N15941

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,204 hrs · 31,225 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 20A INOPERATIVE. R & R LIGHT, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — DEFECTIVE (ZONE 400) · airframe 31,385 hrs · 30,419 cycles

FIRE DETECTION FAIL MESSAGE ON EICAS DURING TAXI. R & R FIRE DETECTOR IAW AMM 26-11-01. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING INSPECTION, RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW EA EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRAKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUYBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING INSPECTION, LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6L. MX PERFORMED A BUSHING REPAIR IAW ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 4 PLACES AT A SINGLE RIVET ON FRAME 79 BELOW STRINGER 05L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/20/2013.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 3R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHNICAL DISPOSITION ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/20/2013.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,245 hrs · 30,282 cycles

DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A SINGLE RIVET ON FRAME 77 BELOW STRINGER 8L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,667 hrs · 29,694 cycles

DURING MX INSPECTION, THE EMERGENCY LIGHT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,194 hrs · 29,216 cycles

ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,734 hrs · 28,751 cycles

DURING A CHECK INSPECTION, THE LT AFT OVERWRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LAMP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 28,943 hrs · 27,940 cycles

DURING C CHECK. LEFT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED LT FWD LOWER ENGINE YOKE IAW EC5450-01052. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 28,943 hrs · 27,940 cycles

DURING C CHECK. RT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED RT ENGINE FWD LOWER YOKE IAW EC5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 27,523 hrs · 26,553 cycles

TYS - A/C WAS IN MOB WHEN A BELTLOADER HIT THE 191 BELLY PANEL AND CRACKED THE PANEL AFT OF THE PORTABLE WATER DOOR. A/C WAS FERRIED TO TYS WHERE THE COMPOSITE SHOP MADE THE REPAIR IAW ETD 2011-145-106533. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE. LOGPAGE 2885492.

Part: COMPUTER — MALFUNCTIONED (NR 2 AHRS) · airframe 27,142 hrs · 26,146 cycles

AIRCRAFT 15941 FLIGHT 2734 AHRS 2 FAIL IAH-XNA DIVERTED TO SHV. SHV MAINTENANCE REMOVED AND REPLACED NUMBER 2 AHRS COMPUTER IAW 34-21-01, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,128 hrs · 26,132 cycles

IAH - FLIGHT 2734, DURING PREFLIGHT INSPECTION THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL INDICATION. MAINTENANCE RESET THE AIRCRAFT, AND THE INDICATION DID NOT REOCCUR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (LANDING GEAR) · airframe 27,030 hrs · 26,037 cycles

IAH - FLIGHT 2318, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT TRAILING ARM PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,969 hrs · 25,974 cycles

MEM - FLIGHT 2998, THE CREW REPORTED A LANDING GEAR AIR/GND FAIL MESSAGE WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH. IAH MAINTENANCE JACKED THE AIRCRAFT AND PERFORMED PROXIMITY SENSOR OPERATIONAL CHECKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 26,901 hrs · 25,902 cycles

IAH - CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. COULD NOT RAISE LANDING GEAR. AIRCRAFT AIR RETURNED AND LANDED UNEVENTFULLY. IC 1-2 WOW INOP AFTER LANDING. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IN REFERENCE TO EMB145 AMM 32-32-02. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BURNED (CABIN) · airframe 26,690 hrs · 25,683 cycles

IAH - POST FLIGHT 2812, THE CREW REPORTED ELECTRICAL SMOKE IN THE CABIN AND COCKPIT, AND SEEMED TO BE STRONGEST AROUND ROWS 8 & 9. IAH MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT CONNECTOR AT ROW 10 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 25,630 hrs · 24,586 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 24,765 hrs · 23,705 cycles

MEM - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL BY ROWS 16-19. MAINTENANCE INSPECTED THE AIRCRAFT AND IDENTIFIED A BAD BALLAST ABOVE ROW 16. THE CABIN LIGHTS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED IN IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — LEAKING (HYDRAULIC SYS) · airframe 24,245 hrs · 23,169 cycles

