N14942

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,570 hrs · 28,605 cycles

THE FORWARD LOWER FUSELAGE INTERNAL SKIN WAS NOTED WITH CORROSION BEYOND LIMITS BETWEEN FRAMES 13 & 14, STRINGER 19L THRU 18R. R & R SKIN PANEL, REMAPPED LT & RT RVSM CRITICAL REGIONS. ACFT STILL IN C-CHECK.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,570 hrs · 28,605 cycles

CIRCUMFERENTIAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 & 14, STRINGER 21L THRU 18R. CUT-OUT CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,570 hrs · 28,605 cycles

LONGITUDINAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 AND 14, STRINGER 19L. REMOVED CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 28,393 hrs · 27,429 cycles

DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX CLEANED THE LIGHT BULB SOCKET, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,393 hrs · 27,429 cycles

DURING MX INSPECTION OF THE EMERGENCY LIGHTS, THE AISLE PATH LIGHT STRIP AT ROW 12 WAS FOUND TO BE INOPERATIVE. MX R & R THE EMERGENCY LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TERMINAL — LOOSE (DC BUSS BAR) · airframe 27,875 hrs · 26,942 cycles

THE CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM BEHIND THE CAPTAINS SEAT. MX R & R BURNED LOOSE TERMINAL LUGS AT DC BUSS NR 1 BUSS BAR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,119 hrs · 25,138 cycles

IAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL ON THE CAPTAINS SIDE WAS FOUND TO BE CRACKED BETWEEN THE CAPTAINS DV WINDOW AND THE CAPTAINS WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 25,040 hrs · 24,023 cycles

IAH - FLIGHT 2336, DURING TAXI THE CREW REPORTED A BATTERY TWO OVERTEMP. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 24,990 hrs · 23,965 cycles

JAN - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 24,949 hrs · 23,917 cycles

IAH - FLIGHT 2547, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 24,886 hrs · 23,858 cycles

IAH - FLIGHT 2034, DURING POST FLIGHT INSPECTION THE CREW REPORTED A STRONG BURNING SMELL IN THE GALLEY, AND THAT THE GALLEY LIGHT BALLAST WAS INOP. MAINTENANCE INSPECTED GALLEY AREA, REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS, AND NO SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENER AT FRAME 75 BETWEEN STRINGERS 1-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-02146. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (COCKPIT) · corrosion level 2 · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE PILOTS WINDSHIELD CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT SCREW HOLES 41, 43, 45, 49. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A BUSHING REPAIR IAW EC5310-01515. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (SPEED BRAKE) · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE LT SPEED BRAKE CENTER ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK IT WAS FOUND THAT THE VERTICAL STABILIZER INTERNAL FITTING WAS FRETTING WITH THE AFT FUSELAGE SKIN AT FRAME 75 BY STRINGER 1L. THE FRETTING CAUSED THE SKIN TO CRACK AND WAS DETECTED USING EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED SKIN AFTER CUTTING OUT THE DAMAGED AREA IAW EC5330-02147 AND EC5310-01317. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (SPOILER) · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE LT GROUND SPOILER ACTUATOR ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC5750-01415. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,640 hrs · 23,606 cycles

SHV-DURING C CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC 5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,640 hrs · 23,606 cycles

SHV - DURING C CHECK THE SPLICE ON STRINGER 18L WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 145 SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,987 hrs · 22,920 cycles

TYS - A/C WAS A OVERNIGHT A/C WHEN INSPECTION FOUND MULTIPLE DENTS IN A SMALL AREA OUT OF LIMITS. MAINTENANCE CUT OUT THE DAMAGE AREA AND FAB A FILLER AND DOUBLER IAW ETD2009-145/10249. ALL WORK WAS ACCOMPLISHED AND RELEASED.

