N16961

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,786 hrs · 28,442 cycles

DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EXIT ROW EMERGENCY FLOOR LIGHTING TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED SECTION OF LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 37,353 hrs · 28,095 cycles

SMOKE IN COCKPIT DURING TAKEOFF, ABORTED TAKEOFF AT 80K. TROUBLESHOT IAW FIM 21-20-00-810-801-A. COULD NOT DUPLICATE. NO FURTHER MX ACTION REQUIRED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,403 hrs · 27,367 cycles

DURING MX INSPECTION THE NR 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND NOT TO BE RECEIVING ACFT VOLTAGE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGING TRAY WITH OPS CHECK PERFORMED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,281 hrs · 26,533 cycles

DURING A-CK INSP THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FRAME 77 BELOW STRINGER 03L. MX REMOVED THE DAMGE, AND PERFORMED AN INSERTION/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,424 hrs · 25,851 cycles

DURING MX INSPECTION, EMERGENCY LIGHT AT ROWS 3 AND 4 WAS FOUND INOPERATIVE. MX R & R THE LIGHT, OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,914 hrs · 25,456 cycles

DURING ROUTINE MX THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: BOLT — LOOSE (PAX DOOR) · airframe 33,536 hrs · 25,155 cycles

DURING PREFLIGHT THE CREW DISCOVERED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MX SECURED LOOSE HARDWARE BY RETORQUING THE INTERNAL HANDLE BOX BOLTS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — BURNED (COCKPIT) · airframe 33,267 hrs · 24,926 cycles

THE CREW REPORTED A BURNING ODOR IN FLIGHT AFTER THE F/O PRESSED THE F/O'S SIDE PA BUTTON WITH NO SMOKE NOTED. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE F/O AUDIO CONTROL PANEL, AND THE F/A AFT HANDSET AND PA AMPLIFIER AS A PRECAUTION. THE SYS OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 31,249 hrs · 23,382 cycles

DURING ROUTINE MX THE NR 2 EMERGENCY LIGHT BATTERY WAS FOUND DISCHARGED. MX REPLACED THE NR2 EMERGENCY LIGHT BATTERY.

Part: FADEC — MALFUNCTIONED (NR 1) · airframe 30,805 hrs · 23,013 cycles

AMA - FLIGHT 4565, DURING CRUISE FLIGHT THE CREW REPORTED THAT THE NUMBER ONE ENGINE N1 DECREASED FROM 82% TO 67% TWICE WHILE ON FADEC A. THE AIRCRAFT LANDED AT AMA WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 1A FADEC, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (FADEC) · airframe 30,826 hrs · 23,026 cycles

TYS FOR BNA. A/C HAD A UNCOMMANDED THRUST TO TAKE PLACE IN FLIGHT. A/C LANDED SAFELY AND MAINTENANCE FOUND A FADEC CONNECTION BETWEEN 1A AND 1B LOOSE AT J3 CONNECTION. RESECURED J3 HARNESS BETWEEN FADECS1A AND 1B. RESET THE FADECS, MESSAGE WAS CLEARED IAW EMB 145 AMM 73-22-01. OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF E1 AND E2 ON FADECS A AND B. NO DEFECTS NOTED. OPS CHECK GOOD, IAW EMB 145 AMM 71-00-01. (WO#2514403) A/C RELEASED TO SERVICE. NO PARTS NEEDED.

Part: CONNECTOR — LOOSE (E&E BAY) · airframe 30,797 hrs · 23,009 cycles

IN CRUISE FLIGHT, THE CREW REPORTED TWO TIMES UNCOMMANDED E1 THRUST REDUCTION. BNA MX FOUND FADEC CONNECT HARNESS BETWEEN 1A AND 1B LOOSE AT J3 CONNECTION. MX RESECURED J3 HARNESS BETWEEN FADECS 1A AND 1B. RESET FADECS, MSG CLEARED IAW EMB 145 MM 73-22-01. OPERATIONAL CHECK GOOD. PERFORMED OPERATIONAL CHECK OF E1 AND E2 ON FADECS A AND B. NO DEFECTS NOTED. OPERATIONAL CHECKS SUCCESSFUL IAW EMB 145 MM 71-00-01. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,714 hrs · 22,943 cycles

