N13969

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,091 hrs · 26,321 cycles

DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — FAULTY (CARGO DOOR) · airframe 34,515 hrs · 25,859 cycles

CREW REPORTED A SLOW CABIN PRESSURE LOSS AT FL 310. CABIN ALTITUDE WENT UP TO 14,600 FT IN EMERGENCY DESCENT. MX REPLACED THE CARGO DOOR TRIM SEAL. CABIN OXYGEN GENERATORS REPLACED. OPS CHECKED PRESSURIZATION SYS GOOD. ACFT RELEASED TO SERVICE.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 33,517 hrs · 25,071 cycles

DURING POST FLIGHT WALKAROUND, CREW REPORTED FINDING A FUSELAGE SKIN CRACK ON THE LT DV WINDOW UPPER FRAME AREA. MX PERFORMED REPAIR ON UPPER BEAM ATTACHED TO DV WINDOW AND WINDSHIELD POST ON LT SIDE IAW SRM 51-40-02. SHV MX ALSO PERFORMED REPAIR ON LT DV WINDOW LOWER STRUT AT FASTENER HOLES IAW SRM 51-40-02 AND SRM 51-20-03. LT LOWER STRUT PN 120-35690-509 AND BEAM PN 123-07751-005. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 33,210 hrs · 24,823 cycles

THE CREW REPORTED A BURNING ELECTRICAL ODOR ON DESCENT IN COCKPIT/CABIN ASSOCIATED WITH WINDSHIELD HEAT NOT WORKING. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD TEMP CONTROLLER. OPS CHECKS WERE GOOD.

Part: CONTROL UNIT — FAULTY (BRAKES) · airframe 32,717 hrs · 24,644 cycles

ON TAXI, BRAKES REQUIRED 50-60 PERCENT ACTUATION ON PEDALS TO ENGAGE FOLLOWED BY BRAKE DEGRADED MESSAGE WHICH CLEARED. ON GATE RETURN, BRAKES COMPLETELY FAILED ABOVE 5 KTS. AND REQUIRED USE OF EMERGENCY BRAKE. MX R & R THE BRAKE CONTROL UNIT WITH TAXI AND OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,668 hrs · 23,554 cycles

STRINGER 21L CORRODED FR. 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,668 hrs · 23,554 cycles

STRINGER 21R CORRODED FR 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,668 hrs · 23,554 cycles

SERVICE DOOR CUT OUT HAS CORROSION AT FR 22. REPAIRED IAW EC5310-01373. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 800) · airframe 31,668 hrs · 23,554 cycles

LT EMERGENCY EXIT LOWER SUPPORT CORRODED. REPAIRED LT EMERGENCY EXIT IAW EC5220-01041. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,668 hrs · 23,554 cycles

LOWER CARGO DOOR CUT OUT SUPPORT CORRODED. R & R CARGO DOOR LOWER CUT OUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,254 hrs · 22,445 cycles

CREW REPORTED ROW 1-7 EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED, CHARGED, AND RE-INSTALLED NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,411 hrs · 21,812 cycles

IAH - FLIGHT 2127, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE ROW 123 A & C SIDE PANEL EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRACK — OBSTRUCTED (WINDOW) · airframe 29,268 hrs · 21,689 cycles

FLIGHT 6029 - IAD - FLIGHT CREW REPORTED FO DV WINDOW NOT CLOSED IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. IAD MX FOUND DEBRIS ON THE DV WINDOW TRACK. MX REMOVED DEBRIS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANTI-ICE VALVE — INOPERATIVE (WING) · airframe 29,213 hrs · 21,641 cycles

FLIGHT 2169 - EWR - FLIGHT CREW REPORTED WING ANTI ICE FAIL DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED WING 1 ANTI ICE VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (RUDDER) · airframe 48,424 hrs · 21,064 cycles

RUDDER HARD OVER PROTECTION MESSAGE ON EICAS. R & R RELAY K0774. OPS CHECK GOOD. CLOSED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,702 hrs · 20,511 cycles

MCI - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — BROKEN (CABIN) · airframe 23,664 hrs · 20,454 cycles

