N15926

Part: SKIN — CRACKED (ZONE 200) · airframe 32,772 hrs · 31,835 cycles

FUSELAGE SKIN BETWEEN THE CAPT WINDOW CUTOUT FRAME FWD TOP CORNER AND CAPT LT WINDSHIELD CUTOUT FRAME TOP OTBD CORNER CRACKED. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED 2 SHIMS AND A DOUBLER IAW ETD2013-145-041246. ACFT RELEASED TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,844 hrs · 30,904 cycles

DURING CYCLE CARD INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE MULTIPLE CRACKS ORIGINATING FROM RIVETS AT FRAME 75 STR 2L AREA. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,844 hrs · 30,904 cycles

DURING CYCLE CARD INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 6MM CRACK AT FRAME 75, STR 2R. MX PERFORMED A DOUBLER REPAIR IAW CHANGE/REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 600) · airframe 30,960 hrs · 30,008 cycles

DURING A-CHECK INSPECTION THE RT WING SKIN WAS FOUND TO HAVE A .70" LOG CRACK AT THE CUT-OUT FOR THE SPOILER CENTER HINGE POINT. INSTALLED A REPAIR DOUBLER TO THE AFFECTED AREA AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TORQUE BOX — GOUGED · airframe 30,352 hrs · 29,404 cycles

HE RT WING TORQUE BOX BOLT HOLE WAS GOUGED. A TEMPORARY REPAIR WAS DONE AND PLACED ON A DMI TO PERFORM A PERMANENT REPAIR WITHIN 300 F/C STARTING 05/21/12 IAW ETD 2012-145-005036. MX REAMED THE RT WING TORQUE BOX HOLE ON THE INBD SIDE TO 9.662 MM IAW EC 5710-01188. ALSO COMPLIED WITH THE HFEC IAW SOP 7511, NO DEFECTS NOTED AT THIS TIME. ACFT WAS RELEASED TO SERVICE UPON COMPLETION OF CLOSING.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,366 hrs · 29,417 cycles

DURING MX INSPECTION THE AFT FACING OVERHEAD EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (HYDRAULIC SYS) · airframe 26,880 hrs · 25,877 cycles

IAH - FLIGHT 2213, THE CREW REPORTED THAT THE AP YAW DAMP, AND RUDDER SYS 1&2 FAILED TWICE DURING FLIGHT. THE CREW PERFORMED QRH BOTH TIMES AND SUCCESSFULLY BROUGHT BACK RUDDER SYS 1&2. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE THE NR 2 RUDDER PRESSURE SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,870 hrs · 25,866 cycles

EMERGENCY LIGHT EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT INOP. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW EMB-145 AMM 33-50-11. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 25,903 hrs · 24,850 cycles

IAH - FLIGHT 2959, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT COMING OUT OF MOB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INLET — CORRODED (NR 1 ENGINE) · airframe 24,688 hrs · 23,564 cycles

TYS ACFT CURRENTLY IN A C-CHECK STATUS AND INSPECTION FOUND THE NR 1 ENGINE INLET ATTACH FLANGE WITH CORRODED HOLES. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHIONS TO REMOVE THE CORROSION. ALL WORK WAS ACCOMPLISHED IAW EC 5420-01158.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 24,613 hrs · 23,479 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 19 WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED A BROKEN WIRE ON THE AISLE PATH LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,215 hrs · 23,032 cycles

IAH - FLIGHT 2526, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT SYSTEM DID NOT HOLD ENOUGH CHARGE TO ILLUMINATE THE CABIN CEILING WING EXIT LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE CABIN CEILING EMERGENCY LIGHT THAT IS FORWARD OF THE WING, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,205 hrs · 23,022 cycles

IAH - FLIGHT 2627, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,083 hrs · 22,890 cycles

IAH - FLIGHT 2606 - DURING PRE-FLIGHT INSPECTION THE EMERGENCY LIGHTS BY THE MAIN CABIN DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,033 hrs · 22,834 cycles

IAH - FLIGHT 2884, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN INOPERATIVE AISLE PATH LIGHT STRIP. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONAL TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 23,534 hrs · 22,311 cycles

FLIGHT 4920 - THE AIR/GROUND FAIL MESSAGE ILLUMINATED DURING CLIMB AND THE CREW ELECTED TO RETURN TO IAH. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH TO CORRECT THE DISCREPANCY, PERFORMED SUCCESSFUL LANDING GEAR EXTENSION/RETRACTION TESTS AND CLEARED THE DISCREPANCY.

