N15932

Part: BATTERY — OVERTEMP (NR 2) · airframe 26,108 hrs · 24,802 cycles

DFW - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 24,616 hrs · 23,206 cycles

IAH - DURING MAINTENANCE INSPECTION AN OIL SMELL WAS REPORTED IN THE CABIN WITH THE NR 2 ENGINE BLEED AND PACS ON FULL HOT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 2) · airframe 24,616 hrs · 23,206 cycles

IAH - FLIGHT 2619, THE CREW REPORTED A BURNING RUBBER SMELL FROM THE PACKS IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,374 hrs · 22,941 cycles

TYS - A/C IN FOR AN A-CHECK WHEN INSPECTION FOUND THE MAIN PAX DOOR EXIT SIGN EMERGENCY LIGHT TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER AND OPS CHECK GOOD IAW EMB 145 AMM 33-50-11. AIRCRAFT RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,916 hrs · 22,444 cycles

IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 8 & 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LANDING GEAR — LOW (NLG) · airframe 23,899 hrs · 22,429 cycles

FLIGHT 2468, AFTER TAKEOFF THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, SERVICED THE NLG, OPS TESTED THE AIR/GRND SYS WITH NO DEFECTS NOTED. THE ACFT WAS SUBSEQUENTLY TEST FLOWN SATISFACTORILY, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 23,899 hrs · 22,428 cycles

FLIGHT 2934, DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMED OPS TEST ON THE GEAR EXTENSION/RETRACTION SYS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 23,770 hrs · 22,302 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: INLET — CORRODED (NR 1 ENGINE) · airframe 23,542 hrs · 22,071 cycles

AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND EIGHT BOLT HOLES ON THE NUMBER ONE ENGINE INTAKE INLET THAT WERE CORRODED. MAINTENANCE REPAIRED THE CORRODED BOLT HOLES IAW EC5420-01158 BY USING REAMERS AND NEW BUSHINGS. ALL WORK WAS COMPLIED WITH AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: INLET — CORRODED (NR 1 ENGINE) · airframe 23,542 hrs · 22,071 cycles

DURING A C-CHECK INSPECTION EIGHT BOLT HOLES WERE FOUND SHOWING CORROSION ON THE NR 1 ENGINE INTAKE MOUNT FLANGE. THE HOLES WERE CLEANED AND REAMED TO REMOVE ALL TRACES OF CORROSION IAW EC 5420-01158. A/C IS STILL IN C-CHECK.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 23,542 hrs · 22,071 cycles

FRAME 31 HAS MAINTENANCE INDUCED DAMAGE STR 15R AND 16R. CUT OUT DAMAGE AREA ON FRAME 31 & FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-04. AIRCRAFT STILL IN C-CHECK.

Part: BALLAST — BURNED (CABIN) · airframe 23,428 hrs · 21,955 cycles

DURING POST FLIGHT INSP, CREW REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT AND F/A JUMPSEAT AREA WITH NO VISIBLE SMOKE. MX INSPECTED THE ACFT, AND R&R THE LIGHTING BALLAST AT SEAT 1A, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG)

THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K)

Part: SKIN — CRACKED (RT WING) · airframe 21,653 hrs · 20,185 cycles

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A CRACK IN THE UPPER RT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08976, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 20,462 hrs · 18,902 cycles

SHV - DURING ROUTINE MAINTENANCE THE BAGGAGE COMPARTMENT SMOKE DETECTOR FAILED THE OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR IAW EMB 145 AMM 26-11-01. THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · corrosion level 2 · airframe 19,613 hrs · 17,975 cycles

SHV - MAJOR - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CRACKED AT FR 22 AND CORRODED BETWEEN FRAMES 19A-22. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED DOUBLER REPAIRS IAW EMB 145 SRM 51-40-02 AND EC5320-01081, REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (FUSELAGE) · airframe 19,613 hrs · 17,975 cycles

SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR IAW EC5310-01359, STEP 1.2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 16,597 hrs · 14,441 cycles

CREW REPORTED, BURNING ODOR COMING FROM RELAY BOX UNDER GEAR PINS. MAINTENANCE PERFORMED VISUAL INSPECTION OF LEFT HAND POWER DISTRIBUTION PANEL, NO ARCING OR BURNED AREAS NOTED. FOUND FORWARD COOLING AIR DUCT DISCONNECTED, RECONNECTED DUCT AND APPLIED POWER TO THE AIRCRAFT FOR FOUR HOURS, NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 16,563 hrs · 14,404 cycles

