N12957

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 36,064 hrs · 27,212 cycles

THE AFT EMERGENCY LIGHTS WERE REPORTED TO REMAIN ON WITH ACFT POWERED OFF. MX R & R THE NR 4 EMERGNENCY BATTERY PACK WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,534 hrs · 26,779 cycles

DURING MX INSPECTION, THE ROW 12 RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 3 BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,631 hrs · 26,051 cycles

FRAME 65, CORRODED BEYOND LIMITS FORWARD OF CARGO DOOR SILL. BLENDED OUT CORROSION AND INSTALLED A DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,631 hrs · 26,081 cycles

ACFT IS IN FOR A C-CHECK INSPECTION, WHEN INSPECTION FOUND FRAME 10 CRACKED BELOW CO-PILOTS WINDOW. MX R & R THE THE DAMAGED SECTION OF FRAME 10 IAW SRM 51-40-02, ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,631 hrs · 26,051 cycles

ACFT WAS HAVING A BIRD STRIKE INSPECTION WHEN MX FOUND A DENT FWD OF F/O WINSHIELD. MX REPAIRED THE SKIN PANEL IAW EC 5300-01033. ALL WO ACCOMPLISHED AND WAS RELEASED.

Part: BALLAST — SHORTED (CABIN LIGHTS) · airframe 32,110 hrs · 24,027 cycles

STRONG ODOR OF SOMETHING BURNING COMING FROM CABIN WITH NO SMOKE OR VISIBLE FLAME. MX R & R BALLAST ABOVE ROW 3 IAW AMM 33-21-05 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN LIGHT) · airframe 32,091 hrs · 24,012 cycles

THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT AND CABIN. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE LIGHTING BALLAST ABOVE ROW 1A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN LIGHT) · airframe 32,060 hrs · 23,989 cycles

THE CREW REPORTED A BURNING ODOR IN THE CABIN BY SEAT 1A. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE CONTROL MODULE, PC BOARD, AND LIGHT BALLAST AT SEAT 1A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — DEFECTIVE (SEAT 1 A) · airframe 32,060 hrs · 23,989 cycles

THE CREW REPORTED A BURNING ODOR IN THE CABIN BY SEAT 1A. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE CONTROL MODULE, PC BOARD, AND LIGHT BALLAST AT SEAT 1A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CIRCUIT BOARD — DEFECTIVE (SEAT 1 A) · airframe 32,060 hrs · 23,989 cycles

THE CREW REPORTED A BURNING SMELL IN THE CABIN BY SEAT 1A. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE CONTROL MODULE, PC BOARD, AND LIGHT BALLAST AT SEAT 1A, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — FAULTY (NR 1 PYLON) · airframe 31,733 hrs · 23,719 cycles

THE CREW REPORTED A NR 1 BLEED LEAK IN FLIGHT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR 1 ENGINE PRECOOLER. OPS CHECKED GOOD.

Part: MODULE — DEFECTIVE (AILERON TRIM) · airframe 31,483 hrs · 23,516 cycles

ROLL TRIM STUCK TO THE LEFT. CANNOT GET FULL TRAVEL LEFT OR RIGHT WITH AILERON EVEN WITH FULL RIGHT/LEFT RUDDER. REMOVED AND REPLACED ROLL TRIM MODULE IAW EMB 145 AMM 20-13-10 PERFORMED ROLL TRIM FUNCTION CHECK IAW EMB 145 AMM 27-14-00. OPS AND DEFLECTIONS CHECKED GOOD.

Part: RELAY — FAULTY (MLG) · airframe 30,230 hrs · 22,547 cycles

CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT ALONG WITH SPOILER FAIL AND E1-E2 IDLE STOP FAIL MESSAGE UPON LANDING. MX INSPECTED AND FOUND AIR/GROUND C/B POPPED. R & R RELAYS KO325 AND KO023. OPS CHECKS WERE GOOD.

Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 29,801 hrs · 22,181 cycles

DEN - FLIGHT 5888, THE CREW REPORTED AN ENGINE 2 FIRE DET FAIL MESSAGE ON EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 29,792 hrs · 22,176 cycles

ORD - FLT 6089 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE WHEEL WOW PROXIMITY SWITCH AND CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 29,704 hrs · 22,101 cycles

FLIGHT 2217 - BOS - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN FROM INSIDE. EWR MX ADJUSTED MAIN CABIN DOOR AFT CABLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUSHING — WORN (SPOILER) · airframe 29,666 hrs · 22,074 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT SPEED BRAKE ATTACH POINT WITH A MIGRATED HAT BUSHING WORN OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EC 5740-01152. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BRACKET — WORN (SPEED BRAKE) · airframe 29,666 hrs · 22,074 cycles

TYS - A/C CURRENTLY IN CHECK WHEN INSPECTION FOUND THE LT SPEED BRAKE MIDDLE ATTACHMENT POINT HAT BUSHION MIGRATED. MAINTENANCE REMOVED THE SPEED BRAKE BRACKET AND REPLACED BRACKET IAW SRM 51-20-03; SRM 51-40-02 AND AMM 20-10-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 29,666 hrs · 22,074 cycles

TYS - PAX DOOR LOWER FRAME HAS CORROSION AT NUT PLATE HOLES. FABRICATED DOUBLERS TO RESTORE DAMAGED AREA TO ORIGINAL FINISH.

