N11536

Part: TERMINAL — BURNED (WINDSHIELD) · airframe 39,817 hrs · 30,914 cycles

CREW REPORTED SMOKE IN THE COCKPIT, VISIBLE SMOKE FROM THE LOWER LEFT CORNER OF FIRST OFFICERS WINDSHIELD. ACFT DIVERTED FROM DESTINATION AND LANDED SAFELY. MX REMOVED AND REPLACED THE NR 2 WINDSHIELD TEMP CONTROLLER. OPS CHECKED GOOD. REMOVED AND REPLACED THE FIRST OFFICER'S WINDOW DUE TO A BURNED TERMINAL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,990 hrs · 29,441 cycles

RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2R. DAMAGE FOUND BY NDT INSPECTION. FUSELAGE SKIN REPAIRED WITH DOUBLER INSTSALLATION (9" X 10") IAW SRM 53-31-01 ITEM 11 DETAIL B

Part: BEARING CAP — CORRODED (NLG) · airframe 37,990 hrs · 29,441 cycles

NOSE LANDING GEAR LEG LOWER BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 32-20-01.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 37,990 hrs · 29,441 cycles

SERVICE DOOR LOWER SILL CORRODED. SERVICE DOOR SILL WAS REPLACED IAW SRM 51-40-02.

Part: FITTING — CORRODED (FRAME 68) · airframe 37,990 hrs · 29,441 cycles

CARGO AFT LATERAL L SHAPE CORRODED ON LOWER SECTION AT FRAME 68. THE L SHAPE WAS REPLACED IAW SRM 53-31-04.

Part: SUPPORT — CORRODED (DOOR SILL) · airframe 37,990 hrs · 29,441 cycles

PAX DOOR SILL SUPPORT CORRODED. THE SUPPORT WAS REPLACED.

Part: BEAM — CORRODED (CARGO BAY) · airframe 37,990 hrs · 29,441 cycles

CARGO ENTRANCE LOWER BEAM CORRODED BEYOND LIMITS. CARGO ENTRANCE LOWER BEAM REPLACED IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 37,990 hrs · 29,441 cycles

CORROSION ON DOUBLER AROUND POTABLE WATER SERVICING NIPPLES. THE DOUBLER WAS REPLACED IAW SRM.

Part: SEAT TRACK — CORRODED (FRAMES 36-47) · airframe 37,990 hrs · 29,441 cycles

LEFT OUTBOARD SEAT TRACK NR 4 BETWEEN FRAMES 36 - 47 CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06.

Part: FLOORBEAM — CRACKED (FRAME 18) · airframe 37,990 hrs · 29,441 cycles

FLOORBEAM ANGLE AT FRAME 18 FOUND CRACKED. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 37,990 hrs · 29,441 cycles

SUPPORT BRACKET CRACKED ON THE CARGO DOOR BALANCE SPRING ASSEMBLY FORWARD OF FRAME 68. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRAMES 47-52) · airframe 37,990 hrs · 29,441 cycles

LEFT OTBD SEAT TRACK NR 5 BETWEEN FRAMES 47 - 52 CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-01-06.

Part: FLOORBEAM — CRACKED (FRAME 18) · airframe 37,990 hrs · 29,441 cycles

FLOORBEAM ANGLE CRACKED AT FRAME 18. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02.

Part: ACM — FAILED (NR 2) · airframe 33,852 hrs · 26,184 cycles

DURING CRUISE, SMOKE APPEARED IN THE CABIN AND ODOR WAS ALSO OBSERVED. ACFT LANDED OK AND THEN WAS FERRIED, MAINTENANCE R & R THE NR 2 ACM IAW AMM 21-51-03, ALSO R & R THE NR 2 CONDENSER MIXER IAW AMM 21-51-04. LEAK AND OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE. SN OF MIXER WAS 200108018.

Part: ACM — SEIZED (NR 2) · airframe 33,836 hrs · 26,171 cycles

AFTER TAKEOFF, AT 4000FT F/A CALLED AND STATED SMOKE IN THE CABIN. PILOT AND F/O COULD SEE SMOKE AND DECLARED EMERGENCY, RETURNED TO AIRPORT. MAINTENANCE INSPECTED ACFT AND FOUND NR 2 ACM SEIZED. PLACED ON MEL. ON 8/4/15 MAINTENANCE R & R NR 2 ACM WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,540 hrs · 25,924 cycles

DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT FLOOR STRIP NR 3 WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R NR 3 FLOOR LIGHT STRIP WITH OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,171 hrs · 21,749 cycles

DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED. (LOCAL LEVEL 2) AT FRAME 50. MX PERFORMED REPAIR TO LT UPPER SEAT TRACK SUPPORT FRAME 50 IAW EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,171 hrs · 21,749 cycles

DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM 65-68 IS CORRODED (LOCAL LEVEL 2). MX PERFORMED REPAIR ON CARGO DOOR CUTOUT LOWER BEAM AT FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — PUNCTURED · airframe 25,575 hrs · 19,668 cycles

A SMALL PUNCTURE IN THE SKIN AT FRAME 10 NEAR STRINGER 14 NEXT TO THE TAT PROBE. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED SKIN, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — TORN (RT WING) · airframe 23,731 hrs · 18,255 cycles

CLE FLT 3095 THE CREW REPORTED ON DEPARTURE FROM CLE THE TOWER INFORMED THEM OF A FLUID LOSS COMING FROM THE RIGHT WING. THE AIRCRAFT RETUNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT WING OUTBOARD FLAPPER VALVE SEAL TORN. THE VALVE WAS REPLACED AND LEAK CHECKS WERE GOOD.

Part: CHECK VALVE — FAULTY (BLEED AIR SYS) · airframe 23,654 hrs · 18,192 cycles

CLE FLT 2510 THE CREW REPORTED A ENGINE NR 2 BLEED LEAK MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE AIR START CHECK VALVE AND RE-SECURED A LOOSE DUCT ON NR 2 PACK AT THE DUAL TEMP CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: BRACKET — WORN (AILERON) · airframe 231,656 hrs · 17,735 cycles

TYS - A/C CURRENTLY IN C-CHECK WHERE INSPECTION FOUND THE LT AILERON BUSHIONS MISSING WHERE THE O/B PCA ROD ATTACHES. MAINTENANCE R/R THE PCA BRACKET IAW EC5750-01177. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: BRACKET — WORN (RT WING) · airframe 23,165 hrs · 17,735 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT PCA BRACKET WORN OUT OF LIMITS. MAINTENACE R/R THE BRACKET IAE EC5750-01177. A/C WILL BE RELEASED AT THE END OF CHECK.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 22,682 hrs · 17,334 cycles

ORD FLT 6144 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AND FORWARD CABIN ON TAXI IN. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE ANY BURNING SMELL. OPERATIONAL CHECKS WERE GOOD IAW 21-20-00-810-801-1. THE SMELL WAS ALSO NOTED ON FLIGHT 5910. MAINTENANCE COULD NOT DUPLICATE ANY BURNING SMELL.

Part: RELAY — INOPERATIVE (AC PACK) · airframe 20,966 hrs · 16,032 cycles

** REFERENCE SDR C2XA10IA192 **GPT - FLIGHT 2643, THE CREW REPORTED THAT PACK ONE WAS BLOWING HOT AIR. THE AIRCRAFT DIVERTED TO GPT WHERE IT LANDED WITHOUT INCIDENT. THE COOLING SYSTEM WAS RESET, OPERATIONALLY TESTED GOOD, AND THE AIRCRAFT CONTINUED TO IAH. IN IAH, THE DISCREPANCY REPEATED AND MAINTENANCE PLACED THE NUMBER ONE PACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 07/09/10, MAINTENANCE REMOVED AND REPLACED RELAYS K0187 AND K0335, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (NR 1 A/C PACK) · airframe 20,966 hrs · 16,032 cycles

FLIGHT 2643, THE CREW REPORTED THAT NR 1 A/C PACK WAS BLOWING HOT AIR. THE AIRCRAFT DIVERTED TO GPT WHERE IT LANDED WITHOUT INCIDENT. THE COOLING SYSTEM WAS RESET, OPERATIONALLY TESTED GOOD, AND THE AIRCRAFT CONTINUED TO IAH. IN IAH, THE DISCREPANCY REPEATED AND MAINTENANCE PLACED THE NR 1 PACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 07/09/10, MAINTENANCE REMOVED AND REPLACED RELAYS K0187 AND K0335, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 20,696 hrs · 15,837 cycles

FLIGHT 2381 - EWR - FLIGHT CREW REPORTED EXHAUST ELECTRONIC BAY FAN C/B POPPED IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FAN ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 18,214 hrs · 13,980 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,923 hrs · 12,352 cycles

NR 4 EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY IAW EMB 145 MM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,705 hrs · 12,200 cycles

FLIGHT 2197 - EWR - FLIGHT CREW REPORTED FLOOR EMERGENCY LIGHTS SEAT ROW 17A INOPERATIVE. EWR MX REMOVED AND REPLACED NR 6 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — FAULTY (WINDSHIELD WIPER) · airframe 15,626 hrs · 12,141 cycles

FLIGHT 2988 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL BURN SMELL WITH WINDSHIELD WIPER ACTIVATED. EWR MX REMOVED AND REPLACED LT WINDSHIELD WIPER SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 15,165 hrs · 11,811 cycles

