N13995

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,155 hrs · 30,742 cycles

SKIN CREASED BETWEEN FRAMES 20-21 AND STRINGER 12L-13L. CUT-OUT DAMAGE, FABRICATED A FILLER, DOUBLER AND INSTALLED. AIRCRAFT STILL IN C CHECK.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 FIRE) · airframe 38,170 hrs · 29,226 cycles

THE CREW REPORTED AN ENGINE 1 FIRE INDICATION IN FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, OPERATIONALLY TESTED THE ENGINE 1 FIRE DETECTION SYS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL CONTROL — FAILED (APU) · airframe 37,212 hrs · 28,435 cycles

THE CREW REPORTED A STRONG FUEL ODOR DURING ROTATION, THROUGHOUT CABIN AND FLIGHT DECK WITH THE ODOR STOPPING SHORTLY AFTER WITH NORMAL FUEL FLOW AND CONSUMPTION. THE ACFT LANDED WITHOUT INCIDENT. R & R THE APU FUEL SOLENOID, OPS TESTED WITH NO DEFECTS, REMOVED THE MEL AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/23/15 THE ITEM REPEATED WITH THE CREW REPORTING THE ODOR FROM APPROXIMATELY 300' TO 1200AGL AND THAT THE ODOR SUBSIDES WITH APU SHUTDOWN. R & R THE APU FUEL CONTROL, OPERATIONALLY TESTED WITH NO DEFECTS. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — LEAKING (APU FUEL) · airframe 37,172 hrs · 28,404 cycles

DURING ROTATION, PILOT REPORTED A STRONG FUEL ODOR THROUGH CABIN AND FORWARD. MAINTENANCE PERFORMED ENGINE RUNS WITH BLEEDS 1 & 2 ON AND NO FUEL ODOR NOTED. FURTHER TROUBLESHOOTING REVEALED FUEL ODOR COMING FROM APU DUE TO LEAK FROM RIGID LINE FUEL FILTER TO FUEL CONTROL. R & R APU FUEL SOLENOID WITH OPS AND LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 36,453 hrs · 27,804 cycles

THE CREW REPORTED VAPOR/SMOKE IN THE CABIN AND COCKPIT WHEN SWITCHED TO ENGINE BLEEDS AFTER TAKEOFF. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 12-13) · airframe 35,765 hrs · 27,262 cycles

DURING C-CHECK, STRINGER 21R CORRODED BETWEEN FRAME 12-13. R & R STR 21R IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 2 ENGINE) · airframe 35,765 hrs · 27,262 cycles

DURING C-CHECK. NR 2 ENGINE FWD LOWER YOKE CRACKED. REPAIR NR 2 ENGINE FWD LOWER MOUNT IAW EC5450-01136. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAME 8-9) · airframe 35,765 hrs · 27,262 cycles

DURING C-CHECK. INTERNAL SKIN CORRODED BETWEEN FRAME 8-9 STR, 20R-21R. R & R SKIN IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAILED (FIRE DETECTION) · airframe 33,655 hrs · 25,613 cycles

THE CREW REPORTED AN ENGINE NR 2 FIRE DETECTOR FAILED MESSAGE DURING CRUISE. LASTED FOR FIVE MINUTES THEN WENT AWAY FOR ONE MINUTE THEN CAME BACK ON. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRE CONTROL MODULE IAW 26-11-03. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,409 hrs · 25,415 cycles

DURING MX INSPECTION THE COCKPIT STEP EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,650 hrs · 24,820 cycles

DURING SCHEDULED MAINTENANCE, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, BETWEEN STRINGERS 2L AND 3L. MAINTENANCE REPAIRED THE AFFECTED SKIN USING AN EXTERNAL DOUBLER. ALL WORK WAS PERFORMED IAW EC5330-02353, REV: ORIG.