Part: WIRE — BROKEN (CABIN) · airframe 18,565 hrs · 9,887 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROWS 16 & 17 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 18,565 hrs · 9,887 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 & 9 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,565 hrs · 21,363 cycles

IAH - DURING A-CK INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 21,799 hrs · 20,583 cycles

IAH - FLIGHT 2684, THE CREW REPORTED THAT THE NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 3 QTS IN FLIGHT WHILE PRESSURE AND TEMPERATURE REMAINED NORMAL. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: STRUCTURE — LOOSE (MAIN DOOR) · airframe 20,704 hrs · 19,497 cycles

CLE FLIGHT 2532 - THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND TIGHTENED BOLTS ON THE MAIN CABIN DOOR INNER HANDLE BOX. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PANEL — CORRODED (WING) · airframe 19,987 hrs · 18,734 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PNL 193 BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED PNL 193 BONDING STRIPS IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (PAX DOOR) · airframe 19,987 hrs · 18,734 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND 4 NUT PLATES LOCATED AT BOTTOM OF MAIN DOOR CORRODED. MAINTENANCE REPAIRED NUT PLATES AT THE BOTTOM OF THE MAIN DOOR IAW EC 5210-01152 ORIG. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (AILERON) · airframe 19,987 hrs · 18,734 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND LOWER AILERON SHROUDS BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED LOWER AILERON SHROUD IAW EC5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,987 hrs · 18,734 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND FRAME 65 WITH CORROSION UNDER CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET. MAINTENANCE REPAIRED CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET IAW EC 5330-01719. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — CONTAMINATED (NR 1) · airframe 18,883 hrs · 17,592 cycles

FLT 4930 - IAD CREW REJECTED TAKE OFF DUE TO SMOKE IN COCKPIT. SMOKE OCCURRED WHEN THRUST WAS ADVANCED TO DETENT. SMOKE CLEARED WHEN THRUST WAS REDUCED AND AFTER ENGINES WERE SHUT DOWN. SMOKE WAS A BLUE/GRAY COLOR. IAD MX RAN NR 1 & 2 ENGINES WITH PAKS TO PURGE THE SYSTEM OF RESIDUAL DE-ICING FLUID. NO MORE SMOKE FOUND AT THIS TIME. ACFT WAS APPROVED TO RETURN TO SERVICE. 02-26-2007.

Part: ENGINE — DAMAGED (NR 1) · airframe 18,888 hrs · 17,597 cycles

TYS A/C HAD SMOKE ON CLIMBOUT AND THEN CLEARED. THEN ANOTHER TIME ON LEVELING OFF, AGAIN LEFT. A/C WAS CHECKED OUT AND FERRIED TO TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW RR TASKCARD 627100. OPS AND LEAK CHECKS WERE GOOD, RELEASED BACK TO SERVICE. [07-24-07] THE CAUSE OF THE SMOKE WAS A LEAKING NR 4 CARBON SEAL.

Part: ENGINE — CONTAMINATED · airframe 18,776 hrs · 17,473 cycles

CLE FLIGHT 2965 THE CREW REPORTED CLIMBING THRU 7500 FT. THE F/A REPORTED SMOKE FILLING THE CABIN. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND PACKS UNTIL SMOKE DISSIPATED. FOUND CAUSE TO BE DEICE FLUID IN ENGINES.

Part: RELAY — SHORTED (LAVATORY LIGHT) · airframe 18,768 hrs · 17,463 cycles

FLIGHT 1281, PILOT REPORTED THAT A LAV SMOKE INDICATION ILLUMINATED DURING CLIMB OUT. A VISUAL INSPECTION WAS PERFORMED AND SMOKE, FIRE AND/OR UNUSUAL ODORS WERE NOT NOTICED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LAV SMOKE WARNING SYSTEM OPERATIONALLY TESTED GOOD. DURING TROUBLESHOOTING RELAY K8100 FOR THE LAVATORY LIGHT ASSEMBLY WAS FOUND TO BE SHORTED. THE RELAY WAS REPLACED AND THE DISCREPANCY CLEARED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,362 hrs · 15,907 cycles

CLE FLIGHT 2808 THE CREW REPORTED THE FORWARD EMERGENCY SIGN OVER THE F/A'S SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,989 hrs · 14,372 cycles

DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 35-39. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAME 38 - FRAME 39 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 52 & 59. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 54 AND AT FRAME 59 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION FR 39-45. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 44 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 45 & 53. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 49 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK RIVET HEAD WEAR MARKS ON BOTTOM RT SIDE OF APU FIREWALL. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC 5310-01337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 22 & 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,512 hrs · 13,861 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FRAMES 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 33 - FRAME 34 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 15,311 hrs · 13,596 cycles

