N41104

Part: A/C PACK — OVERTEMP (NR 2) · airframe 42,324 hrs · 25,974 cycles

PACK 2 OVERHEAT WITH BURING SMELL IN COCKPIT. COMPLIED WITH STEPS 5 BLOCK 1, 2, AND 12 OF EIM TGASK. COMPLED WITH BLOCK 2 STEPS 1 AND 2 WITH BOTH ENGINES AT TAKE OFF POWER. MESSAGE AND BURNING SMELL NOT DUPLICATED. TRANSITORY CONDITION PER BLOCK 12. OPS CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 39,412 hrs · 23,538 cycles

EMERGENCY LIGHT STRIP IS CRACKED ACROSS FROM SEAT 2A. R & R THE LIGHT STRIP, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,575 hrs · 21,223 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,412 hrs · 21,094 cycles

NR 11 MAIN DOOR EXIT MARKER LIGHT IS INOPERATIVE. R & R NR1 BATTERY POWER SUPPLY. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,412 hrs · 21,094 cycles

NR 1 MAIN DOOR EXTERIOR FLOOD LIGHT ON BOTTOM SIDE OF THE PLUG DOOR HINGE IS INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 36,331 hrs · 21,028 cycles

NOSE GEAR DOOR DID NOT CLOSE AFTER GEAR RETRACTION, 1 MAIN GEAR POSSIBLY DOWN DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR FWD DOOR PROXIMITY SWITCH, PERFORMED GEAR SWING AND OPS CHECK GOOD. RETURNED TO SERVICE.

Part: BLEED VALVE — FAILED (APU) · airframe 34,991 hrs · 19,957 cycles

APU BLEED VALVE FAILED MESSAGE FOLLOWED BY APU FAILED MESSAGE ON EICAS, APU INDICATED 28V ON BUSS, ACFT RETURNED TO BLOCKS. REPLACED THE BLEED VALVE, OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 31,740 hrs · 17,837 cycles

THE CENTER OVERHEAD EMERGENCY EXIT LIGHT ABOVE ROW 18 WAS REPORTED INOPERATIVE. MX SECURED CONNECTOR ON SIGN AND OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,739 hrs · 17,836 cycles

THE CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT SIGN WAS REPORTED INOPERATIVE. MX R & R THE LIGHT PANEL ASSY WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,238 hrs · 15,583 cycles

DURING MX INSPECTION, AN OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOPILOT) · airframe 25,677 hrs · 13,898 cycles

DURING CLIMB, THE CREW RECEIVED AN AUTOPILOT FAIL MESSAGE ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SYS AND OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED NOR DID THE INDICATION ILLUMINATE AGAIN. THE DISCREPANCY WAS CLEARED AND THE ACFT RETURNED TO SERVICE.

Part: AOA — BURNED (ZONE 100) · airframe 25,661 hrs · 13,890 cycles

ACFT WAS ENROUTE WHEN LIGHTNING STRUCK ACFT CAUSING A BURNING ODOR IN THE CABIN. THE CREW LANDED SAFELY. MX COMPLIED WITH A LIGHTNING STRIKE INSPECTION IAW AMM2 5-50-01. R & R THE NR 2 AOA VANE IAW AMM 27-36-01. OPS CHECKED GOOD AND WAS RELEASED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,231 hrs · 13,652 cycles

DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,231 hrs · 13,652 cycles

CORRECTED SDR FOR A/C 41104 NEW NUMBER: DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 23,424 hrs · 12,599 cycles

TYS - A/C WAS EN ROUTE FROM IAH TO IND WHEN THE CREW REPORTED A HAZY SMOKE IN CABIN, AFTER LANDING MOSTLY IN THE AFT CABIN. LANDING WAS NORMAL AND NO ICIAS INDICATIONS. A/C WAS FERRIED TO TYS WHERE THE NR 2 ENGINE WAS REMOVED AND REPLACED IAW EMB 145XR AMM-7100-00-00. ALL WORK ACCOMPLISHED AND WAS RELEASED AFTER ALL LEAKS CHECKS AND RUNS C/W.

Part: ENGINE — CONTAMINATED · airframe 23,363 hrs · 12,565 cycles

MHT FLT 2635 - THE CREW REPORTED SMOKE IN THE CABIN, COCKPIT AFTER TAKEOFF. ALSO RECEIVED A LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO MHT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND RESIDUAL DEICE FLUID IN THE ENGINES CAUSING THE SMOKE. THE SYSTEM WAS PURGED OF ALL FLUID. OPERATIONAL CHECKS WERE GOOD AND NO SMOKE WAS NOTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,353 hrs · 12,555 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 48-49. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — DAMAGED (AILERON) · airframe 23,353 hrs · 12,555 cycles

SHV - DURING C-CHECK LT AILERON I/B HAT BUSHING OF O/B ATTACHMENT POINT OF PCA IS MIGRATED. REPLACED ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 23,298 hrs · 12,524 cycles

THE CREW REPORTED A BURNING SMELL IN THE GALLEY. MAINTENANCE INSPECTED AND FOUND PLASTIC DEBRIS ON THE NR 2 COFFEE POT. REMOVED DEBRIS AND OPERATIONAL CHECKS WERE GOOD.

