N14923

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTION) · airframe 38,206 hrs · 29,797 cycles

THE CREW REPORTED LAV SMOKE WARNING INDICATION AT 4000 FT ON CLIMB OUT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FORWARD GALLERY SMOKE DETECTION PANEL AND THE DAU2. OPS CHECKS WERE GOOD. THE ACFT WAS TEST FLOWN SATISFACTORY.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 38,180 hrs · 29,779 cycles

THE CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF WITH NO SMOKE NOTED. THE ACFT CONTINUED TO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 38,155 hrs · 29,763 cycles

CREW REPORTED A "LAV SMOKE" INDICATION IN FLIGHT. MAINTENANCE R & R LAV SMOKE DETECTOR WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (FRAMES 65-68)

DURING C-CK. CARGO DOOR LOWER SUPPORT ANGLE CORRODED AROUND NUTPLATE HOLES. R & R CARGO DOOR LOWER SUPPORT ANGLE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-60) · airframe 36,765 hrs · 28,650 cycles

DURING C-CK. CENTER OMEGA BEAM CORRODED BETWEEHN FRAME 59-60. REPAIRED OMEGA BEAM IAW EC5310-01473. ACFT IS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (LT ENGINE) · airframe 36,765 hrs · 28,650 cycles

DURING C-CK. LT ENGINE FWD LOWER YOKE IS CRACKED. R & R LT ENGINE FWD LWR YOKE IAW EC5450-01172. ACFT APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (RT ENGINE) · airframe 36,765 hrs · 28,650 cycles

DURING C-CHECK. RT ENGINE FWD LOWER YOKE IS CRACKED. R & R RT LOWER FWD YOKE FITTING IAW EC5450-01172. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 36,765 hrs · 28,650 cycles

DURING C-CHECK, THE CARGO DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 36,765 hrs · 28,650 cycles

DURING C-CHECK, CARGO DOOR LOWER SKIN WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (LEFT) · airframe 36,297 hrs · 28,274 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R BOTH ACM'S, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (RIGHT) · airframe 36,297 hrs · 28,274 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R BOTH ACM'S, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RETAINING RING — BROKEN (PAX DOOR) · airframe 34,920 hrs · 27,204 cycles

MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE OF ACFT. MAINTENANCE FOUND THE MAIN CABIN DOOR RETAINER RING OUT OF PLACE AND R & R RETAINER RING ON TORQUE TUBE. OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DEFLECTOR — MISINSTALLED (CABIN) · airframe 34,403 hrs · 26,788 cycles

DURING ROUTINE MAINTENANCE, THE RT OVERWING EMERGENCY EXIT WOULD NOT OPEN. CATHES ON SIDEWALL DEFLECTOR. FURTHER INSPECTION FOUND THE SIDE WALL DEFLECTOR WAS INSTALLED IN THE WRONG LOCATION. MAINTENANCE REPOSITIONED THE SIDE WALL DEFLECTOR AND OPS CHECKS WERE GOOD.

Part: HOUSING — FAULTY (LIGHT) · airframe 34,171 hrs · 26,597 cycles

THE CREW REPORTED LAVATORY SMOKE WARNING, ELECTRICAL FIRE ODOR IN AND AROUND LAV. LAVATORY LIGHT WARM TO TOUCH. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY LIGHT LAMP HOUSING. OPS CHECKED GOOD.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 34,141 hrs · 26,576 cycles

PILOT REPORTED A STRONG ODOR OF SMOKE APPROACH AND SHUTOFF PACKS AND ODOR WENT AWAY. MX INSPECTED ACFT AND DETERMINED NR 1 ENGINE INGESTED A BIRD. MX PERFORMED A BIRD STRIKE INSPECTION, ENGINE COMPRESSOR SECTION BORESCOPE, AND FOD INSPECTION IAW MM 05-50-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,869 hrs · 25,608 cycles

THE CREW REPORTED EMERGENCY LIGHT WAS INOPERATIVE FROM EXIT ROW ON BACK. MAINTENANCE INSPECTED AND PERFORMED RERACK OF NR 4 AND NR 6 EMERGENCY LIGHT INVERTER'S. OPS CHECKED GOOD.