RIC - DURING ROUTINE MAINTENANACE, RIC MX FOUND RT EMERGENCY SIGN OFF. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 5 AND PERFORMED OPERATIONAL CHECK SUCCESSFULY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 30,264 hrs · 22,568 cycles

THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON CLIMB. CYCLED THE GEAR AND THE MESSAGE WENT AWAY. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT GEAR WOW SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 29,757 hrs · 22,191 cycles

IAH - FLIGHT 2042, THE CREW REPORTED THAT THE NUMBER ONE ENGINE DRIVEN HYD PUMP HAD FAILED, AND THAT THE SYSTEM 1 FLUID WAS LOW. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UNLOCK ACTUATOR HYDRAULIC LINE ON THE LEFT MAIN LANDING GEAR, REMOVED AND REPLACED THE NUMBER ONE HYDRAULIC PUMP AS A PRECAUTION, SERVICED HYDRAULICS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERHEATED (MAIN) · airframe 27,728 hrs · 20,632 cycles

IAH - FLIGHT 2856, THE CREW REPORTED A BATTERY ONE OVERTEMP IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,671 hrs · 20,587 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND ROW 17 EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BULB — BURNED OUT (CABIN LIGHT) · airframe 27,480 hrs · 20,452 cycles

SDF - FLIGHT 2431, THE CREW REPORTED A BURNING SMELL IN THE CABIN DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED OVERHEAD LIGHT AT ROW 4A, PLACED CABIN LIGHTING ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MX REPLACED THE LIGHT BULB ABOVE ROW 4A, OPERATIONALLY TESTED WITH NO DEFECTS OR SMELL. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — SHORTED (CABIN) · airframe 27,155 hrs · 20,222 cycles

CLE FLT 2635 THE CREW REPORTED A STRONG ELECTRICAL SMELL/ODOR NEAR 1A AND CABIN DOOR. MAINTENANCE INSPECTED AND REPLACED THE OVERHEAD LIGHT BALLAST. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL MODULE — MALFUNCTIONED (CABIN) · airframe 27,153 hrs · 20,221 cycles

MHT NR 2635 THE CREW REPORTED A STRONG SMELL ABOVE SEAT 1A. MAINTENANCE REPLACED THE CABIN LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 25,212 hrs · 18,732 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,202 hrs · 18,724 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED LT OMEGA BEAM IAW EC 5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — DAMAGED (SPOILER) · airframe 25,202 hrs · 18,724 cycles

SHV - DURING C-CHECK, LT GROUND SPOILER ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REPLACED ATTACHMENT BRACKET IAW EMB 145 AMM 57-51-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (LT AILERON) · airframe 25,202 hrs · 18,724 cycles

SHV - DURING C-CHECK LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REPLACED PCA ATTACHMENT BRACKET IAW EC 5740-01152. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,202 hrs · 18,724 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,202 hrs · 18,724 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 49. REPAIRED LT OMEGA BEAM IAW EC 5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 25,202 hrs · 18,724 cycles

DURING C-CHECK. MAIN DOOR LOWER SCREW HOLES HAVE CORROSION. REPAIRED MAIN DOOR LOWER SCREW HOLES IAW EC5210-01154. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 25,202 hrs · 18,724 cycles

SHV DURING C-CHECK, CORROSION ON SERVICE DOOR LOWER FRAME. REPAIRED SERVICE DOOR LOWER FRAME IAW EC 5210-01154. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR · airframe 25,022 hrs · 18,598 cycles

IAH - FLIGHT 2497 - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO BURNED ITEMS NOTED OR SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,967 hrs · 17,832 cycles

FLIGHT CREW REPORTED A FAINT SMOKE ODOR IN CABIN DURING TAKEOFF. MX RAN BOTH ENGINES AND AIR CONDITIONING PACK AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,583 hrs · 15,527 cycles

SHV - DURING C-CHECK MAINTENANCE, FOUND LT OMEGA BEAM LOWER FLANGE WITH PITTING CORROSION AT FRAME 23. MAINTENANCE REPAIRED LT OMEGA BEAM LWR FLANGE AT FRAME 23 IAW EMB 145 EC 5320-01370. NO FURTHER ACTION REQUIRED. A/C WAS APPROVED TO RETURN TO SERVICE.