Part: PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 22,541 hrs · 12,132 cycles

FLIGHT 3009 - EWR - FLIGHT CREW REPORTED LAV SMOKE TEST INOPERATIVE. EWR MX REMOVED AND REPLACED LAV SMOKE PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — DEFECTIVE (BLEED AIR SYS) · airframe 22,265 hrs · 11,944 cycles

IAH - FLIGHT 2020, THE CREW REPORTED A BLEED ONE OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TEMP SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 20,646 hrs · 11,071 cycles

DURING ROUTINE MAINTENANCE THE AFT CARGO SMOKE DETECTOR FAILED THE TASK CARD 26-15-01-212-001-A00 OPERATIONAL CHECKS. MAINTENANCE REPLACED THE SMOKE DETECTOR AND OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (ZONE 700) · airframe 19,695 hrs · 10,565 cycles

IAH - FLIGHT 2365, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL AND E1-2 TR DISAGREE MESSAGES IN CRUISE. WHEN EXTENDING THE LANDING GEAR ON APPROACH, ALL MESSAGES CLEARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NOSE LANDING GEAR AIR/GROUND PROXIMITY SWITCH. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

ACFT IN C-CHECK AND THE RT FLOOR SILL FROM FR 42 THRU FR 48 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

2 DENTS, LT FUSELAGE BETWEEN FR 19 AND 20. REPAIRED DAMAGE IAW IC2009-145/04712. REFINISHED SURFACE IAW CPM51-21-07, EC5330-01937.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

SERVICE DOOR SILL CORRODED AT SCREW HOLES. BLENDED MINOR CORROSION IAW SRM 51-10-03, RESTORED FINISH.

Part: SILL — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

AIRCRAFT IN C-CHECK STATUS AND THE LT FLOOR SILL AT FRAME 32 THRU FRAME 33 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

ACFT IN C-CHECK AND THE RT FLOOR SILL AT FRAME 33 THRU FRAME 34 WAS FOUND CORRODED. MX BLENDED OUT THE CORROSION, FOUND TO BE WITHIN LIMITS. ALLODINED, PRIMED AND PAINTED IAW SRM 51-10-03 AND SRM 51-21--04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECKS.

Part: SILL — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

ACFT IN C-CHECK AND THE RT FLOOR SILL AT FR 36 THRU FR 42 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

ACFT IN C-CHECK WHEN THE INBD SIDE OF THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 54 THRU FR 58. MX BLENDED THE SURFACE CORROSION IAW SRM 51-10-03 AND ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — GOUGED (PAX DOOR) · airframe 18,741 hrs · 10,035 cycles

ACFT CURRENTLY IN A C-CHECK STATUS WHEN INSP FOUND A GOUGE ON THE PAX DOOR AFT SIDE LWR EDGE. MX MEASURED, BLENDED AND INSTALL A DOUBLER OVER THE DAMAGED AREA. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

LT FLOOR SILL CORRODED AT FRM 47. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

LT FLOOR SILL AT FRM 32-33 HAS CORROSION. REMOVED AND REPLACED SILL IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

SHEAR CLIP HAS A CRACK AT FR 81 AND STR 10L. REMOVED AND REPLACED CRACKED SHEAR CLIP IAW SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

RT FLOOR SILL CORRODED AT FRM 50. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10, RESTORED FINISH.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

FUSELAGE DENTED AT FRM 28, STR 13R. REPAIRED BY CUTTING OUT DAMAGED AREA, FABRICATED FILLER AND INSTALLED DOUBLER IAW EC5330-01936. AIRCRAFT STILL IN C-CHECK.

Part: SILL — CORRODED (GALLEY) · airframe 18,739 hrs · 10,034 cycles

AFT GUSSET IN GALLEY AREA CORRODED. THE AFT GUSSET WAS REMOVED AND REPLACED.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,739 hrs · 10,034 cycles

LT FLOOR SILL IS CORRODED AT FRM 49. REMOVED AND REPLACED FLOOR SILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,739 hrs · 10,034 cycles

LT FLOOR SILL CORRODED AT FRAME 47. REMOVED AND REPLACED FLOOR SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 18,731 hrs · 10,030 cycles

TYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS AND INSPECTION FOUND THE RT FLOOR SILL FROM FR 53 TO FR 59 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RETURNED TO SERVICE AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,731 hrs · 10,030 cycles

TYS - AIRCRAFT IN C-CHECK STATUS AND INSPECTION FOUND THE LT FLOOR SILL AT FR 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: WARNING SYSTEM — MALFUNCTIONED (WINDOW HEAT) · airframe 18,580 hrs · 9,943 cycles

TYS - AIRCRAFT EN ROUTE FROM IAH TO ORF WHEN THE WINDSHIELD HEAT FAIL. AIRCRAFT DIVERTED TO BNA AND SWAPPED AIRCRAFT TO 192. MAINTENANCE COULDN'T DUPLICATE PROBLEM ON GROUND WHEN PRESSURIZED. PLACED ON MEL. MEL 2473864.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 18,576 hrs · 9,941 cycles