Part: SKIN — DENTED (CARGO DOOR) · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK CARGO DOOR INTERNAL SKIN HAS MULTIPLE DENTS, NICKS. MX PERFORMED REPAIR ON CARGO DOOR INTERNAL SKIN AT SECTIONS A, D, AND E IAW EC5230-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK VISUAL INDICATION OF CRACKS ON FUSELAGE BETWEEN FRAMES 78-79, STRINGERS 3L-8L (6). MX PERFORMED REPAIRS TO FUSELAGE SKIN FRAMES 78-79 STRINGERS 3L-8L IAW EC5330-02739. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK VISUAL INDICATION OF CRACK AT FRAME 77 STRINGER 6R. MX PERFORMED REPAIR TO FUSELAGE SKIN, FRAME 77, STRINGER 6R IAW EC5330-02739. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK VISUAL INDICATION OF CRACK FRAME 75 STR 2L. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 75, STR 2L IAW EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 30,976 hrs · 23,483 cycles

SHV-DURING C-CHECK CORROSION AROUND NUTPLATE LOWER MAIN DOOR SECTION. MX PERFORMED REPAIR ON MAIN DOOR LOWER NUTPLATE HOLES IAW EC5210-01154 REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK SHEAR CLIP AT FRAME 65 AT LOWER CUTOUT AT CARGO DOOR IS CORRODED. MX PERFORMED REPAIR FOR SHEAR CLIP AT FRAME 65 AT LOWER CUTOUT CARGO DOOR IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK SHEAR CLIP AT FRAME 68 AT LOWER CUTOUT AT CARGO DOOR IS CORRODED. MX PERFORMED REPAIR OF SHEAR CLIP AND SPLICE AT FRAME 68 AT LOWER CARGO DOOR CUTOUT IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,976 hrs · 23,483 cycles

DURING C-CHECK CARGO LOWER BEAM FRAME 65-68 AT CUTOUT IS CORRODED (LOCAL LEVEL 2). MX PERFORMED REPAIR OF CARGO DOOR LOWER BEAM FRAME 65-68 AT CUTOUT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 1) · airframe 26,416 hrs · 19,829 cycles

FLIGHT 5338 - IAD - FLIGHT CREW REPORTED MAIN BATTERY NR 1 OVERTEMP IN FLIGHT, REACHED 74C AND HIGHER ON GROUND BEFORE SHUTDOWN. CREW DECLARED EMERGENCY. IAD MX REMOVED AND REPLACED NR 1 MAIN BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 26,334 hrs · 19,759 cycles

MCI - FLIGHT 6118, THE CREW REPORTED NR 2 BATTERY OVERTEMP, THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (LANDING GEAR) · airframe 26,076 hrs · 19,559 cycles

FLIGHT 3064 - EWR - FLIGHT CREW REPORTED L/G AIR GROUND FAIL ON EICAS AFTER TAKEOFF (OCCURRED TWICE). EWR MX REMOVED AND REPLACED WOW PROX SWITCH NR 1 CONNECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,033 hrs · 19,528 cycles

IAH - FLIGHT 2798, THE CREW REPORTED AN ELECTRIC BURNING SMELL DURING FLIGHT AND AFTER LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE WINDSHIELD HEATING SYSTEM, RELAY RACKS, AND POWER DISTRIBUTION BOXES ALL WITH NO DEFECTS FOUND, COMPLIED WITH FIM TASK 21-20-00-810-801A WITH NO BURNING SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (GALLEY) · airframe 26,021 hrs · 19,520 cycles

CLE FLT 2078 THE CREW REPORTED A LAV SMOKE WARNING ON THE EICAS. MAINTENANCE REPLACED THE SMOKE DETECTOR AND SMOKE SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,003 hrs · 19,504 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED AT RADIUS AT FRAME 21. MAINTENANCE REMOVED AND REPLACED CORRODED CENTER OMEGA BEAM BETWEEN FRAMES 18-23 IAW EMB-145 SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAULTY (COCKPIT) · airframe 25,414 hrs · 19,079 cycles