Part: TUBE — CHAFED (HYD SYSTEM) · airframe 20,527 hrs · 15,487 cycles

FLT 2246 - EWR - CREW REPORTED HYD 1 LOW QTY AND E1 HYD PUMP FAIL ON EICAS. EWR MX FOUND PUMP RETURN TUBE ASSEMBLY CHAFED / LEAKING IN FUSELAGE AT FR 56. MX REPAIRED THE TUBE ASSY IAW EMB 145 AMM 20-10-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,342 hrs · 15,339 cycles

CLE FLIGHT 2473 THE CREW REPORTED THE ASILE PATH EMERGENCY LIGHTS BETWEEN THE EXIT ROWS WERE INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS AND OPERATIONAL CHECKS WERE GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

DURING C-CHECK, MAINTENANCE FOUND CORROSION ON LT AND CENTER OMEGA BEAM FLOOR BOARD MATTING SURFACE FRAMES 33 TO FRAMES 38. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 33 IAW EC 5320-01251 AND LT OMEGA BEAM AT FRAME 33 I/A/W EC 5320-01242. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

DURING C-CHECK, MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION FROM FRAME 23 TO JUST AFT OF FRAME 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 IAWEC 5320-01242. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FRAME — CRACKED (AFT FUSELAGE) · airframe 15,729 hrs · 11,751 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND APU FIREWALL ATTACHMENT FRAME CRACKED AT THE SIX O'CLOCK POSITION AT FRAME 81 (INTERNAL). MAINTENANCE REPAIRED THE APU FIREWALL IAW EC 5310-01342. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION FROM FRAME 23-JUST AFT OF FRAME 29. MAINTENANCE REPAIRED CENTER OMEGA BEAM FROM FRAME 23 TO FRAME 29 IAW SRM 53-22-10. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM REPAIR WITH CORROSION AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM 53-21-10 AND EC 5320-01137. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

DURING C-CHECK MAINTENANCE FOUND THE CENTER OMEGA BEAM HAS CORROSION FROM FRAME 29- JUST AFT OF FRAME 35. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT CROSSBEAM LOCATED AT FRAME 33 IAW EC 5320-01251, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,729 hrs · 11,751 cycles

DURING C-CHECK MAINTENANCE FOUND THE LT OMEGA BEAM HAS CORROSION IB SIDE AT FRAME 23. MAINTENANCE REPAIRED CORROSION ON LT OMEGA BEAM IB SIDE AT FRAME 23 IAW 145 SRM 53-22-10 AND EC 5320-01140. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 15,729 hrs · 11,751 cycles

CENTER OMEGA BEAM CORROSION AT FS 20. MAINTENANCE REMOVE AND REPLACED CENTER OMEGA BEAM AT FS 18-23 IAW EMB SRM 51-40-02. AIRCRAFT APPROVED TO RETURNED FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 14,784 hrs · 10,995 cycles

EWR - FLIGHT 3450, THE CREW REPORTED THAT THE FORWARD EMERGENCY EXIT LIGHT OVER THE FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (FUSELAGE) · airframe 14,246 hrs · 10,575 cycles

EWR - CREW REPORTED, FORWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY EXIT SIGN INVERTER. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAULTY (EMERGENCY LIGHT) · airframe 14,146 hrs · 10,495 cycles

EWR- CO3479, CREW REPORTED, (PASSENGER EMERGENCY EXIT SIGN CIRCUIT BREAKER POPS WHEN THE NO SMOKING SIGN IS TURNED ON). MAINTENANCE REMOVED AND REPLACED RELAY K8601. OPS CHECKED GOOD IAW EMB145 AMM 33-23-50. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (COCKCPIT)

DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT ARMING SWITCH AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. THE DISCREPANCY WAS THEN CLEARED.

Part: BATTERY — FAULTY (EMERGENCY LIGHT)

CREW REPORTED DURING PREFLIGHT INSPECTION, EMERGENCY EXIT LIGHT BY PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW EMB145 MM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRIP, OPERATIONALLY TESTED THE LIGHTING, AND CLEARED THE DISCREPANCY.