CLE FLIGHT 2592 - THE CREW REPORTED A UNUSUAL LOAD SOUND FROM UNDER THE COCKPIT FLOOR ONLY IN CLIMB AND CRUISE. ALSO REPORTED A SLIGHT VIBRATION OF YOLK AND RUDDER PEDALS. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX "B"PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 15,108 hrs · 11,770 cycles

CLE FLIGHT 2409 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE IN FLIGHT. THE LANDING GEAR WOULD NOT RETRACT, ALSO RECEIVED A ENG REV 1&2 DISAGREE MESSAGE ON THE ECIAS. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR AIR/GROUND PROXIMITY SWITCH AND HARNESS. OPERATIONAL CHECKS WERE GOOD. HARNESS P/N 145-21495-405.

Part: PROXIMITY SWITCH — OBSTRUCTED (RT MLG) · airframe 15,074 hrs · 11,744 cycles

MKE FLIGHT 2560 - THE CREW REPORTED A AIR/GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM RIGHT MAIN LANDING GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 13,630 hrs · 10,676 cycles

FLT 2686 - EWR - CREW REPORTED GALLEY EMERGENCY LIGHT (SEAT 1A) INOP. EWR MX REMOVED AND REPLACED EMERGENCY SIGN AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 10,611 hrs · 13,545 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 18 TO 24 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,701 hrs · 9,952 cycles

DURING ROUTINE MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: BRAKE — MALFUNCTIONED (PARKING) · airframe 12,580 hrs · 9,860 cycles

IND LOG SQUAWK FLT NR 2951 WITH PARKING BRAKE SET AIRCRAFT ROLLS. CYCLED NORMAL BRAKES SEVERAL TIMES AND PERFORMED OPS CHECK OF PARKING BRAKE SYSTEM IAW AMM 32-44-07. OPS CHECK GOOD. CLOSED

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,709 hrs · 7,637 cycles

SDF - EMERGENCY LIGHT OVER GALLEY DOOR INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,901 hrs · 7,002 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND RT EXTERNAL FUSELAGE HAS DENT AT FRAME 4, NEAR TOP FWD CORNER OF PANEL 114 CR. MAINTENANCE REPAIRED DENT IAW EC 5330-01488. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 8,901 hrs · 7,002 cycles

SHV - DURING C-CHECK LIGHTNING STRIKE INDICATION AT FR 16 STR 19R. MAINTENANCE REPAIR DAMAGE LIGHTNING STRIKE AT FR 16 STR 19R IAW EC 5330-01486. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: WIRE HARNESS — DISCONNECTED (GALLEY) · airframe 8,162 hrs · 6,413 cycles

CREW REPORTED, EXIT ROW EMERGENCY LIGHT BURNED OUT OVER GALLEY DOOR. MAINTENANCE RECONNECTED THE CONNECTOR , OPS CHECKED GOOD IAW EMB145 AMM 33-50-00.

Part: LOGIC CARD — CORRUPTED (MLG UPLOCK) · airframe 7,956 hrs · 6,246 cycles

AFTER TAKEOFF, LG AIR/GROUND DISAGREE MESSAGE APPEARED ON EICAS. LANDING GEAR WOULD NOT RETRACT NORMALLY UNTIL OVERRIDE, THEN ENG 1-2 T/R DISAGREE MESSAGE APPEARED ON EICAS. CREW RETURNED TO CHS. ACFT WAS FERRY FLIGHT TO RIC. RIC MX PERFORMED PROX SW FUNCTIONAL CHECK AND FOUND 3RD UPLOCK LOGIC CORRUPTED. MX REMOVED AND CLEANED CONNECTORS P0774 AND P0775. MX PERFORMED RESET OF AIR GROUND LOGIC SYSTEM. LANDING GEAR RETRACTION AND EXTENSION FUNCTIONAL TEST WAS SUCCESSFULLY PERFORMED. THRUST REVERSER OPERATIONAL CHECK WAS SUCCESSFULLY PERFORMED AND ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — DAMAGED (LT MLG) · airframe 7,685 hrs · 6,051 cycles

TYS, CONTINUATION OF CONTROL NR C2XA05TY008, AIR RETURN FOR LANDING GEAR AIR GROUND FAIL ON TAKEOFF. MAINTENANCE FOUND THE LEFT MLG FORWARD AND AFT WOW PROX SWITCHES ONLY 250K RESISTANCE, SHOULD BE 1.4M. MAINTENANCE REMOVED AND REPLACED THE LEFT GEAR CANNON PLUG CONNECTORS AND ALL 4 PROX SWITCHES, (P/N 80-057-01, S/N'S 2898, 2783 AND 2885 TSO 3099.9, CYC 2419 / S/N 3437 TSO 3332, CYC 2617. TEST FLEW SATISFACTORY AND WAS RELEASED TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (MLG) · airframe 7,677 hrs · 6,044 cycles

