N17928

Part: ACM — FAILED (NR 1) · airframe 33,784 hrs · 32,233 cycles

THE CREW REPORTED A STRONG ELECTRICAL ODOR AS NR 1 PACK WAS RUNNING, AND ODOR STOPPED WHEN NR 1 PACK TURNED OFF. ACFT LANDED WITHOUT INCIDENT. MAINTENNACE INSPECTED AND FOUND NR 1 ACM FROZEN. R & R NR 1 ACM, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (ZONE 600) · airframe 33,766 hrs · 32,215 cycles

AIRCRAFT IS IN C-CHECK WHEN INSPECTION FOUND THE RT GROUND SPOILER INBD HINGE FITTING AT THE WING SPAR AREA INBD/OTBD BUSHIONS MIGRATED AND OBLONG THE FITTING. MAINTENANCE R & R THE THE RT GROUND SPOILER FITTING IAW AMM 20-10-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,760 hrs · 31,230 cycles

DURING MX INSPECTION THE AISLE PATH LIGHTING AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,935 hrs · 30,412 cycles

DURING SCHEDULED MX, THE PASSENGER DOOR BOTTOM EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.

Part: FIREWALL — CRACKED (APU BAY) · airframe 31,549 hrs · 30,031 cycles

DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 1.25" TOTAL LENGTH AT THE 9 O'CLOCK POSITION WITH A RIVET IN THE MIDDLE. MAINTENANCE PEFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,549 hrs · 30,031 cycles

SUPPLEMENTAL, DURING A-CHECK INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 5 SEPARATE CRACKS AT 3 DIFFERENT RIVETS AT FRAME 75. THESE INCLUDE 2 CRACKS MEASURING .07" AND .25" ON EITHER SIDE OF 1 RIVET DIRECTLY ABOVE STRINGER 2 LT, 2 CRACKS MEASURING .15" AFT AND .11" 45 DEGREE ANGLE AFT OF RIVET DIRECTLY BELOW STRINGER 2 LT, AND 1 CRACK MEASURING .11" EXTENDING AFT OF THE SECOND RIVET BELOW STRINGER 2 LT AT AN APPROXIMATE 60 DEGREE ANGLE. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR, AND THAT ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 21,488 hrs · 29,969 cycles

DURING A-CHECK INSPECTION, THE PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX RESECURED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — BURNED (ZONE 100) · airframe 29,879 hrs · 28,356 cycles

DURING PREFLIGHT, THE CREW REPORTED A BURNING ODOR FROM THE COAT CLOSET. MX INSPECTED THE ACFT AND R & R RELAY K0454, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — WEAK (ZONE 700) · airframe 29,321 hrs · 27,815 cycles

DURING CLIMB THE CREW REPORTED THAT THE RIGHT MLG WOULD NOT LOCK IN THE UP POSITION. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACED THE RT MAIN GEAR MANUEVERING ACTUATOR, PERFORMED OPS TESTS AND CLEARED THE DISCREPANCY.

Part: DOOR FRAME — CORRODED (CABIN DOOR) · corrosion level 2 · airframe 28,198 hrs · 26,909 cycles

SHV - DURING C-CHECK THE BOTTOM FRAME OF THE MAIN CABIN DOOR WAS FOUND TO BE CORRODED AROUND THE DOOR LINING MOUNT NUT PLATES. MAINTNENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 28,737 hrs · 27,211 cycles

IAH - FLIGHT 2705 THE CREW REPORTED AN AIR/GRND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN LIGHTS) · airframe 28,725 hrs · 27,197 cycles

DURING MAINTENANCE INSPECTION, AN ELECTRICAL ODOR WAS NOTICED IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIDEWALL LIGHT HARNESS AT SEAT 10BC TO BE BURNED. MAINTENANCE DISCONNECTED THE LIGHT AND PLACED IT ON MEL 33-20-00-1 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENNACE REMOVED AND REPLACED THE AFFECTED HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,800 hrs · 26,257 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IN THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 27,429 hrs · 25,885 cycles