Part: CONNECTOR — DIRTY (CABIN)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANTS JUMPSEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE FORWARD INVERTER, CLEANED THE CONNECTOR, AND RE-INSTALLED THE SAME UNIT. THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECK GOOD AND THE DISCREPANCY WAS CLEARED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION SEVERAL SIGNS OF CORROSION WERE FOUND ON THE STRINGER CLIP BETWEEN FRAME 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE STRINGER CLIP AT FRAME 60 BETWEEN STRINGERS 20L AND 21L IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION THE LEFT HAND FLOORBEAM AT FRAME 18 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-60 AND CPM 51-21-04, 51-21-05 AND 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 51-10-02, 53-21-10 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WERE FOUND ON THE SERVICE DOOR CUTOUT SILL. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,833 hrs · 8,733 cycles

DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM CAP AT FRAME 61 WAS FOUND TO BE CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LIGHT — FAULTY

BTV---CO2943, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND RIGHTHAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE.....REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY LIGHT IAW EMB145 AMM #33-50-00. OPS.CHECKED GOOD.

Part: PUMP — INTERMITTENT · airframe 9,288 hrs · 6,679 cycles

EWR---CO3426, CREW REPORTED, "BURNING SMELL DETECTED FROM COFFEE POTS." MAINTENANCE REMOVED AND REPLACED RIGHTHAND PUMP ASSEMBLY IAW EMB145 MM 25-22-01. OPS.CHECKED GOOD. NO ODORS DETECTED AIRCRAFT RETURNED TO SERVICE.

Part: HEATER — DIRTY (GALLEY)

BWI---CO3404, CREW REPORTED, ELECTRICAL BURNING ODOR IN GALLEY AREA. MAINTENANCE INSPECTED GALLEY AND FIRST THREE ROWS OF THE CABIN AFT OF THE GALLEY AND FOUND BURNT COFFEE ON COFFEEMAKER HEAT PAD. CLEANED HEAT PAD, NO FURTHER MAINTENANCE REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE MAIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE.MAINTENANCE REPLACED THE MAIN DOOR EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: PUMP — FAILED (NR 2 ENGINE)

OMA- DURING FLIGHT 3969, THE CREW NOTED THAT THE NUMBER 2 HYDRAULIC OVERHEAT/ HAD ZERO HYDRAULIC PRESSURE ON NUMBER 2 SIDE. THE CREW DECLARED EMERGENCY AND LANDED AT OMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE DRIVEN HYDRAULIC PUMP, PERFORMED A OPERATIONAL AND LEAK CHECK OF THE HYDRAULIC PUMP. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FILTER — DIRTY (NR 2 ENGINE)

OMA- DURING FLIGHT 3969, THE CREW NOTED THAT THE NUMBER 2 HYDRAULIC OVERHEAT/ HAD ZERO HYDRAULIC PRESSURE ON NUMBER 2 SIDE. THE CREW DECLARED EMERGENCY AND LANDED AT OMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE, MAIN AND RETURN HYDRAULIC FILTERS, PERFORMED A LEAK CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN)

CLE, THE CREW REPORTED A BURNING SMELL COMING FROM PACK 2. MAINTENANCE INSPECTED AND OPERATIONAL CHECKS WERE PERFORMED ON THE AIR CONDITIONING SYSTEM. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LATCH — GOUGED (FUSELAGE) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE FUSELAGE CUTOUT FOR LEFT HAND EMERGENCY EXIT HATCH WAS FOUND TO BE GOUGED ON THE UPPER RELEASE LATCH. MAINTENANCE REMOVED AND REPLACED THE LATCH IAW EMB-145 MM 20-10-01, ALL OPERATIONAL AND PRESSURE CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: TAB — DAMAGED (ELEVATOR) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ELEVATOR SPRING TAB WAS FOUND TO BE DAMAGED ON THE TRAILING EDGE. MAINTENANCE ACCOMPLISHED A COMPOSITE REPAIR IAW EMB-145 SRM 51-70-01 AND EMB-145 CPM 51-21-05, 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE AFT PRESSURE BULKHEAD WAS FOUND TO BE DENTED BEYOND MANUFACTURES LIMITS. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMRAER GST-3336/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SHAFT — BROKEN (T/E FLAP) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE RIGHT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FIREWALL — GOUGED (APU) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND IN THE APU FIREWALL AFFECTING A PREVIOUS REPAIR. MAINTENANCE REMOVED ORIGINAL REPAIR AND ACCOMPLISHED THE INSERT/DOUBLER REPAIR IAW EMBRAER GST-3315A/01 AND SRM 53-32-13. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: HOUSING — GOUGED (RT MLG) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND LANDING GEAR SIDE BRACE, AFT UPPER HOLLOW PIN BEARING HOUSING WAS FOUND TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMBRAER GST-3363/01 AND SRM 51-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SHAFT — BROKEN (LT WING) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE LEFT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BUSHING — WORN · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the passenger door airframe fitting for the hold open hook has a displaced & loose lower pin bushing. Maintenance removed and replaced the bushing I.A.W.-EMB-GST-1682/01. Repair were satisfactory, Aircraft will be released to servive upon complection of inspection

