N14960

Part: WIRE HARNESS — ARCED (CABIN LIGHTS) · airframe 36,751 hrs · 27,877 cycles

CREW REPORTED THE CEILING LIGHT OVER ROW 1A WAS PRODUCING A BURNING ODOR. MX R & R THE ELECTRICAL HARNESS NR ROW 1A WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,241 hrs · 24,471 cycles

DURING MX INSPECTION, EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT INOPERATIVE. MX R & R INVERTER & OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,348 hrs · 26,764 cycles

CREW REPORTED A ODOR IN THE CABIN LIKE BURNING PLASTIC. MX PERFORMED PASSENGER CABIN LIGHT TEST WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK, COCKPIT STRINGER 21R CORRODED. MX R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK SHEAR TIE AT FRAME 68 BETWEEN STRINGER 18L-17L IS CORRODED. MX REPAIRED SHEAR TIE IAW SRM 51-20-01 AND CPM 51-21-06. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK COCKPIT STRINGER 21L CORRODED. MX REPAIRED OF STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK, STRINGER SPLICE 21L CORRODED BETWEEN FRAMES 12-13. MX PERFORMED REPAIR ON STRINGER SPLICE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK CORRODED SHEAR CLIP ON RT CROSSBEAM FRAME 65. MX PERFORMED REPAIR ON FRAME 65 RH CROSSBEAM SHEAR CLIP IAW EC5320-01494A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK CARGO DOOR CUTOUT LWR MEMBER CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUT-OUT LWR MEMBER IAW SRM 51-20-01 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK CARGO THRESHOLD TRIANGULAR PLATE AT FRAME 65 CORRODED. (LOCAL LEVEL 2) AROUND NUTPLATES. MX PERFORMED REPAIR ONCARGO COMP THRESHOLD TRIANGULAR PLATE AT FRAME 65 IAW EC5320-01479, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAME 68 CORRODED AROUND NUTPLATES. MX PERFORMED REPAIR ON CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAME 68 IAW EC5320-01479, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK LT OMEGA BEAM FLANGE CORRODED (LOCAL LEVEL 2) BETWEEN FRAMES 18-23. MX PERFORMED REPAIR FOR LT OMEGA BEAM FLANGE AT FRAME 20 IAW SRM 53-00-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — GOUGED (ZONE 200) · airframe 34,688 hrs · 26,241 cycles

DURING C-CHECK FRAME 60 AT STRINGER 5L GOUGED. MX PERFORMED REPAIR AT FRAME 60 STRINGER 5L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (WINDSHIELD HEAT) · airframe 31,960 hrs · 24,029 cycles

THE CREW REPORTED AN 115 VOLT, AC BUSS FAILED ALONG WITH SMOKE ODOR. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,403 hrs · 22,780 cycles

RT OVERWING EMERGENCY LIGHT INOP. REPLACED LAMP IAW EMB 145 AMM33-50-05. OPS CHECK GOOD.

Part: STARTER — FAULTY (NR 1 ENGINE) · airframe 30,205 hrs · 22,615 cycles

EWR FLT 2260 THE CREW REPORTED A NR 1 ENGINE HIGH VIBRATION ON TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR TURBINE STARTER. PERFORMED ENGINE VIBRATION SURVEY AND COMPLIED WITH CMC DOWNLOAD. OPERATIONAL CHECKS WERE GOOD.

Part: STARTER — VIBRATION (NR 1 ENGINE) · airframe 30,205 hrs · 22,614 cycles

FLIGHT 2260 - EWR - FLIGHT CREW REPORTED ENGINE NR 1 HIGH VIBRATION ON TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PLACED ITEM ON DMI FOR 50 FLIGHT HOURS. ACFT WAS APPROVED TO RETURN TO SERVICE. FURTHER TROUBLESHOOTING REVEALED VIBRATION COMING FROM AIR TURBINE STARTER. MX REMOVED AND REPLACED STARTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. DMI CLEARED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — CRACKED (NACELLE) · airframe 29,703 hrs · 22,253 cycles

SHV - DURING C-CHECK NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REMOVED AND REPLACED NR 1 ENG YOKE FITTING IAW EC5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,703 hrs · 22,253 cycles

SHV - DURING C-CHECK RT OMEGA BEAM AT FRAME 18 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 29,703 hrs · 22,253 cycles

SHV - DURING C-CHECK BOUBLER AT FRAME 22 IS CORRODED (LEVEL 2 LOCAL) AND BENT. MAINTENANCE PERFORMED REPAIR ON DOUBLER AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 29,243 hrs · 21,909 cycles

CLE FLT 2690 THE CREW REPORTED THE PRESSURIZATION WAS INOPERATIVE IN BOTH MANUAL AND AUTO. THE AIRCRAFT DIVERTED INTO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: BRAKE — OVERHEATED (LEFT) · airframe 29,013 hrs · 21,738 cycles