FLIGHT 2719, REPORTED A PROMINENT TURBINE CASE OIL BURNED ODOR DURING ALL PHASES OF FLT. ACFT LANDED WHERE MX INSPECTED AND PLACED NR 1 PACK ON MEL, AND AIRCRAFT RETURNED TO SERVICE. MX REMOVED AND REPLACED THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 26,951 hrs · 25,369 cycles

IAH - FLIGHT 2163, THE CREW REPORTED A MAIN BATTERY TWO OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,592 hrs · 25,010 cycles

IAH - DURING MAINTENANCE INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 72 & 73 AT STRINGER 21R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN PANEL, OPERATIONAL CHECKS COMPLETED WITHOUT DEFECT. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 26,474 hrs · 24,890 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT UPPER WING SKIN WAS FOUND TOP BE CRACKED AT THE SPEED BRAKE CENTER HINGE POINT CUTOUT. MAINTENANCE PLACED THE ITEM ON DEFERRED MAINTENANCE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSTALLED A TRIPLER REPAIR, CLEARED THE DEFERRAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,773 hrs · 24,161 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT TOP LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 24,509 hrs · 22,768 cycles

DURING ROUTINE INSP, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 24,542 hrs · 22,802 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 23,169 hrs · 21,417 cycles

IAH - DURING A-CK INSPECTION THE LT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: BALLAST — FAULTY (LAVATORY LIGHT) · airframe 22,917 hrs · 21,176 cycles

CLE FLIGHT NR 2401, THE CREW REPORTED A STRONG BURNING SMELL COMING FROM THE LAVATORY. MAINTENANCE INSPECTED AND REPLACED THE LAV LIGHT BALLAST.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 21,380 hrs · 19,647 cycles

DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED THE WIRE AT THE EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 20,343 hrs · 18,612 cycles

CMH FLIGHT 2930 THE CREW REPORTED THE COFFEE POT WAS SMOKING WHEN TURNED ON.THE COFFEE POT WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT BREWER.OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — BURNED (TEMP) · airframe 20,036 hrs · 18,288 cycles

CLE FLIGHT NR 2676, THE CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN DURING ICE CONDITIONS THROUGHOUT DESCENT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BURNED ON THE CAPTAINS WINDSHIELD TEMP CONTROLLER. THE TEMP CONTROLLER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,765 hrs · 17,970 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,765 hrs · 17,970 cycles

SHV - DURING C-CHECK THE SERVICE DOOR AFT FRAME 22 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLE, BETWEEN STR 15R AND 16R. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,510 hrs · 17,694 cycles

DURING ROUTINE MAINTENANCE THE LT FRONT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR1 EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — FAULTY (EXTERIOR) · airframe 19,470 hrs · 17,653 cycles

DURING ROUTINE MAINTENANCE THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — BURNED (CABIN) · airframe 18,773 hrs · 16,901 cycles

CLE FLIGHT 3156 THE CREW REPORTED A ELECTRICAL BURNING SMELL IN THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BALLAST AT ROW 18. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,574 hrs · 16,687 cycles

IAH - DURING 3A INSPECTION THE RIGHT HAND INTERIOR EMERGENCY EXIT LIGHT BY THE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (VERTICAL STAB) · airframe 16,313 hrs · 14,516 cycles

TYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRICATED AND INSTALLED DOUBLERS, (4 ON EACH SIDE) I/A/W-EC5510-01109, EMB145-SRM-51-40-02, IC2005-145/1502-A AND IC2005-145/0620.

Part: SPAR — CRACKED (WING) · airframe 16,282 hrs · 14,156 cycles

TYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAULTY (NR 2 PACK) · airframe 16,127 hrs · 13,998 cycles

CLE - THE CREW REPORTED IN FLIGHT, IN ICING HAD A VERY HOT RUBBER SMELL AND PACK 2 AIR WAS VERY HOT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PACK DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: NOISE ATTENUATOR — RUPTURED (RECIRC FAN) · airframe 16,000 hrs · 13,865 cycles

DURING APPROACH THE CREW REPORTED A BURNING PLASTIC SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUPTURED NR 2 RECIRCULATION FAN NOISE ATTENUATOR. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE — DETECTED (CABIN) · airframe 15,880 hrs · 13,745 cycles

CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF THE APU AND ENGINES WITH THE BLEED AND PACKS ON. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTERSUNK FLOOR SILL ALLODINED AND INSTALL IAW 135/145 SRM 51-40-02;51-40-06 AND CPM 51-21-04.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPLACED THE STEP UP BRACKET AND CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL 4C WORK.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FLOORBOARD SILL ON THE LT SIDE AT FR 53-58. REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE COMPLETION OF THE 4C INSPECTION.