IAD FLT 6012 - THE CREW REPORTED A "NO TAKEOFF CONFIGURATION" WARNING MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED RELAY KO212. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION · airframe 23,342 hrs · 17,480 cycles

FLIGHT 2710 - DCA - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING DESCENT. CREW PERFORMED SYSTEM RESET SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE HARNESS — CHAFED (NR 2 ENGINE) · airframe 23,000 hrs · 17,222 cycles

ATL FLT 2531 - THE CREW REPORTED A ENGINE NR 2 FIRE/DETECT FAIL MESSAGE ON THE EICAS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,335 hrs · 15,977 cycles

DURING C-CK RT OMEGA BEAM HAS CORROSION AT FR 18. REPAIRED RT OMEGA BEAM IAW IC 2009/03705. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 21,248 hrs · 15,908 cycles

JAX - FLIGHT 2981, THE CREW REPORTED A LARGE VIBRATION FROM UNDER THE NOSE LANDING GEAR WHEEL WELL. THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — FAULTY (NR 2) · airframe 21,220 hrs · 15,889 cycles

CLE FLIGHT 2006 - THE CREW REPORTED A RAM AIR VALVE FAIL MESSAGE AFTER TAKEOFF, FOLLOWED BY A PACK 1 AND 2 CLOSED, BLEED 1 VALVE CLOSED MESSAGES. ALSO REPORTED OIL PRESSURE CLIMBED INTO THE AMBER RANGE WHEN VALVE CLOSED. MAINTENANCE INSPECTED AND REPLACED THE NR 2 DAU AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,106 hrs · 15,073 cycles

PREFLIGHT INSPECTION THE CREW REPORTED AN AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE AISLE PATH LIGHTING WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. FLT HRS-19303. CYC-14520. (A)

Part: PROXIMITY SWITCH — INOPERATIVE (LT MLG) · airframe 18,418 hrs · 13,925 cycles

BTR - FLIGHT 2078, THE CREW REPORTED A BANGING NOISE FROM THE NLG AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH ON 03/15/08 WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,842 hrs · 13,531 cycles

DURING ROUTINE MAINTENANCE, THE AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: BRACKET — WORN (RT AILERON) · airframe 16,630 hrs · 12,676 cycles

RIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.

Part: BRACKET — WORN (RT AILERON) · airframe 16,630 hrs · 12,676 cycles

RIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.

Part: FIRE DETECTOR — SHORTED (NR 1 ENGINE) · airframe 14,713 hrs · 11,179 cycles

CLE FLIGHT NR 2071, CREW REPORTED THAT THE NR 1 ENGINE FIRE DETECTOR FAILED IN FLIGHT. FLIGHT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,102 hrs · 10,718 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 12,029 hrs · 9,127 cycles

DURING A SCHEDULED 2C INSPECTION, THE VERTICAL STABILIZER RT FITTING WAS FOUND TO HAVE CORROSION INSIDE THE SPHERICAL BEARING HOUSING. THE CORROSION WAS REMOVED AND THE BEARING HOUSING WAS REAMED AND BUSHED AS PER EXPRESSJET EC5510-01124.

Part: SEQUENCE VALVE — DEFECTIVE (MLG) · airframe 11,994 hrs · 9,098 cycles

TYS AIRCRAFT ON TAKEOFF HAD A LANDING GEAR/LEVER DISAGREE WARNING.AIRCRAFT RETURN TO BLOCK AND WAS CHECKED OUT FOR A SAFE FERRY FLIGHT TO TYS. MAINTENANCE R/R THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32002.ALL OPS CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,410 hrs · 5,539 cycles

DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW-EMB-135/145-SRM-53-21-10 AND CMP-51-21-04, 05, 06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,410 hrs · 5,539 cycles

DURING A SCHEDULED 2C INSPECTION THE RAMP ANGLE IN GALLEY SHOWED SIGNS OF BEING CORRODED. MAINT. REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 7,410 hrs · 5,539 cycles

