N12540

Part: ACM — FROZEN (NR 2) · airframe 38,069 hrs · 39,409 cycles

THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ACM, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 38,053 hrs · 29,396 cycles

LEFT WING RIB 21 CRACKED. CUT OUT THE SECTION AND INSTALLED FILLER AND DOUBLER.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · airframe 38,053 hrs · 29,396 cycles

RIGHT OMEGA BEAM, FRAME 23 CORRODED BEYOND LIMITS AT SCREW HOLES. REMOVED AND REPLACED THE OMEGA BEAM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,065 hrs · 30,464 cycles

IAH - DURING MAINTENANCE INSPECTION THE UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 36,743 hrs · 28,334 cycles

FLIGHT 4045, THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT TO BE OUT IN THE AISLE NEAR THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND RECONNECTED THE AFFECTED EMERGECY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AXLE — BROKEN (RIGHT MLG) · airframe 36,639 hrs · 28,250 cycles

DURING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER LOWER AXLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT SHOCK ABSORBER LOWER AXLE SPECIAL BOLT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,219 hrs · 25,563 cycles

DURING ROUTINE MAINTENANCE THE GALLEY EMERGENCY LIGHT WOULD NOT TURN ON. MAINTENANCE REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT INVERTERS. OPS CHECKS WERE GOOD.

Part: BEAM — CORRODED (FRAMES 59-68) · corrosion level 2 · airframe 32,604 hrs · 25,079 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 32,604 hrs · 25,079 cycles

DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-17L. MAINTENANCE PERFORMED A FRAME SEGMENT SPLICE REPAIR IAW SRM 53-31-04, FIGURE 212. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 32,604 hrs · 25,079 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5320-02037. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 32,604 hrs · 25,079 cycles

DURING C-CHECK SHEAR TIE AT FRAME 68 CARGO DOOR LOWER BEAM HAS CORROSION. REPAIRED SHEAR TIE AT FRAME 68 IAW SRM 53-31-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,839 hrs · 21,356 cycles

CENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,839 hrs · 21,356 cycles

CORROSION AT GUSSET Y=0.00 CORRODED AROUND SCREW HOLES BEYOND LIMITS. R & R GUSSET

Part: PROFILE — CORRODED (FUSELAGE) · airframe 27,839 hrs · 21,356 cycles

CORROSION AT "T" PROFILE BEYOND LIMITS. R & R T PROFILE LT SIDE AT OMEGA BEAM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,839 hrs · 21,356 cycles

CORROSION AT RT OMEGA BEAM AT NUTPLATE HOLES CORRODED BEYOND LIMITS. R & R HAT SECTION ASSY.

Part: SILL — CORRODED · airframe 27,839 hrs · 21,356 cycles

LT SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: FLOOR SUPPORT — CORRODED · airframe 27,839 hrs · 21,356 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · airframe 27,839 hrs · 21,356 cycles

FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · airframe 27,839 hrs · 21,356 cycles

CORROSION BEYOND LIMITS AT FLOOR SUPPORT. R & R FLOOR SUPPORT.

Part: GUSSET — CORRODED · airframe 27,839 hrs · 21,356 cycles

CORROSION BEYOND LIMITS ON GUSSET. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED · airframe 27,839 hrs · 21,356 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: SILL — CORRODED (ZONE 100) · airframe 27,839 hrs · 21,356 cycles

RT SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED · airframe 27,839 hrs · 21,356 cycles

LT SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 27,167 hrs · 20,827 cycles

DURING ROUTINE MX, THE LT EXTERNAL AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE LIGHT ASSY AND OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,713 hrs · 20,474 cycles

NR 4 BATTERY FOR EMERGENCY LIGHT IN CEILING IS INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,725 hrs · 20,487 cycles

THE REAR FUSELAGE RT SKIN WAS DAMAGED DURING GROUND OPERATIONS. THE DAMAGE IS LOCATED BETWEEN FRAMES 62 & 63, STR 15R & 17R. REPAIRED DENT WITH FILLER AND DOUBLER. CUTOUT DAMAGED PORTION OF FRAME. FABRICATED AND INSTALLED FRAME SPLICE. REMOVED DAMAGED SECTION OF STRINGER 16R, RECONTOURED, PERFORMED EDDY CURRENT INSPECTION AND INSTALLED. ACFT RELEASED AND RETURNED TO SERVICE.