PIT FLT 2864, THE CREW REPORTED AN ELECTRICAL BURNING ODOR. CLEVELAND SENT A MAINTENANCE CREW TO INSPECT AND TROUBLESHOOT THE ODOR, THE MAINTENANCE CREW FOUND A MAGAZINE BLOCKING THE HEATING VENT AND COULD NOT DUPLICATE THE REPORTED CONDITIONS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5320-01177. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED AT FRAME 29. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C-CHECK THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EC5320-0117. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 15,905 hrs · 13,589 cycles

DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE

Part: BEARING CAP — SCRATCHED (LT MLG) · airframe 15,905 hrs · 13,589 cycles

DURING C-CHECK, THE LEFT MAIN GEAR BEARING CAP WAS FOUND SCRATCHED IN THE BEARING TRACK. REPLACED THE AFFECTED CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE

Part: FRAME — CRACKED (FUSELAGE) · airframe 15,905 hrs · 13,589 cycles

DURING C-CHECK EDDY CURRENT INSPECTION OF THE PASSENGER DOOR STOP ATTACHMENT AT STRING 14L HAD A CRACK INDICATION. REAMED HOLE TO OVERSIZED CONDITION INSTALLED BUSHING IAW EC5310-01307. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 15,397 hrs · 13,025 cycles

ATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 14,695 hrs · 12,123 cycles

TYS A/C 932 WAS IN FOR A SERVICE CHECK AND MAINTENANCE FOUND THE LEFT CABIN WALL EXIT LIGHT DAMAGE. MAINTENANCE REMOVED AND REPLACED THE EXIT WALL LENS IAW 145 AMM 33-50-13. OPS CHECK GOOD ALL WORK WAS COMPLIED WITH AND RELEASED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,038 hrs · 11,413 cycles

CREW REPORTED, EMERGENCY AISLE PATH FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY AISLE PATH FLOOR LIGHT STRIP IAW EMB145 MM 33-50-00. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2163 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED.

Part: INVERTER — FAILED (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGNS IN AISLE OVER EXIT DOORS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DIRTY (CABIN)

CLE FLIGHT 2163 THE CREW REPORTED THE EXIT SIGN OVER ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR FOR THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CREW REPORTED A CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE CABIN EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT NR 2066 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT EXIT LOCATOR. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 2256, THE CREW REPORTED THE EXIT LIGHT OUT AT ROW 12A. MAINTENANCE INSPECTED AND RESECURED LOOSE CONNECTOR AT THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT 2300 THE CREW REPORTED THE EMERGENCY EXIT SIGN AT 12A WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — INTERMITTENT (RT MLG)

CLE FLIGHT 3292 THE CREW REPORTED A BANGING NOISE IN THE LANDING GEAR WHEELWELL ON GEAR EXTENSION.THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RT MLG DOWNLOCK PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE · airframe 11,525 hrs · 8,947 cycles

SHV- DURING C-CK INSPECTION, THE MAIN DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CHECK INSPECTION, THE RT OUTBOARD OMEGA BEAM AT FRAME 55 WAS FOUND TO BE CORRODED AROUND A SCREW HOLE. MAINTENANCE REMOVED THE CORRODED SECTION AND INSTALLED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01065, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM AT FRAME 59 WAS FOUND TO BE CORRODED AROUND A NUT PLATE. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01065 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 & 25. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND OUTBOARD BUTT STRAP WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-20-03.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CK INSPECTION, THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 59 & 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 & 23. MAINTENANCE REMOVED THE DAMAGED SECTION OF FLANGE AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01219, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV- DURING C-CK INSPECTION, THE RIGHT HAND INBOARD FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM IAW EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,525 hrs · 8,947 cycles

SHV - DURING C-CK INSPECTION, THE CENTER STRAP AT BETWEEN FRAMES 14 AND 17 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE STRAP, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-21-02, AND THE AIRCRAFT WAS APPROVED FOR RTEURN TO SERVICE.

Part: WIRE — LOOSE (CABIN)

CLE FLIGHT# 3154 THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT WAS NOT ILLUMINATING WHEN TESTING.MAINTENANCE INSPECTED AND RESECURED A LOOSE WIRE ON THE OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPRESSOR — LEAKING (NR 2 ENGINE) · airframe 8,987 hrs · 6,735 cycles

LAV SMOKE WARNING EICAS AND ALARM IN CABIN AFTER TAKEOFF. WARM PACK SMELL, NO VISIBLE SMOKE OR FIRE AIRCRAFT RELEASED IAW MEL 26-14-00 PLACARD 012059. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE AFTER FINDING EVIDENCE OF OIL LEAKAGE IN ENGINE COMPRESSOR SECTION IAW TASK CARD 6271001. OPS CHECKS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 8,961 hrs · 6,711 cycles