Part: ELECTRONIC UNIT — FAULTY (LANDING GEAR) · airframe 23,529 hrs · 22,306 cycles

FLIGHT 4922 - DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED LANDING EXTENSION AND RETRACTION CHECKS THEN CLEARED THE DISCREPANCY.

Part: PROXIMITY SWITCH — OUT OF ADJUST (RT MLG) · airframe 23,529 hrs · 22,305 cycles

FLIGHT 2804 - IAH TO MEM- DURING CLIMB THE LANDING GEAR DID NOT RETRACT WHEN SELECTED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE RIGHT GEAR AIR GROUND PROXIMITY SWITCH WAS FOUND TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE PROXIMITY SWITCH, FUNCTIONALLY TESTED THE LANDING GEAR EXTENSION AND RETRACTION AND THE DISCREPANCY WAS CLEARED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

A/C WAS IN FOR A OVERNIGHT SERVICE CHECK AND NR 4 EMERGENCY LIGHT BATTERY WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECKS GOOD AND WAS RELEASED BACK TO SERVICE. (A)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,265 hrs · 20,814 cycles

OKC, FLIGHT 2033, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT ON THE LEFT CABIN EXIT DOOR AT SEAT 12A WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,356 hrs · 20,118 cycles

IAH - FLIGHT 2806, DURING POST FLIGHT INSPECTION, THE MIDDLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE VERIFIED NORMAL OPERATION OF THE EMERGENCY LIGHT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,152 hrs · 19,895 cycles

IAH - FLIGHT 2213, DURING PREFLIGHT INSPECTION THE AISLE PATH LIGHT STRIP NEXT TO THE LEFT HAND EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 20,975 hrs · 19,705 cycles

IAH - DURING A-CHECK INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE WIRE SPLICE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 20,899 hrs · 19,626 cycles

DURING PREFLIGHT INSPECTION, THE CREW NOTICED THAT THE FLOOR EMERGENCY LIGHTING STRIP DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED A FUSE ON THE NR 2 EMERGENCY LIGHT POWER SUPPLY. THE LIGHTS WERE OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: WIRE HARNESS — DAMAGED (CABIN LIGHTS) · airframe 20,846 hrs · 19,571 cycles

IAH - FLIGHT 2760, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN AT SEAT 3A. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CABIN LIGHTING ON MEL 3320-00/1/C CONTROL NUMBER 123251, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD LIGHTING WIRE HARNESS AT ROW 7A.

Part: LIGHT — SHORTED (CABIN) · airframe 20,835 hrs · 19,560 cycles

IAH - FLIGHT 2091, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL AT ROW 3A. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 20,569 hrs · 19,283 cycles

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

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,569 hrs · 19,283 cycles

IAH - DURING MAINTENANCE INSPECTION, THE NUMBER TWO AND THREE EMERGENCY EXIT FLOOR STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,569 hrs · 19,283 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE NUMBER TWO AND NUMBER THREE AISLE PATH LIGHT STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 20,569 hrs · 19,283 cycles

IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,542 hrs · 19,252 cycles

IAH - FLIGHT 2264, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SOME OF THE AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN (LANDING GEAR) · airframe 20,402 hrs · 19,107 cycles

IAH - FLIGHT 2810, THE CREW REPORTED THAT DURING CLIMB THE NOSE LANDING GEAR FAILED TO RETRACT AND STAYED IN TRANSITION FOR 15-20 SEC AFTER MAIN GEAR RETRACTED. ALSO THE NOSE LANDING GEAR DOORS DID NOT CLOSE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EXTENSION AND RETRACTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU BAY) · airframe 20,013 hrs · 18,662 cycles

SHV - DURING C-CHECK, APU FIREWALL HAS CHAFE DAMAGE BETWEEN 4/8 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT FR 81 IAW EMB 145 EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 19,911 hrs · 18,559 cycles