DAY - FLT 2693 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE AFTER TAKEOFF. THE LEFT BRAKE SHOWED FULL HOT. THE BRAKES WERE COOLED PER THE QRH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BRAKE AND BRAKE TEMP SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,657 hrs · 21,451 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A AND 12A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,657 hrs · 21,451 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A AND 12A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,622 hrs · 19,941 cycles

IAH - DURING MAINTENANCE INSPECTION THE LOWER FORWARD SERVICE DOOR EXIT IDENTIFIER AND NR 1 FLOOR PROX LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER AT CONNECTOR P8527, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAP — OVERSPEED (WING) · airframe 25,948 hrs · 19,431 cycles

FLIGHT 2527 - EWR - FLIGHT CREW REPORTED FLAP OVER SPEED IN CRUISE (FLAP 9 AT 290 KNOTS FOR 5 MINUTES). EWR INSPECTION DEPARTMENT PERFORMED FLAP OVER SPEED INSPECTION AND FOUND NO DAMAGES. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 25,509 hrs · 19,083 cycles

FLIGHT CREW REPORTED CABIN AUTO PRESSURIZATION SYS OPERATED ABNORMALLY ON DESCENT. CREW LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LAV SMOKE DETECTOR TEST PANEL HAS NO POWER. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB-145 AMM 26-14-01. OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE CORRODED FRM 25 AT COMPOSITE CROSSBEAM. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 44. MAINTENANCE REPAIRED LT OMEGA BEAM IAW IC2009-145/00816. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FR 49. MAINTENANCE REPAIRED CORRODED AREA ON LT OMEGA BEAM (CORRODED AREA) AT FRM 49 IAW IC2009-145/00816. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK STR 17R FRMS 16-24 HAS CORROSION. MAINTENANCE REMOVED AND COMPLETED INSTALLATION OF STR 17R AT FRMS 16-24 BY INSTALLING HI-LOKS AT STRINGER SPLICE AT FR 16.5 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT FR 29. MAINTENANCE COMPLETED INSTALLATION OF REPAIR FOR LT OMEGA BEAM AT FRM 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW IC 2009-145/00816. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 33. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM AT FRM 33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,966 hrs · 18,684 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM FRM 25, CORRODED AT COMPOSITE CROSSBEAM. MAINTENANCE REPAIRED CENTER OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 22,430 hrs · 16,909 cycles

THE AFT FACING PORTION OF THE CEILING EMERGENCY EXIT SIGN AT SEAT 12 IS INOP. RESECURED THE CONNECTOR, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: PANEL — CORRODED (WING) · airframe 20,510 hrs · 15,501 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND OVER THE WING TO FUSELAGE PNL 195 WITH CORRODED BONDING STRAPS. MAINTENANCE REPAIRED PNL 195 IAW EC 5750-01315, AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,510 hrs · 15,501 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM FROM FRAME 18 TO 23 WITH CORROSION. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRAME 18 TO 23 IAW SRM 51-40-02. PAINTED & INSTALLED NUT PLATES IAW EC 5320-01140 & EC 5320-01137. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — LEAKING (BRAKE SYSTEM) · airframe 19,795 hrs · 14,928 cycles

EWR FLIGHT 2996 THE CREW REPORTED HYDRAULIC SYSTEM NR 2 FAILURE. TOTAL LOSS OF SYSTEM NR 2 FLUID. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 SYSTEM BRAKE PRESSURE SWITCH LEAKING. THE SWITCH WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 19,461 hrs · 14,677 cycles

BNA - FLT 2278 THE CREW REPORTED THAT THE NOSE GEAR DOORS DID NOT CLOSE UNTIL REACHING AN ALTITUDE OF 11,000 FT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK PROXIMITY SWITCH. THE LANDING GEAR DOORS WERE OPERATIONALLY CHECKED AND THE AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,871 hrs · 12,630 cycles

IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,871 hrs · 12,630 cycles

IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 167,191 hrs · 12,507 cycles

STL - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS AT THE COCKPIT ENTRANCE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (LIGHT) · airframe 15,521 hrs · 11,555 cycles

CLE FLIGHT NR 2249, THE CREW REPORTED AN UNIDENTIFIED BURNING ODOR AT THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED THE CABIN AREA AND FOUND THE CENTER/LEFT CABIN LIGHT NOT ILLUMINATED AND THE LIGHT ASSEMBLY BURNED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE OPERATIONAL TESTS WERE GOOD WITH NO MORE BURNING SMELL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,036 hrs · 11,141 cycles

