N13936

Part: SKIN — CRACKED (ZONE 200) · airframe 30,516 hrs · 29,928 cycles

DURING A-CHECK INSPECTION, TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN EMINATING FROM THE SAME RIVET AT FRAME 75, STRINGER 2R. MX PERFORMED A DOUBLER REPAIR AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 29,099 hrs · 28,511 cycles

CORROSION ON LWR AFT FRAME STRUCTURE OF SERVICE DOOR FRAME 22. CUT OUT DAMAGED AREA, DRILLED AND INSTALLED REPAIR DOUBLER.

Part: ENGINE — LEAKING (NR 2) · airframe 27,742 hrs · 27,171 cycles

IAH - FLIGHT 2448, THE CREW REPORTED THAT THE CREW AND CUSTOMERS WERE COMPLAINING OF AN UNPLEASANT SMELL FROM THE PACK SYSTEM. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED OFR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 25,681 hrs · 25,065 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BATT TWO OVERTEMP INDICATION APPROXIMATELY TWO MINUTES AFTER POWER UP WITH THE GPU SELECTED. BATTERY 2 INDICATED 71DEG AND WAS CLIMBING. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,912 hrs · 74,258 cycles

IAH - FLIGHT 2949, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE GALLEY. THE AIRCRAFT WAS INSPECTED AND THE COFFEE BREWERS PLACED ON NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT SHV ON 02/25/08 WHERE SHV MAINTENANCE INSPECTED THE AIRCRAFT REMOVED BOTH COFFEEMAKERS, INSPECTED THE WIRING WITH NO DEFECTS NOTED. REPLACED THE COFFEEMAKERS OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. REMOVED THE NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,252 hrs · 23,567 cycles

RIGHT FLOORBOARD SILL HAS CORROSION FROM FRM 22 TO FRM 39. REMOVED AND REPLACED FLOOR SILLS IAW EMB SRM 51-40-02, 51-20-03.

Part: INLET — CORRODED (NR 2) · airframe 24,252 hrs · 23,567 cycles

NR 1 AND NR 2 ENGINE INLETS HAVE CORROSION IN THE BOLT HOLES. REMOVED CORROSION IAW EC5420-01158.

Part: SKIN — CRACKED (WINDOW POST) · airframe 24,252 hrs · 23,567 cycles

LEFT WINDSHIELD POST SKIN CRACKED. CUT AND REMOVED AREA OF CRACKED SKIN. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EC5310-01483.

Part: FITTING — CRACKED (LT NACELLE) · airframe 24,252 hrs · 23,567 cycles

LEFT ENGINE FORWARD YOKE LOWER LINKAGE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW EC 5450-01028.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,731 hrs · 22,994 cycles

IAH - FLIGHT 2809, THE CREW REPORTED THAT THE F/O'S WINDSHIELD CRACKED ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S WINDSHIELD, OPERATIONALLY & LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 23,474 hrs · 22,720 cycles

IAH - FLIGHT 2435, ON LANDING THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WITH A NUMBER ONE HYDRAULIC QTY LOW AND NO NOSE STEERING. THE AIRCRAFT WAS TOWED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE PRESSURE LINE ON THE NUMBER ONE MOTOR DRIVEN PUMP, OPERATIONAL AND LEAK CHECKS WERE PERFORMED WITH NO DEFECT, AND THE LANDING GEAR RETRACT AND EXTENSION SYSTEM WAS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,230 hrs · 22,462 cycles

IAH - DURING A-CK INSPECTION NUMEROUS EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT WING/FUSELAGE FRONT EMERGENCY LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (APU BLEED AIR) · airframe 23,127 hrs · 22,354 cycles

IAH - FLIGHT 2812, THE CREW REPORTED A FUEL SMELL COMING FROM THE APU BLEED. MAINTENANCE INSPECTED THE AIRCRAFT. VERIFIED NORMAL OPERATION OF APU BLEED WITH NO SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,841 hrs · 22,059 cycles

IAH - FLIGHT 2524, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE 2ND AND 3RD AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (EMERGENCY LIGHTS)

DURING PREFLIGHT INSP THE CREW REPORTED A SMOKE ODOR COMING FROM SEATS 3 & 4A. THE ACFT WAS RELEASED ON MEL 33-20-00 CAT C CTL NR 153947. THE AC LANDED, WHERE MAINT REMOVED AND REPLACED THE LIGHT SOCKET HARNESS ASSY AT ROW 4A, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K)