CLE FLIGHT 3120, THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 19,265 hrs · 17,859 cycles

RIC - MX DURING ACFT ROUTINE INSPECTION, MX FOUND NR 6 FLOOR PROXIMITY EMERGENCY LIGHT INOP. MX FOUND BROKEN WIRE ON ASSY CONNECTOR. MX REPAIRED BROKEN WIRE. OPERATIONAL TEST WAS PERFORMED SUCCESFULLY. ACFT APPROVED TO RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 18,459 hrs · 16,959 cycles

LANDING GEAR LEVER DISAGREE. NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, BUT HANDLE WAS UP AND MAIN GEAR SHOWED UP AND LOCKED. RECYCLED GEAR PER QRH, AND CONTINUED WITH FLIGHT. LANDED UNEVENTFULLY IN EWR. REMOVED AND REPLACED UPLOCK BOX. PERFORMED WIRING CHECKS OF WIRING OF NOSE GEAR PROXIMITY SWITCHES NR 1. REMOVED AND REPLACED LGEU, PREVIOUS PARTS DID NOT SOLVE PROBLEM. REMOVED AND REPLACED WIRING HARNESSES W014 SWUNG LANDING GEAR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SOLENOID VALVE — FAILED (NLG DOOR) · airframe 17,589 hrs · 16,003 cycles

SHV - PILOT REPORT AFTER TAKEOFF, NOSE GEAR DID NOT NORMALLY RETRACT PERFORMANCE QRH, CYCLE GEAR NOSE GEAR RETACTED NORMALLY. MAINTENANCE REMOVED AND REPLACED NLG DOOR SOLENOID VALVE IAW EMB 145 AMM 32-33-02 OPS AND LEAK CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 16,863 hrs · 15,207 cycles

AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT AND A LANDING GEAR DISAGREE MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT FERRIED TO RIC WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED MULTIPLE LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS. THE LANDING GEAR OPERATIONALLY CHECKED GOOD WITHOUT ANY FAULTS BEING NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT HOURS 16863 CYCLES 15207.

Part: CHECK VALVE — INOPERATIVE (NLG) · airframe 16,431 hrs · 14,652 cycles

CLE FLIGHT 2150, CREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE NOSE LANDING GEAR CHECK VALVE. ALL OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 16,308 hrs · 14,510 cycles

CREW REPORTED, LANDING GEAR LEVER/DISAGREEMENT WARNING ON RETRACTION, NOSE GEAR RED HATCHED INDICATION. PERFORMED CHECKLIST, RECYCLED GEAR, GEAR INDICATED NORMAL AFTER RECYCLE. EXTENDED NORMALLY FOR AIR-RETURN LANDING IN NEWARK. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER IAW EMB145 MM 32-32-01. PERFORMED LANDING GEAR OPERATIONAL CHECK MULTIPLE TIMES, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — GOUGED (STAB BEARING)

VERTICAL STABILIZER TO HORIZONTAL STABILIZER RIGHT SPHERICAL BEARING HOUSING WAS GOUGED. REWORKED HOUSING PER EC5510-01089. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,597 hrs · 13,673 cycles

DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA SHAPE WAS FOUND TO HAVE CORROSION NEAR FRAME 20. MX REMOVED THE CORRODED SECTION OF THE OMEGA SHAPE AND SPLICED IN A NEW SECTION IAW EC5320-01145. THE ACFT WILL BE RELEASED FOLLOWING THE COMPLETION OF THE 4C INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,597 hrs · 13,673 cycles

DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FLOOR SILL AT FRAME 28. THE SILL WAS REMOVED AND REPLACED IAW THE EMB SRM. ACFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,597 hrs · 13,673 cycles

DURING A SCHEDULED 4C INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW THE EMB SRM. ACFT PENDING RELEASE UPON COMPLETION OF 4C INSPECTION.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 15,597 hrs · 13,673 cycles

DURING A SCHEDULED 4C INSPECTION THE PAX DOOR SILL U CHANNEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL U CHANNEL IAW THE MFG SRM. AIRCRAFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION.

