903870. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 23,435 hrs · 20,607 cycles

ON FLIGHT 4413 CREW RECEIVED BAGGAGE SMOKE WARNING MESSAGE ON EICAS, PRESSED BAGGAGE EXT BUTTON AS PER MEMORY ITEM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FWD AND AFT CARGO SMOKE DETECTOR IAW EMB AMM 26-15-01. OPERATIONAL TEST CHECK GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 23,224 hrs · 20,454 cycles

ON FLIGHT 4522 THE CREW REPORTED THE FIRST OFFICER’S READING LIGHT BULB SHATTERED WITH A LOUD BANG AND PRODUCED A BURNING ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S READING LIGHT IAW EMB 135 AMM 33-11-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LENS — MISSING (CABIN) · airframe 23,104 hrs · 20,370 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT WING EMERGENCY LIGHT LENS MISSING. NUT PLATES, LENSE REMOVED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND PLACED THE EMERGENCY EXIT LIGHT RIGHT SIDE OVER THE WING IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,997 hrs · 20,295 cycles

EMERGENCY FLOOR LIGHTING SECOND STRIP BACK FROM FRONT HAS BROKEN WIRE. REMOVED AND REPLACED SECOND BACK FROM FRONT EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-50-01. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — DEFECTIVE (SPOILER) · airframe 22,997 hrs · 20,295 cycles

IN FLIGHT GOT A SPOILER FAIL ON EICAS WITH SPOILER OPN INDICATION DECLARED EMERGENCY UPON ARRIVAL TO XNA AND LANDED WITHOUT INCIDENT. REPLACED PROX SENSOR AND CONNECTOR P1166 ON LEFT OUTBOARD SPOILER IAW EMB-135 AMM 27-63-04 AND SWPM 20-50-01. OPS TEST OF SPOILER SYSTEM GOOD IAW AMM 27-63-01.

Part: FIRE BOTTLE — INOPERATIVE (CARGO BAY) · airframe 22,712 hrs · 20,075 cycles

DURING MAINTENANCE INSPECTION FOUND THE BAGGAGE FIRE BOTTLE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE BAGGAGE HIGH RATE FIRE BOTTLE IAW AMM 26-23-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,579 hrs · 19,965 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD OVERWING EMERGENCY AND MAIN DOOR ENTRANCE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 EMERGENCY BATTERY AND CHARGER ASSEMBLY IAW EMB 135 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 19,856 hrs · 17,585 cycles

DURING PS-1 MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT’S SEAT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT SIGN IAW EMB AMM 33-50-14. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (COCKPIT) · airframe 19,827 hrs · 17,558 cycles

ON FLIGHT 4580 THE CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITH 0 FLAPS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND FLAP ELECTRONIC CONTROL UNIT FAIL, RIGHT SENSOR FAIL ON CENTRAL MAINTENANCE COMPUTER. PERFORMED FIM TASK 27-51-00-810-803-A REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT PER AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 19,075 hrs · 16,903 cycles

ON FLIGHT 4413 A CREW MEMBER REPORTED THAT THE FORWARD CABIN EMERGENCY FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,347 hrs · 16,262 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 24. AIRCRAFT REMOVED FROM SERVICE. REPAIRED OMEGA BEAM AT FRAME 24 IAW EMB SRM 53-00-11 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,347 hrs · 16,262 cycles

DURING THE MAIN BASE INSPECTION, FRAME 65 OF THE CARGO DOOR SILL PLATE WAS FOUND TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL PLATE IAW EMB 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — BURNED (CABIN LIGHTS)

ON FLIGHT, CREW REPORTED PLASTIC BURNING ODOR THROUGH THE CABIN COMING FROM ABOVE 4A. AC REMOVED FROM SERVICE. FOUND LT SIDE WALL BALLAST BY ROW 2A, BURNED AND INOPERATIVE. REMOVED AND REPLACED BALLAST ABOVE ROW 2A IAW MM 33-71-03. OPERATIONAL CHECK GOOD, AC RETURNED TO SERVICE. (K)

Part: LINER — CRACKED (COMBUSTOR) · airframe 16,300 hrs · 14,515 cycles

ON FLIGHT 4599 IN CLIMB CREW EXPERIENCED A MOMENTARY HIGH ITT ON ENGINE NUMBER 1 GOING THRU 3000 FEET FOR 3600 FEET. CREW REDUCED THRUST AND ITT REMAINED IN NORMAL GREEN LIMITS. FADEC A WAS IN CONTROL OF ENGINE NUMBER ONE. FOUND NUMBER ONE ENGINE COMBUSTOR LINER HAS MISSING PIECES. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NUMBER 1 IAW WORK CARD NR 71-00-00. ALL LEAK CHECKS AND RUN UP CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,393 hrs · 12,090 cycles

SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,393 hrs · 12,090 cycles

GALLEY FORWARD GUSSET FOUND TO BE CORRODED. BLENDED THE AREA REMOVING CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EMB IC2007-145/01751, DATED 3-12-07. RETURNED AIRCRAFT TO SERVICE.

