N14953

Part: SKIN — CRACKED (ZONE 200) · airframe 36,402 hrs · 27,415 cycles

DURING 4A INSPECTION THE LT FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 IN 2 PLACES BELOW STRINGER 1R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 36,402 hrs · 27,415 cycles

DURING 4A INSPECTION THE REAR FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STRINGERS 1R AND 2R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 34,484 hrs · 25,879 cycles

LT WING UPPER SKIN T/E WAS FOUND CRACKED AT THE LT GROUND SPOILER HINGE POINT. CUTOUT THE CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER. ACFT STILL IN C CHECK

Part: WINDOW FRAME — CORRODED · airframe 34,486 hrs · 25,881 cycles

LEFT & RIGHT WINDSHIELD FRAME HAS CORROSION IN SEVERAL HOLES. REMOVED CORROSION FROM BOLT HOLES AND SOME OF THE HOLES REQUIRED BUSHINGS TO BE INSTALLED IAW ETD2012-145-014418-A AND EC5310-01633. ACFT IS STILL IN C-CHECK.

Part: UPLOCK — INOPERATIVE (LT MLG) · airframe 31,569 hrs · 23,502 cycles

IAH - FLIGHT 2174, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION WAS SHOWING DASHES OF YELLOW AND GREEN, AND ALTERNATING BACK AND FORTH. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG UPLOCK BOX, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 31,111 hrs · 23,127 cycles

GRR FLT 2904 THE CREW REPORTED THE OVERWING CEILING EXIT LIGHT DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 31,070 hrs · 23,095 cycles

FLIGHT 2287 - EWR - FLIGHT CREW REPORTED THAT, EN ROUTE FROM EWR TO CMH, FMS FAILED, BOTH PFD'S AND NAVS ALSO WENT OUT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED CAPT DC550 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHIM — WORN (NLG) · airframe 30,408 hrs · 22,610 cycles

TYS - A/C WAS TAXI FOR TAKEOFF AND IN CLIMBOUT, WHEN GEAR STOWED, CREW REPORTED A RATTLING NOISE WHEN GEAR STOWED. A/C WAS FERRIED TO TYS FROM BNA WHERE MAINTENANCE REMOVED THE NOSE GEAR AND FOUND THAT GEAR NEEDED TO BE SHIM. MAINTENANCE MEASURED THE BEARING CAPS, ALL GOOD REPLACED AND SHIM THE GEAR IAW 32-20-01-400-801-A AND EC 3220-0106T. OPS CHECK WAS GOOD AND WAS THEN RELEASED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAMES 49-50 IAW EC5310-01466 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON SHEAR CLIP FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK NR 1 ENGINE FORWARD LOWER YOKE FORWARD FLANGE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FORWARD LOWER YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 54 REPAIR IAW EMB-145 SRM 51-00-10. RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 IAW EMB-145 SRM 51-00-10 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,523 hrs · 21,941 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5310-01529. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LANDIND GEAR) · airframe 28,693 hrs · 21,308 cycles

CLE FLT 2632 - THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE BUT CHANGED THE LGEU, ADJUSTED 1 PROXIMITY SWITCH ON LEFT AND RIGHT GEAR AND ADJUSTED NOSE PROXIMITY SWITCH TARGET ON THE NOSE GEAR AND CHANGED THE NOSE GEAR PROXIMITY SWITCH CONNECTOR. ALSO RELAYS KO453, KO352, AND KO353 WERE REPLACED. OPERATIONAL CHECKS OF THE GEAR WERE GOOD.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 27,611 hrs · 20,504 cycles

FLIGHT 2531 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT WOULD NOT TURN OFF. EWR MX REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (DEFIBRILLATOR) · airframe 27,137 hrs · 20,137 cycles

TYS - A/C WAS IN FOR A SERVICE CHECK WHEN INSPECTION FOUND THE AED DEFIBRILLATOR BATTERY INOP. MAINTENANCE REMOVED AND REPLACED THE AED DEFIBRILLATOR BATTERY IAW EC 2560-01065. A/C RELEASED BACK TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,086 hrs · 20,115 cycles

MCI - DURING MAINTENANCE INSPECTION THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 26,748 hrs · 19,847 cycles

FLIGHT 2790 - EWR - DURING DESCENT, FLIGHT CREW REPORTED AN AMBER INDICATION FOR RADIO ALTIMETER ON PFD WITH LANDING GEAR AURAL SOUND FOR 5 SECONDS THEN CLEARED. EWR MX RESET BOTH RA C/B'S AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 26,301 hrs · 19,495 cycles

ACFT IN OVERNIGHT FOR A 2A CHECK, WHEN INSP FOUND THE RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE THE BULB FOR THE LIGHT IAW AMM 33-50-07, OPS CHECK GOOD AND WAS RELEASED.