IAH - FLIGHT 2638, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (EMERGNECY LIGHT) · airframe 14,424 hrs · 12,575 cycles

CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — PINCHED (WINDSHIELD HEAT)

IAH - FLIGHT 2064 THE CREW REPORTED A STRONG ELECTRIC BURNING ODOR WHEN THE WINDSHIELD HEAT WAS SELECTED ON. THE AIRCRAFT LANDED AT IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE WINDSHIELD HEAT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT SHV WHERE MAINTENANCE FOUND A WIRE BUNDLE PINCHED AND ARCING UNDER FLOOR PANEL 222AF. MAINTENANCE REPAIRED THE AFFECTED WIRING, AND REMOVED AND REPLACED THE AFFECTED FLOOR PANEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE CENTER FUSELAGE CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CENTER FUSELAGE CABIN EMERGENCY CEILING LIGHT INVERTER. OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS WERE GOOD.

Part: LIGHT — FAULTY (CABIN)

CREW REPORTED, OVERHEAD EMERGENCY EXIT LIGHT AFT SIDE, WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE AFT SIDE IAW EMB145 AMM . OPS CHECKED GOOD.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV - DURING C-CHECK, THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C CHECK THE LEFT HAND OMEGA BEAM LOWER FLANGE WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24-25. MAINTENANCE REMOVED DAMAGED AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION ON THE LOWER FLANGE BETWEEN FRAMES 24-25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED OMEGA BEAM IAW 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV - DURING C-CHECK, THE AFT DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 TO 18. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED DIGITAL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV - DURING C-CHECK, CENTER BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

DURING C CHECK LAVORATORY'S FLOORBEAMS UPPER SURFACE WHERE FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BUTTSTRAPS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

DURING C-CHECK, THE LT BUTT STRAP WAS FOUND TO HAVE CORROSION BY FRAME 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV - DURING C-CHECK, THE LT BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 19-23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C CHECK THE LEFT SILL AFT OF THE PASSENGER DOOR WAS FOUND HAVE CORROSION BETWEEN FRAMES 19-20. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOUBLER — CORRODED (BEAM) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

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

Part: CHANNEL — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C-CHECK, SERVICE DOOR CENTER THRESHOLD FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED DAMAGE AND PERFORMED DOUBLER REPAIR TO AFFECTED STRUCTURE IAW EMB SRM 145 53-21-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV-DURING C CHECK THE FORWARD DIGITAL BUTT STRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 (REPAIR 4). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (LAVARATORY) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C CHECK LAVARATORY CENTER BUTT STRAP WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV-DURING C CHECK LEFT HAND BUTT STRAP BETWEEN FRAMES 23 AND 29 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (BEAM) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV DURING C CHECK THE RT BUTT STRAP IN LAV WAS FOUND TO HAVE CORROSION AT AFT SECTION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,531 hrs · 9,407 cycles

SHV-DURING C CHECK LEFT HAND OMEGA BEAM BETWEEN FRAMES 14 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY · airframe 10,555 hrs · 8,444 cycles

EWR---CO4131, CREW REPORTED, "ON TAKEOFF GOT LND GEAR AIR/GND FAIL. THEREFORE AIRRETURNED." MAINTENANCE REMOVED AND REPLACED LEFT HAND PROXIMITY SWITCH ON SHOCKABSORBER IAW EMB145 MM #32-63-01. EXTENDED AND RETRACTED LANDING GEAR OPS.CHECKED GOOD IAW EMB145 MM #32-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE CHECK MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE LEFT AND RIGHT OVERWING LIGHTS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 12 TO ROW 19.MAINTENANCE REPLACED THE EMERGENCY LIGHT DC/AC INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CREW REPORTED TO MCC IN IAH THE EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPAIRED LIGHTS.