Part: PANEL — CORRODED (FUSELAGE) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS NOTED ON PANELS 192JR AND PANEL 192HL. MAINTENANCE REMOVED AND REFINISHED 192JR AND 192HL IAW EMB 145 AMM 51-14-003 AND 51-20-00.THE WORK IS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED INSPECTION.

Part: PLATE — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection, several areas of corrosion was found on the forward and aft. floor beam digital plates.. Maintenance removed and replaced the aft floor digital plate, and removed and replaced corroded rivits in the forward digital plate I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the right outbd. flap, inbd. track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection, the right inbd. flap, outbd. track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: BEAM — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection corrosion was found under and around the forward carbon fiber omega beam. Maintenance removed and replaced the top cap, ramp angle, L-profile angle, cross fiber beam and installed shim, filler, plate and external angle. I.A.W.-EMB-135/145-SRM-51-40-02, 53-21-02 and CMP-52-21-04 & 05. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: PLATE — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection, several areas of corrosion was found on the forward and aft. floor beam digital plates.. Maintenance removed and replaced the aft floor digital plate, and removed and replaced corroded rivits in the forward digital plate I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: SPRING — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the left and right springs for the MLG uplock box was found corroded. Maintenance removed and replaced the left and right springs. I.A.W.-EMB-145-MM-32-33-10. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: SUPPORT — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the lavatory sink drain line support at stringer 19L was found corroded around rivits. Maintenance removed and replaced the support. I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection, the right inbd. flap, inbd. track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: FLAP TRACK — GROOVED (T/E FLAP) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION, THE RIGHT INBD FLAP, OUTBD TRACK WAS FOUND TO HAVE GROOVES WORN INTO TRACK. MAINTENANCE BLENDED GROOVED AREAS IAW EMB 145 GST 3350/01. REPAIRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SPRING — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the left and right springs for the MLG uplock box was found corroded. Maintenance removed and replaced the left and right springs. I.A.W.-EMB-145-MM-32-33-10. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left outbd. flap, inbd wing mounted flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: SUPPORT — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the lavatory sink drain line support at stringer 19L was found corroded around rivits. Maintenance removed and replaced the support. I.A.W.-EMB-145-SRM-51-40-02. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the right inbd. flap, inbd. wing mounted track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the right outbd. flap, outbd. wing mounted track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left inbd. flap, inbd wing mounted flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the right outbd. flap, inbd wing mounted track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left inbd. flap, inbd flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left outbd. flap, inbd flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left outbd. flap, outbd flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: BEAM — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection corrosion was found under and around the forward carbon fiber omega beam. Maintenance removed and replaced the top cap, ramp angle, L-profile angle, cross fiber beam and installed shim, filler, plate and external angle. I.A.W.-EMB-135/145-SRM-51-40-02, 53-21-02 and CMP-52-21-04 & 05. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: ANTENNA — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the lower TCAS antenna mating surface to fuselage was corroded. Maintenance removed antenna, cleaned corrosion I.A.W.-EMB-135/145-CPM-51-14-00 and reinstalled antenna I.A.W.-EMB-145-AMM-34-43-03. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the right outbd. flap, outbd. track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left outbd. flap, outbd wing mounted flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: CABLE — CORRODED (MLG WW) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION, THE EMERGENCY EXTENTION CONTROL CABLE IN THE RIGHT WHEEL-WELL WAS FOUND BENT AT THE TURNBUCKEL. MAINTENANCE REMOVED AND REPLACED THE FREE FALL CABLES IN RIGHT WHEEL-WELL. I.A.W.-EMB-145-AMM-32-34-03. REPAIRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: TRACK — GROOVED · airframe 7,362 hrs · 5,263 cycles

TYS During a scheduled inspection, the left inbd. flap, outbd flap track was found to have grooves worn into track. Maintenance blended grooved areas I.A.W.-EMB-145-GST-3350/01. Repairs were satisfactory and the aircraft will be released upon complection of inspection.