TYS - A/C WAS DEPARTING BHM WHEN THE ICAS MESSAGE SHOWED GEAR NOT RETRACTED. A/C RETURNED TO BLOCK AND MAINTENANCE REMOVED AND REPLACED THE LGEU, BUT DID NOT FIX PROBLEM. A/C WAS FERRIED TO TYS AND MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 PROX SWITCHES. A/C WAS REL FOR A TEST FLIGHT AND TEST FLIGHT WAS SATISFACTORY. A/C WAS THEN REL FOR REVENUE SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,345 hrs · 5,794 cycles

RIC - MX DURING ROUTINE INSPECTION, MAINTENANCE FOUND RIGHT WING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — FAULTY (CABIN) · airframe 7,341 hrs · 5,791 cycles

CREW REPORTED FOUL ODOR COMING IN THE CABIN AND THE RECIRCULATION FAN APPEARS TO HAVE NO EFFECT. MAINTENANCE REPLACED THE RECIRCULATION FAN OPERATIONALLY CHECK GOOD NO ODORS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — ODOR (A/C SYSTEM) · airframe 7,331 hrs · 5,784 cycles

CREW REPORTED FOUL SMELL FROM PACK SYSTEM. MAINTENANCE REPLACED THE RECIRCULATING DUCT. OPERATIONALLY CHECK SYSTEM NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,331 hrs · 5,784 cycles

EWR-CO2146, CREW REPORTED EMERGENCY LIGHT OVER SERVICE DOOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT OVER SERVICE DOOR IAW EMB145 AMM NR 33-50-09. OPS CHECKED SYSTEM GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 6,531 hrs · 5,154 cycles

DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE RESECURED EXIT SIGN CONNECTORS AND PERFORMED A SATISFACTORY OPERATIONAL TEST.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

FLIGHT 2541 - CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT)

EWR---CO2430, DURING EWR TURNAROUND MAINTENANCE FOUND EMERGENCY BATTERY PACK TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, IAW EMB145 AMM NR 33-50-00 OPS. CHECKED SYSTEM GOOD.

Part: SIGN — FAULTY (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY EXIT LIGHTS WILL NOT ARM PROPERLY. MAINTENANCE INSPECTED AND REPLACED THE EXIT IDENTIFIER SIGN OVER THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,188 hrs · 3,298 cycles

SHV- DURING C CHECK THE SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION AT SCREW HOLES. MAINTENANCE REPAIRED AFFECTED SILL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK LEFT OMEGA BEAM AT CARBON FIBER CROSSBEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK APU FIRE WALL AT LEFT HAND SIDE HAS A CRACK ALONG THE BOTTOM PORTION OF SUPPORT FLANGE AT 10 O'CLOCK POSITION. MAINTENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK APU FIREWALL CRACKED AT THE RIGHT HAND UPPER VERTICAL STIFFENER. MAITENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK THE APU FIREWALL WAS FOUND CRACKED AT THE RIGHT HAND APU SUPPORT. MAINTENACE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK FOWARD DIGITAL WAS FOUND TO HAVE CORROSION DOWN THE CENTER LINE BETWEEN FRAMES 15 AND 18. MAINTENANCE REPAIRED AFFECTED DIGITAL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — GOUGED (RT COWLING) · airframe 4,188 hrs · 3,298 cycles

SHV DURING C CHECK THE RIGHT HAND LOWER COWLING WAS FOUND TO HAVE A GOUGE MARK AT FRAME 8 ON MOST OUTBOARD STRINGER. MAINTENANCE REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — SCORED (FUSELAGE) · airframe 4,188 hrs · 3,298 cycles

SHV-DURING C CHECK THE EXTERNAL SKIN SCORED NEAR FRAME 20 AT STRINGER 13L. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,188 hrs · 3,298 cycles

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

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,188 hrs · 3,298 cycles

SHV-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: STRINGER — GOUGED (FUSELAGE) · airframe 4,188 hrs · 3,298 cycles

SHV-DURING C CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED THE AFFECTED STRINGER IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — BURNED (GALLEY)

THE CREW REPORTED A BURNING SMELL COMING FROM THE LEFT HOT JUG IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE LEFT HOT JUG CONNECTOR AND HOT JUG. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (NOSE GEAR)

CLE FLIGHT#3915 THE CREW REPORTED A LOUD ROARING NOISE FROM AREA BELOW COCKPIT FLOOR IN FLIGHT.MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT.THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED.OPERATIONAL CHECKS WERE GOOD.