Part: CONNECTOR — OVERHEATED (EMERGENCY LIGHTS) · airframe 22,803 hrs · 21,277 cycles

TUL - FLIGHT 2845, THE CREW REPORTED SMOKE AND A SMELL OF FIRE AT SEAT 18A DURING DESCENT. THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT WHERE MAINTENANCE MEL`D THE PSU FOR SEAT 18A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT CONTINUED TO IAH ON FLIGHT 2886 WHERE MAINTENANCE REMOVED AND REPLACED A CONNECTOR ON THE PSU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,438 hrs · 19,703 cycles

IAH - FLIGHT 2828, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT WAS OUT. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,206 hrs · 19,442 cycles

ICT - FLIGHT 2914, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOP FROM THE FLIGHT ATTENDANT POSITION. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 19,969 hrs · 19,197 cycles

IAH - FLIGHT 2760, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY LIGHT SIGN AS BEING INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — WORN (NR 1 ENGINE) · airframe 13,723 hrs · 18,943 cycles

IAH - FLIGHT 2902, DURING CLIMB THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (OPEN)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,526 hrs · 18,731 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED CORRODED AREA AT FR 20 LEFT OMEGA BEAM IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 19,526 hrs · 18,731 cycles

SHV - DURING C-CHECK RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT IS WORN BEYOND TOLERANCE. MX REPAIRED RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT BY REAMING TO 2ND REWORK AND INSTALLING OVERSIZE BUSHING IAW EMB 145 SRM 55-30-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,101 hrs · 18,249 cycles

IAH - DURING PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT AT THE CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,079 hrs · 18,224 cycles

DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — FAULTY (CABIN) · airframe 17,548 hrs · 16,541 cycles

EMERGENCY EXIT LIGHT STRIP BETWEEN ROWS 10 AND 12 ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT STRIP BETWEEN ROWS 10 AND 12 IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 15,928 hrs · 14,720 cycles

RIC - DURING ROUTINE INSPECTION, EXIT ROW SIGN IN FRONT OF SEAT 3BC WAS FOUND INOP. MAINTENANCE CHECK THE BULBS AND CLEANED THE CONTACTS. OPERATIONAL TEST WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FUEL FILTER — CLOGGED (NR 1 ENGINE) · airframe 15,806 hrs · 14,592 cycles

E1 FUEL IMPENDING BYPASS MESSAGE ILLUMINATED IN FLIGHT. CREW DIVERTED FLIGHT. MX REMOVED AND REPLACED ENGINE 1 FUEL FILTER. OPERATIONAL TEST WAS SUCCESSFULLY PERFORMED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,191 hrs · 13,932 cycles

IAH - FLIGHT 2057 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EXIT SIGNS OVER THE GALLEY, ROW 2B, AND THE FLT ATTENDANTS SEAT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,191 hrs · 13,932 cycles

IAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,191 hrs · 13,932 cycles

IAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 15,120 hrs · 13,849 cycles

TYS, DURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN WAS FOUND CRACKED AT FS 75. MAINTENANCE MEASURED DAMAGED AREA, CUT OUT, FABRICATED A DOUBLER AND INSTALLED I/A/W-EC5310-01320 AND IC2005-145/0271.

Part: SKIN — CORRODED (FUSELAGE) · airframe 15,120 hrs · 13,849 cycles

TYS, DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN INSIDE SURFACE AT THE POTABLE WATER MANIFOLD MOUNT, CORRODED. REMOVED THE CORROSION, ALODINED, FABRICATED NEW REPAIR DOUBLER AND INSTALLED, PAINTED AND PRESSURE CHECKED I/A/W-EC5330-01435.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,120 hrs · 13,849 cycles

TYS - DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA BEAM BETWEEN FS 22 AND FS 23 HAS A BLENDED AREA BELOW LIMITS NEXT TO A NUTPLATE. MAINT CUTOUT THE EFFECTED AREA, FAB`D A SPLICE REPAIR FROM A NEW PART AND FAB`D AN INTERNAL ANGLE, DRILL, ALODINED, PRIMED AND INSTALLED IAW EC 5320-01205. REMOVED TOPCAP AND L-PROFILE AT THE REPAIR AREA AND REINSTALL IAW EMB 135/145 SRM 52-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL AT END OF THE C-CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,964 hrs · 13,654 cycles

IAH - FLIGHT 2474, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW THREE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,296 hrs · 12,775 cycles

DURING PREFLIGHT INSPECTION THE CREW FOUND THE EMERGENCY LIGHT STRIP AT ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING AND CLEARED THE DISCREPANCY.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

CREW REPORTED, STRONG ODOR OF BURNED ELECTRICAL COMPONENTS IN CABIN ROW 7 AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY AT ROW 5 AND 6 AREA IAW EMB 145 MM 33-21-06, OPS CHECKED LIGHTS GOOD.

