N13975

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,132 hrs · 34,675 cycles

IAH - THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT AT ROW THREE TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDOW POST — CRACKED (LEFT) · airframe 44,517 hrs · 34,424 cycles

LEFT COCKPIT WINDSHIELD LATERAL POST WAS CRACKED. REPAIRED THE POST IAW SB 145-53-0029.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,817 hrs · 34,424 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LT FLOOR SILL AT FRAME 32 AND 33 WITH CORROSION. MAINTENANCE R&R THE ENTIRE SILL IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: RIB — CRACKED (LT WING) · airframe 43,864 hrs · 33,665 cycles

LT WING RIB 5 CRACKED. REMOVED AND REPLACED LT RIB 5 IAW ECTC ETD2017-145-104919. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 42,335 hrs · 32,427 cycles

MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,335 hrs · 32,427 cycles

MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 39,074 hrs · 29,780 cycles

DURING MAINTENANCE INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,985 hrs · 29,709 cycles

DURING MAINTENANCE INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYSTEM BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,416 hrs · 29,257 cycles

DURING ROUTINE MAINTENANCE THE MAIN DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE SIGN ASSY AND OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,014 hrs · 26,578 cycles

DURING MAINTENANCE INSPECTION, THE MAIN CABIN DOOR EXTERIOR AND CEILING LIGHTS WERE FOUND INOPERATIVE. R & R THE NR 1 EMERGENCY LIGHT SYS BATTERY POWER SUPPLY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (SMOKE DETECTOR) · airframe 34,228 hrs · 25,976 cycles

PILOT REPORTED LAVATORY SMOKE WARNING ON EICAS IN FLIGHT BUT NO SMOKE OBSERVED IN CABIN OR LAVATORY. MX R & R THE LAVATORY SMOKE DETECTOR PANEL OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,066 hrs · 25,852 cycles

DURING SCHEDULED MX INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 31,277 hrs · 23,653 cycles

CREW REPORTED LOST AUTO PRESSURIZATION. CABIN PRESSURE CLIMBED TO 8400FT, NO EICAS MESSAGE PRESENT. CREW PERFORMED AIR RETURN. MX R & R DIGITAL PRESSURE CONTROLLER AND ALSO R & R ELECTROPNEUMATIC OUTFLOW VALVE WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,252 hrs · 23,636 cycles

DURING C-CHECK, FOUND THE RT WALL SEAT TRACK SUPPORT AT FRAME 50 CORRODED. MX BLENDED OUT THE CORROSION IAW SRM 51-10-03. FOUND AREA TO BE WITHIN LIMITS IAW 53-23-10. R & R ALL CORRODED FASTENERS IAW SRM 51-40-02. REMOVED ALL CORRODED NUTPLATES IAW SRM 51-40-09. FABRICATED AND INSTALLED A NEW DOUBLER AFTER CUTTING OUT THE DAMAGE AREA. INSTALL DOUBLER IAW EC 5320-01534. REFINISH ALL MATERIALS IAW CPM 51-21-07. ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,265 hrs · 23,643 cycles

CORROSION OUT OF LIMITS ON INNER SKIN BAYS BETWEEN STR 20R & 21L & 22L AT FRM 13 & 14. CUTOUT CORRODED AREAS, FABRICATED 2 FILLERS AND ONE DOUBLER. ACFT STILL IN C CHECK.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 27,969 hrs · 20,930 cycles

ORD FLT 5999 THE CREW REPORTED CABIN ALTITUDE BEGAN TO CLIMB AT A HIGH RATE UNTIL IT REACHED 10,500. THE AIRCRAFT WAS AT 34,000. BEGAN A RAPID DESCENT TO 10,500. AMBER DASHES ON CABIN RATE. MASKS DID NOT DEPLOY. LEVELED OUT AT 11,000 MSL AND THE PRESSURIZATION SYSTEM BEGAN TO RESPOND NORMALLY EVENTUALLY REGAINING PRESSURE AND CONTROL. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURE CONTROLLER, THE ELECTRO-PNEUMATIC OUTFLOW VALVE AND THE PNEUMATIC OUTFLOW VALVE. PERFORMED OPERATIONAL CHECKS OF THE MANUAL AND AUTOMATIC PRESSURIZATION SYSYTEM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 23,923 hrs · 19,668 cycles

FLIGHT 2699 - FLIGHT CREW REPORTED LT COFFEEMAKER SMOKING. EWR MX REMOVED AND REPLACED LT COFFEEMAKER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTTON — FAULTY (COCKPIT) · airframe 26,383 hrs · 19,659 cycles