Part: WIRE — CHAFED (ANTI-ICE SYSTEM) · airframe 29,319 hrs · 21,818 cycles

EWR FLT 2540 THE CREW REPORTED A WING ANTI-ICE FAIL MESSAGE IN FLIGHT FOLLOWED BY BLEED 1 LEAK MESSAGE ON THE EICAS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPAIRED WIRE W101-3298-24. ALSO REPLACED A CRACKED BLEED DUCT IN THE CARGO COMPARTMENT. OPERATIONAL CHECKS WERE GOOD.

Part: THERMOSTAT — BROKEN (ANIT-ICE SYS) · airframe 29,037 hrs · 21,590 cycles

FLIGT 2416 - EWR - FLIGHT CREW REPORTED WING ANTI ICE FAIL IN ICING CONDITIONS DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX REMOVED AND REPLACED LT WING ANTI ICE DUCT THERMOSTAT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 22,004 hrs · 16,593 cycles

FLIGHT 2402 - ROC - FLIGHT CREW REPORTED RT LOWER CORNER DELAMINATED ON F/O'S WINDSHIELD. CREW PERFORMED FLIGHT DIVERSION AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED F/O'S WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,729 hrs · 20,553 cycles

SHV - OVERNIGHT A/C N12957 RT OVERWING EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT ASSY IAW EMB-145 AMM 33-50-07. OPERATIONAL CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 1 ENGINE) · airframe 26,465 hrs · 19,587 cycles

NR 1 ENGINE FWD LOWER INBD YOKE HAS A CRACK. REMOVED AND REPLACED THE YOKE IAW EMB EC5450-01028.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 26,165 hrs · 19,356 cycles

FLIGHT 2227 - ALB - FLIGHT CREW REPORTED LIGHTNING STRIKE ON CLIMBING, FOLLOWED BY A BURNING SMELL IN COCKPIT FOR 5 MINUTES. NO OTHER EFFECTS OBSERVED. EWR MX PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND TIP OF RT ELEVATOR DAMAGED AND REPLACED DAMAGED TIP. BURNING SMELL WAS NOT DUPLICATED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INLET — CORRODED (NR 2 ENGINE) · airframe 24,980 hrs · 18,458 cycles

NR 2 ENG AIR INTAKE ATTACH NUTPLATE HOLES HAVE CORROSION. REAMED HOLES TO REMOVE CORROSION, PERFORMED DYE PEN INSP, ALODINED ALL HOLES AND INSTALLED BUSHINGS IAW EC5420-01186. ACFT STILL IN C-CHECK.

Part: INLET — CORRODED (NR 1 ENGINE) · airframe 24,980 hrs · 18,458 cycles

NR 1 ENG INTAKE ATTACH NUT PLATE HOLES HAVE CORROSION. REAMED HOLES TO REMOVE CORROSION ON INTAKE FLANGE, PERFORMED DYE PEN INSP, ALODINED AND INSTALLED BUSHINGS IAW EC5420-01186. ACFT CURRENTLY IN C-CHECK.

Part: ACM — SMOKE (NR 2) · airframe 24,626 hrs · 18,193 cycles

FLIGHT 2994 EWR FLIGHT CREW REPORTED ACFT CABIN FILLED WITH SMOKE WHILE PACK NR 2 DURING PREFLIGHT. EWR MX R&R NR 2 PACK AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

MSP FLIGHT NR 2373, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING DID NOT TEST FROM SEAT 3A TO 5A. MAINT REPLACED THE EMERGENCY LIGHT PATH STRIP. OPERATIONAL CHECKS WERE GOOD. (K)

Part: LIGHT — INOPERATIVE (CABIN)

FLIGHT CREW REPORTED EMERGENCY LIGHT FLOOR STRIP FROM ROWS 3A TO 5A INOPERATIVE. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,099 hrs · 17,814 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT STRIPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: CONNECTOR — LOOSE (NLG) · airframe 22,492 hrs · 16,754 cycles

CLE FLIGHT 2039 - THE CREW REPORTED A LANDING GEAR DISAGREE ON EXTENSION. MAINTENANCE INSPECTED AND RESECURED THE NOSE GEAR UPLOCK BOX CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,763 hrs · 16,215 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR, EXIT SIGN AT SEAT 3BC, AND THE EXIT SIGN AT THE LEFT ESCAPE HATCH WERE ALL INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,206 hrs · 15,831 cycles