IAH - FLIGHT 2895, DURING CLIMB THE CREW REPORTED HYDRAULIC FLUID COMING FROM THE RT WING LOWER WEEP HOLE WHEN THE SPOILERS WERE ACTUATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAK IN A SWAGE FITTING ON THE SPOILER HYDRAULIC LINE. MAINTENANCE RESWAGED THE FITTING, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 24,083 hrs · 23,000 cycles

RIGHT MLG AFT TRUNNION PITTED. REWORKED TRUNNION WITH BORE MACHINE IAW EC5750-01398.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 23,516 hrs · 22,393 cycles

IAH - FLIGHT 2834, THE CREW REPORTED A BLEED 1 LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT BEHIND PANEL 271DLW, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — DEFECTIVE (COCKPIT) · airframe 23,334 hrs · 22,189 cycles

TYS FOR IAH - THERE WAS INTERMITTENT OPERATION OF THE EMERGENCY LIGHTS IN ASSOCIATION WITH THE ECIAS SHOWING NOT ARMED. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE IAW EMB 145 AMM 33-21-01, OPS CHECK GOOD AND WAS RELEASED.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 23,310 hrs · 22,160 cycles

DAL - FLIGHT 2149, DURING PREFLIGHT INSPECTION THE GALLEY, EMERGENCY, AND LAV LIGHTS WERE FOUND TO BE INTERMITTENT, AND NOT OPERATING WITH THEIR RESPECTIVE SWITCHES. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,195 hrs · 22,029 cycles

IAH - FLIGHT 2046, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS DO NOT ALWAYS ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE AISLE PATH LIGHT BETWEEN SEAT 14 AND 17, OPERATIONALLY TESTED EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 22,811 hrs · 21,634 cycles

IAH - FLIGHT 2003 THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE NOSE LANDING GEAR, OPERATIONALLY TESTED THE GEAR RETRACTION AND EXTENSION SYSTEM WITH NO DEFECTS NOTED, AND SUCCESSFULLY TEST FLEW THE AIRCRAFT. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 22,176 hrs · 20,947 cycles

NR 1 EMERGENCY LIGHT BATTERY NOT CHARGING. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,759 hrs · 19,510 cycles

IAH - DURING MAINTENANCE INSPECTION EMERGENCY FLOOR LIGHT STRIP NR 6 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: UNKNOWN — ODOR (COCKPIT) · airframe 20,057 hrs · 18,769 cycles

LFT - FLIGHT 2734, DURING PREFLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND THE ODOR TO BE COMING FROM THE PACKS WITH THE APU RUNNING. MAINTENANCE MEL'D THE APU 49-00-00 (C) CONTRO 128496, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 09/04/07, IAH MAINTENANCE RAN THE APU AND PACKS WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,783 hrs · 18,474 cycles

IAH - FLIGHT 2533, DURING POSTFLIGHT INSPECTION THE RIGHT HAND EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,559 hrs · 18,237 cycles

DENT ON FUSELAGE SKIN AFT OF PAX DOOR. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW EMB 134/145 SRM 51-20-03, 51-40-06, 51-40-02, 53-21-01 & CPM 51-21-04, 05, 06.

Part: RIB — DENTED (LT NACELLE) · airframe 19,559 hrs · 18,237 cycles

LEFT LWR COWL DENTED. REMOVED AND REPLACED DAMAGED RIB IN CENTER SECTION OF COWL, RECON TOURED DENTS AT OIL SERVICE DOOR, FABRICATED AND INSTALLED EXTERNAL DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC 5430-01059. AIRCRAFT STILL IN C-CHECK.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 19,559 hrs · 18,237 cycles

FRAME 68 CRACKED UNDERNEATH CARGO DOOR -HOLD OPEN- HANDLE RETAINING CUP. CUT OUT AFFECTED FRAME, FABRICATED THE FRAME REPAIR SEGMENT FROM A SECTION OF A NEW FRAME AND INSTALLED. WORK ACCOMPLISHED IAW EC 5310-01411, EMB 145 SRM 53-00-04 AND CPM. AIRCRAFT STILL IN C-CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,423 hrs · 13,458 cycles

