N11184

Part: BATTERY — FAULTED (ZONE 200) · airframe 42,653 hrs · 28,468 cycles

MULTIPLE EMERGENCY LIGHTS OUT, SUSPECT BATTERY 2 TO BE BAD. FOUND #2 EMERGENCY LIGHT BATTERY DISCONNECTED. RECONNECTED BATTERY. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 42,576 hrs · 28,376 cycles

CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT HOUSING. OPS CHECK SAT.

Part: BATTERY — INOPERATIVE (UNKNOWN) · airframe 41,375 hrs · 27,265 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED MCD EMERGENCY LIGHT ASSEMBLY & BULB. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NO 1. LIGHT OPS CHECK FAIL. FOUND BROKEN WIRE AT MCD HINGE POINT. REPAIRED WIRING. LIGHT OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,205 hrs · 27,100 cycles

EMERGENCY EXIT HANDLE UNSECURED RIGHT SIDE. RESECURED RIGHT SIDE EMERGENCY EXIT HANDLE COVER ON DOOR

Part: AMPLIFIER — EXTINGUISHED (UNKNOWN) · airframe 41,051 hrs · 26,953 cycles

CABIN AND CAB EMERGENCY LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED PA AMPLIFIER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 40,875 hrs · 26,792 cycles

18CD PSU EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED 18CD OVERWING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 40,320 hrs · 26,288 cycles

EMERGENCY LIGHT BATTERY #1 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #1. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,285 hrs · 26,256 cycles

RF1, CORROSION FOUND ON SKIN U/FLOOR RAD ALT #2 AFT INNER DOUBLER BTW FR 68-69 AND BTW STR 21L-21R. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

CF 1 EXT, MULTIPLE DENTS FOUND ON LH SIDE SKIN BTW FR 18-21 AND BTW STR 11L-13L. SKIN REPAIRED WITH 2 DOUBLERS, DOUBLER 1 LOCATED BTW FR 19-21 AND BTW STR 11L-13L AND DOUBLER 2 LOCATED BTW FR 21-23 AND BTW STR 11L-13L.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

DENT ON RUDDER 1 LEADING EDGE SKIN BTW RIB ZV 2601.0 AND ZV 2890.0. DENT REDRESSED ON LH RUDDER 1, ON LE SKIN BTW ZIB ZV2601-ZV2890

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

CF2, CRACKS (4X) FOUND ON LH OMEGA BEAM #3 FLOOR STRUCTURE BTW FR 29-36. 3 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM, ON INBD FLANGE AT FR 31,32,33, & 34

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

CF3, CRACKS (2X) FOUND ON LH OMEGA BEAM #4 FLOOR STRUCTURE BTW FR 35-39. 2 REPAIR DOUBLERS ON LH CENTER FUSE 3 OMEGA BEAM, ON INBD FLANGE AT FR 36 & 37

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

REPAIR DOUBLER TO REWORK ON LH CENTER FUSE 1 SKIN, BTW FR 19-20 AND BTW STR 13L-14L. REPAIR DOUBLER ON LH CENTER FUSE 1 SKIN, BTW 19-20 AND BTW STL 13L-14L REWORKED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,285 hrs · 26,256 cycles

CORROSION ON REAR FUSE 2 LOWER SKIN, BTW FR 80-81 AND BTW STR 19L-21L. REPAIR DOUBLER ON REAR FUSE 2 LOWER SKIN, BTW FR 80-81 AND BTW STR 18L-21L

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

AT REAR FUSE EXT, HINGE FOUND CRACKED ON RH PNEUMATIC ACCESS DOOR BTW FR 70-71 AND BTW STR 19R-21R. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,285 hrs · 26,256 cycles

CRACK FOUND ON LOWER SECTION FWD SIDE FRAME CARGO DOOR ASSY. CARGO DOOR LOWER SECTION FWD SIDE FRAME REPAIRED WITH L-SHAPED ANGLE (CORROSION LEVEL 2)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,285 hrs · 26,256 cycles