Part: SEAL — DRY (MAIN PAX DOOR)

EWR - FLIGHT 2311, THE CREW REPORTED THAT THE MAIN CABIN DOOR JAMS WHEN OPENING, AND IS VERY DIFFICULT TO OPEN. MAINTENANCE LUBED THE PASSENGER DOOR, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

CREW REPORTED, EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY ASSEMBLIES. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE. P/N OFF 2013-1A; S/N OFF 56460, 72238, 77815, AND 82294.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,462 hrs · 12,428 cycles

DURING 2A INSPECTION MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT AT AFT OF THE CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB AT THE LAST OVERHEAD EMERGENCY LIGHT IAW EMB145 33-50-00 (STANDARD PRACTICES), OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: CONTROL UNIT — FAILED (COCKPIT)

CLE FLIGHT 2693 THE CREW REPORTED THE LT MAIN LANDING GEAR REQUIRED 3 CYCLES BEFORE LOCKING IN UP POSITION. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. ALSO REPLACED THE UPLOCK BOX ASSEMBLY ON THE LEFT GEAR. OPERATIONAL CHECKS WERE GOOD.

Part: UPLOCK — DEFECTIVE (NOSE GEAR)

CLE FLIGHT 2217 THE CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY AND BOTH UPLOCK PROXIMITY SENSORS. OPERATIONAL CHECKS WERE GOOD. PROXIMITY SENSOR P/N 8-527-01 AND S/N'S OFF WERE 5105 AND15960.

Part: ACTUATOR — FAULTY · airframe 12,590 hrs · 10,545 cycles

EWR---CO3628, CREW REPORTED, "LEFTHAND MAIN GEAR WOULD NOT RETRACT." MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED #1 MAIN LANDING GEAR UNLOCK ACTUATOR IAW #32-33-09 (REFERENCE M-602 #430342). OPS.CHECKED GOOD.. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 12,578 hrs · 10,534 cycles

CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS ON TAKEOFF FROM NEWARK. AIRCRAFT AIR RETURNED TO EWR, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 MM 32-63-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAULTY

EWR---CO3533, CREW REPORTED AISLE PATH LIGHTING BETWEEN SEAT ROW 10A AND 12A INOPERATIVE....MAINTENANCE REMOVED AND REPLACED AISLE PATH LIGHTING AT THE EMERGENCY EXIT IAW EMB145 AMM #33-50-08. OPS. CHECKED SYSTEM GOOD.

Part: LIGHT — BLOWN

BTV---DURING SERVICE/ROUTINE OVERNIGHT CHECK MAINTENANCE FOUND AISLE OVERHEAD EMERGENCY LIGHT AT EMERGENCY EXIT ROW TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AT EMERGENCY EXIT OVERHEAD LIGHT IAW EMB145 AMM 33-50-00. OPS. CHECKED LIGHT GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE RIGHT HAND FORWARD WING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND FORWARD WING EMERGENCY LIGHT ASSEMBLY. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE CENTER FLOORBEAM GUSSET WAS CORRODED BETWEEN FRAMES 58 AND 60. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON RELEASE FROM C-CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE RIGHT OUTBOARD FLOORBEAM DIGITAL RECESS WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON RELEASE FROM C-CHECK.

Part: CREASE BEAM — CORRODED (CABIN)

IAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 18 and 20 WAS CORRODED AROUND THE NUT PLATES. IAH- MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM "C" CHECK.

Part: CREASE BEAM — CORRODED (CABIN)

IAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 22 and 23 WAS CORRODED AROUND THE NUT PLATES, IAH- MAINTENANCE REMOVED and REPLACED THE CREASE BEAM, AND, THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE, WHEN RELEASED FROM "C" CHECK.

Part: BULB — BLOWN (CABIN) · airframe 10,379 hrs · 8,383 cycles

TYS During a scheduled inspection the right emergency exit ceiling light was found not working. Maintenance removed and replaced the emergency light bulb, operational checks good I.A.W.-EMB-MM-33-50-08. Aircraft will be released upon complection of inspection.