THE CREW REPORTED A WINDSHIELD HEAT FAIL MESSAGE ON EICAS. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX PLACEDTHE WINDSHIELD HEAT ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 06/05/09 MX REMOVED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER, OPS TESTED WITH NO DEFECTS, CLEARED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (ZONE 400) · airframe 17,359 hrs · 9,276 cycles

IAH - FLIGHT 2160, THE FLIGHT ATTENDANT REPORTED THAT A HAZE DEVELOPED IN THE CABIN FOLLOWED BY A MOMENTARY LAV SMOKE INDICATION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE NR 2 ENGINE, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — DEFECTIVE (LAVATORY) · airframe 17,305 hrs · 9,247 cycles

FLIGHT 2966 - EWR - FLIGHT CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS DURING CLIMBING WITH A SLIGHT SMELL OF SMOKE. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 16,508 hrs · 8,805 cycles

FLIGHT 1228 EWR FLIGHT CREW REPORTED ACFT NO PRESSURIZING IN CLIMBING. AIR CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX R&R DIGITAL PRESSURIZATION CONTROLLER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,117 hrs · 8,086 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT SIGN NOT ILLUMINATING AT SEAT 3BC. MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 7,512 hrs · 13,972 cycles

SAH - DURING C-CHECK CARGO DOOR CUTOUT LOWER THRESHOLD HAS MULTIPLES AREAS OF CORROSION AT FR 64-67. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER THRESHOLD AT FR 64-67 IAW EMB 145 SRM 51-40-02 AND REMOVED AND REPLACED NUT PLATES IAW EMB 145 EC 5320-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CLIP — CORRODED (FUSELAGE) · airframe 9,139 hrs · 4,922 cycles

SHV - DURING C CHECK, THE SHEAR CLIPS ON FRAME 68 AND CARGO SILL SHEAR CLIPS WERE FOUND TO BE CORRODED WITH CORROSION ALL THE WAY THRU IN SOME SPOTS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLIP — CORRODED (FUSELAGE) · airframe 9,139 hrs · 4,922 cycles

SHV - DURING C CHECK, THE CARGO SILL PLATE SIDE SHEAR CLIPS WERE FOUND TO BE CORRODED WITH CORROSION ALL THE WAY THRU IN SOME SPOTS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,139 hrs · 4,922 cycles

SHV - DURING C CHECK, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AROUND THE COMPOSITE CROSS BEAM AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, SECTION 1, FIG 201, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,139 hrs · 4,922 cycles

SHV - DURING C CHECK, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 TO 29. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 201, PG 208, REPAIR NR 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLIP — CORRODED (FUSELAGE) · airframe 9,139 hrs · 4,922 cycles

SHV - DURING C CHECK, THE SHEAR CLIPS ON FRAME 65 AND CARGO SILL SHEAR CLIPS WERE FOUND TO BE CORRODED WITH CORROSION ALL THE WAY THRU IN SOME SPOTS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,907 hrs · 4,805 cycles

IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,801 hrs · 3,665 cycles

DURING ROUTINE MAINTENANCE, THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS INTERMITTENT. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 5,384 hrs · 2,899 cycles

RIC - MX, DURING PRE FLIGHT CHECK, MAINTENANCE FOUND EXTERNAL LT FWD EMERGENCY LIGHT INOP. MAINTENANCE MELED AIRCRAFT. AIRCRAFT WAS RELEASED IAW MEL PROCEDURE 33-50-00/1 CAT "C" CONTROL NR 051445. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. IAH-MX, HOUSTON MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 5,156 hrs · 2,774 cycles

IAH - FLIGHT 3272, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY AFTER LANDING ACCOMPANIED BY EMERGENCY LIGHT NOT ARMED EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,165 hrs · 2,774 cycles

CREW REPORTED EMERGENCY EXIT LIGHTS CAME ON AFTER LANDING WITH AN EMERGENCY LIGHT NOT ARMED WARNING. REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL.

Part: ENGINE — FAILED (NR 2)

CMH FLIGHT NR 2699 THE CREW REPORTED THE NR 2 ENGINE EXCEEDED 950 DEGREES ON CLIMBOUT. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: POTENTIOMETER — ERRATIC (NLG STEERING)

UPON LANDING THE NOSE WHEEL STEERING SYSTEM FAILED CAUSING THE AIRCRAFT TO DEPART THE RUNWAY. THE AIRCRAFT WAS INSPECTED AND DAMAGE WAS NOT FOUND TO THE LANDING GEAR OR AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STEERING POTENTIOMETER, OPERATIONALLY TESTED THE STEERING SYSTEM, AND RETURNED THE AIRCRAFT TO SERVICE.

Part: SOLENOID VALVE — FAULTY (NLG DOOR)

IAH FLIGHT NR 7631, THE CREW REPORTED THE NOSE GEAR DOOR WAS STUCK OPEN AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD.