N14937

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,183 hrs · 31,796 cycles

DURNG MX INSPECTION, SEVERAL FLOOR EMERGENCY LIGHT PROXIMITY STRIPS DID NOT ILLUMINATE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TIRE — FAILED (RT MLG) · airframe 31,712 hrs · 31,320 cycles

FLIGHT 4358. RT MLG NR 3 TIRE BLEW OUT AT V1 DAMAGING OTHER ITEMS. R & R NR 3 TIRE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,442 hrs · 31,040 cycles

DURING 5A INSPECTION THE FUSELAGE CROWN SKIN WAS FOUND TO BE CRACKED ON THE LT SIDE BETWEEN THE WINDSHIELD AND DV WINDOW. MX REMOVED THA DAMAGED SECTION, AND PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 04/22/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,442 hrs · 31,040 cycles

DURING 5A INSP THE LAFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FR78 STR 09L AROUND 1 RIVET. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,442 hrs · 31,040 cycles

DURING 5A INSPECTION, THE FUSELAGE SKIN AT FR 78 BELOW STR 1R WAS FOUND TO BE CRACKED. MX REMOVED THE DAMAGED SECTION, AND PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE/REPAIR EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELEMENT — INOPERATIVE (NR 2 ENGINE) · airframe 27,040 hrs · 26,679 cycles

IAH - FLIGHT 2804 THE CREW REPORTED AN E2 FIRE DETECTOR FAIL MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE FIRE DETECTOR ELEMENT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 26,707 hrs · 26,432 cycles

LCH - FLIGHT 2555, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD WAS ARCING IN FLIGHT, THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 26,469 hrs · 26,089 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST ABOVE SEAT 14B/C, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 26,435 hrs · 26,053 cycles

IAH - DURING CLIMB THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE AIR BETWEEN THE CABIN AND FLIGHT DECK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST AT ROW 12, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 26,435 hrs · 26,053 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE CREW VERIFIED NO SMOKE, AND MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE BAGGAGE SMOKE DETECTOR SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOSE — UNKNOWN (CABIN) · airframe 25,487 hrs · 25,069 cycles

IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 25,482 hrs · 25,062 cycles

IAH - DURING POST FLIGHT INSPECTION, AN ELECTRICAL SMELL MID CABIN WAS REPORTED WITH NO SMOKE OBSERVED. MAINTENANCE REMOVED AND REPLACED THE BALLAST AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 25,487 hrs · 25,069 cycles

IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 25,363 hrs · 24,938 cycles

LRD - FLIGHT 2616, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS AFT OF ROW 12 WERE INOPERATIVE. CONTRACT MAINTENANCE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,324 hrs · 24,895 cycles

IAH - FLIGHT 2217, THE DURING POST FLIGHT THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,599 hrs · 24,119 cycles

LCH - DURING MAINTENANCE INSPECTION THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,092 hrs · 23,559 cycles

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

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - A/C WAS IN A C-CHECK WHEN CORROSION WAS FOUND IN THE FLOOR SILL AT FRAME 24 THRU 30. MAINTENANCE REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - A/C WAS IN A C-CHECK STATUS WHEN THE LEFT FLOOR SILL WAS FOUND CORRODED AT FRAME 30 THRU 35. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - A/C WAS IN A C-CHECK STATUS WHEN CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAMES 20 AND 21. MAINTENANCE REPLACED THE PREVIOUS REPAIR BY REMOVING THE PREVIOUS REPAIR AND INSTALLED A NEW RAMP ANGLE AND A NEW REPAIR FOR THE OMEGA BEAM IAW 135/145 SRM 51-40-02 AND EA-5320-01024. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,780 hrs · 23 cycles

TYS - CORROSION WAS FOUND ON THE TOPCAP AT FRAME 20. MAINTENANCE REPLACED THE TOPCAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - CORROSION WAS FOUND AROUND A NUT PLATE ON THE SERVICE DOOR AFT SILL. MAINTENANCE BLENDED OUT THE CORROSION, FABRICATED AND INSTALL A DOUBLER IAE EMB 145 SRM 53-21-10. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 22. MAINTENANCE BLENDED OUT THE CORROSION IAW EMB 135/145 SRM 51-40-01 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE FWD DIGITAL PLATE. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 51-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE PAX DOOR ENTRYWAY AT THE AFT DIGITAL PLATE. MAINTENANCE BLENDED OUT THE LIGHT CORROSION IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