Part: ANTENNA — CORRODED · airframe 7,362 hrs · 5,263 cycles

TYS Durind a scheduled inspection the lower TCAS antenna mating surface to fuselage was corroded. Maintenance removed antenna, cleaned corrosion I.A.W.-EMB-135/145-CPM-51-14-00 and reinstalled antenna I.A.W.-EMB-145-AMM-34-43-03. Repairs were satisfactory and aircraft will be released upon completion of inspection.

Part: FLAP TRACK — GROOVED (T/E FLAP) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULED INSPECTION, THE RIGHT INBD FLAP, INBD TRACK WAS FOUND TO HAVE GROOVES WORN INTO TRACK. MAINTENANCE BLENDED GROOVED AREAS IAW EMB 145 GST 3350/01. REPAIRS WERE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LENS — MISSING (FIRE BOTTLE) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULE INSPECTION THE LEFT ENGINE FIRE BOTTLE GAUGE, LENS IS MISSING. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE IAW EMB 145 AMM 26-21-02. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GAUGE — UNSERVICEABLE (FIRE BOTTLE) · airframe 7,362 hrs · 5,263 cycles

TYS DURING A SCHEDULE INSPECTION THE APU ENGINE FIRE BOTTLE GAUGE IS UNREADABLE. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE IAW EMB 145 AMM 26-22-01. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: UNKNOWN — ODOR (CABIN) · airframe 6,111 hrs · 4,393 cycles

TYS FLIGHT 4355. THE CREW REPORTED THAT DURING TAKEOFF ROLL THE RT ENGINE OIL PRESSURE WENT TO 116 PSI AND THERE WAS A STRONG ODOR IN THE COCKPIT AND CABIN. THE CREW REJECTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED GROUND RUN OPERATIONAL CHECKS IAW ROLLSROYCE MM 72-00-00, ALL PARAMETER WERE WITHIN LIMITS AND NO ODOR WAS DETECTED IN COCKPIT OR CABIN. THE AIRCRAFT RELEASED FOR SERVICE.

Part: UPLOCK — INOPERATIVE (LT MLG)

IAH - FLT 3925 - AFTER TAKEOFF FROM SAV, ON GEAR RETRACTINO, THE CREW REPORTED A LEFT GEAR UNSAFE LIGHT AND A LANDING GEAR LEVER DISAGREE MESSAGE, THE CREW CYCLED THE GEAR AND ALL WARNINGS WENT AWAY. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG UPLOCK BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: TANK — CRACKED (RT ENGINE)

IAH- FLT 4276 - DURING POST FLT INSPECTION, THE CREW REPORTED THAT THE NUMBER TWO ENGINE WAS LEAKING OIL. MX INSPECTED THE NR 2 ENGINE AND FOUND THE OIL TANK TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OIL TANK IAW EMB145 MM 79-1101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SUBSEQUENTLY, PRIOR TO TAKEOFF ON 4197, THE CREW REPORTED LOW OIL QTY ON THE NR 2 ENGINE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE OIL TANK TO AGAIN BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (EMERGENCY EXIT)

IAH - DURING 3A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURNEDTO SERVICE. (M)

Part: CONTROL MODULE — INOPERATIVE (CABIN)

IAH - DURING CONFORMITY CHECK WHILE PERFORMING EMERGENCY LIGHT FUNCTIONAL CHECK, FOUND THE EICAS INDICATED 'EMERGENCY LIGHTS NOT ARMED' WITH THE LIGHTS PLACED IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE IAW EMB-145 MM 33-21-01 AND PERFORMED FUNCTIONAL CHECK OF THE EMERGENCY LIGHTS IAW EMB-145 MM 33-50-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)