N12967

Part: STRINGER — CRACKED (FRAME 13) · airframe 35,344 hrs · 26,729 cycles

STRINGER 6R CRACKED AT FR 13. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FRAMES 20-22) · airframe 35,344 hrs · 26,729 cycles

SERVICE DOOR SILL CORRODED. R & R SERVICE DOOR SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 35,344 hrs · 26,729 cycles

SKIN CRACKS AROUND RIVETS, FR 77, STR 8R. REPAIRED SKIN CRACKS IAW SRM 53-32-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FRAMES 65-68) · airframe 35,344 hrs · 26,729 cycles

CARGO DOOR LOWER CUT OUT CORRODED BETWEEN FR 65-68. RT CARGO DOOR LOWER CUT OUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,828 hrs · 25,614 cycles

DURING A SCHEDULED INSP, THE AFT OVERWING EMERGENCY EXIT LOCATER LIGHT WAS FOUND TO BE INOPERATIVE. THE NR 4 EMERGENCY LIGHT INVERTER WAS REPLACED, OPS CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 32,725 hrs · 24,707 cycles

DURING MX INSPECTION, ROW 12 AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX RESECURED LOOSE WIRE ON ROW 12 EMERGENCY LIGHT ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,026 hrs · 24,145 cycles

DURING MX INSPECTION, VARIOUS OVERWING EMERGENCY EXIT LIGHTS/SIGNS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — CONTAMINATED (NR 1 ENGINE) · airframe 31,874 hrs · 24,028 cycles

THE CREW REPORTED A SMOKE ODOR IN COCKPIT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX DETERMINED ODOR TO BE COMING FROM 1 ENGINE 14TH STAGE Y DUCT THAT WAS R & R ON 07-21-12 REF. PURGED BLEED AIR DUCTS IAW EMB 145 MM 21-20-00-100-805A. NO FURTHER SMELL NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,726 hrs · 23,906 cycles

DURING ROUTINE MX, THE RT OVERWING EMERGENCY LIGHT MARKER IN CABIN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,093 hrs · 23,409 cycles

THE CREW REPORTED THAT THE NR 3 AISLE PATH LIGHT STRIP WAS INOP, COMES ON INTERMITTENTLY AFTER ABOUT 10 MINUTES. MX R & R THE EMERGENCY LIGHT INVERTER IN THE GALLEY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,093 hrs · 23,409 cycles

THE CREW REPORTED THE NR 2 AND 3 AISLE PATH LIGHT STRIPS TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,016 hrs · 23,351 cycles

THE CREW REPORTED THE NR 2 AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MX PLACED THE AFFECTED LIGHT STRIP ON MEL 33-50-00-2 CAT C, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT SUBSEQUENTLY LANDED IN MCI WHERE MX R & R THE AFFECT AISLE PATH LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,093 hrs · 23,409 cycles

FLIGHT 5900 THE CREW REPORTED THAT THE NUMBER 5 AISLE PATH LIGHT WAS INOPERATIVE. MX R & R THE NR 5 LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (CABIN LIGHTS) · airframe 30,964 hrs · 23,306 cycles

SMOKE WAS REPORTED COMING OUT OF THE CEILING LIGHT ABOVE SEAT 1A. MX INSPECTED AND ISOLATED THE LIGHT HARNESS FOR THE LIGHT ABOVE SEAT 1A TO BE FAULTY. MX REMOVED THE LIGHT ASSY AND HARNESS AND DEFERRED IAW NEF CB-02 CAT "D". ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,498 hrs · 22,946 cycles

DURING C-CHECK. SKIN CRACKED AROUND RIVETS AT FR 75, STR 2L-3L. REPAIRED SKIN IAW EC5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,498 hrs · 22,946 cycles

DURING C-CK. SKIN CRACKS AT FR 75, STR 1R-3R. REPAIRED SKIN IAW EC5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — BLOWN (HYDRAULIC SYS) · airframe 29,340 hrs · 22,060 cycles

MKE FLT2000 THE CREW REPORTED A HYDRAULIC SYSTEM NR 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE O-RING ON THE NR 2 HYDRAULIC SYSTEM PRESSURE TRANSDUCER/TRANSMITTER. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERTEMP (NR 2) · airframe 28,813 hrs · 21,636 cycles

FLIGHT 6129 - IAD - DURING APPROACH MAIN BATTERY NR 2 OVERTEMP. CREW LANDED WITH BATTERY TEMP AT 61 C, IT REACHED 81 C BY THE TIME TO DEPOWER ACFT. CREW EVACUATED PASSENGERS THROUGH MCD PER ARFF DIRECTIONS WITHOUT INCIDENTS. IAS MX REMOVED AND REPLACED NR 2 MAIN BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: HOSE — WORN (A/C PACK) · airframe 28,395 hrs · 21,317 cycles

FLT 6002 - THE CREW REPORTED A SMOKE SMELL WHEN THE NR 1 PACK WAS SELECTED. MAINTENANCE PLACED THE NR 1 PACK ON MEL. MAINTENANCE REPLACED THE HOSES AT THE DUAL TEMP CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — OVERHEATED (CABIN) · airframe 27,845 hrs · 20,879 cycles

IAH - FLIGHT 2090, THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR LIGHT ASSEMBLIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 27,845 hrs · 20,879 cycles

IAH - FLIGHT 2090 THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR CABIN LIGHT ASSEMBLIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 27,845 hrs · 20,879 cycles

IAH - FLIGHT 2090, THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR LIGHT ASSEMBLIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INTERMITTENT (BRAKE SYSTEM) · airframe 27,611 hrs · 20,690 cycles

THE CREW REPORTED DURING TAXI THE BRAKES SEEMED INTERMITTANT AND THEN GRAB HARD. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 26,221 hrs · 19,628 cycles

CREW REPORTED BURNING SMELL AT FLIGHT ATTENDANT WINDSCREEN AREA. MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST AT ROW NUMBER ONE. OPERATIONALLY CHECKED LIGHTS. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 26,228 hrs · 19,635 cycles

IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTICED AT SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE LIGHTING BALLAST ABOVE SEAT 1A, OPERATIONALLY CHECKED THE LIGHTING WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR · airframe 25,861 hrs · 19,367 cycles

IAH - FLIGHT 3047, THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DUE TO A BRIGHT FLASH AND A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 59-60. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 59-60 IAW EC5330-02032. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) UNDER SEALANT AT FRAME 58 WATER HEATERS. MAINTENANCE PERFORMED ALL WORK IAW EC5330-02032. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 58-59. MAINTENANCE REPAIRED FUSELAGE SKIN WHERE CORROSION WAS FOUND AT FRAME 58-59 STRINGER 18L-18R IAW EC 5330-02032. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CRACKS AROUND RIVETS AT FRAME 77-78 LT SIDE. MAINTENANCE REPAIRED THE FUSELAGE SKIN AT MARKED RIVETS AT FRAMES 77-78 LT SIDE IAW EC 5330-02026 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AROUND NUT PLATE HOLE AT FRAME 18. MAINTENANCE INSTALLED REPAIRED RT OMEGA BEAM AT FRAME 18 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 3) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 57-58. MAINTENANCE REPAIRED AREA OF CORRODED FUSELAGE SKIN AT STRINGERS 18L-18R FRAMES 57-58 IAW EC5330-02032. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CRACKS AROUND RIVETS AT FRAME 75, 77 AND 79 RT SIDE. MAINTENANCE REPAIRED FUSELAGE SKIN AT MARKED RIVETS AT FRAME 75, 77 AND 79 RT SIDE IAW EC5330-02026 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, FUSELAGE SKIN CORRODED AT FR 58. REPAIRED SKIN IAW EC5330-02032. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 26 STRINGER 14R-15R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 STRINGER 14R-15R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 54. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT, INTERNAL, LOWER L-SHAPE CORRODED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR, INTERNAL, LOWER L-SHAPE CORRODED LEVEL 3 LOCAL. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 25 STRINGER 15R-16R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 STRINGER 15R-16R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 24 STRINGER 15R-16R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 STRINGER 15R-16R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 24 STRINGER 16R-17R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 STRINGER 16R-17R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 59. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 24. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT FRAME 29 CROSS BEAM AREA. MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM CROSS BEAM AREA AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT LOWER FLANGE BETWEEN FRAME 29-32. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT LOWER FLANGE FRAME 32 IAW EC5320-01513. REMOVED AND REPLACED RIVETS AT FLANGE SPLICE FRAME 29-30 IAW EMB-145 SRM 51-40-02. PREPPED, PRIMED AND PAINTED CENTER OMEGA BEAM FRAME 29-32 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 52-59. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, FR 10 CRACKED AT STR 9R. REMOVED AND REPLACED SECTION OF FR 10 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,516 hrs · 19,128 cycles