TYS - CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 22 TOPCAP. MAINTENANCE REPLACED THE TOPCAP IAW EMB 135/145 SRM 51-40-07. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: FITTING — CHAFED (VERTICAL STAB) · airframe 23,980 hrs · 23,425 cycles

TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND CORROSION ON FRAME 75 VERTICAL STAB FITTING, 4 BOLT HOLES HAD SOME CORROSION. MAINTENANCE REMOVED THE FITTING AND REAMED THE FOUR HOLES AND BUSHINGS INSTALLED. THEN REINSTALL THE FITTING IAW EC 5530-01185A. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,979 hrs · 23,425 cycles

CRACKED SHEAR CLIP AT FRM 10 JUST BELOW DV WINDOW. REMOVED CRACKED SHEAR CLIP, PARTIAL CRACKED FRM AND GUSSET AT FRM 10 JUST BELOW DV WINDOW. INSTALLED NEW SECTION OF FRM 10, REINSTALLED CONNECTING GUSSET. REPLACED SHEAR CLIP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,979 hrs · 23,425 cycles

SERVICE DOOR EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD.

Part: SILL — CORRODED (ZONE 100) · airframe 23,980 hrs · 23,425 cycles

ACFT IN C-CHECK AND THE RT FLOOR SILL WAS FOUND CORRODED BETWEEN FR 24 THRU FR 30. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (ZONE 800) · airframe 23,980 hrs · 23,425 cycles

ACFT CURRENTLY IN A C-CHECK STATUS AND CORROSION WAS FOUND UNDER THE SVC DOOR THRESHOLD PLATE AROUND THE NUT PLATES. MX REMOVED AND REPLACED SVC DOOR THRESHOLD SILL IAE SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLANGE — CORRODED (NR 2 INLET) · airframe 23,979 hrs · 23,425 cycles

NR 2 ENG INLET MOUNTING FLANGE HAS CORROSION AT MOUNTING HOLES. CLEANED AREA AND FOUND 3 HOLES TO HAVE CORROSION. REPAIRED THE MOUNTING FLANGE HOLES IAW EC5420-01158.

Part: BUSHING — MISSING (RUDDER) · airframe 23,979 hrs · 23,425 cycles

RUDDER II UPPER CONTROL ROD UPPER MOUNT HAT BUSHING ON RUDDER MISSING. REMOVED AND REPLACED MOUNT IAW EC 5540-01028.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

CORROSION ON AFT LOWER END OF SERVICE DOOR CUT OUT FRAME. DOUBLER WAS MADE FROM A SPARE FRAME AND INSTALLED IAW EC 5310-01373.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

CORROSION ON CENTER OMEGA BEAM AND STEP UP AT FRM 18. CORROSION WITHIN LIMITS. BLENDED OUT, ALODINED, PRIMED, AND PAINTED.

Part: CAP — CORRODED (LT LAVATORY) · airframe 23,980 hrs · 23,425 cycles

LT LAV TOP CAP CORRDED, WITHIN LIMITS, BLENDED, ALODINED, PRIMED, AND PAINTED.

Part: CAP — CORRODED (RT LAVATORY) · airframe 23,980 hrs · 23,425 cycles

RT LAV TOP CAP HAS CORROSION. BLENDED MINOR CORROSION, ALODINED, PRIMED, AND PAINTED.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

RT FLOOR SILL CORRODED BETWEEN FRM 29-35. FLOOR SILL WAS REMOVED AND REPLACED.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 23,980 hrs · 23,425 cycles

NR 1 ENGINE FWD/LWR YOKE WEBBING CRACKED. REMOVED AND REPLACED NR 1 ENGINE FWD/LWR YOKE WEBBING. CLOSED

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

CORROSION ON LT FLOOR SILL AT FRM 43. REMOVED AND REPLACED LT FLOOR SILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

CORROSION ON LT FLOOR SILL FROM FRM 18-23. FLOOR SILL WAS REMOVED AND REPLACED.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,980 hrs · 23,425 cycles

CORROSION ON LT FLOOR SILL FROM FRM 18-23. REPLACED SILL.