Part: FMU — FAULTY (RIGHT ENGINE) · airframe 26,433 hrs · 20,237 cycles

CREW REPORTED ENGINE NR 2 STARTED SURGING (ERRATIC ACCEL & DECEL) ON DESCENT BETWEEN FL 260& FL250 N1 SPIKE 45-65 ITT SPIKE BETWEEN 400-600. MX R & R ENGINE NR 2 FPMU WITH OPS AND LEAK CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,100 hrs · 19,957 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,102 hrs · 19,958 cycles

DURING POSTFLIGHT INSP THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. THE EMERGENCY LIGHT SYS WAS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 25,331 hrs · 19,319 cycles

CREW REPORTED LOSS OF CABIN PRESSURIZATION AT FL330. CREW MANUALLY DEPLOYED PAX O2 MASK AT 12,100 FT WITH CABIN ALT SHOWING 20,000 FT IAW ENGINEERING INSTRUCTIONS AND ASSISTANCE MX R & R THE DIGITAL PRESSURIZATION CONTROLLER, CABIN PRESS. AQUISITION MODULE (CPAM), ELECTROPNEUMATIC AND PNEUMATIC OUTFLOW VALVES ALONG WITH AFFECTED O2 MASKS AND GENERATORS. OPS CHECKS WERE SUCCESSFUL AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,466 hrs · 18,667 cycles

THE CREW REPORTED SEVERE TURBULANCE AT FL360. LOST ABOUT 1000FT, AP DISENGAGED AND THEY ALSO REPORTED A BURNING ODOR FOR ABOUT A MINUTE. MX COMPLIED WITH TURBULENCE INSPECTION. NO DEFECTS WERE NOTED. AUTOPILOT OPS CHECKED GOOD. NO DEFECTS FOUND. PERFORMED ENGINE OPS CHECKS AND NO BURNING ODOR WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: FLASHLIGHT — MELTED (CABIN) · airframe 23,945 hrs · 18,257 cycles

FLT 4154 EWR - CREW REPORTED A ELECTRICAL SMELL NEAR MAIN CABIN DOOR WITH OBSERVATION OF F/A FLASHLIGHT MELTED. EWR MX REMOVED AND REPLACED THE FWD F/A FLASHLIGHT AND CRADLE ASSY IAW EMB 145 AMM 33-50-16 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,932 hrs · 18,244 cycles

DURING SCHEDULED MAINTENANCE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX RESET SYSTEM AND OPERATIONALLY CHECKED THE LIGHT SUCCESSFULLY IAW EMB145 AMM 33-50-00-700-801A. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — WORN (NLG) · airframe 23,762 hrs · 18,122 cycles

CLE FLT 5850 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL, AND A ENGINE 1/2 REV DISAGREE MESSAGE DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE STRUT DEFLATED. DURING REPACK OF THE NOSE STRUT THE LEG STRUT WAS FOUND WORN. THE NOSE LEG STRUT ASSEMBLY WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 23,050 hrs · 17,560 cycles

AVP - FLT 6089 THE CREW REPORTED A LOUD BANGING NOISE FROM UNDER FIRST OFFICER'S FLOOR. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH AND THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,025 hrs · 17,535 cycles

MINOR CORROSION FWD AND AFT OF THE CARGO DOOR SILL. REMOVED CORROSION AND FOUND TO BE SERVICABLE IAW EC5330-01458 ALODINE, PRIMED AND PAINTED IAW EMB 135/145 CPM 51-21-04, 05&06.