CLE FLIGHT NR 2107, CREW REPORTED THAT THE GALLEY AND BULKHEAD EMERGENCY LIGHTS WERE INOP. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, AND DID NOT FIND AND DEFECTS. SYSTEM OPERATIONALLY CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY LIGHT ASSEMBLY CANNON PLUG LOOSE. THE CONNECTOR WAS RESET, THE LIGHT OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 12,690 hrs · 9,316 cycles

CREW REPORTED, SIDEWALL LAMP FLICKERING AND SMELL OF SMOKE IN SEAT 1A. MAINTENANCE REMOVED THE BULB AIRCRAFT RELEASED IAW MEL 33-20-00/1 CATEGORY-C ITEM CONTROL NUMBER 038985. AIRCRAFT ARRIVED EWR, MAINTENANCE REMOVED AND REPLACED HARNESS FOR LAMP INSERT SEATS 1A AND 2A, AND INSTALLED LAMP IAW EMB145 WM 33-21-50, OPS CHECKED GOOD. MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NACELLE) · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO GOUGED AT FRAME 71L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

SHV- DURING C-CHECK, THE CARGO DOOR LOWER STRUCTURE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE LT HAND BUTTSTRAP BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE LT HAND SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — GOUGED (FUSELAGE) · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE CENTER BUTTSTRAP AT FRAME 18 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE CENTER BUTTSTRAP BETWEEN FRAMES 16 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 61 AND 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,267 hrs · 8,192 cycles

DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,297 hrs · 8,192 cycles

SHV-DURING C-CHECK THE CENTER FLOORBEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — FAULTY (NOSE GEAR)

THE CREW REPORTED AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT.THE CREW RECYCLED THE GEAR WITH NO SUCCESS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — LEAKING (NR 2 PYLON)

CLE FLIGHT 2067 THE CREW REPORTED A LAV SMOKE WARNING INFLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND A INTERNAL OIL LEAK ON THE NR 2 ENGINE. THE NR 2 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: GROUND WIRE — LOOSE (LAV)

CLE FLIGHT#2131 THE CREW REPORTED A LAV SMOKE WARNING DURING CLIMB.THE CREW CONFIRMED NO SMOKE PRESENT.MAINTENANCE INSPECTED AND REPLACED LAV SMOKE DETECTOR PANEL.MAINTENANCE ALSO RESECURED A LOOSE GROUND WIRE ON THE LAV SMOKE DETECTOR.OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 10,609 hrs · 7,618 cycles

EWR---CO2260, LAV SMOKE WARNING PASSING THROUGH 7500 FEET. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW EMB145 AMM 26-44-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN)

CREW REPORTED OVERHEAD EMERGENCY SIGN WOULD NOT ILLUMINATE WHEN TESTED MAINTENANCE RESECURED CONNECTOR PLUG AND VERIFIED NORMAL OPERATION

Part: BULB — BLOWN (CABIN) · airframe 7,478 hrs · 5,259 cycles

TYS During a scheduled inspection, the emergency light above seat 12A was found not working. Maintenance removed and replaced the light bulb, operational checks good I.A.W.-EMB-MM-33-50-09. Aircraft released to servive.

Part: BULB — BLOWN (CABIN) · airframe 7,478 hrs · 5,259 cycles

TYS During a scheduled inspection, the emergency light in the service door was found not working. Maintenance removed and replaced the light bulb, operational checks good I.A.W.-EMB-MM-33-50-09. Aircraft released to servive.

Part: CONTROL CABLE — MISROUTED (RT AILERON)

DAL-IAH - FLT 4208 - DURING FLIGHT, THE CREW REPORTED A BINDING AND GRINDING DURING AILERON MOVEMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE RIGHT UPPER AILERON CABLE TO BE MISROUTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CABLE IAW EMB145 MM 27-11-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01032, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE SKIN WAS FOUND TO BE DENTED AT FRAMES 20 AND 21 AT STRINGERS 7L AND 8L. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR IAW EMB145 SRM 51-21-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STIFFENER — DENTED (LT NACELLE)

IAH - DURING C-CHECK INSPECTION, THE NR 1 ENGINE UPPER COWLING Z SECTION STIFFENER WAS FOUND TO BE DENTED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED SECTION OF STIFFENER IAW EMB145 SRM 54-10-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE NR 8 EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REPAIRED THE AFFECTED WIRE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01032, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — LEAKING (RIGHT)

IAH - DURING FLIGHT 3998, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE CREW RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY)

IAH - DURING FLIGHT 3919, THE CRWE REPORTED THE LAVATORY AND BAGGAGE SMOKE WARNING ILLUMINATED AFTER TAKEOFF. THE CREW DISCHARGED THE BAGGAGE FIRE BOTTLES AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE CARGO SMOKE DETECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (LT EMER EXIT)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT FORWARD EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-55-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)