CREW REPORTED, LAV SMOKE WARNINGS ON TAKEOFF. NO VISIBLE SMOKE OR SMELL. EWR MAINTENANCE INSPECTED AIRCRAFT TROUBLESHOT NR 1 ENGINE CARBON SEAL LEAKING AIRCRAFT MAINTENANCE FERRIED TO BTV FOR ENGINE SEAL REMOVAL AND REPLACE. FOR COMPANY CONVENIENCE, NR 1 ENGINE REMOVED AND REPLACED IAW TASK CARD 6271001. ALL OPERATIONAL AND LEAK CHECKS COMPLETED. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 8,960 hrs · 6,708 cycles

FLIGHT CREW REPORTED, LAV SMOKE DETECTOR IS GIVING NUMEROUS FALSE WARNINGS IN FLIGHT. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB145 MM REFERENCE 26-14-01, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 8,954 hrs · 6,702 cycles

CREW REPORTED, LAV SMOKE WARNING AFTER DEPARTURE WITH NO INDICATION OF SMOKE IN LAV. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION SYSTEM, OPS CHECKED GOOD IAW EMB145 MM REFERENCE 26-14-00.

Part: RECEPTACLE — BURNED (GALLEY)

CLE FLIGHT 3992 THE CREW REPORTED A BURNING SMELL IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE OUTBOARD HOT JUG RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: O-RING — LEAKING (BLEED AIR SYS)

CLE FLIGHT 4293, THE CREW REPORTED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED AN O-RING ON THE NR 1 BLEED LINE IN THE CARGO BAY. OPERTIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

BTV - FLT 3944 - DURING 4A INSPECTION, MAINTENANCE FOUND TWO INOPERATIVE EMERGENCY LIGHTS AT PSU SEAT 12A AND SEAT 12BC LOCATIONS. REMOVED AND REPLACED BULB WITH SERVICEABLE UNITS. OPS CHECKED GOOD. (M)

Part: SMOKE — DETECTED (CABIN)

YUL - FLT 4005 - THE CREW REPORTED SMOKE IN CABIN AND COCKPIT. THE AIRCRAFT RETURNED TO YUL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE AIR CONDITION SYSTEM IAW 21-00-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: BUSHING — GROOVED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GROOVED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE PITTED AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GROOVED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — CORRODED (VERTICAL STAB)

IAH-DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER TO HORIZONTAL STABILIZER LEFT HAND AND RIGHT HAND SPHERICAL BEARINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS IN ACCORDANACE WITH EMB145 M/M 55-37-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING C-CHECK INSPECTION THE NUMBER ONE AND NUMBER TWO EMERGENCY LIGHT POWER SUPPLIES WERE FOUND TO BE INOPERATIVE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE NR ONE 1 AND NR 2 EMERGENCY LIGHT POWER SUPPLIES WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) REF C2XA00IA331.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

REFERENCE OPEN SDR C2XAOOIA331 DURING CHECK INSPECTION THE NUMBER ONE AND NUMBER TWO EMERGENCY LIGHT POWER SUPPLIES WERE FOUND TO BE INOPERATIVE. MX REMOVED/REPLACED AFFECTED EMERGENCY LIGHT POWER SUPPLIES, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

REFERENCE OPEN SDR C2XAOOIA338-IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM GUSSET AT FRAME 20-23 WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.CLOSED BY:C2XA00IA355

Part: FLOORBEAM — CORRODED (CABIN)

DURING C-CHECK INSPECTION, RT FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. SDR FILED OPEN AWAITING FINAL CORRECTIVE ACTION.

Part: GUSSET — CORRODED (CABIN)

REFERENCE OPEN SDR C2XA00IA336 DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM GUSSET AT FRAME 20-23 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED GUSSETT IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM RAMP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP IAW EMBRAER 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: GUSSET — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM GUSSET AT FRAME 20-23 WAS FOUND TO BE CORRODED. MX REMOVED / REPLACED THE AFFECTED GUSSETT IN ACCORDANCE WITH EMB 145 SRM 51-40-02 AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND FLOOR BEAM REPAIR DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED REPAIR DOUBLER IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

REFERENCE OPEN SDR C2XAOOIA338 DURING C-CHECK INSPECTION RT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMBRAER 145 SRM 5140-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

DURING C-CHECK INSPECTION, THE LT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.

Part: PIN — CORRODED (HORIZONTAL STAB)

REFERENCE OPEN SDR C2XAOOIA337-IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN AND A/C WAS APPROVCED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND FLOORBEAM GUSSET AT FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

DURING C-CHECK INSPECTION R/H HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.