Part: BALLAST — OVERHEATED (CABIN) · airframe 23,932 hrs · 23,374 cycles

IAH - FLIGHT 2414 - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN ROW 1. MAINTENANCE REMOVED AND REPLACED THE LIGHTING BALLAST ABOVE ROW 1, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,876 hrs · 22,248 cycles

OKC - FLIGHT 2176, THE CREW REPORTED THAT PRESSURIZATION FAILED ON DESCENT INTO OKC. THE AIRCRAFT LANDED IN OKC WITHOUT INCIDENT WHERE MAINTENANCE PLACED PRESSURIZATION ON MEL 21-30-00/3 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT TON'D AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE DIGITAL CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 21,142 hrs · 20,498 cycles

IAH - FLIGHT 2618, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WHILE EN ROUTE FROM SHV TO IAH WITH A RED "X" ON THE RT MAIN GEAR INDICATOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 21,653 hrs · 20,185 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE UPPER LT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08980, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (CABIN) · airframe 20,531 hrs · 19,863 cycles

CLE FLIGHT 2457. THE CREW REPORTED THE EMERGENCY LIGHTS WOULD TURN OFF VIA THE DIM SWITCH ON THE F/A CONTROL PANEL. MAINTENANCE INSPECTED AND REPLACED THE F/A'S CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 19,966 hrs · 19,277 cycles

FLT 2534 - EWR - CREW REPORTED EMERGENCY LIGHT ON EXIT ROW INOP. MX MAINTENANCE RE-SECURED CONNECTOR BEHIND EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: NUT PLATE — MISSING (RUDDER) · airframe 19,319 hrs · 18,594 cycles

TYS - DURING A CURRENT 1C INSPECTION FOUND A MISSING NUT PLATE FOR THE PROTRACTOR ATTACHMENT ON RUDDER 2. MAINTENANCE REPAIRED RUDDER 2 IAW EC 5540-01063. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: ATTACH BRACKET — WORN (RT AILERON) · airframe 19,319 hrs · 18,594 cycles

RIGHT AILERON ATTACH BRACKET WORN AT THE HOLES FOR THE HAT BUSHINGS. REMOVED AND REPLACED AILERON PCA BRACKET IAW EC5750-01177. AIRCRAFT IS STILL IN C-CHECK.

Part: ATTACH BRACKET — DAMAGED (LT AILERON) · airframe 19,319 hrs · 18,594 cycles

LEFT AILERON PCA ATTACH BRACKET HAS DAMAGED HAT BUSHING HOLES. REMOVED AND REPLACED BRACKET IAW EC5750-01177. AIRCRAFT IS STILL IN C-CHECK.

Part: FUEL CONTROL — FAULTY (APU) · airframe 18,359 hrs · 17,524 cycles

CREW REPORTED AIR CONDITIONING PACK NR 1 PRODUCES STRONG FUEL SMELL WHEN SELECTED ON WITH APU BLEED. SMELL RE-OCCURRED IN FLIGHT WITH ENGINE BLEED SELECTED. SMELL WAS ONLY PRESENT IN THE COCKPIT, NOT IN THE CABIN. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT FOR THE APU IAW EMB145 AMM 49-32-01. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,209 hrs · 13,740 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01185. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,209 hrs · 13,740 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT NR 2015. THE CREW REPORTED THAT THE FORWARD MID CABIN CEILING OVER WING EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MID CABIN OVER WING EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL MODULE — FAULTY (EMPENNAGE) · airframe 12,552 hrs · 10,911 cycles

CREW REPORTED, AFTER TAKEOFF PITCH TRIM SYSTEM NR 1 AND NR 2 INOPERATIVE. RETURNED FOR LANDING BACK IN NEWARK. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT (HSCU) IAW EMB145 AMM 27-40-01. OPS CHECKED PITCH TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

EWR FLIGHT 2403, THE CREW REPORTED THE PITCH TRIM 1/2 WAS INOPERATIVE. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (COCKPIT)

SYR FLIGHT 2479 THE CREW REPORTED UPON APU START THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE ODOR DISSIPATED ON SHUTDOWN. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00.