CLE - FLT 2339 - THE CREW REPORTED THE BAG EXTINGUISHER PUSH BUTTON DID NOT ILLUMINATE DURING FIRE DETECTION TEST. MAINTENANCE INSPECTED AND REPLACED THE BAG EXTINGUISHER PUSH BUTTON. OPERATIONAL CHECKS WERE GOOD.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 26,374 hrs · 19,652 cycles

RIGHT LAV TOP CAP HAS SURFACE CORROSION AT CARBON CROSS BEAM. REMOVED AND REPLACED RT TOP CAP IAW EMB SRM 51-40-09.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,195 hrs · 19,527 cycles

IAH - FLIGHT 2804, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE RESET THE ELECTRICAL SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,535 hrs · 19,039 cycles

FLIGHT 2074 - EWR - FLIGHT CREW REPORTED NR 1 FLOOR EMERGENCY LIGHT STRIP AND SERVICE DOOR EXIT LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,178 hrs · 18,766 cycles

DURING ROUTINE MAINTENANCE THE NR 4 AND 5 EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. THE NR 5 EMERGENCY LIGHT INVERTER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (NLG) · airframe 25,005 hrs · 18,636 cycles

CLE FLT 2866 THE CREW REPORTED THE LANDING GEAR HANDLE AND GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND RESECURED THE NOSE LANDING GEAR PROXIMITY SWITCH HARNESS CONNECTOR. THE NOSE STRUT WAS ALSO SERVICED.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 24,905 hrs · 18,572 cycles

EMERGENCY LIGHT CIRCUIT BREAKER POPPING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 1, MOUNT TRAY AND CONNECTOR IAW EMB145 AMM 33-50-04, 20-13-07 AND 20-50-00. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. BATTERY CHARGER ASSY PN 11-0049, S/N 13615 UNICORP BATTERY POWER SUPPLY P/N 11-0049, S/N 12825 UNICORP EMERGENCY LIGHT BATTERY P/N 2013, S/N 98868.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,123 hrs · 17,991 cycles

RIC MX - DURING ROUTINE INSPECTION, MX FOUND EMERGENCY LIGHT STRIP BY SEATS 1A AND 2A INOPERATIVE. RIC MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,750 hrs · 16,938 cycles

AIRCRAFT IN FOR A OVERNIGHT INSPECTION WHEN THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD AND WAS RELEASED.

Part: CONNECTOR — DIRTY (NLG WW) · airframe 22,406 hrs · 16,676 cycles

ON TAKEOFF ROLL THE CREW REPORTED RELAYS CLICKING, AND AFTER TAKEOFF CLICKED AGAIN VERY LOUD AND A JOLT WAS FELT THROUGH THE YOLK AND RUDDER PEDALS. AT 12000 FT, THE LOUD CLICKING OCCURRED SEVERAL TIMES AND RECEIVED EMERG LIGHTS NOT ARMED AND ELEC EMERG ABNORMAL MSGS APPEARED ON EICAS AND THEN WENT AWAY. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND CLEANED THE NLG UPLOCK BOX PROX SWITCH CONNECTOR, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 21,820 hrs · 16,244 cycles

RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND FORWARD EMERGENCY LIGHT STRIP NOT ILLUMINATING. MX RECONNECTED LOOSE WIRING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — DISCONNECTED (CABIN) · airframe 21,820 hrs · 16,244 cycles

RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MX FOUND ONE WIRE DISCONNECTED FROM THE SPLICE. MX RECONNECTED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY)

SHV - DURING C-CHECK IT WAS FOUND THAT THE APU FIREWALL WAS CRACKED AROUND RIVETS AT 3 O`CLOCK POSITION. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5330-01827. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,836 hrs · 14,891 cycles

FLIGHT 2875 IAH-MFE, THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION AND SYSTEM CHECKS. THE BURNING SMELL COULD NOT BE DUPLICATED AND THE DISCREPANCY WAS CLEARED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 19,594 hrs · 14,723 cycles

FLT 3035 - EWR - CREW REPORTED 3 AFT EMERGENCY LIGHT STRIPS INOPERATIVE. EWR MX FOUND BROKEN WIRE AT EMERGENCY LIGHT NR 8. ME REPAIRED WIRING AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,709 hrs · 14,070 cycles

BAN - DURING MAINTENANCE INSPECTION THE NUMBER 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,475 hrs · 16,614 cycles

CLE FLIGHT NR 2351 - THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT STRIP AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 16,531 hrs · 12,403 cycles

SHV - DURING C-CHECK STR 21R HAS CORROSION BETWEEN FR 12-13. MAINTENANCE REMOVED DAMAGE STR & SPLICED IN NEW SECTION 21R FR 10-13 IAW EMB 145 SRM 53-00-03 ITEM 2 CPE 11001-1 FIGURE 201. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 16,531 hrs · 12,403 cycles