Part: SWITCH — DEFECTIVE (BLEED AIR SYS) · airframe 20,492 hrs · 15,590 cycles

FLIGHT 2183 - EWR - FLIGHT CREW REPORTED BLEED NR 2 LOW TEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED NR PUSH BUTTON SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LINE — LEAKING (ANTI-ICE SYSTEM) · airframe 19,852 hrs · 15,098 cycles

TYS - A/C WAS EN ROUTE TO ATL FROM EWR WHEN A STAB ANTI ICE FAIL MESSAGE SHOWED. CREW DIVERTED TO TYS AND CHANGE PLANES AND CONTINUED. MAINTENANCE FOUND A LINE LEAKING GOING TO A PRESSURE SWITCH.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 19,688 hrs · 14,978 cycles

IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE OUTSIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,584 hrs · 14,905 cycles

FLIGHT 2603 - EWR - FLIGHT CREW REPORTED FUEL SMELL IN COCKPIT AFTER APU START. EWR MX PROCEEDED WITH APU OPERATIONAL CHECK BUT COULD NOT DUPLICATE ANY TYPE OF SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,581 hrs · 14,181 cycles

GSP - FLIGHT 2675 - THE FLIGHT ATTENDANT REPORTED THE PASSENGER READING LIGHT AT 18C STARTED SMOKING MIDWAY THROUGH THE FLIGHT AND WOULD NOT TURN OFF. THE FLIGHT ATTENDANT USED THE RESET SWITCH BUTTON, AND THE LIGHT EXTINGUISHED AND SMOKE STOPPED. THE AIRCRAFT CONTINUED TO GSP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED SEAT 18C READING LIGHT ON NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE PSU AT SEAT 18BC, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,480 hrs · 14,108 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,480 hrs · 14,108 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON LT OMEGA BEAM FACE AND FLANGE BETWEEN FRAMES 20-23 AND CRACKED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED AND COMPLETED REPAIR OF LT OMEGA BEAM BETWEEN FRAME 20-22 BY INSTALLING A BEAM SPLICE AT FRAME 19.5 TO FRAME 23 IAW EC5320-01229. INSTALLED OUTBOARD ANGLE AND T-BRACKET IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,480 hrs · 14,108 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR AT CENTER OMEGA BEAM FRAME 20 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (ZONE 500) · airframe 21,824 hrs · 13,921 cycles

SHV - DURING C-CK, LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 21,824 hrs · 13,921 cycles

SHV - DURING C-CK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 20 AND 23. REPAIRED OMEGA BEAM IAW EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (ZONE 600) · airframe 21,824 hrs · 13,921 cycles

SHV - DURING C-CK, RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 21,824 hrs · 13,921 cycles

SHV - DURING C-CK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 18,252 hrs · 13,921 cycles

SHV - DURING C-CHECK, FRAME 10 JUST ABOVE STR 10R CRACKED. REMOVED AND REPLACED FR 10 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · airframe 21,824 hrs · 13,921 cycles

SHV - DURING C-CK, CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (ZONE 500) · airframe 18,252 hrs · 13,921 cycles

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

Part: BRACKET — DAMAGED (ZONE 300) · airframe 18,252 hrs · 13,921 cycles

SHV - DURING C-CHECK, RUDDER 2 UPPER ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED RUDDER 2 UPPER HINGE BRACKET IAW SRM 55-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (CABIN) · airframe 17,366 hrs · 13,283 cycles

DURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: UPLOCK SWITCH — FAULTY (NLG)

CLE FLIGHT 2141 - THE CREW REPORTED A LOUD RUMBLING FROM THE NOSE GEAR WITH GEAR RETRACTED INDICATING UP AND LOCKED. THE CREW SUSPECTED THE GEAR DOORS WERE NOT CLOSED. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK SQUENCE SWITCH. OPERAITONAL CHECKS WERE GOOD. (A)

Part: BOLT — SHEARED (MLG STRUT) · airframe 16,171 hrs · 12,407 cycles

DURING INSTALLATION OF MAIN LANDING GEAR OLEO STRUT ASSEMBLY, LOWER ATTACHMENT BOLT SHEARED AT TORQUE BELOW 1200 IN LBS. RIC MX REMOVED AND REPLACED LOWER ATTACHMENT BOLT, APPLIED TORQUE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. (S)