CF4, CORROSION FOUND ON RH GUSSET IN TOILET AREA BTW FR 59-61. RH OMEGA BEAM REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

RH ELEVATOR, LOWER SKIN FOUND CRACKED AT RIB YH 1310.0. RH ELEVATOR, CRACKED LOWER SKIN AT RIB YH 1310.0 REPAIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,285 hrs · 26,256 cycles

REPAIR DOUBLER TO REWORK ON LH REAR FUSE 1 SKIN, BTW FR 62-63 AND BTW STR 16L-18L. LH REAR FUSE 1, SKIN, BTW FR 62-63 AND BTW STR 16L-18L REPAIR DOUBLER REWORKED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,285 hrs · 26,256 cycles

RF1, UPPER BEAM OF CARGO DOOR SURROUND STRUCTURE BTW FR 65-68 FOUND CORRODED. RF1, UPPER BEAM OF CARGO DOOR SURROUND STRUCTURE BTW FR 65-68 REPAIRED

Part: LIGHT — INOPERATIVE · airframe 39,430 hrs · 25,495 cycles

EMERGENCY LIGHT STRIP ROW 10-11 MISSING. RESECURED EMERGENCY LIGHT STRIP

Part: NONE — NONE · airframe 38,203 hrs · 24,398 cycles

BLEED 1 OVERTEMP DURING CLIMB IN ICING. FAN AIR VALVE DEFECTIVE. LEFT SIDE FAN AIR VALVE REMOVED. RIGHT SIDE FAN AIR VALVE REMOVED AND INSTALLED IN LEFT POSITION. VALVE FUNCTIONING AS IT SHOULD. VALVE THAT WAS INSTALLED FOR T/S, REMOVED AND REINSTALLED IN RIGHT POSITION

Part: STIFFENER — CORRODED (FR.65) · airframe 36,692 hrs · 23,152 cycles

TYS A/C IS IIN FOR A C-CHECK WHEN INSPECTION FOUND A CORRODED NUT PLATE AT FRAME 65. MAINTENANCE REPAIRED THE NUTPLATE AT FRAME 65 IAW ECTC ETD 2019 145-132803. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,692 hrs · 23,152 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE L/H OMEGA BEAM CENTER ISLE FLOOR BOARD SUPPORT CORRODED AT FRAME 45 THRU 52. MAINTENANCE REMOVED AND REPLACED THE L/H OMEGA BEAM IAW EMB 145 SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,381 hrs · 22,909 cycles

DURING MX INSPECTION SEAT 18A CEILING EMERGENCY LIGHT FOUND INOP. MX R&R CEILING EMERGENCY LIGHT BULB WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 36,539 hrs · 22,288 cycles

IAH - FLIGHT 4196 THE CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING

THE CREW REPORTED WHEN ANTI-ICE SYSTEM WAS SELECTED AND HIGH PSI VALVE OPENED A TOXIC ODOR CAME THROUGH THE ENVIRONMENTAL CONTROL SYSTEM AND REMAINED FOR OVER 30 MINUTES. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,962 hrs · 19,084 cycles

DURING C-CK. RT FUSELAGE SKIN IS CRACKED AT RIVET AT FR 79. REPAIRED FUSELAGE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 25,869 hrs · 15,453 cycles

THE CREW REPORTED SMOKE IN THE CABIN AND COCKPIT DURING CRUISE. ISOLATED BLEED NR 1 AND SMOKE CLEARED. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,816 hrs · 15,415 cycles

DURING SCHEDULED MX INSPECTION, THE CABIN AFT OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MX R & R THE OVERHEAD EMERGENCY EXIT SIGN AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,816 hrs · 15,415 cycles

DURING SCHEDULED MX INSPECTION THE LT LOWER EMERGENCY EXIT SIGN NEAR PASSENGER ESCAPE HATCH WOULD NOT ILLUMINATE. MX R & R THE LT EMERGENCY EXIT SIGN WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROFILE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 25,028 hrs · 14,891 cycles

DURING C-CHECK, THE PAX DOOR BOTTOM PROFILE, FRAME, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-013707. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 25,028 hrs · 14,891 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 18. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01938. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 25,028 hrs · 14,891 cycles

DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,597 hrs · 11,959 cycles

DURING MX INSPECTION THE AFT FACING CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX R & R THE AFT FACING CEILING EMERGENCY LIGHT WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 19,532 hrs · 11,325 cycles

NR 1 ENGINE FWD LOWER MOUNT BRACKET IS CRACKED. R & R BRACKET.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 19,243 hrs · 11,040 cycles

MX REPORTED THE FORWARD CEILING EMERGENCY EXIT MARKER WAS INOPERATIVE. MX REPLACED THE NR 6 AC/DC EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 16,282 hrs · 9,053 cycles

FLIGHT 3084 - LGA - FLIGHT CREW REPORTED AUTO PRESS FAIL MSG ON EICAS. EWR MX REMOVED AND REPLACED DIGITAL PRESSURE CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 14,883 hrs · 8,266 cycles

FLIGHT 3145 - RIC - DURING ROUTINE MAINTENANCE, MX FOUND ROW 12A EMERGENCY EXIT LIGHT INOPERATIVE. MX RE-SECURED ELECTRICAL CONNECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,883 hrs · 8,266 cycles

FLIGHT 3145 - RIC - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 7. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (FIRE DETECTION) · airframe 12,682 hrs · 7,076 cycles

FLIGHT 2352 - EWR - FLIGHT CREW REPORTED BAGG FIRE DETECT LIGHT WOULD NOT ILLUMINATE DURING TEST. EWR MX REMOVED AND REPLACED RELAY K0629 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TUBE — LOOSE (APU) · airframe 10,142 hrs · 5,722 cycles

FLIGHT 2590, A STRONG GAS SMELL WAS NOTED WITH THE ENGINE OFF AND APU RUNNING AT THE GATE. MX INSPECTED THE APU, FOUND A LOOSE B-NUT ON THE TUBE ASSY FROM FUEL CONTROL TO FUEL FLOW SENSOR, THE B-NUT WAS TIGHTENED, OPS AND LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 10,064 hrs · 5,683 cycles

FLIGHT 1200 - EWR - FLIGHT CREW REPORTED "SPS ADVANCE" ON EICAS WITH FLAP LOW SPEED CAUTION ON APPROACH AS FLAPS 9 DEGREES SELECTED. CREW DECLARED EMERGENCY AND LANDED ACFT WITHOUT INCIDENT. EWR MX PERFORMED FLAP SYSTEM RESET AND PERFORMED OPS CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK SHEAR CLIP AT FR 65 CARGO DOOR CUT OUT HAS CORROSION. MX REPAIRED FRAME 65 CARGO DOOR CUTOUT LOWER CORNER SHEAR CLIP IAW EC5330-01458. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K)

Part: DOOR FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, BAGGAGE DOOR CUTOUT LOWER BEAM CORRODED IN VARIOUS AREAS MARKED. MX REMOVED AND REPLACED BAGGAGE DOOR LOWER FLOORBEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K)

Part: SIGN — INOPERATIVE (CABIN)

FLT MX - ONT - WHILE PERFORMING 3A CHECK INSPECTION ON EXIT SIGN ON ROW NR12 IT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT SIGN. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: SIGN — BURNED OUT (EMERGENCY LIGHTS)

FLT MAINTENANCE - ONT - WHILE PERFORMING 3A CHECK INSPECTION ON EXIT SIGN ON ROW NR 1 IT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY AND LIGHT SIGN. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 7,536 hrs · 4,154 cycles

FLT 7672 - SLC TO SLC - FLIGHT CREW REPORTED SMOKE IN CABIN AND COCKPIT. MX PERSONNEL PERFORMED OPERATIONAL CHECK OF THE ENGINE TO DUPLICATED, BUT COULD NEVER DUPLICATE FAULT AGAIN. SUSPECTED DEICING FLUID. A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,635 hrs · 2,474 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145XR SRM 53-00-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,635 hrs · 2,462 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02 AND EMB 145XR CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.