N14930

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,987 hrs · 29,827 cycles

DURING MX INSPECTION, THE PASSENGER CABIN FWD EMERGENCY EXIT LOCATING SIGN ON 253CLC FAILED TO ILLUMINATE. MX R & R THE AFFECTED SIGN EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 30,946 hrs · 29,791 cycles

THE CREW REPORTED THE EXIT SIGN OVERWING EXIT WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RECONNECTED THE SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 28,465 hrs · 27,349 cycles

DURING C-CHECK. CENTER OMEGA BEAM CORRODED AT FR 20. REPLACED OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (ENGINE) · airframe 28,465 hrs · 27,349 cycles

DURING C-CHECK. RT FWD LOWER ENGINE MOUNT CRACKED. R & R RT LOWER FWD ENGINE MOUNT IAW EC 5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,465 hrs · 27,349 cycles

DURING C-CHECK. CRACKS AROUND RIVETS ON RT FUSELAGE SKIN AT FR 75. REPAIRED SKIN CRACKS IAW EC 5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 28,465 hrs · 27,349 cycles

DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 49. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 28,465 hrs · 27,349 cycles

DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 44. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,144 hrs · 27,036 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING NR 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,744 hrs · 26,633 cycles

IAH - FLIGHT 2886, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING IN THE BACK HALF OF THE AIRCRAFT WAS 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: DAMPER PLATE — DAMAGED (APU BAY) · airframe 27,558 hrs · 26,438 cycles

IAH - DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO HAVE SEVERAL DAMAGED VIBRATION ABSORPTION PADS. MAINTENANCE REPAIRED THE VIBRATION ABSORPTION PADS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERHEATED (NR 2) · airframe 25,557 hrs · 24,409 cycles

IAH - FLIGHT 3121, THE CREW REPORTED A BATTERY TWO OVER-TEMP ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR — MALFUNCTIONED (COCKPIT) · airframe 24,921 hrs · 23,745 cycles

IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, AND LANDING GEAR ELECTRONICS UNIT, LGEU, TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 24,921 hrs · 23,745 cycles

IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, AND LANDING GEAR ELECTRONICS UNIT, LGEU, TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR — INOPERATIVE (COCKPIT) · airframe 24,905 hrs · 23,726 cycles

DFW - FLIGHT 2114 DURING CLIMB THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE, AND THREE RED X'S ON THE EICAS. THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — OVERHEATED (NR 1) · airframe 24,450 hrs · 23,238 cycles

IAH - FLIGHT 2030, DURING TAXI THE CREW REPORTED THAT THE NUMBER ONE PACK OVERHEATED WITH A BURNING ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 PACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — DEFECTIVE (WINDSHIELD) · airframe 24,213 hrs · 22,978 cycles

IAH - DURING CLIMB THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE WINDSHIELD AREA. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CAPTAINS HUMPSEAL ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REPAIRED THE CAPTAINS HUMPSEAL. REMOVED THE DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — BURNED (CABIN LIGHTS) · airframe 24,113 hrs · 22,869 cycles

FLIGHT 2526, DURING TAXI THE CREW REPORTED A STRONG ELECTRICAL PLASTIC BURNING ODOR COMING FROM THE GALLEY AREA. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT SOCKET ON THE CEILING LIGHT AT ROW 1A, TO BE BURNED. MAINTENANCE REMOVED POWER FROM THE AFFECTED LIGHT ASSY, AND PLACED THE LIGHT ON MEL 33-20-00/1 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE BURNT LIGHT SOCKET HARNESS, RECONNECTED THE BALLAST, OPERATIONALLY TESTED THE CABION LIGHTING WITH NO DEFECTS NOTED, AND THE AIRCRTAFT WAS APPROVED FOR RETURN TO SERVICE

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 23,858 hrs · 22,598 cycles

IAH - FLIGHT 2605 - THE CREW REPORTED A LANDING GEAR DISAGREE ON CLIMBOUT AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND TEST FLOWN SATISFACTORILY. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: CONTROL HANDLE — INOPERATIVE (COCKPIT) · airframe 23,838 hrs · 22,574 cycles

IAH - FLIGHT 2104 - THE CREW REPORTED WHEN COMMANDED GEAR SW TO UP, GEAR DID NOT RETRACT. TEN TO FIFTEEN SECONDS LATER CREW RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS, AND THE GEAR RETRACTED, AND EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,640 hrs · 22,369 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED LT OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,640 hrs · 22,369 cycles