Part: BELLCRANK — BROKEN (LT ELEVATOR)

MYR - DURING ROUTINE INSPECTION, THE LEFT HAND ELEVATOR BELLCRANK ASSEMBLY WAS FOUND TO BE BROKEN AT THE TORQUE TUBE MATING AREA. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BELLCRANK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FCU — FAILED (NR 1 ENGINE)

IAH - FLIGHT 3838, THE CREW REPORTED THAT ON TAKEOFF ROLL, A NUMBER ONE ENGINE CONTROL B FAIL, AND CONTROL A DEGRADE MESSAGE APPEARED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1A FADEC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (CABIN)

IAH - FLIGHT 4213, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN DOOR)

EWR - FLT 3572 - CREW REPORTED EMERGENCY LIGHT AT PAX DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED SATISFACTORY. (M)

Part: UPLOCK — FAILED (NLG)

CLE - FLT 3670 - THE CREW REPORTED THAT AFTER TAKEOFF FROM CLEVELAND, THE NOSE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK BOX ASSY IAW EMB MM 32-33-07. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: CLAMP — LOOSE (CARGO BAY)

JAN - FLT 3941 - THE CREW REPORTED A NR 1 BLEED LEAK INDICATION ON EICAS IN CRUISE, THE CREW CLOSED NR 1 BLEED VALVE AND THE BLEED LEAK MESSAGE STAYED ON. THE FLIGHT WAS DIVERTED TO JAN. THE AIRCRAFT LANDED AT JAN WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND THE RIGHT UPPER GAMMA CLAMP ASSY, IN CARGO COMPARTMENT, LOOSE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB145 AMM 36-11-09. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

DURING CONTINENTAL EXPRESS C-CHECK, THE LAST EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND WITH A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — CORRODED (VERTICAL STAB)

DURING CONTINENTAL EXPRESS C-CHECK, THE NR 1 RUDDER BOTTOM ATTACH FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ATTACH FITTING IAW EMB145 MM 55-31-01-400-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — DAMAGED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT MACHINED BULKHEAD AT FRAME 70 WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED OUT THE AFFECTED AREA IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EX5330-01135, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (SERVICE DOOR)

DURING CONTINENTAL EXPRESS C-CHECK, THE SERVICD DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (SERVICE DOOR)

DURING CONTINENTAL EXPRESS C-CHECK, THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB145 MM 33-50-09, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: DRAIN LINE — CORRODED (TOILET SERVICE)

DURING CONTINENTAL EXPRESS C-CHECK, THE DISCHARGE CUP AT TOILET SERVICE PORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DISCHARGE CUP IAW EMB 145 SRM 50-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, THE FUSELAGE SKIN AFT OF CARGO DOOR CUTOUT WAS FOUND TO BE GOUGED. MAINTENANCE INSTALLED A RIVET THROUGH SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01136, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEARING — CORRODED (RT MLG)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT MLG LEG FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IAW EMB145MM 32-10-01-400-9-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEARING — CORRODED (RT MLG)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT MAIN LANDING GEAR LEG AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IAW EMB145MM 32-10-01-400-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT FUSELAGE SKIN AFT OF FRAME 29 HAD A LIGHTNING STRIKE EXIT MARK. MAINTENANCE REPAIRED THE AFFECTED AREA OF SKIN USING A RIVET REPAIR IAW EMB 145 SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CHAFED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FRAME 68 WAS FOUND TO BE CUT BY THE LEFT OUTBOARD RUDDER CONTROL CABLE. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRES ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01028. REF C2XA98IA475. (M)

Part: SKIN — CRACKED (RT NACELLE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE AND FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR. (M)

Part: BEAM — CORRODED (CABIN)

IAH - DURNG C-CHECK INSPECTION, CORROSION WAS FOUND BETWEEN THE COMPOSIT FLOOR CROSS BEAMS AND OMEGA BEAMS AT FRAMES 20 AND 25 THE DAMAGED SECTIONS OF OMEGA BEAM WERE REPAIRED. (M)

Part: SUPPORT BRACKET — CORRODED (CABIN)

IAH - REFERENCE CONTINENTAL EXPRESS SDR CONTROL NUMBER C2XA98IA472, DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM SUPPORT RAMP WAS FOUND TO BE CORRODED FROM FRAME 13 TO FRAME 18 AND WAS REMOVED AND REPLACED. (M)