Part: SUPPORT BEAM — CORRODED (GALLEY) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT. REMOVED AND REPLACED ALL TOP CAPS IN THE GALLEY AREA IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 4C INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 4C INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FR 25. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FR 22 AND FR 25. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-40-02 AND WILL BE RELEASED UPON COMPLETION OF ALL 4C WORK.

Part: SUPPORT — CORRODED (FLOOR SILL) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 23 TO 30. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 61 TO FRAME 65. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 51-40-02, 53-21-10,51-40-06, 51-20-03, AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE FLOORBOARD SUPPORT FROM LAV TO CARGO. MAINT. REMOVED AND REPLACED THE SUPPORT FROM THE LAV TO THE CARGO IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FWD SERVICE DOOR SILL. MAINT. REMOVED AND REPLACED THE FWD DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL, BE REL. UPON COMPLETION OF ALL 4C WORK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION THE CENTER OMEGA BEAM UNDER THE LAV FLOOR WAS CORRODED. MAINTENANCE CLEANED UP THE DAMAGE AREA, BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02;03 AND CPM 51-21-04 AND 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF THE 4C INSPECTION.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

TYS DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON PAX DOOR THRESHOLD. MAINT REMOVED AND REPLACED PAX DOOR FWD AND AFT SILLS IAW EMB 135/145 SRM 51-40-02.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. AT THE COMPLETION OF THE 4C INSPECTION.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION,CORROSION WAS FOUND ON THE AFT SERVICE DOOR SILL. MAINT REMOVED AND REPLACED THE AFT DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C WORK.

Part: CAP — CORRODED (LAVATORY) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RIVETS AT THE CENTER LAV TOP CAP. MAINT REMOVED AND REPLACED THE LAV TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 25. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 61-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 29. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PLATE — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

DURING A SCHEDULED 4C INSPECTION AT FR 59 STR 19R,THE WATER SERVICE BASE PLATE, CORROSION WAS FOUND ON THE RIVETS. MAINTENANCE CLEANED THE EFFECTED AREA, BLENDED, ALLODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITOR COMPOUND. ALL WORK WAS ACCOMPLISHED IAW CPM 51-01-00; SRM 51-10-03;04;05 AND CPM 51-61-00. A/C WILL BE RELEASED UPON COMPLETION OF THE 4C INSPECTION.

Part: ATTACH BRACKET — BENT (CARGO DOOR) · airframe 15,407 hrs · 13,240 cycles

DURING A 4C INSPECTION THE CARGO DOOR RAMP ANGLE SUPPORTS AT FR.66 AND FR.67 WERE FOUND BENT. MAINT. REMOVED AND REPLACED THE CARGO DOOR RAMP ANGLE SUPPORTS IAW SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,407 hrs · 13,240 cycles

TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SILL AT FRAME 18. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB SRM 51-60-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG)

IAH - FLIGHT 2891 DURING CLIMBOUT OF LCH THE CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (LT MLG)

FLIGHT 2072 - PILOT REPORTED THAT THE MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX. THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM WAS OPERATIONALLY TESTED GOOD AND THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,398 hrs · 12,002 cycles

DURING 2A INSPECTION MAINTENANCE FOUND THE CABIN ENTRANCE DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LAMP IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD.