FLIGHT 3134 - EWR - FLIGHT CREW REPORTED AFT EMERGENCY LIGHT BRACKET BROKEN. EWR MX REMOVED AND REPLACED BRACKET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — WORN (VERTICAL STAB) · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 AT 12:00 POSITION WAS FOUND TO HAVE ELONGATED BOLT HOLES AND CAUSING FRETTING WITH ADJACENT SKIN PANELS. MAINTENANCE PERFORMED REPAIRS TO THAT AREA IAW EC5310-01317 AND EC5310-01521. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CARGO DOOR LOWER INNER SKIN WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO HAVE CRACKS AT FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02182. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01522. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2L-8L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02182. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,736 hrs · 19,756 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,675 hrs · 19,716 cycles

FLIGHT 3063 - EWR - FLIGHT CREW REPORTED BURNING PLASTIC SMELL DURING FLIGHT. EWR MX PERFORMED FIM TASK FOR ABNORMAL SMELL IN COCKPIT AND COULD NOT DUPLICATE ANY SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (SMOKE DETECTION) · airframe 26,130 hrs · 19,283 cycles

ATL - FLIGHT 2432, THE CREW REPORTED A BAGG SMOKE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED THE BAGG SMOKE DETECTOR, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (THRUST REVERSER) · airframe 25,630 hrs · 18,929 cycles

DAY FLT 2234 THE CREW REPORTED A NR 2 T/R DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED AND TAXIED BACK TO THE GATE. MAINTENANCE PLACED THE T/R SYSTEM ON MEL AND RELEASED THE AIRCRAFT FOR SERVICE. NR 2 PYLON CONNECT P1770 WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 23,872 hrs · 17,595 cycles

FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DISCONNECT TRIGGER AND BROUGHT ACFT TO STOP. CREW WAS UNABLE TO USE TILLER NOR CLEAN STEERING INOP MESSAGE ON EICAS. EWR MX REMOVED AND REPLACED FEEDBACK POTENTIOMETER AND STEERING MANIFOLD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POTENTIOMETER — DEFECTIVE (NLG STEERING) · airframe 23,872 hrs · 17,595 cycles

FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DISCONNECT TRIGGER AND BROUGHT ACFT TO STOP. CREW WAS UNABLE TO USE TILLER NOR CLEAN STEERING INOP MESSAGE ON EICAS. EWR MX REMOVED AND REPLACED FEEDBACK POTENTIOMETER AND STEERING MANIFOLD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,677 hrs · 17,455 cycles

FLIGHT 4932 - EWR - FLIGHT CREW REPORTED STRONG ODOR OF SMOKE IN THE COCKPIT SHORTLY AFTER INITIAL DESCENT. EWR MX RAN PACKS, PRESSURIZED AIRCRAFT, TURNED W/S HEAT ON AND HYDRAULIC PUMPS. NO SMELL WAS DETECTED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,674 hrs · 17,454 cycles

FLIGHT - 2554 - EWR-JAX - FLIGHT CREW DIVERTED TO SAV DUE TO LIGHTNING STRIKE ACCOMPANIED WITH STRONG BURNING SMELL IN COCKPIT. MX INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF LIGHTNING STRIKE. FLIGHT CREW RAN PNEUMATIC SYSTEMS AND COULD NOT DUPLICATE SMELL IN COCKPIT. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,344 hrs · 16,471 cycles

RIC MX DURING ROUTINE INSPECTION RIC MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. RIC MX R&R EMERGENCY LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,029 hrs · 15,554 cycles

FLIGHT 2076 CREW REPORTED BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED REAR EMERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,029 hrs · 15,554 cycles

FLIGHT 2076 CREW REPORTED BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 16,846 hrs · 12,407 cycles

SHV DURING C-CHECK, RT HORIZONTAL STAB L/E HAS SEVERAL AREAS OF CORROSION ON SKIN AROUND RIVET HEAD AND SOME RIVET HEADS PULLING THROUGH SKIN. MAINTENANCE REPAIRED RT HORIZONTAL STAB L/E IAW EC5530-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,846 hrs · 12,407 cycles

SHV- DURING C-CHECK, CENTER OMEGA BEAM AT FS 20 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FS 20 IAW EMB 145 SRM 51-40-02. THE AIRCAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,190 hrs · 9,532 cycles

LFT - THE CREW REPORTED, THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: TIMES/CYCLES NOT TRACKED ON THIS PART.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 13,190 hrs · 9,532 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 13,190 hrs · 9,532 cycles

IAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 13,166 hrs · 9,510 cycles

CLE - THE CREW REPORTED THE EMERGENCY EXIT LIGHT OUT AT 3B. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,365 hrs · 8,913 cycles

DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT LOCATED ON THE COCKPIT STEP INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 12,134 hrs · 8,737 cycles

PILOT REPORTED THAT THE EMERGENCY LIGHTING DID NOT WORK WHEN TESTED DURING PREFLIGHT INSPECTION. THE ENGINES WERE RUN TO RECHARGE THE BATTERY PACKS AND AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM WAS ACCOMPLISHED. THE EMERGENCY LIGHTS TESTED GOOD AND THE DISCREPANCY WAS CLEARED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,018 hrs · 8,649 cycles

SHV - DURING ROUTINE MAINTENANCE THE AISLE PATH LIGHTS 1 THRU 3 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 SRM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 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) · airframe 12,018 hrs · 8,648 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE CROSSMEMBER BETWEEN THE LEFT HAND SILL AND THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · airframe 12,018 hrs · 8,648 cycles

DURING C-CHECK THE CENTER BUTTSTRAP FROM FRAME 59 TO FRAME 61 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 (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FLOORBEAM) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP DOUBLERS AT FRAMES 20 AND 23 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CARGO BAY) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE LEFT HAND CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 60 AND FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 12,018 hrs · 8,648 cycles

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

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE LEFT HAND SIDE WALL DOUBLER AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 12,018 hrs · 8,648 cycles

SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 12,018 hrs · 8,648 cycles

SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, STEP 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DISCONNECTED (CABIN)

CREW REPORTED DURING PREFLIGHT, AFT FLOOR EMERGENCY PROXIMITY STRIP LIGHTING INOPERATIVE. MAINTENANCE RESECURED THE AFT EMERGENCY FLOOR PATH LIGHT STRIP. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

DURING ROUTINE MAINTENANCE THE CAPTAINS EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C CHECK, CORROSION WAS FOUND ON LT LAV AREA FLOORBEAM. MAINTENANCE REMOVED AND REPLACED LT LAV AREA FLOORBEAM, ALODINED, PRIMED AND PAINTED IAW EMB 135/145 SRM 53-30-01; 51-40-02; 51-21-03; 51-40-01 AND EMB 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C INSPECTION, THE AFT SERVICE DOOR SILL WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT DOOR SILL IAW EMB 135/145 SRM 53-21-10; 51-20-03; 51-40-06 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C INSPECTION THE AFT PAX DOOR SILL WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SILL AT AFT PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION THE PASSENGER DOOR SILL WAS TO BE CORRODED ON THE LEFT HAND AFT SECTION. MAINTENANCE REMOVED AND REPLACED THE SILL SECTION IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS TO HAVE CORROSION ON THE FORWARD SECTION. MAINTENANCE REMOVED AND REPLACED THE SILL SECTION IAW EMB145 SRM 53-21-10, 51-20-03 AND 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED AT THE AFT SECTION. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB GST 1927/02A AND EMB145 CPM 51-21-05, THE REPAIR WAS FOUND TO SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — GOUGED (RT WING) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND LEADING EDGE NR 2. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 2649/02 AND EMB145 AMM 57-41-00. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION THE TOP CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 1927/02A AND EMB145 CPM 51-21-04, 51-21-05 AND 51-21-06. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DOUBLER — CORRODED (FRAME 20) · airframe 8,096 hrs · 5,526 cycles

TYS During a scheduled inspection, corrosion was found on a doubler at the right hand beam hat section at frame 20. Maintenance accomplished a blend-out repair IAW EMB GST #1927/02A and EMB145 CPM 51-21-04,05 and 06. The repair was satisfactory, the aircraft will be released upon completion of inspection.

Part: SKIN — GOUGED (RT WING) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND NR 1 LEADING EDGE. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 2512/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 1927/02A, EMB145 CPM 51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (GALLEY FLOOR) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND THE GALLEY GUSSET CORRODED. MAINTENANCE R/R NEW GUSSET IAW EMB 135/145 SRM 51-40-02. COUNTERSUNK HOLES IAW EMB 135/145 SRM 51-40-06,PAINTED TOP GUSSET IAW CPM 51-21-06. ALL WORK WAS ACCOMPLISHED AND WIL BE REL. UPON COMPLETION OF ALL WORK.