DURING A SCHEDULED INSPECTION THE PAX DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD IAW-EMB-145-AMM-20-10-01 AND CMP-51-14-02, 04, 05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF THE INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,410 hrs · 5,539 cycles

DURING A SCHEDULED 2C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED. MAINT. CUT OUT THE AFFECTED AREA AND FAB. A NEW FLOORBEAM, INSTALL A DOUBLER FILLER AND SHIMS. ALLODINED,PRIMED AND PAINTED IAW EMB 135/145 SRM 53-21-10 AND EMB 145 CPM 51-21-04,05.06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (PAX DOOR) · airframe 7,410 hrs · 5,539 cycles

DURING A SCHEDULED 2C INSPECTION THE PAX DOOR THRESHOLD WAS FOUND WITH CORROSION. MAINT. REMOVED AND REPLACED THE PAX DOOR THRESHOLD. CLEANED CORROSION UNDER DOOR SEAL RESTORED THE TOPCOAT AND TREATED THE ALUMINUM SURFACE IAW EMB 145 SRM 51-14-02;CPM 51-21-04'05'06 AND EMB 145 AMM 20-10-01. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: O-RING — DEFECTIVE (APU)

CLE FLIGHT 2230 CREW REPORTED STRONG FUEL ODOR WITH NR 1 PACK BEING SUPPLIED BY APU BLEED. MAINTENANCE REMOVED AND REPLACED O-RING AND RETAINING RING ON FUEL SOLENOID. OPERATIONAL AND LEAK CHECKS GOOD.

Part: BULB — BURNED OUT (CABIN)

DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: FCU — INTERMITTENT (TE FLAPS)

FLIGHT NR 3109, THE CREW REPORTED THE FLAPS WOULD NOT EXTEND OUT OF (0) DEGREES FOR LANDING. THE CREW DECLEARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE AIRCRAFT WAS TEST FLOWN AND THEN RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 2,159 hrs · 1,494 cycles

EWR---CO4009, CREW REPORTED ON DESCENT INTO EWR, LAV SMOKE INDICATION (CAME ON), NO VISUAL INDICATION OF FIRE OR SMOKE. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR PANEL IAW EMB145 MM 26-14-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE - FLIGHT 4015, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST SECTION OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — BURNED (COCKPIT)

CLE - FLT 3613 - THE CREW REPORTED SMOKE IN THE COCKPIT INBOUND TO CLEVELAND. A EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE TAT 2 CURRENT SENSOR (KO 494) RELAY AND RECEPTACLE BURNED. THE RELAY AND RECEPTACLE WERE REPLACED IAW EMB MM 20-21-00, 20-13-02 AND 30-33-01 AND 30-53-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SMOKE DETECTOR — FAULTY (INTERIOR)

BTV - FLT 4218 - CREW REPORTED, LAV SMOKE INDICATION ON CLIMB-OUT. MAINTENANCE MEL AIRCRAFT AND RELEASED IAW MEL 26-14-00 CATEGORY C CONTROL NR 002376. ON 10-13-00 MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW EMB145 MM 26-14-01. OPS CHECKED GOOD. REMOVED FROM MEL. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SENSOR — FAULTY (INTERIOR)

TYS CO3991 CREW REPORTED LAV SMOKE ECIAS INDICATION ON CLIMBOUT, NO SMOKE NOTED MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB 145 AMM 26-14-01. OPS. CHECK GOOD IAW EMB 26-14-00.

Part: SMOKE — DETECTED (CABIN)

CVG - FLT 4275 - DURING TAKEOFF, THE CREW REPORTED A LAVATORY SMOKE INDICATION ACCOMPANIED BY THE ODOR OF SMOKE. THE CREW PERFORMED AN AIR RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED APU AND ENGINE RUN-UPS, OPERATIONAL CHECKS OF BLEED AIR AND AIRCONDITIONING SYSTEMS AND OPERATIONAL TEST OF THE LAVATORY SMOKE DETECTOR (REF EMB145 AMM 26-14-00). NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)