Part: SENSOR — FAULTY (CARGO BAY) · airframe 14,289 hrs · 11,901 cycles

CREW REPORTED, MASTER WARNING AND LAVATORY SMOKE INDICATION ON EICAS. AIR RETURNED TO EWR, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR SENSOR (PART NUMBER: FDS765A-2 SERIAL NUMBER: 203574) IAW EMB145 AMM 26-14-01. REMOVED AND REPLACED SMOKE DETECTOR PANEL FORWARD GALLEY (PART NUMBER: FAU751A-4 SERIAL NUMBER: 042797) IAW EMB145 AMM 26-14-02, RAN BOTH ENGINES TO TAKEOFF POWER FOR FIVE MINUTES OPS CHECKED GOOD, LAVATORY SMOKE DETECTION SYSTEM OPS CHECKED GOOD IAW EMB145 AMM 26-14-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

GSP---CO2600, CREW, DURING PREFLIGHT, NOTED EMERGENCY AISLE PATH LIGHTS AT ROW 7-12 ARE INOPERATIVE. CLT MAINTENANCE WENT TO GSP AND REMOVED AND REPLACED THE EMERGENCY BATTERY SUPPLY CHARGER ASSEMBLY, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2101 THE CREW REPORTED HALF OF THE EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED NR 2 AND NR 3 EMERGENCY AISLE PATH LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — CONTAMINATED (NOSE GEAR)

CLE FLIGHT#2408 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FOLLOWED BY ENGINE 1-2 REV. DISAGREE.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR AIR/GROUND PROXIMITY SWITCH.THE NOSE STRUT WAS ALSO SERVICED TO PROPER LIMITS.OPERATIONAL CHECKS WERE GOOD.

Part: HARNESS — SHORTED (NR 1 ENGINE) · airframe 12,646 hrs · 10,297 cycles

CREW REPORTED NR 1 ENGINE UNCOMMANDED SHUTDOWN ON APPROACH TO SYR, CONTINUED INTO SYR, LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED NR 1B FADEC ENGINE HARNESS IAW RR AE3007 MM #71-00-00 AND REMOVED AND REPLACED FADEC NR 1B DUE TO SHORT IN HARNESS AND DAMAGE TO FADEC #1B IAW EMB145 MM #73-22-01. OPERATIONAL CHECKED ENGINE AND AIRCRAFT GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CLOSED.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 12,107 hrs · 9,782 cycles

CREW REPORTED, "GEAR NOT RETRACTING." MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND LANDING GEAR CONTROL LEVER IAW EMB145 AMM 32-32-01 AND 32-32-02. OPERATIONAL CHECKED SYSTEM GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: UPLOCK — FAULTY (RT MLG)

IAH- DURING A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM THE MECHANIC NOTED THAT THE RIGHT HAND MLG WAS NOT SHOWING THE CORRECT INDICATION UPON RETRACTION. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MLG UPLOCK BOX, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

IAH- AFTER TAKEOFF THE LEFT MAIN LANDING GEAR, LANDING GEAR DISAGREE MESSAGE APPEARED, THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 11,473 hrs · 9,155 cycles

SHV - DURING C-CHECK INSPECTION, THE NUMBER THREE EMERGENCY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES.

Part: SPRING — CORRODED (T/E FLAP) · corrosion level 2 · airframe 11,473 hrs · 9,155 cycles

SHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD AND OUTBOARD LOWER FLAP SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPRING — CORRODED · corrosion level 2 · airframe 11,473 hrs · 9,155 cycles

SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND INBOARD AND OUTBOARD FLAP LOWER SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COWLING — CRACKED (APU COWLING) · airframe 11,473 hrs · 9,155 cycles

SHV - DURING C-CHECK INSPECTION, THE LOWER RIGHT HAND APU COWLING MOUNT OPENING WAS FOUNDS TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK, AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (TAIL)

DURING APPROACH FLIGHT 3649, THE CREW NOTED THAT THE APU FAILED ON APPROACH/STRONG FUEL ODOR IN CABIN AND COCKPIT. IAH- MAINTENANCE INSPECTED THE APU, AND, THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATINAL CHECK OF THE APU, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FAILED (A/C BAY)