TYS DURING A C-CHECK INSPECTION THE CENTER AISLE SUPPORT STRUCTURE ON THE LEFT SIDE WAS FOUND WITH CORROSION FROM FRAME 20 TO 60. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM ASSEMBLY FROM FR 20 TO 29 AND BLENDED FROM 29 THRU 60 AND WAS FOUND WITHIN LIMITS. AREA WAS ALODINED, PRIMED AND PAINTED.

Part: FITTING — LOOSE (VERTICAL STAB) · airframe 15,423 hrs · 13,458 cycles

DURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE DEFECTIVE BUSHING WAS REMOVED; THE FITTING HOLE WAS DIMENSIONALLY CHECKED AND FOUND TO BE WORN. MAINTENANCE OVERSIZED THE FITTING HOLE AND INSTALLED A NEW BUSHING AS PER THE EXPRESSJET ENGINEERING DOCUMENT EC5540-01034.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 15,423 hrs · 13,458 cycles

TYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, DYE PENATRANT TESTED THE AREA, TREATED FOR CORROSION, DRILLED AND INSTALLED A NEW FITTING IAW EC5310-01317, EMB-135/145, SRM 51-10-03, 51-20-03, 51-40-02 AND CMP 51-21-04.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 15,423 hrs · 13,458 cycles

TYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INTERNAL L ANGLE DOUBLERS ON FR 21 BETWEEN STR 21L AND 21R. ALODINED, PRIMED AND INSTALLED IAW EC5310-01328 AND EMB 135/145 CPM 51-21-04/05.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,790 hrs · 12,796 cycles

CLE FLIGHT 2481 THE CREW REPORTED THE EMERGENCY LIGHTS AT THE CENTER OF THE AIRCRAFT WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES IN THE CEILING AT ROW 12. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 14,735 hrs · 12,741 cycles

CREW REPORTED, EMERGENCY EXIT LIGHT INVERTER INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,675 hrs · 12,672 cycles

DURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: CONTROL VALVE — INOPERATIVE (BRAKE) · airframe 14,167 hrs · 12,053 cycles

SHV - DURING TAXI TO THE GATE BRK OUTBD INOP WAS OBSERVED ON THE EICAS. CREW RESET THE CIRCUIT BREAKERS AND THE MESSAGE WENT AWAY. DURING TAXI TO THE HANGER THE MESSAGE REAPPEARED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE IAW EMB 145 AMM 32-41-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (CABIN)

CLE FLIGHT 3253 THE CREW REPORTED THE EMERGENCY LIGHT AISLE PATH LIGHTING STAYED ON. MAINTENANCE REPLACED THE FLIGHT ATTENDANT'S CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING ROURINE MAINTENANCE THE NR 5 EMERGENCY LIGHT INVERTER WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 5 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — MALFUNCTIONED (CABIN)

SDF FLIGHT NR 2135 THE CREW REPORTED THE OVERHEAD EMERGENCY LIGHT EXIT SIGN OVER THE EXIT ROW FAILED TO TEST. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT NR 2243, THE CREW REPORTED THE EMERGENCY LIGHTS ABOVE THE GALLEY AREA AND COCKPIT ENTRANCE DID NOT WORK. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INTERMITTENT (OVERWING)

CLE FLIGHT 2917 THE CREW REPORTED THE EMERGENCY LIGHTS FOR THE MAIN CABIN DOOR AND OVERWING EXIT LIGHT DID NOT WORK. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2123 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON MID CABIN WALL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — INOPERATIVE (CABIN)

During postflight inspection the mid cabin emergency exit light would not illuminate. Maintenance removed and replaced the exit light bulb. The system tested good and the aircraft was returned to service.