Part: BEARING CAP — CORRODED (ZONE 700) · corrosion level 2 · airframe 13,393 hrs · 12,090 cycles

RIGHT NOSE LANDING GEAR BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-02. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,393 hrs · 12,090 cycles

CENTER BEAM RAMP SUPPORT IN GALLEY AREA FOUND TO BE CORRODED. REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,393 hrs · 12,090 cycles

LEFT OMEGA BEAM RAMP SUPPORT IN GALLEY FOUND CORRODED. REMOVED AND REPLACED RAMP SUPPORT IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: INSULATION — LOOSE (E/E BAY)

RDU - FLT 4672 - IN DESCENT, A BURNING ELECTRICAL SMELL WAS EVIDENT IN THE COCKPIT. FLIGHT ATTENDANT SMELLED IT ONLY IN THE FORWARD CABIN. CHECKED NR 2 TEMP CONTROLLER FOR DEFECTS NONE NOTED. CHECKED NR 2 CONTACTOR AND FUSE FOR DEFECTS NONE NOTED. FOUND FORWARD AVIONICS INSULATION BEING SUCKED INTO AVIONICS FAN. RESECURED INSULATION. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CLT - FLT 4892 - CREW REPORTED THE EMERGENCY LIGHTING SYSTEM FLOOR PROXIMITY STRIPS BY ROW 3, 4, 5 AND 6 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY AND CHARGER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN DOUBLER AT FRAME 20 HAS CORROSION NEAR IB EDGE. MAINTENANCE REMOVED AND REPLACED NEW DOUBLER IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR FORWARD SILL HAS CORROSION IN SEVERAL AREAS OF THE UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD WEB (SILL) IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: BRACKET — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE MAIN CABIN DOOR SHAPE U HAS CORROSION AROUND NUTPLATES AT FRAME 16. INSTALLED NEW CABIN DOOR U-SHAPE BRACKET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOOR DIGITAL HAS CORROSION IN SEVERAL AREAS OF UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR DIGITAL IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOORBEAM HAT SECTION HAS CORROSION THROUGH TOP IB EDGE AT FR 20 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION, MAINTENANCE FOUND THE MAIN CABIN DOOR SILL AFT U-SHAPE HAS CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND NEW CABIN DOOR SILL AFT U-SHAPE BRACKET SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: GUSSET — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING INSPECTION THE FORWARD CABIN FLOOR GUSSET FRAME 20 TO FRAME 23 HAS CORROSION IN SEVERAL AREAS. INSTALLED NEW FLOOR GUSSET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR CHANNEL HAS CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL CHANNEL IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501913) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOOR SUPPORT AT FRAME 20 HAS CORROSION THROUGH AFT END AT LAP JOINT WITH GUSSET. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN PROFILE (Z) AT FRAME 22 HAS CORROSION IN SEVERAL FORWARD SURFACE AREAS. MAINTENANCE REMOVED AND REPLACED NEW PROFILE (Z) IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 8,493 hrs · 7,948 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE OMEGA BEAM AT FRAME 20 LT SIDE CORRODED. MAINTENANCE REPLACED CORRODED DOUBLER IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K)

Part: PRESSURE SWITCH — FAILED (NR 2) · airframe 8,362 hrs · 7,838 cycles

DURING CLIMB, THE YAW DAMP FAILED FOLLOWED BY RUDDER SYS-1 INOPERATIVE. FOLLOWED BY THE RUDDER SYS-2 INOPERATIVE. AIRCRAFT WAS CONTROLLABLE AND RETURNED AS A PRECAUTION . MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501805) (K)

Part: CONTROL UNIT — INOPERATIVE (SPOILERS)

NAS - FLT 4739 - DURING TAKEOFF ROLL THRUST LEVERS AT THRUST SETTING, SPOILER DEPLOYED UNCOMMANDED. CREW REPORTED A TAKEOFF MISCONFIG MESSAGE AND WHLE TAXIING BACK TO GATE RECEIVED DAU 1 MISCOMPARE. MAINTNENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

BGR - FLT 4655 - EMERGENCY EXIT LIGHT ON AFT GALLEY BULKHEAD INOPERATIVE. RESECURED LOOSE CONECTOR OVER GALLEY CEILING LIGHT. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DIRTY (COCKPIT)

BGR - FLT 4622 - DURING TAKEOFF, THE FIRST OFFICERS SEAT SLIPPED LOOSE TO THE FULL AFT POSITION. MAINTENANCE FOUND THE OUTBOARD SEAT TRACK TO BE DIRTY. SEAT TRACKS WERE INSPECTED, SEAT TRACK PIS WERE REMOVED, CLEANED AND REINSTALLED IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MODULE — INOPERATIVE (FIRE DETECTION)

DURING FLIGHT CREW RECEIVED AN E2 FIRE WARNING. ENGINE WAS SHUTDOWN AND LIGHT EXTINGUISHED. AIRCRAFT WAS DIVERTED TO ALB. AFTER LANDING CREW RECEIVED ANOTHER FIRE WARNING. FIRE BOTTLE WAS FIRED AND AN EMERGENCY EVACUATIO AS DONE ON THE TAXIWAY. MAINTEANCE INSPECTED ENGINE FOR BLEED LEAKS AND INSPECTED FIRE LOOPS WITH NO DEFECTS FOUND, THE RIGHT ENGINE FIRE CONTROL BOX WAS REMOVED AND REPLACED IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. THE FIRE BOTTLE WAS ALSO REPLACED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 19) 53-21-10 PARA 2 FIG 201 SHEET 2 AND STANDARD SRM PRACTICES. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORF - FLT 4524 - CREW REPORTED THE OVERWING INTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. AIRCRAFT WAS INSPECTED AND FERRIED TO BOS FOR CORRECTIVE ACTION. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

CHA - FLT 4418 - CREW REPORTED TWO SECTIONS OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY BATTERY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DUCT — FAILED (BLEED AIR)

LGA - FLT 4510 - DURING CLIMB-OUT, CREW NOTED ENGINE BLEED 1 LEAK IND. DURING THIS A LOUD NOISE WAS HEARD FROM AFT AREA. CREW RETURNED TO LGA SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED DUCT IAW AMM. OPS CHECK GOOD. (M)