N14939

Part: STARTER GEN — MALFUNCTIONED (TAIL) · airframe 32,364 hrs · 31,321 cycles

THE CREW REPORTED AN ELECTRICAL PROBLEM WITHTHE MAIN BUS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL SMELL CAME IN THE COCKPIT, AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING WITHOUT INCIDENT. MX INSPECTED COCKPIT POWER SUPPLIES WITH NO EVIDENCE OF SMOKE OR BURNING, AND FOUND THE APU GENERATOR AND GCU TO BE SENDING THE ACFT INTO ESSENTIAL POWER. MX R & R THE APU STARTER GENERATOR AND APU GCU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GCU — MALFUNCTIONED · airframe 32,364 hrs · 31,321 cycles

THE CREW REPORTED AN ELECTRICAL PROBLEM WITH THE MAIN BUSS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL ODOR CAME IN THE COCKPIT) AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING IN BPT WITHOUT INCIDENT. MX INSPECTED COCKPIT POWER SUPPLIES WITH NO EVIDENCE OF SMOKE OR BURNING, AND FOUND THE APU GENERATOR AND GCU TO BE SENDING THE ACFT INTO ESSENTIAL POWER. MX R & R THE APU STARTER GENERATOR AND APU GCU, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,121 hrs · 30,049 cycles

DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.

Part: CDU — SHORTED (COCKPIT) · airframe 29,138 hrs · 28,074 cycles

THE CREW REPORTED A STRONG ELECTRICAL ODOR FROM BEHIND THE CAPTAIN`S SEAT AREA. MX INSPECTED AND FOUND THE FMS, CMU TO BE CAUSING THE ODOR. MX R & R THE FMS CDU, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (NR 4 BRAKE) · airframe 28,995 hrs · 27,941 cycles

DURING TAKEOFF ROLL AT APPROX 90KTS, THE CREW REPORTED THAT THEY SMELLED SMOKE AND RECEIVED A BRAKE OVERHEAT MESSAGE. TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE WHERE MX INSPECTED THE ACFT R & R A FAULTY BRAKE TEMP SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 900) · corrosion level 2 · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK SERVICE DOOR THRESHOLD CORRODED AROUND NUTPLATES. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 75 STRINGER 3R-4R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 75 STRINGER 3R-4R IAW EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 5R-6R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 79 STRINGER 5R-6R IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK, WORKING RIVETS AT FRAME 77, STRINGER 4R-10R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 77, STRINGER 4R-10R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 6R-7R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 78, STRINGER 6R-7R IAW EC5330-02501 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 4R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501 ORIG. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,498 hrs · 27,455 cycles

DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 7R-8R. MX PERFORMED REPAIR OF FUSELAGE AT FRAME 78, STRINGER 7R-8R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 28,460 hrs · 27,418 cycles

IAH - FLIGHT 4664 THE CREW REPORTED THAT FUEL QUANTITY NR 1 DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY TESTED THE FUEL QUANTITY SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — BROKEN (STABILIZER) · airframe 27,747 hrs · 26,689 cycles

IAH - FLIGHT 2481, THE CREW REPORTED AN INFLIGHT ABNORMAL VIBRATION IN THE YOKE WHILE AIRBORNE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE SPRING TAB FAIRING BRACKET, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTY (AHARS) · airframe 27,451 hrs · 26,380 cycles

IAH - FLIGHT 3127, THE CREW REPORTED THAT AHRS NR 1 FAILED IN FLIGHT TWICE FOR 30 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — VIBRATION (NR 2) · airframe 27,244 hrs · 26,152 cycles

IAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 26,867 hrs · 25,761 cycles

FLIGHT 2967, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRIC BURNING ODOR AROUND ROW 5 OR 6. MAINTENANCE INSPECTED THE AIRCRAFT, FOUND A BAD LIGHT SOCKET AT ROW 5A LATERAL LIGHT. MAINTENANCE REMOVED THE BULB AND PLACED THE LIGHT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY AT ROW 5, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ECU — INOPERATIVE (TE FLAP) · airframe 25,212 hrs · 24,064 cycles

LCH - FLIGHT 2214, THE CREW REPORTED A FLAP FAIL DURING CRUISE. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (NACELLE YOKE) · airframe 24,487 hrs · 23,302 cycles

DURING C-CHECK, NR 1 ENG FWD LOWER YOKE FITTING CRACKED. REMOVED AND REPLACED FWD LOWER YOKE FITTING IAW EC5450-01021. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPLICE — BROKEN (EMERGENCY LIGHTS) · airframe 24,291 hrs · 23,081 cycles

IAH - DURING MAINTENANCE INSPECTION THE AFT SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BROKEN SPLICES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 24,058 hrs · 22,820 cycles

IAH - FLIGHT 2115 - DURING POST FLIGHT INSPECTION THE LEFT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 24,002 hrs · 22,755 cycles

EMERGENCY LIGHT IN THE MAIN DOOR AND THE SERVICE DOOR INOP. REMOVED AND REPLACED THE LIGHT SOCKETS IAW EMB AMM 33-50-06. OPS CHECK GOOD.

