N12567

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,898 hrs · 29 cycles

INSPECTION FOUND A BROKEN WIRE ON THE EMERGENCY LIGHT STRIP. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 37,898 hrs · 29,467 cycles

FOUND THE RT HORIZONTAL STAB LEADING EDGE DAMAGE AT THE LOWER SIDE SCREW HOLES. MAINTENANCE REPAIRED THE LOWER HORIZONTAL STAB LEADING EDGE IAW ETD 2018-145-037750.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 37,897 hrs · 29,467 cycles

RIGHT HORIZONTAL STAB LEADING EDGE HAS DAMAGE AT THE SCREW HOLES ON LOWER SIDE. CONTOURED THE AREA BY COLD FORMING. INSTALLED DIMPLED WASHER IAW ETD2018-145-037750.

Part: DOOR FRAME — CORRODED · airframe 37,897 hrs · 29,467 cycles

DOOR FRAME HAS CORROSION ON AFT LOWEST DOOR STOP ON SERVICE DOOR. REMOVED DAMAGED SECTION OF THE DOOR FRAME 22. DRILLED AND FABRICATED A DOUBLER SECTION OF THE FRAME AND INSTALLED.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,897 hrs · 29,467 cycles

CRACKED SKIN AT FRAME 75. CUT OUT A 2 X 2 INCH SECTION OF THE SKIN AND INSTALLED FILLER AND DOUBLER.

Part: YOKE — CRACKED (NR 1 ENGINE) · airframe 37,897 hrs · 29,467 cycles

#1 ENGINE PYLON LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED FORWARD YOKE. AIRCRAFT STILL IN C CHECK.

Part: CONTROL UNIT — FAULTY (BRAKE SYS) · airframe 39,525 hrs · 32,487 cycles

PILOT REPORTED RIGHT BRAKE PEDAL WHEN COMMANDED RESULTS IN ALMOST NO BRAKING ACTION. ADDITIONALLY THE RIGHT IB BRAKE TEMP ALWAYS STAYED AT ZERO DESPITE THE RIGHT OB BRAKE TEMP GOING INTO THE AMBER INDICATION AFTER MODERATE BRAKING. MX REMOVED AND REPLACED BRAKE CONTROL UNIT WITH OPS CHECK GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,043 hrs · 27,233 cycles

CREW REPORTED MOST AFT CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — ODOR (CABIN LIGHTS) · airframe 33,781 hrs · 26,243 cycles

HEAVY ELECTRICAL SMOKE ODOR REPORTED FROM MAIN CABIN DOOR AREA SPREAD TO THE GALLEY. R & R CABIN LIGHT CONTROL MODULE WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,631 hrs · 24,499 cycles

DURING MAINTENANCE INSPECTION, THE LT FWD FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER AND REPAIRED WIRE NR W192-8593-20 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 31,381 hrs · 24,308 cycles

DURING ROUTINE MAINTENANCE THE LT FWD EXTERNAL EMERGENCY LIGHT AND AISLE CEILING LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,825 hrs · 23,872 cycles

DURING A-CK INSPECTION, THE LT WING FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 26,962 hrs · 20,870 cycles

ACFT LT AND RT HORIZONTAL STABILIZER SPHERICAL BEARINGS HAD PLAY IN THE HOUSING. MX REAMED BOTH HOUSINGS AND REPAIRED AND INSTALLED SPHERICAL BEARINGS IAW SRM 55-30-02. COMPLIED WITH BACKLASHES IAW AMM 27-40-00; ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE, ALL CHECKS WERE GOOD. REF TASK CARD 6855001.

Part: TRANSDUCER — FAULTY (BRAKES) · airframe 26,728 hrs · 20,689 cycles

PILOT REPORTED DURING BRAKE APPLICATION (RT ONLY) CLUNKING NOISE COMES FROM FWD OF COCKPIT UNTIL HARD BRAKE APPLICATION. BRAKING ACTION REDUCED UNTIL HARD APPLICATION. MX R & R NR 3 WHEEL SPEED TRANDUCER AND HARNESS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,168 hrs · 20,263 cycles

DURING MX INSPECTION THE EMERGENCY LIGHT PROXIMITY STRIP BETWEEN ROW 4 AND 7 WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — DISCONNECTED (CABIN AIR) · airframe 24,853 hrs · 19,204 cycles