IAH- THE CREW NOTED WHITE SMOKE IN THE COCKPIT DURING PARKING WITH NR 1 ENGINE AND APU RUNNING, (NO WARNINGS). MAINTENANCE REMOVED AND REPLACED NR 1 ACM, PERFORMED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DETERIORATED (BLEED AIR)

CLE FLIGHT 3321 THE CREW REPORTED ON DEPARTURE AT FULL TAKEOFF THRUST, RECEIVED A BLEED 1 LEAK EICAS MESSAGE. QRH COMPLETED AND THEN RECEIVED A BLEED 2 LEAK MESSAGE. AFTER EXITING ICING CONDITIONS THE MESSAGES CLEARED. MAINTENANCE REPLACED THE O-RINGS IN THE BLEED DUCT LINES. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CLAMP — LOOSE (BLEED AIR)

CLE FLIGHT 3011 THE CREW REPORTED A BLEED LEAK WARNING AFTER TAKEOFF ALONG WITH A ANTI-ICE FAIL MESSAGE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RESECURED A V-BAND CLAMP ON THE BLEED DUCT FOR THE STAB ANTI-ICE SYSTEM IN THE AFT AVIONICS BAY.

Part: HOSE — BLOWN

CLE FLIGHT#3860 THE CREW SHUT DOWN THE #1 ENGINE ON LANDING INTO CLEVELAND DUE TO A #1 ENGINE BLEED LEAK WARNING AND PRESSURIZATION PROBLEM.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE BLEED DUCT HOSE HAD BLOWN OFF BETWEEN THE ACM AND THE HEAT EXCHANGER FOR THE # 1 PACK.THE HOSE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 9,998 hrs · 7,810 cycles

EWR---CO4141, CREW REPORTED APU FAILED INFLIGHT (ON APPROACH). ELECTRICAL ODOR IN COCKPIT ASSOCIATED WITH THE FAILURE. MAINTENANCE INSPECTED AIRCRAFT AND DETERMINED APU FAULTY, AIRCRAFT PLACED ON MEL 49-00-00 CONTROL 013729. APU REMOVED AND REPLACED. MEL CLEARED AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — FAILED (NR 1)

IAH - FLIGHT 3761, THE CREW REPORTED A STRONG ODOR IN THE CABIN WITH THE NUMBER ONE PACK RUNNING. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NUMBER ON PACK ON MEL 21-51-00 CAT-C CONTROL NUMBER 00962, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 02/13/01 WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO AIR CYCLE MACHINE. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FLOOR SUPPORT)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOOR SUPPORT BEAM GUSSET AT FRAME NR 60 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT BEAM GUSSET ON LEFT SIDE FRAME NR 60 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOOR SUPPORT — BENT (CABIN)

IAH - DURING C-CHECK INSPECTION, FLOOR SUPPORT BEAM AT FRAME NR 68 LEFT WAS FOUND TO BE BENT. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — WORN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CAPTAINS INBOARD SEAT TRACK WAS FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145 AMM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CHAFED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FRAME NR 64 INNER FLANGE CHAFED BY CARGO LINER ATTACH FASTENERS. MAINTENANCE CLEANED AND BLENDED THE DAMGED AREAS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5310-01133. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — WORN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CAPTAINS OUTBOARD SEAT TRACK WAS FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145 AMM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CAP — CORRODED (RT MLG)

IAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CAP — CORRODED (LT MLG)

IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CAP — CORRODED (LT MLG)

IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOOR SUPPORT — BENT (CABIN)

IAH - DURING C-CHECK INSPECTION, FLOOR SUPPORT BEAM AT FRAME NR 67 LEFT WAS FOUND TO BE BENT. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CHAFED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FRAME NR 70 INNER FLANGE CHAFED BY CARGO LINER ATTACH FASTENERS. MAINTENANCE CLEANED AND BLENDED THE DAMAGED AREAS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5310-01133. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CAP — CORRODED (RT MLG)