Part: FAN — INOPERATIVE (NR 1 AHRS) · airframe 23,898 hrs · 22,638 cycles

IAH - FLIGHT 3042, ON CLIMB, THE CREW REPORTED AN AHRS 1 OVERHEAT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 23,835 hrs · 22,573 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: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,829 hrs · 22,567 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAD CORROSION AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM WITH REPAIR AT FRAME 20 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 23,829 hrs · 22,567 cycles

SHV - DURING C-CHECK RT CARGO FRAME 64 HAD A DAMAGED RIVET BETWEEN STRINGER 8R-9R. MAINTENANCE REPAIRED FRAME 64 STRINGER 8R-9R WITH REPAIR IAW IC2009-145/03545. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,829 hrs · 22,567 cycles

SHV - DURING C-CHECK CARGO CUTOUT LOWER BEAM HAD CORROSION. MAINTENANCE REMOVED AND REPLACED CARGO LOWER BEAM AT FRAME 65-68 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,829 hrs · 22,567 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAD CORROSION AT NUT PLATE HOLES AT FRAME 20. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 20 IAW EC5320-01461. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 23,829 hrs · 22,567 cycles

SHV - DURING C-CHECK FRAME 10 JUST ABOVE STRINGER 10L WAS CRACKED AND PIECE MISSING. MAINTENANCE REMOVED AND REPLACED FRAME 10 STRINGER 10L IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,484 hrs · 22,213 cycles

NR 2 EMERGENCY LIGHT BATTERY LOW VOLTAGE. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,476 hrs · 22,205 cycles

IAH - FLIGHT 2931, DURING PREFLIGHT INSPECTION THE AISLE PATH EMERGENCY LIGHT STRIP BY THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS NOTED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMER BRK HANDLE) · airframe 22,473 hrs · 21,183 cycles

IAH - FLIGHT 3056 ON TAKEOFF ROLL THE CREW REPORTED SEEING HOT EMBERS AND DETECTING SMOKE FROM UNDER THE CAPTAINS DASH, WITH THE CIRCUIT BREAKER ON THE OVERHEAD POPPING. THE CREW ABORTED TAKEOFF, AND TAXIED BACK TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY BRAKE HANDLE PANEL LIGHT, REPAIRED SEVERAL BURNT WIRES UNDER CAPTS DASH, OPERATIONALLY CHECKED SYSTEMS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 21,831 hrs · 20,557 cycles

IAH - FLIGHT 2106, THE CREW REPORTED A LOUD BANGING NOISE UNDER THE FLIGHT COMPARTMENT FLOOR, AND THAT THE RIGHT MAIN LANDING GEAR INDICATION CYCLING BETWEEN UP AND AMBER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 21,705 hrs · 20,430 cycles

IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT LOCATED ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FUSE FROM THE NUMBER TWO BATTERY PACK POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 21,695 hrs

TYS - DURING A CURRENT 5A INSPECTION THE RT WING UPPER SKIN I/B GROUND SPOILER WAS FOUND CRACKED. MAINTENANCE REMOVED THE DAMAGED SKIN, FABRICATED A FILLER, THE DOUBLER TRIPLED DRILL AND COUNTERSUNK. ALODINED, PRIMED AND INSTALLED IAW EC5740-01141. RESTORED TO THE ORIGINAL FINISH. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 21,410 hrs · 20,126 cycles

IAH - FLIGHT 2203, THE CREW REPORTED THAT THE LEFT MAIN GEAR COMES DOWN MUCH FASTER THAN NOSE OR RIGHT GEAR CAUSING YAW. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY CHECKED THE LANDING GEAR EXTENSION & RETRACTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (BRAKES) · airframe 20,082 hrs · 18,722 cycles