Part: ENGINE — HIGH OIL PRESS (RIGHT)

RDU - FLT 4059- DURING TAKEOFF ROLL, THE PILOT REPORTED HIGH OIL PRESSURE IN THE NR 2 ENGINE. THE PILOT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (ROW 3/6)

EWR - FLT 4281 - CREW REPORTED PSU LIGHTS OVER EMERGENCY LIGHTS ROWS 3 AND 6 AS INOPERATIVE. EMERGENCY LIGHTS TESTED GOOD, REPLACED BULBS IN PSU'S AS NECESSARY. NO EMERGENCY LIGHT PROBLEM FOUND. (M)

Part: BULB — LOOSE (LT EXTERIOR)

BTV - DURING 4A INSPECTION, FOUND LEFT OUTSIDE EMERGENCY LIGHT INOPERATIVE, FORWARD OF THE WING. MAINTENANCE RESECURED LIGHT BULB IN LEFT, FORWARD OUTSIDE EMERGENCY LIGHT SOCKET. OPS CHECKED LIGHTS GOOD. (M)

Part: VALVE — FAILED (HORIZ STABILIZER)

CLE - FLT 4099 - CREW REPORTED THAT DURING CRUISE, THE HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAILED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ANTI-ICE VALVE IAW EMB-145 MM 30-12-01, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 30-00-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (SERVICE DOORWAY)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (ROW 2)

IAH - DURNIG POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT EXIT ROW 2 RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: VALVE — FAILED (MLG)

IAH - FLT 4240 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM PRIORITY VALVE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — DAMAGED (BS 20-25)

IAH - DURING C-CHECK INSPECTION, FOUND CORROSION BETWEEN THE COMPOSITE FLOOR CROSS BEAMS AND OMEGA BEAMS AT FRAMES 20 AND 25. MAINTENANCE REPAIRED THE DAMAGED SECTIONS OF OMEGA BEAM IAW EMBRAER FAX SST-2125/98, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (BS 13-18)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CRACKED (RT NACELLE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER MODULE UPPER SKIN WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK, INSTALLED A REPAIR DOUBLER, AND REPLACED THE SHEARED FASTENERS IAW EMB145 SRM 54-40-02, AND 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CHAFED (BS 88)

IAH - DURING C-CHECK INSPECTION, FRAME 68 WAS FOUND TO BE CUT BY THE LEFT OUTBOARD RUDDER CONTROL CABLE. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01028, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CUP ASSY — CRACKED (FUSELAGE)

FLT 4225 - CREW REPORTED AIR START CONNECTOR DAMAGED BY RAMP PERSON. MAINTENANCE REMOVED AND REPLACED AIRSTART CONNECTOR BOX. OPS AND PRESS CHECKED GOOD. (M)

Part: ACTUATOR — FAILED (LT ENGINE)

EWR - FLT 4023 - CREW REPORTED DURING CLIMB-OUT, RECEIVED A LOW N1 WARNING ON THE LEFT ENGINE. THE ENGINE WAS SHUT DOWN AS A PRECAUTION AND THE AIRCRAFT RETURN TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE COMPRESSOR VARIABLE GUIDE VANE ACTUATOR IAW EMB-145 MM 75-33-01. OPERATIONAL CHECKS WERE SATISFACTORY, FEDEC 1A WAS ALSO REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — FAILED (RIGHT)

CLE - FLT 4057 - CREW REPORTED DURING CLIMB, THE RIGHT HAND ENGINE OIL PRESSURE READ IN THE UPPER 80'S (PSI) AND OCCASSIONALLY HIT THE 92 PSI CAUTION RANGE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. (X)

Part: FAIRING — ERODED (RT HORIZ STAB)

CLE - DURING THE ACCOMPLISHMENT OF A SCHEDULED INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER END CAP FAIRING WAS FOUND TO HAVE SEVERE EROSION DAMAGE ALONG THE LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND HORIZONTAL STABILIZER END CAP FAIRING IAW EMB-145 MM 55-15-00. A/C TOTAL TIME 1,635.8 HOURS. A/C TOTAL CYCLES, 1,464. (X)