Part: BOLT — SHEARED (MLG STRUT) · airframe 16,171 hrs · 12,407 cycles

DURING INSTALLATION OF MAIN LANDING GEAR OLEO STRUT ASSEMBLY, UPPER ATTACHMENT BOLT SHEARED AT TORQUE BELOW 1200 IN LBS. RIC MX REMOVED AND REPLACED UPPER ATTACHMENT BOLT, APPLIED TORQUE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. (S)

Part: FIRE LOOP — INOPERATIVE (LEFT NACELLE) · airframe 14,289 hrs · 11,141 cycles

IAH - FLIGHT 2713, THE CREW REPORTED THE ENGINE 1 FIRE DETECTOR FAIL CAUTION MESSAGE ON EICAS IN FLIGHT. THE CREW COMPLETED THE QRH WITH THE MESSAGE NOT CLEARING, AND NO OTHER ISSUES NOTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FIRE LOOP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — DEFECTIVE (TE FLAPS) · airframe 13,778 hrs · 10,778 cycles

FLT 2692 - EWR - CREW REPORTED FLAP FAIL & SPS ADVANCE MESSAGE IN FLIGHT. CREW DECLARED EMERGENCY. ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED FECU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 13,443 hrs · 10,531 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND CARGO DOOR CUTOUT WITH VARIOUS AREAS OF CORROSION AT LOWER SECTION. MAINTENANCE INSTALLED NEW LOWER SECTION AT CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02 & CPM 51-21-07. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 12,477 hrs · 9,805 cycles

EWR LOG SQUAWK FLT 2490 LAV SMOKE MESSAGE ON EICAS. REMOVED AND REPLACED SMOKE DETECTOR TEST PANEL IAW EMB145 CMM 26-14-01. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 11,662 hrs · 9,169 cycles

IAH - FLIGHT 2840, THE CREW REPORTED A LANDING GEAR AIR/GND WARNING DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR PROX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,189 hrs · 8,787 cycles

AMA - FLIGHT 2709, THE CREW REPORTED THAT THE FORWARD FACING EMERGENCY EXIT LIGHT AT ROW TWELVE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT WITH NO HELP, AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE RECONNECTED THE NEW LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG) · airframe 11,063 hrs · 8,688 cycles

IAH - FLIGHT 2524, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAILURE ON CLIMB PASSING 10,000 FEET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED AND RESECURED THE RIGHT HAND REAR PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (LANDING GEAR) · airframe 10,790 hrs · 8,471 cycles

EWR - CREW REPORTED, LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE LGEU OPS CHECKED GOOD IAW EMB145 NR 32-32-01. AIRCRAFT TEST FLOWN SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 10,763 hrs · 8,452 cycles

IAH - FLIGHT 2931, ON TAKEOFF, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,324 hrs · 8,105 cycles

STL - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHT AT THE OVERWING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,594 hrs · 7,523 cycles

BTR - FLIGHT 2818, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW 11 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — DAMAGED (APU) · airframe 8,723 hrs · 6,836 cycles

SHV - DURING C-CHECK, THE APU COWLING MATING SURFACE TO FUSELAGE (FIREWALL) HAS SEVERAL DAMAGED RIVETS AT 6 O'CLOCK POSITION. MAINTENANCE REPAIRED THE APU MATING SURFACE (FIREWALL) AT 6 O'CLOCK POSITION IAW EC5330-01496.