FLT 2489 - EWR - CREW REPORTED OB BRAKE INOP MSG ON EICAS AND DECLARED EMERGENCY. ACFT LANDED WITHOUT INCIDENTS. EWR MX REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,458 hrs · 18,046 cycles

DURING SCHEDULED MAINTENANCE THE PASSENGER DOOR EMERGENCY LIGHT DID NOT ILLUMINATE. THE AFFECTED EMERGENCY LIGHT WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,269 hrs · 17,842 cycles

SHV - DURING C-CHECK, FS 23 LT OMEGA BEAM I/B L-FLANGE HAS AREA WITH CORROSION. MAINTENANCE REPAIRED LT OMEGA BEAM I/B L-FLANGE FR 23 IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,922 hrs · 17,448 cycles

EWR LOG SQUAWK SECOND EMERGENCY LIGHT STRIP ON FLOOR OUT. REMOVED AND REPLACED SECOND EMERGENCY LIGHT STRIP ON FLOOR IAW EMB145 AMM 33-50-08. OPS CHECK GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 18,720 hrs · 17,238 cycles

CLE FLIGHT NR 3176, THE CREW REPORTED EMERGENCY AISLE PATH LIGHTS INOP ON ROWS 1 AND 2. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 2. OPS CHECKS REPORTED GOOD.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 18,567 hrs · 10,483 cycles

DURING CRUISE, AC WILL NOT PRESSURIZE NEITHER AUTO NOR MANUAL MODE. AC DIVERTED TO RIC. RIC MX REMOVED AND REPLACED DIGITAL CONTROLLER. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — BURNED OUT (PITOT TUBE) · airframe 17,909 hrs · 16,325 cycles

DAL - FLIGHT 3167, DURING FLIGHT THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN WITH A PITOT 3 INOP MESSAGE. THE AIRCRAFT RETURNED TO DAL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSOR AND SOCKET FOR THE NUMBER THREE PITOT TUBE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,489 hrs · 15,822 cycles

SKIN ON POST BETWEEN CAPTAINS WINDSHIELD AND LT DV WINDOW HAS A CRACK. REMOVED DAMAGED SKIN, PERFORMED NDI ON UNDERLYING STRUCTURE. NO DEFECTS NOTED. FABRICATED A FILLER, EXTERNAL DOUBLER AND SHIMS. ALODINED, PRIMED AND PAINTED. PERFORMED PRESSURE CHECK AND CHECKED GOOD. ALL WORK PERFORMED IAW CONTINENTAL EXPRESS EC5310-01367, EMB IC2006-145/1088A AND CPM 51-21-04,05,06. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,464 hrs · 15,796 cycles

IAH - DURING MAINTENANCE INSPECTION, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 15,458 hrs · 13,527 cycles

THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE AFFECTED LIGHT, OPS CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED AND NO TIMES/CYCLES ARE AVAILABLE.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 15,427 hrs · 13,487 cycles

CRP - MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED.

Part: LAMP — BURNED OUT (GALLEY) · airframe 15,419 hrs · 13,475 cycles

IAH - CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENENCE RELAMPED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED.

Part: LAMP — BURNED OUT (GALLEY) · airframe 15,415 hrs · 13,469 cycles

IAH - CREW REPORTED THAT THE BACKLIGHTING IN THE EMERGENCY EXIT LIGHT OVER THE GALLEY DOOR WAS INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART IS NOT SERIALIZED & HAS NO S/N).

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 15,415 hrs · 13,469 cycles

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT ASSEMBLY, OPS CK WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE - THIS PART IS NOT SERIALIZED, AND IS NOT TRACKED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 15,353 hrs · 13,397 cycles

DURING C-CHECK THE LEFT AND RIGHT FRAME 65 AND FRAME 68 SHEAR CLIPS WERE FOUND CORRODED. REPAIRED IAW SRM 51-30-01 AND IC2004-145/5946. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (LT AILERON) · airframe 15,353 hrs · 13,397 cycles

DURING 4C INSPECTION, FOUND THE LEFT AILERON LEADING EDGE DENTED BEYOND LIMITS. REPAIRED IAW EC5750-01233. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 15,158 hrs · 13,187 cycles

FLIGHT NR 2805, THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. SIR REMAINS OPEN PENDING ADDITIONAL INFORMATION

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,098 hrs · 13,121 cycles

CREW REPORTED EMERGENCY SIGN ABOVE ROW 12 LEFT SIDE INOPERATIVE. REPLACED THE NUMBER 4 INVERTED. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,912 hrs · 12,917 cycles