Part: FLAP TRACK — CRACKED (RT WING) · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION, RT HAND OUTBOARD FLAP CENTER TRACK WAS FOUND TO HAVE A CRACK DUE TO LIGHTING STRIKE. MAINTENANCE REPAIRED DAMAGE IAW CONTINENTAL EXPRESS EC 5750-01185. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION, CORROSION WAS FOUND AT CENTER FLOORBEAM SUPPORT RAMP BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGED SECTION, PERFORMED AN ANGLE REPAIR, AND REPLACED AFFECTED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CARGO) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV- DURING C CHECK INSPECTION CENTER FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION ON NUTPLATES AND NUTPLATES HOLES. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION, LT LATERAL FLOORBEAM WAS FOUND TO HAVE CORROSION AT RE-ENFORCEMENT ANGLE BETWEEN FRAMES 19 AND 21. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-30-01, SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK, DENT WAS FOUND ON SKIN DOUBLER JUST BELOW PANEL 113EL. MAITENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION, RT FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION IN NUTPLATE HOLES. MAITENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUSHING — DAMAGED (RUDDER) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK, ALL HAT BUSHINGS ON THE RUDDER ATTACHING BRACKETS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED ALL HAT BUSHINGS ON RUDDEDR ATTACHING BRACKETS IAW EMB AMM 20-10-08. THE AURCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION AT NUTPLATE HOLES AND UNDER DOUBLER. MAINTENANCE REMOVED DAMAGED SECTION AND PERFORMED A FLOORBEAM REPAIR IAW EC 5320-01077. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV-DURING C CHECK INSPECTION, LT LATERAL FLOORBEAM AROUND NUTPLATE HOLES WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A FLOORBEAM REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV DURING C CHECK, NUTPLATE HOLES WERE FOUND WITH CORROSION ON LT LATERAL FLOORBEAM BETWEEN FRAMES 15 AND 17. MAITENANCE REMOVED DAMAGED SECTION AND PERFORMED FLOORBEAM REPAIR IAW EC 5320-01078. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CARGO) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION, CORROSION AND PITTING WAS FOUND AROUND RIVETS ON BUTTSTRAP BETWEEN FRAMES 59 AND 61. MAITENANCE REMOVED 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 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION BUTTSRAP ON CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CARGO) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV-DURING C CHECK FLOORBEAM DOUBLER AT FWD CARGO PARTITION WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED DOUBLER IAW EMB 145 SRM 51-20-03 AND SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV-DURING C CHECK, LT CARGO SILL FLOORBEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED AND REPLACED AFFECTED SILL FLOORBEAM IAW EMB SRM 57-220-03, SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV-DURING C CHECK INSPECTION NUTPLATE WAS FOUND WITH CORROSION ON CENTER FLOORBEAM AT FRAME 22. MAINTENANCE REMOVED DAMAGE AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — GOUGED (NR 1 NACELLE) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV DURING C CHECK INSPECTION GOUGE WAS FOUND ON NR 1 ENGINE LOWER COWLING AFT OF ENGINE DRAIN. MAINTENANCE REMOVED DAMAGED SETION AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV-DURING C CHECK INSPECTION DOUBLER ON RT LATERAL FLOORBEAM AT FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK CORROSION WAS FOUND ON NUTPLATE HOLES ON LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION NUTPLATE WAS FOUND CORRODED ON CENTER FLOORBEAM AT FRAME 18. MAINTENANCE REMOVED AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.

Part: FLOORBEAM — CORRODED (GALLEY) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT GALLEY MOUNT HOLES BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION CORROSION WAS FOUND ON NUTPLATE AT LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED LT SILL BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

DURING C CHECK INSPECTION SPLICED ANGLE AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17 WAS FOUND CRACKED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — GOUGED (NR 1 NACELLE) · corrosion level 2 · airframe 11,129 hrs · 9,497 cycles

SHV DURING C CHECK INSPECTION SUPPORT ANGLE WAS FOUND GOUGED ON NR 1 ENGINE LOWER COWLING JUST AFT OF MOST FOWARD PIVOT POINT. MAINTENACE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