Part: FRAME — CRACKED (ZONE 200) · airframe 31,899 hrs · 24,853 cycles

DURING C-CHECK, FRAME 10 CRACKED UNDER LT DV WINDOW CUTOUT. MX R & R FRAME 10 CHANNEL UNDER LT DV WINDOW CUTOUT SIDE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,899 hrs · 24,853 cycles

DURING C-CHECK SKIN SPLICE HAS CORROSION, FR 13-14, STR 21L-21R. MX PERFORMED AND COMPLETED REPAIR OF SKIN SPLICE FR 13-14, STR 21L-21R IAW SRM 53-00-02 AND CPM 51-21-07. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 31,899 hrs · 24,853 cycles

DURING C-CHECK, THE LT AFT MLG TRUNNION FITTING WAS FOUND TO HAVE CORROSION IN MULTIPLE AREAS OF THE BACK WALL AND IN THE GREASE CHANNEL. MX PERSONNEL PERFORMED A REAMING AND BUSHING REPAIR IAW EC5750-01528. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 31,800 hrs · 24,779 cycles

CREW REPORTED A LAVATORY SMOKE INDICATION ON EICAS TWICE DURING FLIGHT. CREW PERFORMED QRH AND CONTINUED TO DESTINATION. MX INSPECTED AND FOUND NO EVIDENCE OF LAVATORY FIRE. MX PERFORMED OPS CHECK OF LAVATORY SMOKE SYS, SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED OUT (GALLEY) · airframe 28,759 hrs · 22,318 cycles

THE CREW REPORTED SMOKE IN THE CABIN NEAR SEAT 2A & NEAR THE GALLEY COMING FROM CEILING PANELS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE FORWARD GALLEY LIGHT BURNED OUT WITH NO OTHER EVIDENCE OF BURNS OR DAMAGE. REPLACED THE FORWARD GALLEY LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,023 hrs · 21,708 cycles

DURING SCHEDULED MX INSPECTION, THE FWD CABIN EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE FWD CABIN EMERGENCY EXIT INVERTER IAW AMM 33-50-11 WITH OPS CHECK SUCCESSFUL. AC WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 28,023 hrs · 21,708 cycles

DURING SCHEDULED MX INSPECTION, THE LT WING/FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY EXIT LIGHT IAW AMM 33-50-07. OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,998 hrs · 20,928 cycles

DURING ROUTINE MAINTENANCE, RIC MX FOUND THE EMERGENCY EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. RIC MX REMOVED AND REPLACED EXIT SIGN AT 3B AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (LAVATORY) · airframe 24,928 hrs · 19,265 cycles

THE CREW REPORTED A LAV SMOKE MESSAGE ON THE EICAS WHILE PARKED AT THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: ROTARY SWITCH — INOPERATIVE (COCKPIT) · airframe 24,845 hrs · 19,199 cycles

DSM - FLIGHT 6008 OMA-ORD DIVERTED TO DSM DUE TO AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT DSM WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE NR 1 AND NR 2 MAIN BATTERY SELECTOR SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — FAULTY (APU) · airframe 24,390 hrs · 18,766 cycles

THE CREW REPORTED A FUEL SMELL WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: DUCT — CONTAMINATED (AC SYSTEM) · airframe 24,370 hrs · 18,746 cycles

THE CREW REPORTED APU GENERATOR OFF BUS MESSAGE AFTER PUSHBACK DURING NR 2 ENGINE START ACCOMPANIED BY FAINT ACRID SCENT. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS ON NR 1 AND NR 2 ENGINE AND APU. PERFORMED DECONTAMINATION OF AIR CONDITIONING SYSTEM AND NO FURTHER SMELL WAS NOTED.