DURING PREFLIGHT FOR FLIGHT 2180 OUT OF CLE THE CREW DISCOVERED THE GALLEY EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN BULBS AND IT OPERATED PROPERLY. FLIGHT 2180 CONTINUED WITHOUT FURTHER INCIDENT.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 14,771 hrs · 12,773 cycles

CLE FLIGHT NR 2153, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR IS INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOOSE CONNECTION ON THE EMERGENCY LIGHT. MAINTENANCE RESECURED THE CONNECTION. ALL OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — BURNED OUT (EMERGENCY EXIT) · airframe 14,593 hrs · 1,358 cycles

DURING 5A INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT SIGN OVER SERVICE DOOR, NOT OPERATING. REMOVED AND REPLACED EMERGENCY EXIT SIGN LIGHT OVER SERVICE DOOR IAW AMM NR 33-50-06. OPS. CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,697 hrs · 11,640 cycles

SHV-THE EMERGENCY EXIT SIGN WAS FOUND TO OPERATE INTERMITENTLY. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY SIGN INVERTER IAW MFG AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THAT THE CABIN EMERGENCY EXIT SIGN WAS INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

CREW REPORTED, EMERGENCY EXIT SIGN IN FORWARD CABIN NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN IN FORWARD CABIN IAW EMB145 MM 33-50-01. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 2498 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE ON THE BULKHEAD IN FRONT OF SEAT 3B. MAINTENANCE INSPECTED AND RESECURED A LOOSE CONNECTOR ON EMERGENCY LIGHT INVERTER NR 3, OPERATIONAL CHECKS WERE GOOD.

Part: PUMP — FAILED (#2 ENGINE)

CLE FLIGHT#2257 THE CREW REPORTED #2 HYDRAULIC SYSTEM FAILED ON APPROACH INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE DRIVEN HYDRAULIC PUMP.OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN)

BNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE JNOPERATIVE. BNA- MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT BATTERY. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

BNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY BATTERY,PERFORMED A OPERAIO9NAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — LEAKING (WING ROOT)

IAH- FLIGHT 3498, THE CREW NOTED THAT #2 BLEED LEAK INFLIGHT,(FOLLOWED QRH, MX CONTROL ADVISED RETURN TO IAH), THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SECURED RIGHT WING ANTI ICE VALVE SENSOR LINE,PERFORMED A LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, A GOUGE WAS FOUND ON FRAME 63 BETWEEM STRINGERS 6 AND 8. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, A GOUGE WAS FOUND ON FRAME 64 BETWEEM STRINGERS 6R AND 8R. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.

Part: STRUCTURE — GOUGED (NR 1 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK NR 1 ENG LOWER NACELLE WAS FOUND TO HAVE A GOUGE AT FORWARD OUTBOARD ATTACHEMENT. MAITENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED EDGE MEMBER IAW EMB 145 SRM54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (LAVARATORY) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV-DURING C CHECK LAVARATORY'S FLOOR BEAMS WERE FOUND WITH CORROSION BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, BUTT STRAP RT OF CENTER FLOORBEAM AT FRAME 18 WAS FOUND TO HAVE CORROSION ANROUND NUTPLATE HOLES. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-0179. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FAIRING — CRACKED (APU INLET) · airframe 11,325 hrs · 9,271 cycles

SHV- DURING C CHECK, RT FAIRING ON APU FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED RT FAIRING IAW CONTINENTAL EXPRESS EC 5350-01032. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV- DURING C CHECK LT FLOORBEAM FOWARD OF FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (NR 2 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK NR 2 ENGINE LOWER NACELLE DISH AROUND INTERIOR OF ENGINE DRAIN WAS FOUND TO HAVE A GOUGE. MAINTENANCE REMOVED AND REPLACED DISH IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV- DURING C CHECK, LT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV-DURING C CHECK SUPPORT RAMP ON CENTER FLOORBEAM BETWEEN FRAME 18 AND FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV-DURING C CHECK THE CENTER FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, SUPPORT UNDER PASSENGER DOOR THRESHOLD WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED SUPPORT IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.

Part: STIFFENER — WORN (NR 2 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK NR 2 LOWER ENGINE NACELLE HAD WEAR MARKS 12 INCHES INBOARD OF CENTER. MAITENANCE REMOVED DAMAGE AREA AND PEFORMED AN ANGLE REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,325 hrs · 9,271 cycles

SHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAITENANCE REMOVED AND REPLACED AFFECTED FLOORBEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RIB — GOUGED (NR 2 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK INSPECTION, NR 2 ENGINE LOWER NACELLE OUTBOARD RIB WAS FOUND TO HAVE A GOUGE APPROXIMATE 4 INCHES AFT OF AFT HINGE. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RIB — GOUGED (NR2 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, NR 2 ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON THIRD RIB PLATE FROM THE END. MAINTENANCE REMOVED DAMAGE AND REPAIRED RIB PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NR 1 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK, NR 1 ENGINE TOP NACELLE AFT STIFFENER 10 INCHES INBOARD OF CENTER WAS FOUND TO HAVE A GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NR 2 ENG NACELLE) · airframe 11,325 hrs · 9,271 cycles

DURING C CHECK INSPECTION, NR 2 LOWER ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON AFT STIFFENER NEAR CENTER. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — GOUGED · airframe 11,325 hrs · 9,271 cycles

SHV-DURING C CHECK #1 ENGINE LOWER COWLING WAS FOUND TO HAVE A GOUGE ON INERIOR SKIN 24 INCHES AFT CENTER OF COWLING. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — DEFECTIVE (RIGHT ENGINE)

CLE FLIGHT#3397 THE CREW REPORTED #2 ENGINE EXCEEDED THE LIMITS FOR OIL TEMPERATURE WHILE CLIMBING THRU 5000'.POWER WAS REDUCED AND THE TEMPERATURE RETURNED TO NORMAL.THE OIL TEMPERATURE EXCEEDED LIMITS AGAIN A FEW MINUTES LATER AND THE ENGINE WAS SHUTDOWN FOR PRECAUTIONARY PURPOSES.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 OIL TEMPERATURE SENSOR.OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — FAULTY

BTV---CO3398, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT OVERHEAD AISLE EMERGENCY LIGHT TO BE INOPERATIVE.....REMOVED AND REPLACED THE LAMP IN THE AISLE OVERHEAD EMERGENCY LIGHT. OPS.CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT 3223 THE CREW REPORTED THE EXIT LIGHT SIGN ON THE RIGHT SIDE BULKHEAD WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — STICKING (APU)

CLE FLIGHT# 3020 THE CREW REPORTED A STRONG FUEL SMELL WHEN THE APU WAS STARTED ON THE GROUND.MAINTENANCE INSPECTED AND REPLACED THE APU COMBUSTION DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE.MAINTENANCE REPLACED EMERGENCY EXIT LIGHT BULB.OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — LACK OF LUBE (EMERGENCY EXIT)

DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT DOOR DID NOT INDICATE A OPEN MESSAGE ON THE EICAS WHEN THE DOOR WAS OPEN. MAINTENANCE INSPECTED AND FOUND THE MICROSWITCH ACTUATION PIN TO BE STICKING. THE PIN WAS LUBRICATED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — DIRTY (LANDING GEAR) · airframe 9,385 hrs · 7,435 cycles

EWR---CO4143 CREW REPORTED LANDING GEAR INDICATION DISAGREEMENT. AFTER TROUBLESHOOTING PROBLEM, MAINTENANCE CLEANED LANDING GEAR PROXIMITY SWITCHES IAW EMB145 MM CHAPTER 32-61-00. AIRCRAFT TEST FLOWN SATISFACTORY AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3638 THE CREW REPORTED EMERGENCY LIGHT AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLT 4270 THE CREW REPORTED FORWARD PART OF ROW 12 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT#3489 THE CREW REPORTED THE EMERGENCY LIGHTS OVERWING AT EXIT ROW 12 WERE INOPERATIVE.MAINTENANCE APPLIED POWER TO THE AIRCRAFT TO CHARGE THE EMERGENCY BATTERY PACKS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLT 3680 THE CREW REPORTED EMERGENCY LIGHT ABOVE ROW 11 AND 12 NOT ILLUMINATING ON TEST. MAINTENANCE REPLACED LAMP. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY LIGHT ABOVE ROW 11 AND 12 FAILED TO ILLUMINATE. CLE- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BULB, PERFORMED A OPERATIONAL CHECK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT 3882, THE CREW REPORTED THE EMERGENCY EXIT SIGN AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESEATED THE CANNON PLUG ON THE INVERTER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLIGHT 4230, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — MISSING (FIRE EXTINGUISH)