SHV - DURING C-CHECK, FR 10 CRACKED AT STRINGER 9L. REMOVED AND REPLACED SECTION OF FR 10 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (COCKPIT) · airframe 25,172 hrs · 18,869 cycles

CLE FLT 2629 - THE CREW REPORTED A SPOILER FAIL, SPS ADVANCED, LANDING GEAR AIR/GROUND FAIL/E1 IDLE STOP FAIL, AND WOW INOP MESSAGE ON THE EICAS WHILE TAXIING. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,695 hrs · 18,499 cycles

DURING ROUTINE MX, THE EMERGENCY EXIT SIGN OVER THE GALLEY SERVICE DOOR WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE EXIT SIGN AND OPS CHECKS WERE GOOD.

Part: BLADE — FRACTURED (NR 2 ENGINE) · airframe 24,557 hrs · 18,386 cycles

CLE - FLT 2135 - THE CREW REPORTED A NR 2 ENGINE UNCOMMANDED SHUTDOWN IN FLIGHT. ENGINE WOULD NOT RESTART AND THE AIRCRAFT DIVERTED INTO CVG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. TEAR DOWN REPORT FROM ROLLS ROYCE INDICATES THE FAILURE OF THE NR 2 ENGINE WAS DUE TO FRACTURE OF THE 1ST STAGE COMPRESSOR BLADE. FRACTURE INITIATED AT LEADING EDGE 0.6 INCH ABOVE DOVETAIL CORROSION WAS PRESENT AT FRACTURE ORIGIN AND ON SEVERAL OTHER BLADES.

Part: CLAMP — LOOSE (PACK VALVE) · airframe 24,280 hrs · 18,178 cycles

BTR - FLIGHT 2515, THE CREW REPORTED SMOKE IN THE COCKPIT CAPTAINS SIDE VENT, AND PACK 1 VALVE CLOSED TWO TIMES. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE CLAMP ON PACK VALVE ONE AND TWO, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 23,660 hrs · 17,700 cycles

DURING ROUTINE MX THE CAPTAINS OXYGEN MASK WAS FOUND TO BE LEAKING. MX INSPECTED AND REPLACED THE O2 STORAGE BOX. OPS AND LEAK CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,239 hrs · 17,382 cycles

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

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,455 hrs · 13,177 cycles

IAH - FLIGHT 2016, DURING PREFLIGHT INSPECTION THE CREW REPORTED A SLIGHT ELECTRICAL BURNING ODOR COMING FROM THE LAV. MAINTENANCE REMOVED AND REPLACED THE LAV LIGHT BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 15,867 hrs · 11,751 cycles

TYS - DURING A SCHEDULED INSPECTION CHAFFING WAS FOUND ON FRAME 65 BETWEEN STRINGERS 2L AND 3L. MAINTENANCE REPAIRED FRAME 65 IAW EMB-145-SRM-53-00-04 PAGE 211, FIGURE 206.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,687 hrs · 11,751 cycles

TYS - DURING A SCHEDULED INSPECTION THE AFT DOUBLER ON RIGHT OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED THE OLD DOUBLER, FABRICATED AND INSTALLED A NEW DOUBLER, ALODINED AND PRIMED IAW EMB-145-SRM-51-40-02/03/06 AND CMP-51-21-04/05/06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,687 hrs · 11,751 cycles

TYS - DURING A SCHEDULED INSPECTION, THE LEFT OMEGA BEAM SHOWS SIGNS OF CORROSION ON PREVIOUS REPAIR AT FRAME 20. MAINTENANCE REMOVED PREVIOUS REPAIR PIECES, FABRICATED NEW PIECES, ALODINED, PRIMED AND INSTALLED IAW EMB-145-SRM-51-40-02, 53-00-10, CPM-51-20-04/05.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 15,454 hrs · 11,564 cycles

CREW REPORTED, THE EMERGENCY LIGHT ON THE LEFTHAND SIDE WING/FUSELAGE FAIRING IS NOT OPERATING AND EMERGENCY LIGHT IN CABIN NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145AMM 33-50-04, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAULTY (EMERGENCY LIGHT) · airframe 15,214 hrs · 11,366 cycles

DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THAT THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT IS NOT FUNCTIONING. REMOVED AND REPLACED BULB IAW EMB145 MM NR 33-50-01; OPS CHECKED GOOD.