IAH - CREW REPORTED THAT ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS DID NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 3 FLOOR STRIP CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED, THE FLOOR STRIP OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

MEM - CREW REPORTED THAT THE EMERGENCY LIGHTING STAYED ON WITH SWITCH SELECTED TO THE OFF POSITION. AN ELECTRICAL RESET OF THE SYSTEM WAS ACCOMPLISHED AND THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT)

IAH- FLIGHT 3935, DURING CLIMB THE CREW NOTED THAT THE GEAR WOULD NOT RETRACT AS SELECTED, GEAR HANDLE DISAGREE. THE CREW RETURNED THE GEAR HANDLE TO THE DOWN POSITION AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB 145 MM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE BOTTLE — DEFECTIVE (NR 1 ENGINE)

CLE FLIGHT 3157 THE CREW REPORTED A ENGINE 1 (2) EXTINGUISHER BOTTLE A INOP MESSAGE DURING FLIGHT. THE MESSAGE WENT OUT DURING DESCENT. MAINTENANCE REPLACED THE FIRE BOTTLE A. OPERATIONAL CHECKS WERE GOOD.

Part: HARNESS — DEFECTIVE (CABIN)

CLE FLIGHT 4109 THE CREW REPORTED SMOKE APPEARED FROM CABIN LIGHTS ABOVE SEAT 1A. MAINTENANCE INSPECTED AND REPLACED THE UPPER CABIN LIGHT HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — SMOKE (LAVATORY)

IAH - FLIGHT 4128, THE CREW REPORTED THAT THE LAV LIGHT EMITTED A BURNING ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PLACED THE LAV ON MEL 25-60-02/6 CONTROL NUMBER 010247, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,465 hrs · 6,236 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IN ACCORDANCE WITH EMB145 M/M 33-50-02-000-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (CABIN) · airframe 7,465 hrs · 6,236 cycles

IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IN ACCORDANCE WITH EMB145 M/M 33-26-04-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,465 hrs · 6,236 cycles

IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT ON PANEL 243DLC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IN ACCORDANCE WITH EMB145 M/M 33-50-04-000-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — CORRODED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER FITTING HINGE SUPPORT FOR THE HORIZONTAL STAB WAS FOUND TO BE CORRODED IN THE PIN BORE. MAINTENANCE OVERSIZED THE BORE ON THE FITTING HINGE SUPPORT IAW CONTINENTAL EXPRESS ENGINEERING CHANGE EC5510-01021, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOOR)

IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL PLATE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

BNA - DURING SERVICE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE AND WERE PLACED ON CATEGORY C MEL IAW EMB145 33-50-00. UPON ARRIVAL AT IAH, MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04. THE EMERGENCY LIGHTS WERE REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: THRUST REVERSER — MALFUNCTIONED (NR 1)

CREW REPORTED THAT THE NUMBER ONE ENGINE THRUST REVERSER OPEN LIGHT ILLUMINATED IN FLIGHT. A/C RETURNED TO IAH WITHOUT INCIDENT. MX INSPECTED, AND OPERATIONALLY TESTED NR 1 THRUST REVERSER. NO DEFECTS NOTED. MX PLACED THRUST REVERSER ON MEL, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE)

EWR - THE RIGHT FORWARD FUSELAGE SKIN WAS FOUND TO HAVE GROUND DAMAGE. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMBRAER FAX SST-0123100, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ACTUATOR — BROKEN (LT ENGINE)

EFD - FLT 938A - THE CREW REPORTED ENGINE ONE REVERSER DISAGREE, ENGINE ONE REVERSER FAIL, NR 1 REVERSER LEVER INOPERATIVE DURING TAXI, AND THE NR 1 UPPER THRUST REVERSER BUCKET WAS FOUND TO BE OPEN ON ENGINE SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRUST REVERSER ACTUATOR IAW EMB145MM 78-32-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIEC. (M)

Part: BLADE — DAMAGED (TURBINE)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE TURBINE BLADES WERE FOUND TO HAVE DAMAGED EDGES AND APPEAR TO BE RUBBING. THE DAMAGE WAS FOUND BEYOND MANUFACTURER'S LIMITS. THE RIGHT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (X)