Part: SELECTOR — MALFUNCTIONED (MLG)

ROC FLIGHT 2025 THE CREW REPORTED THE LANDING GEAR WOULD NOT FULLY RETRACT AFTER DEPARTURE FORM ROC. THE GEAR WAS RECYCLED AND STILL DID NOT FULLY RETRACT. THE AIRCRAFT RETURNED AND LANDED IN ROC WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED ICE AND SNOW FROM ALL 3 LANDING GEAR AND REMOVED AND REPLACED THE LANDING GEAR SELECTOR HANDLE FOR CAUTIONARY PURPOSES. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DIRTY (CABIN)

CLE FLIGHT#2025 THE CREW REPORTED EMERGENCY LIGHTING OVERHEAD IN FORWARD GALLEY WAS INOPERATIVE.MAINTENANCE INSPECTED AND CLEANED CONNECTOR FOR LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — FAULTY (COCKPIT AREA) · airframe 11,303 hrs · 9,021 cycles

CVG/EWR---CO2547, CREW REPORTED "SMOKE COMING OUT PA PHONE BEHIND CAPTAINS HEAD." CVG MAINTENANCE TROUBLESHOT PROBLEM TO FORWARD PA UNIT. DISABLED PA SYSTEM, PULLED PA AND INTERPHONE CIRCUIT BREAKERS AND FORWARD PA CANNON PLUG CONNECTOR. AIRCRAFT MAINTENANCE FERRIED TO EWR. EWR MAINTENANCE REPOSITIONED CIRCUIT BREAKERS INTO NORMAL POSITION IAW EMB145 AMM #20-13-06. REMOVED AND REPLACED FLIGHT ATTENDENTS FORWARD HANDSET IAW EMB145 AMM #23-31-03. FOUND TWO WIRES TO BE BROKEN AND CANNON PLUG P8300 TO BE BAD. REMOVED AND REPLACED CANNON PLUG IAW EMB145 AMM #20-50-00, AND REPAIRED BROKEN WIRES IAW EMB145 MM #20-21-00. OPS.CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN)

MKE FLIGHT#2135 THE CREW REPORTED THE EMERGENCY EXIT AISLE PATH LIGHTING FROM ROW 7 FORWARD WAS INOPERATIVE.THEY ALSO REPORTED THE EXIT LIGHT ON THE FORWARD CABIN PARTITION AND THE LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A BROKEN GROUND WIRE (GS8506DC)FOR THE EMERGENCY LIGHTS BATTERY 2,INVERTER 2 AND INVERTER 3.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FRAME — GOUGED · airframe 11,263 hrs · 8,977 cycles

SHV DURING C CHECK FRAME 81 WAS FOUND GOUGED AT BOTTOM CENTER. MAINTENANCE REMOVED DAMAGED SECTION AND REPAIRED FRAME 81 IAW CONTINENTAL EXPRESS EC 5310-01223. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — DAMAGED (RUDDER) · airframe 11,263 hrs · 8,977 cycles

SHV - DURING C-CHECK RUDDER 1 CENTER HINGE POINT LOWER LEADING EDGE SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — DAMAGED (RUDDER) · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C-CHECK RUDDER NUMBER 1 CENTER HINGE POINT UPPER LEADING EDGE SKIN SUPPORT WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RIB — CRACKED (RUDDER) · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C-CHECK RIB FOUND CRACKED ON RUDDER NUMBER 1 AT LOWER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — CRACKED · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C CHECK PULLEY BRACKET INSIDE PANEL 325 LR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,263 hrs · 8,977 cycles

SHV DURING C CHECK SILL ON RIGHT SIDE SERVICE DOOR WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 SECTION 7 AND GST-3627/02.