EWR - FLT 4142 - DURING RON CHECK, MAINTENANCE FOUND WATER BOTTLE FIRE EXTINGUISHER MISSING DATA PLAT ON BOTTLE. REMOVED AND REPLACED BOTTLE WITH SERVICEABLE UNIT. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, MAINTENANCE FOUND THE TWO AFT CABIN CEILING EMERGENCY AISLE PATH LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM GUSSET STRAP WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF GUSSET STRAP IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTACTOR — BURNED (COCKPIT)

IAH-CREW REPORTED SMOKE IN COCKPIT AFTER ATTEMPTING TO START THE APU, A/C LANDED AT IAH WITHOUT INCIDENT. MX INSPECTED THE A/C AND FOUND THE APU START CONTACTOR TO HAVE A MELTED LUG AND HEAT DAMAGE TO THE BUSS BAR AND LINE CONTACTOR. MX REMOVED/REPLACED THE AFFECTED START CONTACTOR, BUSS BAR, AND LINE CONTACTOR, OPERATIONALLY CHECKED A/C, AND APPROVED FOR RETRURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

PWM - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ON THE FORWARD PARTITION WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SIGN — INOPERATIVE (CABIN)

IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERHEAD EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EXIT SIGN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: DOOR SEAL — TORN (PAX DOOR)

CVG-EWR - FLT 4226 - AFTER TAKEOFF, THE AIRCRAFT PRESSURIZATION SYSTEM WENT INOPERATIVE. THE AIRCRAFT DIVERTED INTO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPAIRED SERVICE DOOR SEAL IAW EMB 145 MM 52-00-00. MAINTENANCE ALSO RERACKED THE CABIN PRESSURE ACQUISITION MODULE AND PERFORMED TEST IAW 21-32-01. THAE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, CREW REPORTED A CEILING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: SENSOR — CRACKED (RT MLG)

CLE - FLT 4053 - THE CREW REPORTED THAT ON TAKEOFF ROLL, RECEIVED NR 1 THRUST REVERSER DISAGREE MESSAGE ALONG WITH A SPOILER OPEN MESSAGE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT NR 2 WOW PROXIMITY SENSOR IAW EMB-145 MM 32-63-01. MAINTENANCE ALSO REPAIRED RIGHT OUTBOARD HUB CAP WHEEL SPEED TRANSDUCER DRIVE CLIP. PERFORMED OPERATINOAL CHECKS OF N1 THRUST REVERSER IAW 78-31-01. OPERATIONAL CHECKS OF THE SPOILERS WERE DONE IAW 27-62-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: ENGINE — MAKING METAL (RIGHT)

TYS - DURING A SCHEDULED INSPECTION THE RIGHT ENGINE WAS FOUND TO BE MAKING METAL BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SEAT TRACK — WORN (COCKPIT)

IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICERS SIDE INBOARD SEAT TRACK WAS FOUND TO BE WORN AROUND THE LOCKING HOLES. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB145 MM 53-01-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (FRAME 15-19)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP BETWEEN FRAMES 15 AND 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REPAIR DOUBLERS IAW EMBRAER REPAIR DRAWING SST1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD LEFT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTIN, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD RIGHT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FRAME 29)

IAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED UNDER THE COMPOSITE FLOOR PANEL SUPPORT AT FRAME 29. MAINTENANCE REMOVED THE DAMAGED SECTION AND INSTALLED A REPAIR DOUBLER IAW EMB145 REPAIR DRAWING SST-1274/99 AND EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

BTV - DURING SERVIEC CHECK, MAINTENANCE FOUND BAGGAGE SMOKE DETECTOR INOPERATIVE ON THE GROUND. REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. OPS CHECK GOOD. (M)

Part: CONTROL MODULE — INOPERATIVE (CABIN)

BTV - CREW REPORTED EMERGENCY LIGHTS WOULD NOT TEST FROM FLIGHT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL MODULE AND OPS CHECK EMERGENCY LIGHTS GOOD. (M)

Part: VALVE — LEAKING (RT WING)

BDL-CLE - FLT 4035 - EN ROUTE REPORTED LOSING 600 LBS OF FUEL IN 30 MINUTES. FLIGHT DIVERTED INTO BUF. MAINTENANCE DISPATCHED AND FOUND A LEAKING FUEL VENT VALVE ON RT SIDE. REMOVED AND REPLACED UNIT AND RETURNED A/C TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (E/E COMPT)

IAH - FLT 4151 - DURING FLIGHT, CREW REPORTED A LANDING GEAR DISAGREEMENT INDICATION. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS APPROVED FOR RETURN TO SERVICE. (X)