MSP FLIGHT 3155 - THE CREW REPORTED THE EMERGENCY EXIT SIGN AT SEATS 3B AND 12A WERE INOPERATIVE. THE CREW PERFORMED A SYSYTEM RESET AND OPERATIONAL CHECKS WERE GOOD. UPON ARRIVAL IN CLEVELAND THE EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,474 hrs · 15,283 cycles

IAH - DURING MAINTENANCE INSPECTION, THE FIRST TWO AILSE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 20,451 hrs · 15,267 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND THE SVC DOOR CUTOUT AT FRM 22 WITH CORROSION AROUND TRIM NUT PLATE, BELOW LOWER AFT DOOR STOP. MAINTENANCE INSTALLED DOUBLER AT THE SVC DOOR CUTOUT FRM 22 LOWER AFT CORNER AT NUT PLATE AREA IAW EC 5310-01373. AIRCRAFT APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,435 hrs · 15,253 cycles

IAH - DURING A-CHECK INSPECTION THE SECOND AISLE PATH LIGHTING STRIP FROM THE FRONT EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 19,274 hrs · 14,327 cycles

BAGGAGE EXTINGUISHER LIGHT WILL NOT TEST. REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR IAW EMB 145 MM 26-15-01. OPS CHECK GOOD.

Part: LEVER — DEFECTIVE (MLG) · airframe 18,138 hrs · 13,457 cycles

IAH - FLIGHT 2973, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT WITH NO ASSOCIATED EICAS INDICATIONS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 17,196 hrs · 12,716 cycles

CREW REPORTED, OVERWING EMERGENCY LIGHT NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY [POWER SUPPLY] AND OPS CHECKED SYSTEM GOOD IAW EMB145 AMM NR 33-50-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,853 hrs · 12,441 cycles

CLE - FLIGHT 2917 THE CREW REPORTED THE 1ST ROW OF THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT PATH STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 16,294 hrs · 12,003 cycles

DURING MAINTENANCE INSPECTION, THE RIGHT FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITHOUT DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,630 hrs · 11,495 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY CENTER OMEGA BEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY CENTER OMEGA BEAM IAW EMB-145 SRM-51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,630 hrs · 11,494 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 + 30. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM IAW EMB 135/145 SRM-51-40-02.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 14,740 hrs · 10,824 cycles

EWR- CO2355, CREW REPORTED THE FORWARD OVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT SIGN INVERTER IAW EMB 145 MM NR 33-50-11. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,500 hrs · 10,637 cycles

DURING INSPECTION FORWARD LOWER AND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER 1 INVERTER. OPS CHECK GOOD.

Part: LIGHT — INTERMITTENT (EMERGENCY LIGHTS) · airframe 15,872 hrs · 11,682 cycles

PREFLIGHT INSP FOUND EXIT LIGHTS WERE INOP. MX RESET SYSTEM. OPS CHECKED EXIT LIGHTS WITH NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

CLE FLIGHT 2390, PILOT REPORTED THAT THE COCKPIT ENTRANCE EMERGENCY LIGHT OPERATES INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND OPERATIONALLY TESTED THE LIGHT ASSEMBLY.

Part: PUMP — LEAKING (NR 2 ENGINE)

FLIGHT 2680, DURING DESCENT THE CREW NOTED THAT HYD. 2 LOW QTY MES ON EICAS, LOSS OF FLUID IN FLIGHT, DECLAIRED EMERGENCY, AND, PERFORMED EMERGENCY DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED A LEAK CHECK, AND, A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (PAX DOOR) · airframe 11,582 hrs · 8,358 cycles

DURING A SCHEDULE 3-C INSPECTION, THE PAX DOOR CENTER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR CENTER SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: COMPUTER — FAULTY (COCKPIT)

IAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE PITCH TRIM MAIN SYSTEM WAS INOPERATIVE AND NO TRIM INDICATION. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER, PERFORMED OPERATIONAL CHECKS AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTY (COCKPIT)

IAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE CABIN ALTITUDE AND RATE WERE MISSING, AND THE CREW WAS UNABLE TO CONTROL THE CABIN ALTITUDE. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 8,930 hrs · 6,262 cycles

TYS DURING A ROUTINE CHECK, MAINTENANCE FOUND THE LEFT FORWARD FAIRING EXT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE INVERTER FUSE AT THE NR 1 EMERGENCY POWER SUPPLY IAW EMB 145 AMM 30-50-50. OP'S CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE)

CLE FLIGHT 3303 THE CREW REPORTED ON APPROACH THE NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUT. AFTER ADVANCING LEVER RAPIDLY THE ITT SPIKED TO APPROX 800 DEGREES. THE CAPTAIN SHUT DOWN THE NR 2 ENGINE AS A PRECAUTION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND HIGH PRESSURE TURBINE BLADE DAMAGE TO 3 BLADES. THE DAMAGE WAS OUT OF LIMITS. THE ENGINE WAS REPLACED ALONG WITH THE TWO FADECS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEARING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 7,565 hrs · 5,293 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND HORIZONTAL STABILIZER SPHERICAL BEARING HOUSINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 7,565 hrs · 5,293 cycles

IAH - DURING C-CHECK INSPECTION, THE HORIZONTAL STABILIZER SLIDING BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED · airframe 7,565 hrs · 5,293 cycles

IAH - DURING C-CHECK INSPECTION, THE FIXED BUSHINGS ON THE HORIZONTAL STABILIZER ATTACHMENT WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,565 hrs · 5,293 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM AT FRAME 20 TO FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,565 hrs · 5,293 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM FROM FRAME 59 TO 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — LEAKING (RT ENGINE) · airframe 7,019 hrs · 4,911 cycles

EWR FLIGHT 4187. CREW REPORTED SMOKE IN THE COCKPIT AND CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT HAND ENGINE ZERO BEARING TO BE LEAKING. THE AIRCRAFT WAS FERRIED TO TYS AND THE RIGHT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 7,019 hrs · 4,911 cycles

EWR---CO4187 CREW REPORTED SMOKE IN COCKPIT AND AIRPLANE. DECLARED EMERGENCY AND RETURNED TO EWR. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING FOUND NR ENGINE LEAKING OIL AT BOTTEM OF FAN, SUSPECT ZERO BEARING. RAN BOTH ENGINES AT POWER, NO SMOKE NOTED. AIRCRAFT BEING MAINTENANCE FERRIED TO TYS FOR ENGINE CHANGE.

Part: FIRE BOTTLE — FAULTY (TAIL) · airframe 6,960 hrs · 4,872 cycles

EWR---CO4148, DURING CRUISE FLIGHT SEGMENT CREW REPORTED FIRE EXT BTL E1-E2 BTL A INOPERATIVE DURING MOST OF CRUISE FLIGHT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND A FAULTY FIRE BOTTLE A-POSITION. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE IN A-POSITION AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NUT — WORN (CABIN DOOR)

MSP FLIGHT 4089 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED AND FOUND THE BOLT AND NUT ON THE INTERNAL HANDLE ASSEMBLY TO BE WORN. THE HARDWARE WAS REPLACED AND OPERATIONAL CHECKS OF THE DOOR WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. BOLT P/N IS AN3-13A.

Part: ENGINE — DAMAGED (LEFT)

AUS - FLT 3868 - THE CREW REPORTED THAT THE NR 1 ENGINE LOST OIL PRESSURE IN FLIGHT. THE CREW SHUTDOWN THE NR 1 ENGINE AND LANDED AT AUS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310--1-32, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTT STRAP WAS FOUD TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REPAIRED THE AFFECTED SECTION OF FLOOR BEAM IAW CONTINENTAL EXPRESS ENGINEEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01123, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED SECTION OF OMEGA BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01122, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BRAKE — FAILED (TE FLAPS)

CLE - FLT 3973 - THE CREW REPORTED THEY GOT A FLAP FAIL CAUTION MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT AND LEFT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27-51-01, AND REMOVED AND REPLACED THE RIGHT FLAP FLEXIBLE SHAFT NR 5 IAW EMB145 MM 27, THE FLAP CONTROL SYSTEM OPS CHECKED GOOD IAW EMB145 MM 27-51-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: STRUCTURE — DAMAGED (FUSELAGE)

BTV - FLT 4218 - DURING 1A INSPECTION, MAINTENANCE FOUND EVIDENCE OF A LIGHTNING STRIKE. PERFORMED LIGHTNING STRIKE INSPECTION, FOUND AND REPAIRED DAMAGE WITH DOUBLERS, FILLERS, AND PATCHES. PRESSURIZED AIRCRAFT LEAK CHECKED GOOD. LIGHTENING STRIKE DAMAGE JUST AFT OF FR 52 ON STR 2L, 3 RIVETS. LIGHTENING STRIKE DAMAGE ON FR 41 STR 2L, 3 RIVETS. LIGHTENING STRIKE DAMAGE ON FR 38, STR 2L, 4 RIVETS. LIGHTENING STRIKE DAMAGE IN FRONT OF FR 31, STR 2L. AFTER REPAIR AND CHECKS, ACFT RETURNED TO SERVICE. ACFT TT: 1,853.2. ACFT CYCLES: 1,330. (X)