Part: FLOORBEAM — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED FLOORBEAM IN ACCORDANCE WITH EMBRAER SST 1274/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

REFERENCE OPEN SDR C2XA00IA332 DURING C-CHECK INSPECTION, RT FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. MX REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

REFERENCE OPEN SDR C2XAOOIA332 IAH-DURING C-CHECK INSPECTION, RT FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 59 TO FRAME 61. MX REMOVED/REPLACED THE AFFECTED SECTION OF FLOORBEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — CORRODED (HORIZONTAL STAB)

REFERENCE OPEN SDR C2XA00IA337 DURING C-CHECK INSPECTION, LT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND FLOOR BEAM GUSSET AT FRAME 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM AT FRAME TWENTY WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE DAMAGED SECTION OF FLOORBEAM. (M)

Part: UNKNOWN — SMOKE (CABIN)

YUL - FLT 4005 - AIR RETURNED DUE TO SMOKE FILLING CABIN AND COCKPIT. MAINTENANCE OPERATIONALLY CHECKED AIRCONDITIONING IN REF TO EMB145 MM 21-00-00. OPS CHECKED GOOD. SUBMITTER STATES, SUSPECT DE-ICING FLUID ON T/O RAN INTO APU INLET CAUSING SMOKE. (M)

Part: SENSOR — INOPERATIVE (NR 1 NACELLE)

EWR - FLT 4027 - CREW REPORTED SMELL OF SMOKE IN FLIGHT AT FULL CLIMB POWER. FOUND SMOKE SMELL CAUSED BY PRECOOLER SENSOR INOPERATIVE. REMOVED AND REPLACED PRECOOLER SENSOR, OPERATIONALLY CHECKED AND TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: APU — SMOKING (CABIN)

CLE - FLT 4233 - THE CREW REPORTED THAT AFTER THEY STARTED THE APU, THEY GOT THE LAV AND BAGGAGE SMOKE WARNING ALONG WITH SMOKE IN THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED THE APU AND PLACED IT ON MEL 49-00-00 CONTROL NR 18372B CAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: BULB — FAILED (ROW 11)

BTV - DURING ROUTINE, FOUND EMERGENCY LIGHT IN CEILING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB IN EMERGENCY EXIT LIGHTS. OPS CHECKED GOOD. (M)

Part: ENGINE — FAILED (RIGHT)

CLE - DURING A SCHEDULED BORESCOPE INSPECTION THE RIGHT ENGINE HIGH PRESSURE TURBINE BLADE TRACK WAS FOUND TO HAVE SEVERAL BURN HOLE THAT WERE BEYOND MANUFACTURE LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTENENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM AT FRAME TWENTY WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE DAMAGED SECTION OF FLOORBEAM IAW WITH CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (LT EMER EXIT)

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

Part: CONNECTOR — MALFUNCTIONED (LT ENGINE)

CLE - FLT 4019 - CREW REPORTED THAT DURING CRUISE THE LEFT ENGINE OIL TEMPERATURE PEGGED OUT (135 DEGREES CELSIUS) AND WOULD NOT DECREASE WITH A THRUST DECREASE, A PRECAUTIONARY ENGINE SHUT DOWN WAS PERFORMED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FAULTY CONNECTOR IN THE INDICATION SYSTEM. THE CONNECTOR WAS REMOVED AND REPLACED REFERENCES EMB-145 MM 79-30-50. (M)

Part: CLAMP — BROKEN (CARGO BAY)

BNA - FLT 4048 - CREW REPORTED AFTER TAKEOFF AND AT ABOUT 11,000 FT, HEARD LOUD NOISE AND RECEIVED A NR 1 DUCT LEAK LIGHT AND CARGO SMOKE WARNING. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCARFT AND FOUND A BLEED DUCT UNDER THE CARGO FLOOR HAD SEPARATED AT THE UNION. MAINTENANCE REMOVED AND REPLACED A CLAMP AT THE DUCT UNION IAW EMB-145 MM 36-11-09, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ACTUATOR — FAILED (RT MLG UNLOCK)

CLE - FLT 4032 - CREW REPORTED THAT UPON TAKEOFF THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UNLOCK ACTUATOR IAW EMB145 MM 32-33-09, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

CLE - FLT 9500 - CREW REPORTED DURING TAKEOFF, THE LEFT ENGINE OIL PRESSURE EXCEEDED MANUFACTURES LIMITS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPERSS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: O-RING — FAILED (NR 1 HYD SYSTEM)

CLE - FLT 4227 - CREW REPORTED WHILE EN ROUTE FROM EWR, THEY RECEIVED A HYDRAULIC LOW QUANTITY SYSTEM 1 INDICATION FOLLOWED BY PRESSURE LOSS AND THE FAILURE OF THE SYSTEM. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A FAILED O-RING AT THE NR 1 HYDRAULIC SYSTEM PRIORITY VALVE IAW EMB-1465 MM 29-10-13. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS ALSO REMOVED AND REPLACED IAW EMB-145 MM 29-10-03 AS A PRECAUTION. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)