SHV - DURING C-CHECK STR 21L HAS CORROSION BETWEEN FR12-13. MAINTENANCE REMOVED AND REPLACED STR 21 FR 8-13 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,531 hrs · 12,403 cycles

SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 65 BETWEEN STRINGERS 15 AND 16 L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — BROKEN (FUSELAGE) · airframe 15,572 hrs · 11,650 cycles

CLE FLIGHT NR 2541, CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIR RETURN. MAINTENANCE INSPECTED FOUND AIR SERVICE CHECK VALVE DOOR BROKEN. DOOR ASSEMBLY REMOVED AND REPLACED. ALL OPERATIONAL CHECKS REPORTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,538 hrs · 11,630 cycles

CRP - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING STRIP AT SEAT 14A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (GALLEY LIGHT) · airframe 14,851 hrs · 11,079 cycles

DURING ROUTINE MAINTENANCE THE GALLEY HAD A BURNING ODOR. MAINTENANCE INSPECTED AND FOUND THE GALLEY LIGHT BALLAST BURNED. THE BALLAST WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 14,011 hrs · 10,402 cycles

CREW REPORTED, ODOR OF BURNING PLASTIC OCCURRED IN CRUISE, TURNED OFF RECIRCULATING FAN, ODOR WENT AWAY. ODOR ONLY IN COCKPIT. INSPECTED CABIN AND COCKPIT FOR BURNING ODOR. NO UNUSUAL ODOR. PERFORMED OPERATIONAL CHECK OF RECIRCULATION FAN IAW EMB145 MM 21-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. CREW REPORTED STRONG ODOR IN COCKPIT ON DESCENT, SIMILAR TO THAT AS DISCRIBED IN LAST ENTRY. ODOR COULD ALSO BE DESCRIBED AS AN INTENSE MILDEW. MAINTENANCE PERFORMED ENGINE RUNS IAW EMB MM 71-00-01. ALSO RAN APU AND ALL BLEED SYSTEM IAW EMB145 MM 49-00-00 AND 36-00-00. COULD NOT DUPLICATE ODOR. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 14,764 hrs · 10,841 cycles

IAH - FLIGHT 2890, DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,668 hrs · 8,573 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT THE CROSSBEAM BETWEEN FRAMES 24 AND 25. 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: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,668 hrs · 8,573 cycles

SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,668 hrs · 8,573 cycles

SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 11,668 hrs · 8,573 cycles

DURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, THE ENSUUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HARNESS — SHORTED (CABIN)

LIT FLIGHT#2474 THE CREW REPORTED THE CABIN LIGHT AT ROW 6A SHORTED OUT CAUSING SPARKS AND ELECTRICAL SMELL IN THE CABIN.MAINTENANCE INSPECTED AND REPLACED THE WIRING HARNESS ASSEMBLY FOR ROW 6A LIGHTING.OPERATIONAL CHECKS WERE GOOD.

Part: FITTING — BENT · airframe 7,744 hrs · 5,450 cycles

TYS. During a scheduled inspection, the left aileron PCA fitting attach lug was found bent. Maintenance removed and replaced the fitting. I/A/W-EC5750-01177. The repair was satisfactory and the aircraft will be released upon complection of the check.

Part: INTAKE — DAMAGED (NR 1 ENGINE) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED 2-C INSPECTION, THE NR 1 ENGINE INLET INNER SKIN WAS FOUND PROTRUDING ON AFT SIDE OF SKIN AT 4:00 AND 10:00 O`CLOCK POSITIONS. MAINT. MEASURED THE PROTRUDING SKINS ON THE AFT SIDE .THEY RECONTOURED THE AFFECTED AREA TO THE ORIGINAL SHAPE AND PERFORMED NDI; NO CRACKS NOTED, APPLIED SEALANT, ALODINED, PRIMED AND PAINTED IAW GST 3274/02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED. UPON COMPLETION OF ALL WORK.

Part: SKIN — DENTED (RUDDER) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A DENT IN NR 1 RUDDER, RT SIDE BETWEEN RIB 2890.0 AND 2601.0. THE AREA WAS CUT OUT AND A EXTERNAL DOUBLER WAS FABRICATED. DRILLED,ALODINED,PRIMED AND PAINTED AND INSTALL THE DOUBLER. ALL WORK WAS ACCOMPLISHED IAW GST 3254/02;EMB 145 SRM 51-40-02'03 CPM 5121-04-05-06. A/C WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE GALLEY FLOOR FORWARD FLOORBEAM CAP WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB-145 SRM 53-21-10, 51-40-02 AND CPM 51-21-04,05,06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE RT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 1927/02A, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE RIGHT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE LEFT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CHANNEL — CORRODED (GALLEY FLOOR STR) · airframe 7,744 hrs · 5,450 cycles