THE CREW REPORTED ODOR OF SMOKE AT SEATS 6-7. MX INSPECTED AND FOUND DUCT AT NR 2 RECIRCULATION FAN OFF UNDER FLOOR. MX REINSTALLED DUCT AT NR 2 RECIRCULATION FAN AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,428 hrs · 18,849 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO OFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 EMERGENCY LIGHT BATTERY PACKS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,428 hrs · 18,849 cycles

DURING PREFLIGHT INSP THE CREW REPORTED TAHT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO IFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 EMERGENCY LIGHT BATTERY PACKS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED · airframe 23,820 hrs · 18,344 cycles

CORROSION ON REPAIR DOUBLER RT SILL FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED, PAINTED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 23,820 hrs · 18,334 cycles

SHEAR CLIP FOUND CRACKED AT FRAME 61 BETWEEN STR 6L AND 7L. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE CENTER) · airframe 23,820 hrs · 18,334 cycles

THE RT OTBD OMEGA BEAM SUPPORT WAS FOUND CRACKED AT FRAME 47 TO 48. MX R & R THE SUPPORT IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 23,820 hrs · 18,334 cycles

CORROSION WAS FOUND IN THE ISLE AT FRAME 20 CROSS-MEMBER THAT WAS BLENDED OUT OF LIMITS. MX R & R THE CROSS-MEMBER IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CANNING (CARGO DOOR) · airframe 23,820 hrs · 18,334 cycles

DENT ON THE CARGO DOOR. MX RECONTOURED DENT, SKIN HAD A OIL CAN, SO THEY CUT OUT DAMAGE, FABRICATED A FILLER AND DOUBLER, THEN INSTALL FILLER AND DOUBLER IAW SRM 53-20-01 AND ETD 2011-145-102644. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,820 hrs · 18,334 cycles

THE LEFT OTBD SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS AT FRAME 50. MX R & R THE SUPPORT AT FRAME 50 IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 23,820 hrs · 18,334 cycles

SHEAR CLIP CRACKED AT FRAME 80 AT THE APU FIRE BOTTLE. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BRACKET — CORRODED · airframe 23,820 hrs · 18,334 cycles

CORROSION ON BRACKET AT PAX DOOR ENTRANCE BELOW FLOOR. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,820 hrs · 18,334 cycles

CORROSION IN GUSSET CENTER OMEGA BEAM FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 20,823 hrs · 15,937 cycles

ICT FLT 6056 THE CREW REPORTED A LAV SMOKE EICAS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED LAV SMOKE SYSTEM OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,373 hrs · 14,810 cycles

SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 78-79 AND STRINGERS 2-10R. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC 5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,373 hrs · 14,810 cycles

SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R (RIGHT BELOW THE RT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,373 hrs · 14,810 cycles

SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L (RIGHT BELOW THE LT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,373 hrs · 14,810 cycles

SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2-10L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (BATTERY) · airframe 18,352 hrs · 14,058 cycles

TYS - A/C IN FOR A 3A CHECK WHEN INSPECTION FOUND THE LT FWD OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FUSE IN BATTERY TRAY 1. OPS CHECK GOOD IAW EMB 135/145 VCMM 33-21-20 AND EMB 145 AMM 33-50-00. RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,132 hrs · 13,895 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 18,100 hrs · 13,874 cycles

IAH - FLIGHT 2263, THE CREW REPORTED AN ALTITUDE AND IAS ERROR WITH A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE DRAINED THE WATER FROM THE PITOT STATIC SYSTEM. INSPECTED THE COCKPIT, CURRENT RELAY SENSORS WITH NO DEFECTS NOTED, OPERATIONAL CHECKS WERE COMPLETED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 16,081 hrs · 12,367 cycles

LCH - DURING MAINTENANCE INSPECTION THE COCKPIT CEILING AND NR 1 AISLE PATH, CEILING, AND WING TO FUSELAGE FRONT FAIRING LEFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 16,033 hrs · 12,327 cycles

AIRCRAFT HAD TWO DENTS BETWEEN FRM 20/21 AND STR14L/16L. REPAIRED DENTED AREA BY FABRICATING L-ANGLE IAW IC2009-145/01434A. RE-CONTOURED SKIN, PERFORMED NDT, INSTALLED L-ANGLE AND RESTORED ORIGINAL FINISH IAW IC 2009-145/01434A. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 15,876 hrs · 12,217 cycles