Part: STRAP — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS FOUND FWD DIGITAL PLATE AT GALLEY CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW FWD STRAP IAW EMB 145 SRM 53-21-10; SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS, DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM WAS FOUND CORRODED AROUND SEVERAL FASTENERS IN LAV. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW-EMB-135/145-SRM-51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BUSHING — CORRODED (SERVICE DOOR) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND THE DAMPER BUSHING ON THE SERVICE DOOR SIDE SHOWING SIGN'S OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE DAMPER, CLEANED AND INSPECTED AREA IAW EMB 145 AMM 52-43-00. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FRAME — CHAFED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND CHAFING ON FRAME 70 AT STRINGER 13R. MAINTENANCE INSPECTED AND BLENDED AREA,THEN ALODINE, PRIME AND PAINTED IAW EMB 135/145 SRM 51-102. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,096 hrs · 5,526 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD RAMP ANGLE AT FRAME 19 AND 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: BATTERY — BURNED OUT

TYS DURING A ROUTINE CHECK THE EMERGENCY PROXIMITY STRIPS WERE OUT. MAINTENANCE R/R #4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK WAS GOOD. AIRCRAFT WAS REL. TO SERVICE UPON COMPLETION OF WORK.

Part: CARBON SEAL — LEAKING (RT ENGINE)

TYS. CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED LAVATORY SMOKE ALARM & WARNINGS WHEN BLEEDS WERE TURNED ON. A/C RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED THE RT ENGINE CARBON SEAL, ALL-OPERATIONAL AND LEAKS CHECKS WERE SATISFACTORY. IAW ROLLS-ROYCE AE3008A MAINTENANCE MANUAL 72-00-00 AND EMB 145 M.M. 71-03-01. A/C RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (FUSELAGE)

EWR-CREW REPORTED LAV SMOKE WARNING ON CLIMBOUT. NO SMOKE NOTED. MX REMOVED/REPLACED SMOKE DETECTOR IAW EMB145 MM 26-18-01 OPS CHECKED SATISFACTORY IAW EMB 145 MM 26-14-00. REFERENCE M-602 #313920 FOR WORK ACCOMPLISHED.

Part: COMPUTER — FALSE INDICATION (LAVATORY)

THE FLIGHT CREW REPORTED A FALSE LAV SMOKE WARNING DURING CLIMB. MX RELEASED A/C IAW MEL 26-14-00, PLACARD #005807. EFD MX REMOVED/REPLACED #2 DAU (DATA ACQUISITION UNIT) IAW EMB145 AMM 31-41-01. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAV)

CREW REPORTED A LAV SMOKE WARNING DURING CLIMB. MX RELEASED A/C IAW MEL 26-14-00, PLACARD 005797. BNA MX REMOVED/REPLACED LAV SMOKE DETECTOR IAW 26-14-01 AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: DETECTOR — INOPERATIVE (LAVATORY)

IAH - FLT 4095 - THE CREW REPORTED A LAVATORY SMOKE WARNING ON CLIMB-OUT THROUGH 6000 FEET WITH NO SMOKE NOTED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE LAVATORY SMOKE DETECTOR WAS PLACED ON MEL 26-14-00 CONTROL NR 005501, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLT 3744 WHERE MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR AND REMOVED THE MEL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: GENERATOR — SHORTED (NR 1 ENGINE)

FLT 4219 - IAH-AMA - THE CREW REPROTED THAT THE NR 2 GENERATOR OFF BUS LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT AMA WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE NR 2 GENERATOR TO HAVE SHORTED INTERNALLY, BURNING AND SPLITTING THE HOUSING. MAINTENANCE REMOVED AND REPLACED THE GENERATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (ROW 7)

BTV - FLT 4218 - DURING SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT ROW SEVEN INOPERATIVE. SECURED LOOSE CONNECTION ON OVERHEAD EMERGENCY LIGHT AT ROW SEVEN. OPS CHECKED GOOD. (M)

Part: BULB — FAILED (CABIN)

BTV - FL 3944 - MAINTENANCE FOUND DURING 2A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECKED, SYSTEM GOOD. (X)