Part: BUSHING — WORN (SERVICE DOOR)

CLE - FLIGHT NR 2512 - CREW REPORTED GALLEY SERVICE DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BUSHINGS ON GALLEY SERVICE DOOR CRANK ASSEMBLY. OPERATIONAL CHECKS REPORTED GOOD.

Part: PROXIMITY SWITCH — CRACKED (NLG)

CLE FLIGHT 2826, THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/0718. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE LEFT BUTTSTRAP AT FRAME 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 11,540 hrs · 8,478 cycles

DURING C CHECK THE GALLEY CENTER FLOORBEAM FROM FRAME 16-24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

DURING C CHECK THE CENTER FLOORBEAM FROM FRAME 18 TO FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

DURING C CHECK THE CENTER RAMP ANGLE FROM FRAME 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 1 ENGINE) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 2 ENGINE) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE RIGHT HAND FORWARD FLOOR SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (RT COWLING) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE RIGHT HAND ENGINE UPPER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE CHAFED AND EXCEEDED BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (LT COWLING) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,578 cycles

SHV- DURING C-CHECK THE LAVATORY CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CRACKED (RT WING) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE RIGHT WING UPPER NUT PLATE CHANNEL ON SPAR 1 WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

SHV-DURING C-CHECK EXTERIOR STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,540 hrs · 8,478 cycles

SHV- DURING C-CHECK THE LEFT FORWARD SILL IN THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (CABIN)

EWR---DURING PREFLIGHT INSPECTION, FOUND RIGHT FRONT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY IAW EMB145 MM 33-50-04 AND EXTERNAL EMERGENCY LIGHT ASSY (PART NUMBER 1317) IAW EMB145 MM 33-50-10. OPS CHECKED GOOD.

Part: BULB — BLOWN (CABIN)

DURING ROUTINE MAINTENANCE THE RIGHT HAND EMERGENCY EXIT CEILING LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB AND OPERATIONAL CHECKS WERE GOOD.

Part: BULB — BLOWN (CABIN)

DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT ON THE CEILING WAS FOUND INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB AND OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — FAULTY (THRUST REVERSER)

CREW REPORTED A NR 1 ENGINE THRUST REVERSER FAIL MESSAGE ILLUMINATED DURING FLIGHT. THE CREW SHUTDOWN THE NR 1 ENGINE AND THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 THRUST REVERSER ON MEL. AFTER TROUBLESHOOTING THE NR 4 STOW AND TRANSIT, SWITCH WAS FOUND TO BE FAULTING. THE AFFECTED SWITCH WAS REMOVED AND REPLACED, THE AIRCRAFT WAS OPERATIONALLY CHECKED, THE MEL CLEARED, AND THEN RETURNED TO SERVICE.

Part: INLET — MISALIGNED (APU)

CLE FLIGHT 3301 THE CREW REPORTED A GLYCOL SMELL AND SMOKE IN THE CABIN ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND GLYCOL IN THE APU INLET AND THE INLET WAS MISALIGNED. THE GLYCOL WAS CLEANED UP AND THE INLET WAS ALIGNED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANGLE — CORRODED (FUSELAGE)

IAH- DURING C-CHECK INSPECTION, NOTED: THE RIGHT FLOOR CROSS BEAM LOWER ANGLE HAS CORROSION BETWEEN FR 23 AND 24. MAINTENANCE CUT OUT THE CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION.

Part: LOCK — OUT OF ADJ (SERVICE DOOR)

SDF FLIGHT 4072 THE CREW REPORTED THE SERVICE DOOR WAS JAMMED, WOULD NOT OPEN OR CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE SERVICE DOOR LOCKING MECHANISM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BLEED VALVE — INOPERATIVE (#1 ENGINE)

MAF - FLIGHT 3752, THE CREW REPORTED AN ATTCS NO MARGIN WARNING ON TAKE OFF ROLL. THE TAKE OFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE LOWER COMPRESSOR BLEED VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (CABIN)

IAH- DURING 5A CHECK IT WAS NOTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE FUSE, PERFORMED A OPERATIONAL CHECK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

EWR - FLT CO4228 - CREW REPORTED RIGHT EMERGENCY LIGHT LENSE CRACKED. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY. OPS CHECK SYSTEM GOOD. (X)