IAH - DURING C-CHECK INSPECTION, THE RIGHT MLG GEAR AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — WORN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICERS OUTBOARD SEAT TRACK WAS FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145 AMM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — WORN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICERS INBOARD SEAT TRACK WAS FOUND TO BE WORN. MAINTEANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145 AMM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: GUSSET — CORRODED (FLOOR SUPPORT)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FLOOR SUPPORT BEAM GUSSET AT FRAME NR 60 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT BEAM GUSSET ON RIGHT SIDE FRAME NR 60 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE FORWARD GUST LOCK MOUNT STRUCTURE CROSSBEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01098. (M)

Part: SOCKET — CORRODED (FUSELAGE)

BTV - FLT CO4218 - MAINTENANCE FOUND PASSENGER MAIN EXIT EXTERNAL EMERGENCY LIGHT INOPERATIVE. CLEANED CORROSION FROM THE LIGHT SOCKET AND OPS CHECKED, LIGHTS GOOD. (X)

Part: POWER SUPPLY — INOPERATIVE (FUSELAGE)

BTV - FLT CO4218 - MAINTENANCE FOUND LEFT NR 1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPAIRED BURNED WIRES ON LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT AND REMOVED AND REPLACED EMERGENCY EXIT POWER SUPPLY. OPS CHECKED, LIGHTS GOOD. (X)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED JUST FORWARD OF FRAME 25 THE CORRODED SECTION OF OMEGA BEAM WAS REMOVED AND REPLACED AND PERFORMED A DOUBLER REPAIR. (M)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE DAMAGED SECTION OF OMEGA BEAM WAS REMOVED AND REPLACED. (M)

Part: BULB — FAILED (CABIN)

PIT - FLT 4299 - CREW REPORTED SMOKE FROM SIDEWALL LIGHT SEAT 4B, TROUBLESHOT AND FOUND BURNED BULB SOCKET AT 4D SIDEWALL LIGHT, SYSTEM RELEASED UNDER MEL 32-20-00 CAT C CONTROL NUMBER 211401. AIRCRAFT RETURNED TO SERVICE. CLE, MAINTENANCE REMOVED AND REPLACED BULB AND LIGHT ASSY. OPS CHECKED LIGHTS GOOD. NO SMOKE NOTED. MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: TR UNIT — MALFUNCTIONED (NR 2 ENGINE)

PVD - FLT 4043 - THE CREW REPORTED THE ENGINE NR 2 REV DISAGREE INDICATION ON TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE DEACTIVATED THE T/R IAW EMB145 MM 78-31-01 AND 78-33-01 AND RELEASED THE AIRCRAFT IAW MEL 78-34-00 CAT 'C' CONTROL NUMBER 184953. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (NR 2 TR)

CLE - FLT 4030 - THE CREW REPORTED THE ENGINE NR 2 TR DISAGREE MESSAGE ILLUMINATED ON TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00 CONTROL NUMBER 184939. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: GENERATOR — MALFUNCTIONED (NR 3)

CLE - FLT 4049 - THE CREW REPORTED THE NR 3 GENERATOR DROPPED OFF LINE NUMEROUS TIMES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 24-31-01 CAT 'C' CONTROL NUMBER 184935. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: TR LIGHT — ILLUMINATED (NR 2 ENGINE)

CLE-MSP - FLT 4059 - THE CREW REPORTED THAT ON TAKEOFF ROLL THE 'ENGINE 2 REV DISAGREE' WARNING APPEARED, THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00 CONTROL NUMBER 184857. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE RAMP SUPPORT WAS FOUND TO BE CORRODED AT FRAME 20 RIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD FORWARD FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER LEFT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED JUST FORWARD OF FRAME 25. MAINTENANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS DRAWINGS COEX03TYY05/06 AND COEX03TYY06/06, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD AFT FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT BATTERY AT STATION 17540.8 WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW EMB145 AMM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE FORWARD GUST LOCK MOUNT STRUCTURE CROSS BEAM WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED AN INTERIM REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01098, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01030, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — FAILED (LT ENG OIL PRESS)

CLE - DURING ENGINE RUN OPERATIONAL CHECKS, THE LEFT HAND ENGINE OIL PRESSURE EXCEEDED MANUFACTURER'S LIMITS. THE LEFT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (X)