TYS During a scheduled inspection the aft galley floor step-up channel was found to be corroded at frame 23. Maintenance removed and replaced the channel IAW EMB-145 SRM 51-40-02, the repair was satisfactory. The aircraft will be released upon completion of inspection.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST 1927/02A, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FITTING — GOUGED (HORIZONTAL STAB) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE HORIZONTAL STAB LEFT INBOARD LUG FOR THE MOUNT PIN WAS FOUND TO BE GOUGED. MAINTENANCE POLISHED OUT THE DAMAGED AREA IAW EMBRAER GST 3175/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE AFT FLOORBEAM TOP CAP WAS FOUND CORRODED UNDERNEATH THE GALLEY AREA. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-145 SRM 53-21-10 AND CPM 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE AFT GUSSET UNDERNEATH THE GALLEY AREA WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB145 SRM 53-21-10 AND CPM 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,744 hrs · 5,450 cycles

DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM TOP CAP WAS FOUND CORRODED UNDERNEATH THE GALLEY AREA. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-145 SRM 53-21-10, 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: OIL SYSTEM — OVERSERVICED (APU)

EWR FLIGHT 3505 THE CREW REPORTED THE APU EMITS STRONG FUMES IN THE CABIN. MAINTENANCE INSPECTED AND PLACED ON MEL. THEN FOUND APU OIL LEVEL TO BE TOO HIGH. THE OIL LEVEL WAS REDUCED TO PROPER LEVEL AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHROUD — CRACKED (EMPENAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE APU COWLING EXHAUST SHROUD WAS FOUND CRACK. MAINTENANCE REPAIRED THE APU COWLING IAW EMB-145 GST-0771/01. THE REPAIR WAS SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING STRIP WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING STRIP IAW EMB-145 MM 33-50-12, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.

Part: TAB — CHAFED (RT ELEVATOR) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ELEVATOR SPRING TAB ACTUATOR INBOARD FAIL SAFE TAB, WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE FAIL SAFE TAB IAW EMB GST-0705/01 AND EMB-145 CPM 51-21-06, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: SKIN — GOUGED (FUSELAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT WAS FOUND TO BE GOUGED FROM STATION 20793 THROUGH 25581. MAINTENANCE REPAIRED CARGO DOOR CUTOUT IAW EMB GST-0707/01 AND EMB-145 CPM 51-21-04, 05, 06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE SUPPORT STRUCTURE FOR THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED SUPPORT STRUCTURE BY INSTALLING DOUBLER IAW EMB-145 SRM 53-21-10 AND 53-40-02. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FITTING — GOUGED (FUSELAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION, THE FITTING FOR STRINGER 36 WAS FOUND TO BE GOUGED AT THE UPPER AFT EDGE OF THE PASSENGER DOOR CUTOUT. MAINTENANCE REPAIRED THE FITTING IAW EMB GST-0723/01, AND EMB-145 CPM 51-21-03, 04, 06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: SKIN — DAMAGED (EXIT DOOR) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR, INNER SKIN BY WINDOW WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED SKIN BY BLENDING IAW EMB GST-0720/01 AND EMB-145 CPM 51-21-03,04,06. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: SKIN — DAMAGED (EXIT DOOR) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULE INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT DOOR, INNER SKIN BY WINDOW WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED SKIN BY BLENDING IAW EMB GST-0720/01 AND EMB-145 CPM 51-21-03,04,06. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,825 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FLIGHT RECORDER — FAILED (EMPENAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULE INSPECTION THE FLIGHT DATA RECORDER FAILED FUNCTIONAL CHECKS, REFER TO CONTINENTAL EXPRESS TASK CARD 31-31-00-720-001-A00. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DATA RECORDER IAW EMB-145 MM 31-31-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION.

Part: HEAT SHIELD — GOUGED (FUSELAGE) · airframe 3,835 hrs · 2,620 cycles

TYS DURING A SCHEDULED INSPECTION THE APU FIREWALL HEAT BLANKET WAS FOUND GOUGED AT THE BLEED VALVE MOUNT BRACKET. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL HEAT BLANKET IAW EMB-145 SB 145-53-0004. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF SCHEDULED INSPECTION.

Part: FIRE LOOP — FAULTY (RT ENG PYLON)

YHZ - CREW REPORTED E2 FIRE DETECTOR FAILED. DISPATCHED MAINTENANCE TO HALIFAX. TROUBLESHOT PROBLEM AND FOUND A BAD NR 2 ENGINE FIRE LOOP. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PYLON FIRE LOOP. OPS CHECKED GOOD IAW EMB 145 AMM, JIC 26-11-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERABLE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE FOWARD EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)