Part: BATTERY — OVERHEATED (NR 2) · airframe 23,789 hrs · 18,186 cycles

ACFT N14923 HAD BATT NR 2 OVERTEMP REACHED 83 DEGS CELSIUS DURING DESCENT. MAINTENANCE REMOVED AND REPLACED BATT NR 2 IAW EMB-145 AMM 24-36-01. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAULTY (SMOKE WARNING) · airframe 23,430 hrs · 17,858 cycles

CAK FLT 5781 THE CREW REPORTED THE BAG SMOKE PUSH BUTTON LIGHT WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED RELAY KO629. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,323 hrs · 17,756 cycles

EXIT ROW EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,323 hrs · 17,756 cycles

MAIN PAX DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD.

Part: LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 22,550 hrs · 17,058 cycles

FLIGHT 2068 - JAX - FLIGHT CREW REPORTED LOST OF AIRSPEED INDICATION IN CRUISE. FLIGHT CREW PERFORMED EMERGENCY DESCENT AND LANDED UNEVENTFULLY. MX DRAINED WATER FROM RIGHT AND LEFT PITOT STATIC LINES AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED OMEGA BEAM IAW EC 5320-01443. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK DOUBLER AT FRAME 20 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK SHEAR CLIP AT FRAME 81 AT 3 O'CLOCK POSITION GOUGED. MAINTENANCE REMOVED AND REPLACED CRACKED AND GOUGED SHEAR CLIP AT FRAME 81 AT 3 O'CLOCK POSITION IAW EMB-145 SRM 51-30-01 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK DOUBLER AT FRAME 22 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 22. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 73 BETWEEN STRINGERS 8R AND 9R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 73 BETWEEN STRINGERS 8R AND 9R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AFT DOUBLER (AFT OF CROSSBEAM) IS CORRODED (LEVEL 2 LOCAL) AT FRM 20A. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 53-00-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAMES 22-23 HAS TOOLING MARKS. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAMES 18-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,164 hrs · 16,756 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 68 SHEAR CLIP NEAR STRINGER 17L. MAINTENANCE FABRICATED AND INSTALLED REPAIR ON FRAME 68 SHEAR CLIP STRINGER 17L IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — UNSECURE (AC PACK) · airframe 21,725 hrs · 16,426 cycles

AIRCRAFT DIVERTED INTO TYS FOR A BLEED 1 LEAK. SECURED DUCT LINE TO PAC 1 AND HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: STRUT — LEAKING (NLG) · airframe 21,430 hrs · 16,191 cycles

FLIGHT 2554 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AND GEAR WOULD NOT RETRACT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NOSE LANDING GEAR STRUT ASSEMBLY AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (MLG) · airframe 20,530 hrs · 15,508 cycles

CLE FLIGHT NR 2890 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG DURING CLIMBOUT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX R&R THE LANDING GEAR ELECTRONIC CONTROL UNIT (LGEU). OPS CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 20,434 hrs · 15,434 cycles

MFE - FLIGHT 2451, THE CREW REPORTED THAT A LANDING GEAR LEVER DISAGREE MSG WAS RECEIVED AND THE LANDING GEAR DID NOT RETRACT. THE ACFT LANDED AT MFE WITHOUT INCIDENT WHERE MX INSPECTED AND APPROVED THE ACFT FOR A FERRY FLIGHT TO IAH. THE ACFT LANDED IN IAH WITHOUT INCIDENT AND MX R&R THE LGEU, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 20,434 hrs · 15,434 cycles

CREW REPORTED THAT A LANDING GEAR LEVER DISAGREE MESSAGE WAS RECEIVED AND THE LANDING GEAR DID NOT RETRACT. THE ACFT LANDED WITHOUT INCIDENT WHERE MX INSPECTED AND APPROVED THE ACFT FOR A FERRY FLIGHT. THE ACFT LANDED WITHOUT INCIDENT AND MX REMOVED AND REPLACED THE LANDING GEAR LEVER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED (CABIN)