Part: RIB — BENT (RUDDER 1) · airframe 11,263 hrs · 8,977 cycles

SHV DURING C CHECK RIB WAS FOUND BENT ON RUDDER NUMBER ONE AT LOWER SIDE OF UPPER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,263 hrs · 8,977 cycles

SHV DURING C CHECK SILL FOWARD OF SERVICE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CAP — GOUGED (CABIN) · airframe 11,263 hrs · 8,977 cycles

SHV-DURING C CHECK CROSSBEAM CAP WAS FOUND GOUGED BETWEEN CENTER AND RIGHT HAND OMEGA BEAMS AT FRAME 22. MAINTENACE REMOVED AND REPLACED AFFECTED CROSSBEAM CAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — DENTED (CABIN) · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C CHECK ANGLE WAS FOUND DENTED ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (NR 2 NACELLE) · airframe 11,263 hrs · 8,977 cycles

DURING C CHECK, NR 2 LOWER NACELLE STRUCTURE WAS FOUND TO HAVE A GOUGED EDGE MEMBER AT STATION XN=776.8MM. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C CHECK NUMBER 2 LOWER COWLING STIFFENER WAS FOUND GOUGED NEAR CENTER LINE AT STAION XN=2180.0MM. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: GUSSET — NICKED · airframe 11,263 hrs · 8,977 cycles

SHV DURING C CHECK GUSSET WAS FOUND NICKED ON NUMBER 2 LOWER COWLING AT STAION XN=3167.5MM. MAINTENANCE REMOVED AND REPLACED AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED · corrosion level 2 · airframe 11,263 hrs · 8,977 cycles

SHV- DURING C CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-06. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,263 hrs · 8,977 cycles

DURING C CHECK, CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE SECTION AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — GOUGED (FUSELAGE) · airframe 11,263 hrs · 8,977 cycles

DURING C CHECK CENTER OMEGA BEAM WAS FOUND GOUGED AT FRAME 23. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ON THE CEILING ADJACENT TO THE GALLEY FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLT 3292 CREW REPORTED THAT THE EMERGENCY EXIT IDENTIFIER SIGN IN THE CENTER CABIN CEILING IS INOP.

Part: BALLAST — DEFECTIVE (GALLEY)

EWR---CO3869, ON POSTFLIGHT INSPECTION, CREW REPORTED SMOKE IN THE GALLEY. BAD GALLEY BALLAST. MAINTENANCE REMOVED AND REPLACED BALLAST FOR GALLEY LIGHT. AIRCRAFT RELEASED FOR SERVICE.

Part: SENSOR — DEFECTIVE (#1 ENGINE)

CLE FLIGHT# 3033 THE CREW REPORTED #1 ENGINE OIL TEMPERATURE WAS HIGH DURING CLIMB.THE ENGINE WAS SHUT DOWN BY THE CREW AND THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 ENGINE OIL PRESSURE/TEMPERATURE SENSOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAULTY (COCKPIT)

CLE - FLIGHT 3218, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE GALLEY EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POSITION #2, PERFORMED A OPERATIONAL CHECK NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVECD, WHEN RELEASED FROM MOD LINE.

Part: RECEPTACLE — BURNED (GALLEY)

CLE FLIGHT 3169 THE CREW REPORTED A BURNING SMELL IN GALLEY. MAINTENANCE INSPECTED AND FOUND THE RIGHT COFFEE JUG RECEPTACLE TO BE BURNT. MAINTENANCE REPLACED THE LEFT AND RIGHT HOT JUG RECEPTACLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

EWR---CO2951, CREW REPORTED GALLEY DOOR EMERGENCY EXIT LIGHT BURNED OUT. MAINTENANCE REMOVED AND REPLACED GALLEY EMERGENCY DOOR EMERGENCY EXIT LIGHT. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERWING SECTION OF THE AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE)

BDL FLT 4122 THE CREW REPORTED NR 2 ENGINE FIRE DETECTION FAILED TEST. MAINTENANCE REPLACED NR 2 ENGINE FIRE DETECTION LOOP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,265 hrs · 6,231 cycles

BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND ROW 12A EMERGENCY LIGHT IN PSU INOPERATIVE. REMOVED AND REPLACED 12A EMERGENCY LIGHT BULB IAW EMB145 MM 33-50-08. OPS, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,265 hrs · 6,231 cycles

BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT IN THE SERVICE DOOR TO BE INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR LIGHT ASSY AND FUSE F2 IN NR 2 POWER SUPPLY IAW EMB145 MM 33-50-10 AND EMB145 CMM 25-60-03. EMERGENCY LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,265 hrs · 6,231 cycles

BTV---CO3944, DURING 4A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT ABOVE PASSENGER/CREW DOOR TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ABOVE PASSENGER/CREW DOOR IAW EMB145 MM 33-50-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 3943 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE AT ROWS 9-11. MAINTENANCE INSPECTED AND SECURED THE LOOSE CONNECTION AT ROW 11A BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 4149 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE AT SEATS 9-11. MAINTENANCE RESECURED CONNECTOR ON BATTERY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE - FLIGHT 4058, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTS IN THE CENTER CABIN WERE INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE AFFECTED POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3690 THE CREW REPORTED THE 4TH AND 5TH SECTION OF EMERGENCY LIGHTS WERE NOT OPERATING. MAINTENANCE INSPECTED THE EMERGENCY LIGHTS AND RESET THE BATTERY PACK AT SEAT 12A. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3722, THE CREW REPORTED THE MIDDLE TWO EMERGENCY LIGHT STRIPS WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3897 THE CREW REPORTED THE EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AT THE WING EMERGENCY EXIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,947 hrs · 5,978 cycles

TYS DURING A SCHEDULED INSPECTION THE FWD RIGHT HAND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-145 MM 33-50-07, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

HSV-FLIGHT3951, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. THE AIRCRAFT RETURNED TO HSV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE AIR/GROUND CIRCUIT BREAKER, OPERATIONALLY CHECKED RETRACTION SYSTEM WITH NO DEFECTS FOUND. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CIRCUIT BREAKER — POPPED (COCKPIT)

IAH - FLIGHT 3951, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE MID-CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE AFFECTED CIRCUIT BREAKER, AND PERFORMED AN OPERATIONAL TEST WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE - FLT 4019 - THE CREW REPORTED THE FORWARD EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT STRIP IAW EMBRAER MM 33-50-12. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST STRIP 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: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,472 hrs · 5,592 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP FROM FRAME 59 TO FRAME 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE.

Part: PIN — CORRODED (HORIZ STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER HINGE PINS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE PINS IAW EMB145 MM 55-10-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEARING — CORRODED (HORIZ STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER SPHERICAL BEARINGS WERE FOUND TO BE WORN AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPHERICAL BEARINGS IAW EMB145 MM 55-37-00-400-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BUSHING — CORRODED (HORIZ STAB HINGE)

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

Part: BUSHING — CORRODED (HORIZ STAB HINGE)

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

Part: ENGINE — FAILED (RT NACELLE)

AMA-CREW REPORTED THAT NR 2 ENGINE SHUTDOWN FOLLOWING A LOUD BANG. A/C LANDED AT AMA WITHOUT INCIDENT. MX REMOVED AND REPLACED NR 2 ENGINE AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — FAILED (NR 2 ENGINE)

AMA - FLT 4210 - THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN FOLLOWING A LOUD BANG. THE AIRCRAFT LANDED AT AMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DEFECTIVE ENGINE WAS ROUTED TO ROLLS ROYCE WHERE IT WAS INSPECTED AND FOUND TO HAVE HAD A FAILURE OF THE 1ST STAGE HP COMPRESSOR BLADE. (M)

Part: CONNECTOR — SHORTED (AFT GALLEY)

CRP - FLT 4198 - DURING CLIMB, THE CREW REPORTED AN ELECTRICAL SMELL IN THE CABIN. THE CRWE PERFORMED AN AIR RETURN, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TRACKED THE SMELL TO A GALLEY COFFEE POT WHICH WAS THEN REMOVED AND PLACED ON MEL IAW EMB145 MEL 25-60-02, CONTROL 001242. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE GALLEY COFFEE POT ELECTRICAL CONNECTOR IAW EMB145 CMM 25-31-98. THE COFFEE POT WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAL — FAILED (CARGO BAY)