Part: PROXIMITY SWITCH — BROKEN (NLG) · airframe 26,301 hrs · 19,495 cycles

TYS - AIRCRAFT WAS EN ROUTE TO IAH FROM EWR WITH A STOP AT TYS, WHEN LEAVING TYS THE LDG WOULDN'T RETRACT SO CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED THE NLG PROX SWITCH IAW EMB 145 AMM 32-63-02 AND OPS CHECK GOOD. RELEASED BACK TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 25,719 hrs · 19,055 cycles

FLIGHT 2996 - EWR - FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHT INOPERATIVE ABOVE F/A SEAT. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

DSM FLIGHT NR 2636 THE CREW REPORTED A FUEL 1 LOW LEVEL MSG IN FLIGHT. THE FLIGHT DIVERTED IN DSM AND LANDED WITHOUT INCIDENT. THE FUEL QUANTITY INDICATOR WAS ACCURATE. THE SYSTEM WAS PLACED ON MEL SUPPLEMENT TO FOLLOW.

Part: HANDLE — UNSECURE (PAX DOOR)

FLIGHT 2807 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE FROM INSIDE. EWR MAINTENANCE SECURED MAIN CABIN DOOR HANDLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: SKIN — CRACKED (RT WING) · airframe 22,971 hrs · 17,150 cycles

IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 03/24/08 THE DAMAGED SECTRION OF SKIN WAS REMOVED, AND TRIPLERS INSTALLED AS A FINAL REPAIR, AND THE AIRCRAFT WAS APPROCVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 22,878 hrs · 17,089 cycles

IAH - FLIGHT 2099 DURING PREFLIGHT INSPECTION SOME EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED A FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HANDLE — FAILED (MLG) · airframe 22,352 hrs · 16,729 cycles

LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR HANDLE IAW EMB 145 MM 32-32-02, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: COMPUTER — SHORTED (AUTOPILOT SYSTEM) · airframe 22,343 hrs · 16,722 cycles

CLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND REPLACED THE GUIDANCE CONTROL COMPUTER. OPERATIONAL CHECKS WERE GOOD.

Part: DOUBLER — MISSING (RUDDER)

TYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AND A INTERNAL DOUBLER. ALODINED AND EPOXY PRIMED THE PARTS. INSTALL FABRICATED PARTS ON THE RUDDER IAW EC 5540--01077. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,443 hrs · 16,063 cycles

FLT 2774 - DAY - CREW REPORTED MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. DAY MX RECYCLED BATTERY SWITCHES AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,518 hrs · 15,362 cycles

IAH - FLT NR 3116, DURING A TEST THE EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESET THE EMERGENCY LIGHTING SYSTEM AND OPERATIONALLY TESTED THE SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND WAS THEN CLEARED.

Part: WIRE — LOOSE (CABIN) · airframe 19,382 hrs · 14,475 cycles

IAH - DURING A-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE SIGN, RE-SECURED THE CONNECTORS, AND RE-INSTALLED THE SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — OVERHEATED (A/C BAY)

FLT 2862 - CREW REPORTED SMOKE IN THE CABIN AFTER REACHING 10,000 FT CLIMBOUT. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE FOUND THE NR 2 ACM TO BE OVERHEATING. THE ACM WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CORRODED (STAB TO FUSELAGE) · airframe 15,326 hrs · 11,286 cycles

TYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FITTING AT FRAME 75, CLEANED AND INSPECTED THE SKIN AND FITTING (NO CORROSION OR DAMAGE WAS FOUND), ALODINED, APPLIED SEALANT AND REINSTALLED IAW-EC5310-01288, EC5310-01314, 135/145-SRM-51-40-02, 51-10-02 AND AMM-21-31-00.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 15,326 hrs · 11,286 cycles

TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145-AMM-21-31-00 / 135/145 SRM 51-40-00 AND 52-20-03, CABIN LEAKAGE AND FUNCTIONAL CHECKED GOOD.

Part: HINGE — WORN (VERTICAL STAB) · airframe 15,326 hrs · 11,285 cycles

DURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,918 hrs · 10,956 cycles

BTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE)

BTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITAL PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — LOOSE (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE-SECURED THE LAMP IN THE LIGHT FIXTURE. THE LIGHT OPERATIONALLY CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING 3A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — GOUGED (CABIN) · airframe 11,414 hrs · 8,192 cycles

SHV-DURING C-CHECK THE AFT FLOORBEAM BUTT STRAP WAS FOUND TO HAVE A GOUGE AT FRAME 18 CENTER LINE. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK THE SUPPORT PLATE BETWEEN LT OMEGA BEAM AND LT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE LT SILL BETWEEN FRAMES 59 AND 61 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: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE LT BUTT STRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE LT OUTBOARD FLOOR SUPPORT AT FRAME 18 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE RT BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE RT BUTT STRAP AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,414 hrs · 8,192 cycles