Part: SOCKET — DAMAGED (CABIN)

BTV-CO2248, DURING 4A INSPECTION, MAINTENANCE FOUND THE LEFTHAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP SOCKET ASSEMBLY. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 2193 THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

CLE FLIGHT 3451 THE CREW REPORTED THE EMERGENCY LIGHT SIGN AT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED CONNECTORS ON THE EMERGENCY EXIT SIGN AT SEAT 3BC. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN)

FLIGHT NR 2103 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED LOOSE CONNECTOR ON THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: UPLOCK — INOPERATIVE (LT MLG)

IAH FLIGHT 2072, PILOT REPORTED THAT THE LEFT MAIN LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR UPLOCK BOX. THE LANDING GEAR EXTENSION/RETRACTION SYSTEM WAS OPERATIONALLY CHECKED AND NO DISCREPANCIES WERE FOUND.

Part: HOUSING — INOPERATIVE (EXTERIOR)

DURING ROUTINE MAINTENANCE THE NR 1 EMERGENCY LIGHT WAS INOPERATIVE ON WING TO FUSELAGE PANEL. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT HOUSING ASSEMBLY IAW 33-51-10.OPERATIONAL CHECKS WERE GOOD.

Part: SELECTOR — DIRTY (COCKPIT) · airframe 12,294 hrs · 10,732 cycles

CREW REPORTED, LANDING GEAR WARNING ON LANDING WITH LANDING GEAR DOWN AND THREE GREEN LIGHTS. MAINTENANCE CLEANED LANDING GEAR HANDLE CANNON PLUG, OPS CHECKED SYSTEM GOOD IAW EMB145 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT 2327, THE CREW REPORTED THE EMERGENCY LIGHTS ABOVE 3B WOULD NOT COME ON. MAINTENANCE REPLACED THE EMERGENCY EXIT LOCATOR SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2268 THE CREW REPORTED EMERGENCY EXIT LIGHT WAS INOPERATIVE ON THE RIGHT SIDE BULKHEAD IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS.NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STOP — CRACKED (CARGO DOORFRAME) · airframe 11,624 hrs · 10,025 cycles

SHV- DURING C-CHECK THE FOWARD EXTERNAL FRAME ON CARGO DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — CRACKED · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C CHECK THE BRACKET SUPPORTING THE ELEVATOR PULLEYS WAS FOUND CRACKED AND DEFORMED LOCATED IN VERTICAL STABILIZER BY PANEL 325LR. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 11,624 hrs · 10,025 cycles

SHV- DURING C-CHECK A RAMP ANGLE WAS FOUND CRACKED ON LEFT HAND FLOORBEAM FOWARD OF FRAME 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED AND ANGLE REPAIR IAW EMB SRM 51-30-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-06.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

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

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

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

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION.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 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-21-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 24.MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND RIGHT FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE LEFT HAND STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 53-31-19 AND 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND LEFT HAND FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE RIGHT SILL AND RIGHT FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND AND CENTER FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C CHECK AFT BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AFT BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-01.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE RIGHT HAND SILL AT FRAME 61 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: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND SILL AND THE LEFT HAND FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP AT FRAME 61 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: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

SHV-DURING C-CHECK THE RIGHT HAND 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: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,624 hrs · 10,025 cycles

DURING C-CHECK THE RIGHT DIGITAL BEAM AFT OF SERVICE DOOR WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 TO 23. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: COMBUSTION LINER — CRACKED (#1 ENGINE)

CLE FLIGHT#3280 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT AFTER TAKEOFF FROM CLEVELAND.THE ODOR WAS NOTED WHEN THE PACKS WERE OPERATED FROM THE ENGINE BLEED.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED THE #1 ENGINE AND FOUND MULTIPLE CRACKS IN THE COMBUSTION LINER.THE #1 ENGINE WAS REPLACED.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN)

CLE FLIGHT THE CREW REPORTED THE FLIGHT ATTENDENT'S FLASHLIGHT SWITCH CAME OFF. MAINTENANCE REPLACED THE FLASHLIGHT AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

IAH- DURING PREFLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY EXIT SIGN IN ROW 12 RIGHT SIDE INOP. IAH- MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE,

Part: INVERTER — INOPERATIVE (CABIN)

IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT IN MAIN DOOR WAY INOP. (NEAR FLOOR). MAINTENANCE REMOVED AND REPLACED THE FWD.EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (A/C BAY)

IAH- PACK #1 GIVES SMOKE WHEN OPERATING ON APU BLEED. IAH- MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 ACM. PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LEFT GEAR)

CLE FLIGHT#3848 THE CREW REPORTED THE LEFT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR UPLOCK PROXIMITY SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEARING — FAILED (NLG WHEEL)

IAH - FLIGHT 4137, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE LEFT HAND NOSE WHEEL INBOARD BEARING HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE NOSE STRUT, AND BOTH WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 7,700 hrs · 6,362 cycles

IAH - DURING C-CHECK INSPECTION, THE AFT EXIT ROW CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IN ACCORDANCE WITH EMB145 M/M 33-50-11-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 7,700 hrs · 6,362 cycles

IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IN ACCORDANCE WITH EMB-145 M/M 33-50-04-000-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE AISLE PATH LIGHTING STRIP AT THE EMERGENCY EXIT WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB-145 M/M 33-50-12-000-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (ELEVATOR) · airframe 7,700 hrs · 6,362 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER BUSHING ON THE RIGHT HAND SERVO TAB WAS FOUND TO HAVE PITTING CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB-145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (P/N PE64042K5-028-022S).

Part: TIRE — BLOWN (MLG)

EWR - FLT 4282 - CREW REPORTED BRAKES LOCKED ALL FOUR MAIN TIRES BLOWN ON LANDING. MAINTENANCE PERFORMED INSPECTION AS PER AMM 05-50-03, EMB SST 2232/00 AND SST 2234/00. REMOVED AND REPLACED ALL FOUR MAIN LANDING GEAR WHEEL ASSY NR 1 THROUGH NR 4. REFERENCE M-602 NR 293366 IAW AMM 32-49-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BRAKE ASSY — SEIZED (MLG)

EWR - CREW REPORTED BRAKES LOCKED ALL FOUR MAIN TIRES BLOWN ON LANDING. (M)

Part: ENGINE — FAILED (RIGHT)

CLE - FLT 4399 - AFTER TAKEOFF FROM CLEVELAND THE CREW RECEIVED A LAVATORY SMOKE WARNING INDICATION. SMOKE ENTERED THE AFT CABIN AREA. THE ARICRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DETERMINED THAT THE NR 2 ENGINE 0 CARBON SEAL WAS LEAKING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW CONTINENTAL EXPRESS GMM VOLUME 13 SECTION 2 TASK CARD 6271001. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERABLE (EMERGENCY EXIT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE LEFT AND RIGHT HAND EXTERIOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW WITH EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: RAMP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE RAMP UNDER THE CARBON FIBER FLOOR SUPPORT AT FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP IAW EMB145 SRM 51-40-02, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND 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. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE FORWARD RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND 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. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REPAIR DOUBLERS IAW EMBRAER REPAIR DRAWING SST-1287/99. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X)

Part: BULB — FAILED (EXTERNAL)

IAH - DURING MAINTENANCE INSPECTION, THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LT PACK — ODOR (CABIN)

CLE - FLT 4011 - CREW REPORTED THE LEFT PACK FILLED THE COCKPIT WITH SMOKE, AFTER THE PACK WAS TURNED OFF THE SMOKE CLEARED. AIRCRAFT WAS RELEASED IAW MEL 21-51-00 NR 173666. THE NEXT DAY MAINTENANCE INSPECTED THE NR 1 PACK ASSOCIATED COMPONENTS AND PERFORMED OPERATIONAL CHECKS WITH APU AND ENGINE BLEED AIR WITH NO DEFECTS NOTED IAW EMB-145 MM 21-51-00. REMOVED FROM MEL. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

EWR - FLT 4028 - THE CREW REPORTED THAT ON CLIMB, THE LEFT HAND ENGINE OIL PRESSURE EXCEEDED 90 PSI. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE. MAINTEANCE REMOVED AND REPLACED THE LEFT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)