YUL - FLT 4005 - THE CREW REPORTED THAT DURING CLIMB THROUGH ICING CONDITIONS THE F/A HEARD A 'LOUD BANG' NE THE LAV AREA, THE APU WAS ALREADY SHUTDOWN AND BLEED LEAK 1-2 WAS NOTED. BLEED LEAK 1 CLEARED AFTER ABOUT 1 MIN BLEED LEAK 2 REMAINED. ENGINE NR 2 WAS SHUTDOWN PER THE QRH. THE AIRCRAFT LANDED BACK TO YUL UNDER WEIGHT AND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RING ON GAMAH JOINT ON THE NR 2 BLEED DUCT BY THE RADIO ALTIMETER IN THE LOW AFT WING FAIRING IAW EMB145MM 36-11-09, LEAKS AND OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ENGINE — FAILED (RIGHT)

EWR - FLT 4133 - CREW REPORTED THAT THEY ABORTED TAKEOFF DUE TO HIGH OIL PRESSURE ON THE RIGHT ENGINE. THE AIRCRAFT WAS MAINTENANCE FERRIED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL CHECK WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — FAILED (RIGHT)

EWR - FLT 4133 - CREW REPORTED THAT THEY ABORTED TAKEOFF DUE TO HIGH OIL PRESSURE ON THE RIGHT ENGINE. AIRCRAFT WAS MAINTENANCE FERRIED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BULBS — FAILED (EXTERIOR)

BTV - FLT 4218 - DURING 3A INSPECTION, MAINTENANCE FOUND BOTH RT AND LT EXTERIOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT BULBS ON LT AND RT. OVERWING EMERGENCY EXIT LIGHTS. OPS CHECKED SYSTEM GOOD. (M)

Part: DRAG ANGLE — CRACKED (EMPENNAGE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101; AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X)

Part: STRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE BUTT CENTER BUTT STRAP WAS FOUND CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REPAIRED THE AFFECTED BUTT STRAP IAW EMBRAER FAX SST-1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X)

Part: CHARGER — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE NR 1 EMERGENCY LIGHT BATTERY CHARGER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. (X)

Part: GUSSETT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, THE LEFT WING OUTBOARD LEADING EDGE OUTBOARD ATTACH GUSSETT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSETT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X)

Part: SUPPORT — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 20 LEFT WAS FOUND CORRODED. MAINTENANCE REPAIRED THE AFFECTED FLOOR SUPPORT IAW EMBRAER FAX SST-1274/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X)

Part: DRAG ANGLE — CRACKED (EMPENNAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X)

Part: BULB — FAILED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT ON PANEL 8AAXW WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING MODIFICATION, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145MM 33-50-07 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM)

BRAKE FAIL MESSAGE, BRAKE INBOARD AND OUTBOARD INOPERATIVE. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS CHECKED GOOD. (M)

Part: CONTROLLER — FAILED (CABIN)

EWR - CREW REPORTED 'EMERGENCY LIGHTS WILL NOT SHUT OFF. MAINTENANCE FOUND A FAULTY EMERGENCY LIGHT CONTROLLER. REMOVED AND REPLACED UNIT. OPS CHECKED GOOD. (X)

Part: O-RING — WORN (VERTICAL STAB)

CLE - FLT 4043 - CREW REPORTED WHILE CLIMBING THROUGH 5,000 FEET WITH ANTI-ICE ON, THEY RECEIVED A LEFT HAND ENGINE BLEED LEAK ON EICAS AND A RED LEAK MESSAGE IN BLEED SWITCH ON OVERHEAD PANEL. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED AN O-RING IN THE VERTICAL STAB DEICE DUCT COUPLING IAW EMB-145 MM 30-12-07, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 406.6 HOURS. TOTAL CYCLES: 294. (X)