AC WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE LOWER SERVICE DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-09. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. (K)

Part: RELAY — BURNED (CURRENT SENSOR) · airframe 17,779 hrs · 13,596 cycles

CMH FLIGHT NR 3142 - THE CREW REPORTED PITOT 2 INOP MESSAGE ON THE EICAS IN FLIGHT AT 25000. THEY ALSO REPORTED SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND PITOT 2 CURRENT SENSOR RELAY (K0054) AND SOCKET (XK0054) BURNED. THE RELAY AND SOCKET WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,325 hrs · 13,283 cycles

NR 3 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (BRAKE ASSY) · airframe 16,244 hrs · 12,461 cycles

IAH - FLIGHT 2217, DURING TAXI THE CREW REPORTED SEVERAL OUTBOARD BRAKE INOP MESSAGES ON EICAS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE OUTBOARD BRAKE SHUT OFF VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 15,327 hrs · 11,754 cycles

IAH - FLIGHT 2980, THE CREW REPORTED A BURNED RUBBER ODOR EMINATING FROM PACK 2 IN THE COCKPIT AND CABIN WITH NO SMOKE VISIBLE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED AIR SYS — CONTAMINATED · airframe 10,302 hrs · 7,825 cycles

CLE - FLT NR 2139 - AFTER TAKEOFF, THE CREW GOT THE LAVATORY SMOKE INDICATION ON THE EICAS WITH A NOTICABLE SMOKE SMELL. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND DE-ICING FLUID IN THE BLEED SYSTEM. CLEARED DE-ICING FLUID FROM BLEED SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FLIGHT 3388 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING AT MID-CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

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

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV-DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 8,018 hrs · 6,065 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE VERTICAL STIFFENER AND THE RIGHT ENDS OF THE 2ND AND 3RD HORIZONTAL STIFFENERS AND THE RIGHT UPPER APU MOUNTING BRACKET. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW CONTINENTAL EXPRESS EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV- DURING C-CHECK, THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV- DURING C-CHECK, THE LEFT HAND BUTTSTRAP FROM FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV-DURING C-CHECK, THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV- DURING C-CHECK THE ATTACHMENT ANGLE BETWEEN THE RIGHT SILL AND THE CROSS BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 58 AND 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCEMENT DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE 5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,018 hrs · 6,065 cycles

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

Part: REINFORCEMENT — GOUGED (FUSELAGE) · airframe 8,018 hrs · 6,065 cycles

DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19 RT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (COCKPIT) · airframe 6,870 hrs · 5,141 cycles

EWR---CO3289, FOUND BAGGAGE FIRE EXTINGUISHER WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED BAGGAGE FIRE TEST SWITCH. OPS. CHECKED SYSTEM GOOD. IAW EMB145 MM NR20-13-04. AIRCRAFT RETURNED TO SERVICE.

Part: OUTFLOW VALVE — LEAKING (CABIN PRESSURE)

CLE FLIGHT NR 3219 THE CREW REPORTED DURING CLIMBOUT THE AIRCRAFT PRESSURIZATION SURGED, CABIN RATE WENT FROM 1750 TO 1800. RESET TO MANUAL AND LOST CABIN ALTITUDE INDICATION. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE PNEUMATIC OUTFLOW VALVE WAS LEAKING. THE OUTFLOW VALVE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

IAH- DURING FLIGHT 3921, THE CREW NOTED THAT THE NUMBER 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ILLUMINATED ON THE EICAS. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT.

Part: BULB — FAULTY (CABIN)

BTV---DURING ROUTINE INSPECTION ON RON IN BTV, MAINTENANCE FOUND AFT UPPER AISLE EMERGENCY LIGHT TO BE INOPERATIVE....REMOVED AND REPLACED LIGHT BULB IAW EMB145 MM 33-50-08. OPS.CHECKED GOOD.