Part: FIREWALL — CRACKED (APU BAY) · airframe 8,723 hrs · 6,836 cycles

SHV - DURING C-CHECK MAINTENANCE, FOUND APU FIREWALL CRACKED AT 3 O'CLOCK POSITION AROUND RIVETS. MAINTENANCE REPAIRED APU FIREWALL AT 3 O'CLOCK POSITION IAW EC 5330-01496 DISPOSITION 2.0. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 7,852 hrs · 6,163 cycles

IAH - FLIGHT 2942, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW TWELVE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY LIGHT CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 7,289 hrs · 5,724 cycles

EWR - CO2514, CREW REPORTED, ON SHORT FINAL, AUTOPILOT DISCONNECTED, YAW DAMPENER FAIL, AND RUDDER SYSTEM NR 1 AND NR 2 FAIL INDICATION, CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. OPS CHECKED GOOD, REQUIRES SYSTEM TEST FLIGHT. FLEW AIRCRAFT AND FOUND TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — FAILED (EMERGENCY EXIT) · airframe 7,229 hrs · 5,676 cycles

CREW REPORTED, EMERGENCY EXIT [SIGN] LIGHT ON BULKHEAD IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT SIGN ASSEMBLY IAW EMB145 AMM 33-50-15, OPS CHECKED GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 6,246 hrs · 4,914 cycles

DURING SERVICE AND ROUTINE INSPECTION MAINTENANCE FOUND THE LT EMERGENCY LIGHT FORWARD LEADING EDGE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT)

DURING ROUTINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS NOT WORKING WHEN IN ARMED AND IN AUTO ESSENTIAL ELECTRICAL MODE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECKED GOOD IAW EMB 145 MM 33-50-00.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 5,281 hrs · 4,189 cycles

IAH - A/C 12540 WAS FOUND WITH AN INOP OVERWING EXIT LIGHT. MAINT REMOVED AND REPLACED THE LIGHT AND OPS CHECK WAS GOOD. A/C RELEASED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE BULB TO BE BURNED OUT. THE AFFECTED BULB WAS REPLACED AND THE DISCREPANCY CLEARED.

Part: CHARGER — FAULTY (EMERGENCY LIGHT)

DURING ROUTINE INSPECTION MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT AT THE COCKPIT ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM.

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLIGHT 2021, THE LEFT FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED LIGHT ASSEMBLY AND OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM.

Part: SKIN — DENTED (PAX DOOR) · airframe 4,106 hrs · 3,282 cycles

DURING A SCHEDULED INSPECTION THE PASSENGER ENTRY DOOR EXTERIOR SKIN WAS FOUND TO BE DENTED JUST AFT OF THE RELEASE HANDLE. MAINTENANCE RECONTOURED THE SKIN AND PERFORMED A NDT ON THE AFFECTED AREA WITH NO DISCREPANCIES NOTED, ALL WORK ACCOMPLISHED IAW EMB IC NR 2003-145/3275 AND CPM 51-21-04,05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,106 hrs · 3,282 cycles

DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04/05/06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SELECTOR — DEFECTIVE (TE FLAPS)

IAH FLIGHT 2584 THE CREW REPORTED A LANDING GEAR WARNING IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR HANDLE. OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — FAULTY · airframe 2,626 hrs · 2,045 cycles

EWR---CO2095, CREW REPORTED, " UPON TAKEOFF, GEAR HANDLE MOVED UP, GEAR CAME UP WITH AURAL WARNING. CONTINUOUSLY SOUNDED." AIRCRAFT AIRTURNED TO EWR. MAINTENANCE REMOVED AND REPLACED LANDING GEAR MODULE IAW EMB145 MM #32-32-02. SWUNG LANDING GEAR AND CLEANED UPLOCK SWITCHES. OPERATIONAL TEST OF LANDING GEAR GOOD IAW EMB145 MM #32-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAULTY (CABIN AREA) · airframe 2,611 hrs · 2,029 cycles

BTV---CO2002, CREW REPORTED, EMERGENCY LIGHT OVER SERVICE DOOR INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT SOCKET IAW EMB145 AMM #33-50-10. OPS.CHECKED GOOD.

Part: CONTACTOR

EWR FLIGHT#3764 THE CREW REPORTED WHILE IN FLIGHT DURING CROSS FEED OPERATION PUMP 1B INDICATED OFF.THE PUMP WORKED ON THE GROUND.MAINTENANCE INSPECTED AND REPLACED THE 1B FUEL PUMP CONTACTOR.OPERATIONAL CHECKS WERE GOOD.