Part: MOTOR — FAILED (STICK SHAKER) · airframe 9,072 hrs · 7,067 cycles

TYS DURING A SCHEDULED INSPECTION THE CAPTAINS STICK PUSHER FAILED OPERATIONAL CHECKS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS STICK PUSHER MOTOR IAW EMB-145 27-36-04, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT RELEASED FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

IAH - FLIGHT 4152, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,455 hrs · 5,646 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND OUTBOARD FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMB145 SRM51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,455 hrs · 5,646 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (SPOILER) · corrosion level 2 · airframe 7,455 hrs · 5,646 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT WING SPOILER CENTER ATTACH BUSHING WAS FOUND TO BE RUSTY. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — FAULTY (GALLEY)

EWR - FLT 4088 - CREW REPORTED BURNING SMELL FROM COFFEE CONNECTOR NR 2 POSITION. MAINTENANCE REMOVED AND REPLACED NR 2 COFFEE POT CONNECTOR IAW EMB145AMM NR 25-16-02, OPS CHECKED GOOD. (M)

Part: INVERTER — INOPERATIVE (CABIN)

EWR - DURING MAINTENANCE INSPECTION, THE LAST SET OF AISLE PATH EMERGENCY EXIT LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED INVERTER IN ACCORDANCE WITH EMB145 M/M 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE)

BTV-MX FOUND (DURING A 4A INSPECTION) THE LT AND RT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED RT AND LT EMERGENCY LIGHT ASSYS IAW EMB145 MM 33-50-10. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

BTV - FLT 4218 - DURING 3A INSPECTION, MAINTENANCE FOUND EMERGENCY AISLE PATH LIGHTS ROM SEATS 12A TO 19A WILL NOT STAY ON. REMOVED AND REPLACED NR 4 EMERGENCY EXIT LIGHT BATTERY PACK IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. (M)

Part: CARTRIDGE — DISCHARGED (FIRE EXTINGUISHER)

IAH - DURING SCHEDULED MAINTENANCE ON 3-10-00, THE H2O FIRE EXTINGUISHER WAS REMOVED AND ROUTED FOR FUNCTIONAL TESTING. BEFORE SHIPPING ON 3-16-00, AN INDENTATION WAS NOTED ON THE C-O2 CARTRIDGE FACE, WHILE NO HOLE WAS FOUND FROM THE PIERCING PIN. THE C-O2 CARTRIDGE WAS PLACED BACK INTO THE FIRE BOTTLE, THE BOTTLE ACTIVATED, AND THE CARTRIDGE WAS FOUND DEPLETED. THE AFFECTED FIRE BOTTLE, BEING ALREADY REMOVED FROM THE AIRCRAFT, WAS FORWARDED TO ENGINEERING TO RELAY THE DEFECT FOUND TO THE MANUFACTURER. (X)

Part: SWITCH — CONTAMINATED (MLG) · airframe 4,884 hrs · 3,682 cycles

EWR - FLT 4164 - CREW REPORTED LANDING GEAR WOULD NOT RETRACT DURING GO AROUND. RETURNED TO THE FIELD AND LANDED UNEVENTFULLY. MAINTENANCE FOUND ICE ON ALL PROXIMITY SWITCHES. CLEANED SWITCHES AND OPERATIONALLY CHECKED GOOD ON TEST FLIGHT. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

CLE - FLT 4177 - THE CREW REPORTED A LAVATORY SMOKE INDICATION AFTER TAKEOFF FROM CLEVELAND. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL 36-12-01. (X)

Part: DRAG ANGLE — CRACKED (VERT STABILIZER)

IAH - DURING C-CEHCK INSPECTION, THE VERTICLE STABILIZER TO FUSELAGE LEFT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: DRAG ANGLE — CRACKED (VERT STABILIZER)

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

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMBRAER145 FAX SST=1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATAIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (E/E BAY)

HPN - FLIGHT 4053 - CREW REPORTED THAT DURING BEFORE TAKEOFF CHECKS THE TAKEOFF CONFIGURATION WARNING SOUNDED FOR 'TRIM'. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB-145 MM 27-40-01. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FADEC — FAILED (NR 1 ENGINE)

SAV - FLT 4020 - CREW REPORTED DURING DESCENT, THE NR 1 ENGINE CONTROL 'B' FAILED AND THE ENGINE WAS SHUT DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED FADEC 1A IAW EMB-145 MM 73-22-01. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (X)