ACFT WAS FOUND WITH THE AFT CEILING EMERGENCY LIGHT INOP. MX R&R THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW AMM 145 33-50-04. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (SMOKE DETECTOR) · airframe 14,138 hrs · 10,998 cycles

FLIGHT 2648 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT WOULD NOT ILLUMINATED ON TEST. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INTERMITTENT (NLG) · airframe 13,566 hrs · 10,593 cycles

FLIGHT 2761 - EWR - CREW REPORTED THAT AFTER ROTATION, LDG/AIR GRD FAIL MESSAGE AND REV DISAGREE MESSAGE APPEARED ON EICAS. MESSAGES CLEARED UPON GEAR EXTENSION NEAR EWR. EWR MX REMOVED AND REPLACED NLG AIR/GRD PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 12,984 hrs · 10,179 cycles

FLT 2490 - EWR - CREW REPORTED THAT LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. CREW PROCEEDED WITH AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,172 hrs · 8,855 cycles

MCI - DURING MAINTENANCE INSPECTION AISLE PATH LIGHTS 6, 7 & 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — LOOSE (EMERGENCY LIGHT) · airframe 10,422 hrs · 8,269 cycles

BTV 2A CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP BASE IAW EMB145 AMM 33-50-10. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 9,437 hrs · 7,501 cycles

IAH - FLIGHT 3225, DURING PREFLIGHT INSPECTION, THE CREW REPORTED EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE RECHARGED THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,240 hrs · 7,356 cycles

STL - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHT STRIPS 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 8,807 hrs · 7,014 cycles

SHV - DURING C-CHECK THE FUSELAGE SKIN AT FRAME 7 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,807 hrs · 7,014 cycles

SHV - DURING C-CHECK THE AFT LOWER SERVICE DOOR CUTOUT FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTACTOR — FAILED (APU LINE) · airframe 5,365 hrs · 4,314 cycles

CREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CONTACTOR. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,134 hrs · 3,363 cycles

DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC-2004145/2152. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,134 hrs · 3,363 cycles

DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED AT THE CARBON SUPPORT. MAINTENANCE REPAIRED THE LT FLOORBEAM, ALODINED AND PAINTED IAW EMB 135/145 SRM 53-21-10; AND CPM 51-21-04; 05; 06 ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 4,134 hrs · 3,363 cycles

DURING A SCHEDULED 1C INSPECTION THE AFT GALLEY STEP-UP WAS FOUND CORRODED. MAINTENANCE REMOVED THE AFT GALLEY STEP-UP. NEW STEP-UP, ALODINED, PRIMED, PAINTED AND INSTALL IAW EMB 135/145 SRM 51-40-03; 51-21-03; 04; 05 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY LIGHTS IN ROW NR 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW EMB145 33-50-04.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED, FIRST TWO SETS OF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04.

Part: BATTERY PACK — DISCHARGED (CABIN)

EWR---CO 2342, DURING PREFLIGHT CREW REPORTED THAE THE EMERGENCY PATH LIGHTING FORWARD STRIP STRIP WAS INOPERATIVE, MAINTENANACE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. IAW EMB145AMM 33-50-04.

Part: BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE DURING TEST. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

IAH- DURING SERVICE CHECK THE MECHNIC NOTED THAT THE GALLEY EMERGENCY EXIT LIGHT WOULDN'T ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLEVELAND FLIGHT 2357 THE CREW REPORTED THE EMERGENCY LIGHT ABOVE THE PASSENGER ENTRY DOOR WAS INOPERATIVE.MAINTENANCE RESECURED THE CONNECTOR AT THE INVERTER OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN)

CLE FLT NR 2004 THE CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY DOOR NOT ILLUMATING. MAINTENANCE REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 2,435 hrs · 1,996 cycles

EWR, GALLEY EMERGENCY LIGHT WILL NOT COME ON. ADJUSTED GALLEY EMERGENCY LIGHT CONNECTION. PERFORMED OPERATIONAL CHECK. OPS CHECK GOOD IAW EMB145 MM 33-50-00.