DURING C-CHECK. BAGGAGE DOOR CUTOUT LOWER SILL HAS CORROSION. REPAIRED CARGO LOWER SILL IAW IC 2009-145/03445. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,640 hrs · 22,369 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED RT OMEGA BEAM IAW IC2009-145/00907. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK FRAME 80 HAS CRACKED SHEAR CLIP BETWEEN STR 6-7R. MAINTENANCE REMOVED AND REPLACED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STR 6-7R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — DAMAGED (RT AILERON) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK RT AILERON MOST O/B HINGE BRACKET I/B HOUSING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON MOST O/B HINGE SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (RT AILERON) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK RT AILERON NR 2 HINGE FROM O/B HAS MIGRATED BUSHINGS. REMOVED AND REPLACED RT AILERON NR 2 HINGE FROM O/B SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — WORN (RT AILERON) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK RT AILERON NR 1 HINGE FROM O/B HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED RT AILERON NR 1 HINGE FROM O/B SUPPORT BRACKET ASSY (WITH NEW BUSHINGS) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — SLOW (RT MLG) · airframe 23,620 hrs · 22,344 cycles

IAH - FLIGHT 2798, THE CREW REPORTED THE LANDING GEAR TOOK OVER 30 SECONDS TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,433 hrs · 22,153 cycles

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

Part: WIRE — SHORTED (COCKPIT) · airframe 23,385 hrs · 22,100 cycles

GPT - FLIGHT 2304 - THE CREW REPORTED AN ELECTRICAL BURNING SMELL BEING EMITTED FROM THE ELECTRICAL PANEL BEHIND THE CAPTAINS SEAT. THE AIRCRAFT LANDED AT GPT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND WIRE W179-0001-00 TO THE CENTRAL DC BUS I TO BE SHORTED. MAINTENANCE REPAIRED THE AFFECTED WIRE, OPERATIONALLY TESTED THE AFFECTED SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,370 hrs · 21,063 cycles

IAH - DURING MAINTENANCE INSPECTION THE 2ND AISLE PATH LIGHT STRIP ON THE FLOOR WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 21,967 hrs · 20,652 cycles

A 1.26 LONG CRACK WAS DISCOVERED ON THE LT WING UPPER TRAILING EDGE SKIN ADJACENT TO THE CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01140. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SENSOR — BURNED (COCKPIT) · airframe 21,609 hrs · 20,293 cycles

IAH - FLIGHT 2137, WHILE "SITTING AT THE GATE" THE CREW REPORTED A BURNT SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PITOT NUMBER ONE CURRENT SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 21,550 hrs · 20,235 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT WING SKIN TO BE CRACKED AT THE SPOILER HINGE POINT. THE CRACK WAS INSPECTED AND PLACED ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING FINAL CORRECTIVE ACTION.

Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 21,411 hrs · 20,089 cycles

SHV - FLT 2395, DURING CLIMB AND UPON MOVING THE LANDING GEAR SELECTOR TO RETRACT THE CREW OBSERVED A HYDRAULIC SYSTEM 1 ADVISORY. THE CREW MOVED THE LANDING GEAR SELECTOR BACK TO EXTEND AND PERFORMED THE ABNORMAL INDICATION PROCEDURES. THE AIRCRAFT MADE AN UNEVENTFUL LANDING BACK TO JAN. UPON INSPECTION MAINTENANCE FOUND A RUPTURED HYDRAULIC PRESSURE LINE. MAINTENANCE REMOVED AND REPLACED THE PRESSURE LINE; AS A PRECAUTIONARY REMOVED AND REPLACED THE NR 1 ENGINE HYDRAULIC PUMP IAW EMB 145 AMM 29-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,044 hrs · 19,700 cycles

EMERGENCY LIGHT IN SERVICE DOOR AND AT SEAT 12 BC AT TOP INOP. REMOVED AND REPLACED BULBS IAW EMB 145 AMM 33-50-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 19,294 hrs · 17,805 cycles

SHV - DURING C-CHECK THE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS FOUND TO BE ERRODED AND HAVE PITTING CORROSION ON THE UPPER AND LOWER SURFACES. MAINTENANCE REMOVED AND REPLACED THE LEFT HORIZONTAL STABILIZER LEADING EDGE IAW EMB 145 AMM 55-15-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 12,924 hrs · 17,805 cycles

SHV - DURING C-CHECK THE NR 2 ENGINE INTAKE FLANGE WAS FOUND TO BE CORRODED AROUND THE BOLT HOLES. MAINTENANCE REMOVED AND REPLACED THE INTAKE IAW EMB 145 AMM 71-60-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 19,294 hrs · 17,805 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 24 AND 29. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED SHIM FILLER REPAIRS AT FR 24 AND 29 IAW EMB 145 SRM 53-00-10, PG 212, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,294 hrs · 17,805 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE CLEANED THE AREAS OF CORROSION AND FOUND THE DAMAGE TO BE OUT OF LIMITS AT FRAME 24 AND FRAME 29. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED SHIM FILLER REPAIRS IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,294 hrs · 17,805 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 203 DET A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,294 hrs · 17,805 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLES. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER/FILLER REPAIR IAW EC5320-01257, REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — FAILED (NR 2 ENGINE) · airframe 18,662 hrs · 17,015 cycles

VCT - FLIGHT 2482, THE CREW REPORTED A LAV SMOKE WARNING FOLLOWED BY A LOW OIL PRESSURE INDICATION, AND AN ENGINE 2 FIRE WARNING. THE CREW SHUTDOWN THE NUMBER TWO ENGINE, AND DIVERTED TO VCT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (COCKPIT) · airframe 16,569 hrs · 14,539 cycles

IAH - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL ON TAKEOFF AND A WEIGHT ON WHEEL FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0453 & K0352, OPERATIONALLY CHECKED WITH NO DEFECTS, THE AIRCRAFT WAS SATISFACTORILY TEST FLOWN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. BOTH RELAYS ARE THE SAME PART NUMBER, NOT SERIALIZED, AND NO TIMES ARE AVAILABLE.

Part: CONTROL UNIT — INOPERATIVE (LANDING GEAR) · airframe 16,565 hrs · 14,532 cycles

CRP - THE CREW REPORTED THAT DURING TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (MLG) · airframe 16,428 hrs · 14,345 cycles

DURING CLIMB THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. THE CREW PERFORMED AN OVER-RIDE TO RETRACT GEAR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). THE GEAR OPERATIONALLY TESTED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — DISCONNECTED (CABIN) · airframe 15,841 hrs · 2,802 cycles

IAH- FLIGHT 2729, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE LAST THREE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER SIX INVERTER TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 15,760 hrs · 13,472 cycles

CLE - FLIGHT 2562, THE CREW REPORTED THE AFT HALF OF THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESEATED THE CONNECTOR AT THE AFT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — BURNED (CABIN) · airframe 15,346 hrs · 12,991 cycles

CRP - FLIGHT 2207, DURING POST FLIGHT INSPECTION THE CREW REPORTED A ELECTRIC BURNING SMELL COMING FROM THE FORWARD CABIN. MAINTENANCE REMOVED THE LIGHT BULB FROM ROW 6/7, AND MEL'D THE LIGHT UNDER MEL 33-20-001 CONTROL 044887, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/10/04, IAH MAINTENANCE REMOVED AND REPLACED THE SIDEWALL LIGHT FIXTURE AT SEAT 6A, IAW EMB-145 M/M 33-21-06, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SERVICE DOOR LOWER THRESHOLD 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 WILL BE RETURNED TO SERVICE UPON COMPLETION OF C-CHECK.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 15,249 hrs · 12,861 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

DURING C-CHECK THE SHEAR CLIP AT FRAME 67, BETWEEN STRINGER 6L AND 7L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 15,249 hrs · 12,861 cycles

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

Part: FIREWALL — CRACKED (APU BAY) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 3, FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CRACKED (BATTERY BAY) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE BATTERY COMPARTMENT CENTER RIB WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: SILL — CRACKED (CABIN) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR CLEAT AT FRAME 73 STR 9R-11R WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR CLEAT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

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

Part: SILL — CORRODED (CABIN) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 59-61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: SILL — CORRODED (CABIN) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AT FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59-61 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: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM JUST FORWARD OF FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01129. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED AT FRAME 68 AND STRINGERS 6R-7R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

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

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED FROM FRAME 17 TO 18. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE FORWARD DIGITAL A FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

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

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SVH - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPAR — CRACKED (LT WING) · airframe 15,249 hrs · 12,861 cycles

DURING C-CHECK EDDY CURRENT INSPECTION USING EDDY CURRENT PROBE TEST BLOCK TB-M030B AS A STANDARD, LT WING SPAR 3 UPPER O/B HOLE FOR TORQUE BOX 1 ATTACH REVEALED A CRACK. MX REAMED HOLE TO 8.382MM(.330) AND REINSPECTED. CRACK WAS NOT REMOVED. HOLE WAS REAMED TO 8.763MM (.345) AND REINSPECTED. CRACK FOUND TO BE REMOVED. SINCE 2ND OVERSIZE CORRESPONDING FASTENER TO REAMED HOLE SIZE, P/N AIC791-05011Y, IS NOT AVAILABLE. MX REAMED HOLE TO .377 - .378 (V-SIZE REAMER) AND INSTALLED MS21134-06011 USING TORQUE VALUES OF 175 IN-LB, (19.8 N-M). MX INSTALLED A WASHER (MS21299-C6) UNDER THE HEAD OF THE BOLT, AND WASHER (MS21299-6) AND NUT (MS21133-06). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 2, FIG 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CARGO) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 61 AND 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (NR 2 NACELLE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CARGO FORWARD PARTITION FRAME DOUBLER WAS FOUND TO BE CORRODED AT FRAME 61 BETWEEN STRINGERS 16L AND 17L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (NR 2 NACELLE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CRACKED (FRAME) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE DOUBLER ON FRAME 61 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 39-45. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 15,243 hrs · 12,855 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

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

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 53-58. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 15,243 hrs · 12,855 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

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

Part: RIB — CHAFED (ENGINE COWL) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE NR 1 UPPER ENGINE COWLING FT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,259 hrs · 12,861 cycles

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

Part: DOUBLER — CORRODED (FRAME) · airframe 15,249 hrs · 12,861 cycles

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

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 15,249 hrs · 12,861 cycles

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

Part: BRACKET — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 TO 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · airframe 15,243 hrs · 12,855 cycles

SHV - DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,243 hrs · 12,855 cycles

SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. MAINTENANCE WILL REPLACE THE AFFECTED BUTTSTRAP WHEN PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,249 hrs · 12,861 cycles

SHV - DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02 AND WILL REPLACE THE AFFECTED ANGLE WHEN THE PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: WARNING SYSTEM — FALSE INDICATION (MLG)

CLE FLIGHT 2201 THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE DURING APPROACH INTO SDF. THE LANDING GEAR WAS RECYCLED AND THE MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED MULTIPLE GEAR OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT)

CLE FLIGHT 2067 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE FORWARD RIGHT EMERGENCY EXTERIOR WING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: STALL WARNING — FAULTY (COCKPIT) · airframe 12,585 hrs · 10,150 cycles

CREW REPORTED, TAKEOFF CONFIGURATION WARNING ON TAKEOFF ROLL THROUGH 50 KNOTS, WITH AIRCRAFT IN PROPER CONFIGURATION. TAKEOFF ABORTED AND RETURNED TO GATE. MAINTENANCE PERFORMED TAKEOFF CONFIGURATION CHECK TEST IAW EMB145 AMM 31-51-00. OPS CHECKED GOOD. NO FAULTS FOUND AS PER FIM REFERENCE 31-51-00-810-804-A. ON NEXT TAKEOFF ATTEMPT CREW REPORTED, TAKEOFF CONFIGURATION WARNING ON TAKEOFF ROLL THROUGH 60 KNOTS WITH AIRCRAFT IN PROPER CONFIGURATION. MAINTENANCE REMOVED AND REPLACED STICK PUSHER IAW EMB145 AMM 27-36-04. OPS CHECKED GOOD. AIRCRAFT TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: TRACK — WORN · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the right inboard flap, outbd track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: ARM — GOUGED · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the upper rotation arm on the cabin door was found gouged. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0360/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: TRACK — WORN · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the right outboard flap, inbd. track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: BUSHING — OUT OF POSITION (PAX DOOR) · airframe 10,914 hrs · 8,556 cycles

TYS, DURING A SCHEDULED 1C INSPECTION, THE MAIN CABIN DOOR HOLD OPEN LATCH BUSHING MIGRATING. MAINTENANCE REINSTALLED BUSHING IAW-EMB-GST-1682/01, REPAIR PROCEDURES ARE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BELLCRANK — GOUGED · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the left elevator attach bellcrank was found gouged. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0415/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: TRACK — WORN · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the right outboard flap, outbd. track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: TRACK — WORN · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the right inboard flap track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection.

Part: AXLE — GOUGED (NLG) · airframe 10,914 hrs · 8,556 cycles

TYS DURING A SCHEDULED 1-C INSPECTION THE NLG AXLES HAD SOME SMALL GOUGES NOTED. A GST WAS ISSUED GST 0389/02 THAT STATED BLEND AREA AND APPLY NDI AND IF NO CRACKS ARE FOUND, RESTORE PROTECTIVE FINISH. NO CRACKS WERE FOUND. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BRACKET — GOUGED (Zone 300) · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection a gouge was found on the outboard fitting of the left elevator spring tab. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored the protective finish I/A/W-EMB-GST-0361/02, repair procedures were satisfactory and the aircraft will be released upon complection of inspection.

Part: FITTING — GOUGED · airframe 10,914 hrs · 8,556 cycles

TYS, During a scheduled 1C inspection, the forward left drag brace, frame side of the nose landing gear main brace strut bearing surface was found gouged. Maintenance blended the damage and performed dye penetrant inspection (no defects noted) alodined, primed and panted I/A/W-GST-0348/02. Repair procedures are satisfactory, aircraft will be released upon complection of inspection.

Part: FITTING — DAMAGED (RUDDER) · airframe 10,914 hrs · 8,556 cycles

DURING A SCHEDULED 1C INSPECTION, THE NR 3 HINGE FITTING FROM TOP OF RUDDER 1, AFT EDGE HAS DAMAGE. MAINTENANCE BLENDED THE DAMAGE AND PERFORMED DYE PENETRANT INSPECTION (NO DEFECTS NOTED) ALODINED, PRIMED AND PANTED I/A/W-GST-0362/02. REPAIR PROCEDURES ARE SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION.

Part: PITOT TUBE — MISWIRED (PITOT HEAT) · airframe 10,914 hrs · 8,556 cycles

DURING A SCHEDULED 1C INSPECTION, THE PITOT AND STATIC PORT HEATING CHECK FAILED STEP 29 OF TASK CARD 30-31-00-710-001-AOO, WHEN HEATING/PITOT 1 CIRCUIT BREAKER IS PULLED THE STATIC PORTS 1 AND 2 BECAME COOL INSTEAD OF 1 AND 4. MAINTENANCE REWIRED STATIC PORT HEATERS NR 2 AND 4, OPERATIONAL CHECKED GOOD. REPAIR PROCEDURES ARE SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION.

Part: CHARGER — DEFECTIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — LOOSE (CONNECTOR)

IAH - FLIGHT 3426, THE CREW REPORTED MULTIPLE UNCOMMANDED RUDDER DEFLECTIONS WITH THE YAW DAMPER ENGAGED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND PIN 12 ON CONNECTOR J0881 TO BE LOOSE. MAINTENANCE RESECURED THE PIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — DIRTY (PAX DOOR)

IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED CLEANED AND REINSTALLED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOORBEAM AT FRAME 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

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

Part: STRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP AT FRAME 59 THROUGH FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: APU — FAILED (APU COMPARTMENT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SMOKE COMING FROM THE LEFT PACK. MAINTENANCE REMOVED AND REPLACED THE AUXILLARY POWER UNIT AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL MODULE — INOPERATIVE (COCKPIT)

EWR - CREW REPORTED EMERGENCY LIGHT SWITCH ON F/A PANEL WILL NOT ON EMERGENCY LIGHTS. MAINTENANCE FOUND BAD EMERGENCY LIGHT CONTROL MODULE. REMOVED AND REPLACED WITH A SERVICEABLE UNIT AND OPS CHECKED SYSTEM GOOD. (M)

Part: ENGINE — FAILED (RIGHT)

EWR - FLT 4106 - CREW REPORTED THAT DURING CLIMB, THE RIGHT ENGINE OIL PRESSURE WAS HIGH. THE AIRCRAFT WAS FERRIED TO CLE, AFTER TROUBLESHOOTING THE OIL SYSTEM THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRSS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FADEC — INOPERATIVE (NR 1 ENGINE)

IAH - FLT 4152 - DURING FLIGHT, CREW NOTICED THE NR 1 ENGINE N1 WAS LOW. THE ENGINE WENT INTO AUTO SHUTDOWN AND AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE B-SYSTEM FADEC IAW EMB-145 MM CHAPTER 73-22-01 AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: TORQUE TUBE — BROKEN (RT ENGINE)

STL - FLT 4097 - CREW REPORTED THE RIGHT ENGINE HAD LOW N1 INDICATED. THE AIRCRAFT LANDED AT STL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT ENGINE AND FOUND THE COMPRESSOR VARIABLE VANE TORQUE TUBE BROKEN. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)