SHV-DURING C-CHECK, REPAIR DOUBLER ON T-REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, REPAIR DOUBLER ON TEE REINFORCEMENT ON STRINGER 19 LT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 14 AND 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-20-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (CABIN) · corrosion level 2 · airframe 11,414 hrs · 8,192 cycles

DURING C-CHECK, THE PASSENGER DOOR THRESHOLD SUPPORTS WHERE FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (RT MLG)

EWR- CREW REPORTED AFTER TAKEOFF LG/GEAR DISAGREEMENT (INDICATION), RT MAIN GEAR. AIRCRAFT AIR RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED RT MAIN LANDING GEAR UPLOCK BOX IAW EMB145 MM 32-33-10 AND PROXIMITY SWITCH IAW EMB145 MM 32-61-01. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (RT MLG)

EWR- FLIGHT 4161, THE CREW NOTED THAT THE LANDING GEAR DISAGREEMENT LIGHT ILLUMINATED FOR THE RIGHT MAIN GEAR. THE CREW RETURNED TO EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE

BNA - Maintenance found the left and right overwing emergency lights to be inoperative. Maintenance removed and replaced the #4 power supply. The system operationally checked good and the aircraft was approved for return to service.

Part: MODULE — FAULTY (CABIN)

MKE- WHILE AT THE GATE FLIGHT 4052 THE CREW NOTED A BURNING ODOR FROM AROUND THE FLIGHT ATTENDANT LIGHTING CONTROL PANEL. THE SYSTEM WAS PLACED ON MEL, AND THE AIRCRAFT WAS RELEASED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHTING CONTROL MODULE, PERFORMED A OPERATIONAL CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — VIBRATION (RT)

TYS - THE RIGHT ENGINE WAS REMOVED AND REPLACED DUE TO HP VIBRATION IN THE YELLOW RANGE ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED THE ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: LIGHT — SHORTED (SEAT 15)

EWR - FLT 4147 - CREW REPORTED SEAT 15A OVERHEAD LIGHT SHORTED OUT AND WAS SMOKING. MAINTENANCE VERIFIED LIGHT WAS INOPERATIVE AND MEL''D AIRCRAFT IAW MEL NR 33-20-00 PLACARD NR 264161, AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: LIGHT — SHORTED (FUSELAGE)

EWR - FLT 4204 - REPORTED WING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM AND FOUND SHORTED WIRE IN LEFT WING EMERGENCY EXIT LIGHT ASSEMBLY AND BLOWN FUSE. REPLACED FUSE AND REPAIRED SHORTED WIRE AND OPS CHECKED SYSTEM GOOD. (M)

Part: LIGHT — FAILED (FUSELAGE)

EWR - FLT 4073 - CREW REPORTED RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED SYSTEM GOOD. (M)

Part: SEALS — FAILED (CARGO COMPT)

MCI - FLT 4108 - PILOT REPORTED A BAGGAGE SMOKE WARNING INDICATION WAS NOTED DURING FLIGHT. THE ACFT RETURNED TO MCI WTHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND THE LEFT BLEED SYSTEM WAS FOUND LEAKING IN THE CARGO BAY. THE SEALS ON THE BLEED TUBE GAMA JOINT WERE FOUND HARDENED AND BROKEN ALLOWING THE RETAINING SLEEVE TO FALL OUT OF POSITION. SUBSEQUENT DAMAGE OCCURRED TO WIRING GOING TO THE BLEED LEAK SENSOR AT THE GAMA JOINT. THE AIRCRAFT WAS FERRIED TO BTV WHERE MAINT REPLACED THE AFFECTED SEALS, GAMA JOINT CLAMP, AND PERFORMED REPAIRS TO THE WIRING DAMAGE. ACFT APPROVED FOR RETURN TO SERVICE. (X)

Part: BATTERY CHARGER — FAILED (NR 1/4)

EWR - FLT 4201 - LEFT AND RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND BOTH NR 1 AND NR 4 BATTERY CHARGER ASSY TO BE FAULTY. REMOVED AND REPLACED WITH SERVICEABLE UNITS, AND OPS CHECKED SYSTEM GOOD. (M)

Part: BULB — FAILED (AFT CABIN)

ATL - FLT 4207 - PILOT REPORTED SMOKE IN THE CABIN. THE CREW DIVERTED INTO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO BULBS AT THE AFT CABIN AREA THAT WERE BURNED ON THE ENDS. THE AIRCRAFT WAS RELEASED UNDER MEL NR 33-20-00. THE MEL WAS CLEARED AT IAH, FLT 4207 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS. NO FURTHER INCIDENTS HAVE BEEN REPORTED. (X)