N14562

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,098 hrs · 30,995 cycles

DURING MX INSPECTION THE #3 EMERGENCY LIGHT BATTERY PACK WILL NOT ILLUMINATE LIGHTS. MX R&R #3 EMERGENCY LIGHT BATTERY WITH OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,098 hrs · 30,995 cycles

DURING MX INSPECTION THE #1 EMERGENCY LIGHT BATTERY PACK WILL NOT ILLUMINATE LIGHTS. MX R&R #1 EMERGENCY LIGHT BATTERY WITH OPERATIONAL CHECK GOOD.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 38,566 hrs · 30,562 cycles

IAH - FLIGHT 4309 MX REPORTED THAT THE EMERGENCY LIGHT CEILING PANEL AISLE LIGHT #2 ND R/H FWD EXTERIOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 37,481 hrs · 29,667 cycles

DURING C CHECK INSPECTION A CRACK WAS FOUND ON CARGO DOOR SKIN AT HANDLE HOUSING CUT-OUT. MAINTENANCE REPAIRED CRACK IAW 52-30-01.

Part: FLAP — DELAMINATED (RT WING) · airframe 37,481 hrs · 29,667 cycles

CORRECTION: RIGHT INBOARD FLAP DELAMINATED. MAINTENANCE REPAIRED INBOARD FLAP IAW SRM 51-72-09. ITEM 3 TYPE B ROOM TEMPERATURE REPAIR.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 37,481 hrs · 29,667 cycles

RIGHT INBOARD FLAP FAIRING INBOARD SUPPORT CORRODED. MAINTENANCE REPAIRED INBOARD FLAP SUPPORT IAW SRM 51-70-06. ITEM 3 REPAIR OF EXPANDED COPPER FOIL.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,481 hrs · 29,667 cycles

RIGHT INBOARD FLAP LOWER SURFACE DELAMINATED. MAINTENANCE REPAIRED RIGHT INBOARD FLAP SURFACE I/A/W SRM 51-72-09.ITEM 3 REPAIR OF EXPANDED COPPER FOIL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,311 hrs · 27,947 cycles

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

Part: SOCKET — BURNED (CEILING LIGHT) · airframe 35,201 hrs · 27,860 cycles

STRONG ELECTRICAL BURNING ODOR IN THE CABIN. FOUND A SOCKET FOR A LIGHT AT A4 BURNED. REMOVED AND REPLACED THE CEILING LIGHT ASSY. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 21,420 hrs · 24,841 cycles

THE CREW REPORTED A BURNING ODOR NEAR ROWS 2 & 3, AND WERE UNABLE TO TURN THE CABIN LIGHTS OFF. THE ACFT WAS FERRIED WHERE MAINTENANCE INSPECTED THE ACFT. R & R THE CABIN LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DFECTS OR OTHER DISCREPANCIES NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — BURNED OUT (COCKPIT) · airframe 29,975 hrs · 23,695 cycles

PILOT REPORTED F/O'S PFD BLANK AND ELECTRIC ODOR PRESENT WITH POWER ON ACFT. ITEM INTIALLY PLACED ON MEL. MAINTENANCE R & R NR 4 PFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, RT FUSELAGE SKIN AT FRAME 75 STRINGER 1R-2R CRACKED AT RIVET HOLE VERIFIED WITH EDDY CURRENT. REPAIRED THE SKIN IAW EC5330-02976. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, FRAME 10 CRACKED JUST UNDER LT DV WINDOW. R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, FRAME 65 HAS CORROSION AT LOWER CARGI DOOR GUIDE. MAINTENANCE REPAIRED THE FRAME BETWEEN STRINGERS 15-16L IAW EC5330-02975. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, RT EMERGENCY EXIT DOOR FOUND CORRODED ON LOWER STRUCTURE. REPAIRED THE EMERGENCY EXIT LOWER FRAME IAW EC5220-01063. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, CARGO DOOR CUTOUT LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R THE CUTOUT LOWER BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, LT FUSELAGE SKIN AT FRAME 75 AT STRINGER 1L-2L CRACKED, VERIFIED WITH EDDY CURRENT. REPAIR THE SKIN IAW EC5330-02976. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAMES 37-38) · corrosion level 2 · airframe 28,126 hrs · 22,244 cycles

FUSELAGE SKIN FOUND CORRODED FRAMES 37-38, STRINGER 21L-21R. REPAIRED THE SKIN IAW SRM 53-23-01.. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAMES 38-39) · corrosion level 2 · airframe 28,126 hrs · 22,244 cycles

DURING C-CHECK, INNER SKIN FOUND CORRODED FRAMES 38-39, STRINGER 21L-21R. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-23-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · airframe 28,126 hrs · 22,244 cycles

SERVICE DOOR CENTER SILL CORRODED. R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — ODOR (CABIN) · airframe 27,920 hrs · 22,077 cycles

THE CREW REPORTED AN ELECTRICAL ODOR IN THE FORWARD CABIN. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. R & R THE NR 2 EXHAUST FAN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 27,468 hrs · 21,728 cycles

THE CREW REPORTED A SMOKE INDICATION IN THE CARGO AREA. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED BOTH CARGO SMOKE DETECTORS. OPS CHECKED GOOD.

Part: FIRE LOOP — FAILED (NR 1 PYLON) · airframe 27,207 hrs · 21,516 cycles

THE CREW REPORTED NR 1 ENGINE FIRE DETECTOR FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE PYLON FIRE LOOP. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FRAMES 20-22) · airframe 26,021 hrs · 20,599 cycles

TWO DENTS AND A CREASE WERE FOUND ON THE LT FUSELAGE BETWEEN FRAME 20 AND 22. MAINTENANCE RECONTOURED DENTS FROM FRAME 20 THRU FRAME 22. INSTALL A FILLER AND DOUBLER ON THE CREASE AREA. PERFORMED A NDT AND NO CRACKS WERE NOTED. WORK WAS DONE IAW ETD 2014-145-023920. ALL WORK ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL STORAGE) · airframe 23,866 hrs · 18,950 cycles

THE CREW REPORTED A FUEL LEAK FROM THE RIGHT WING. MX INSPECTED AND REPLACED THE RT WING FLAP VALVE. OPS CHECKED GOOD.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 23,240 hrs · 18,473 cycles

ACFT IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE NR 1 ENGINE LOWER YOKE FWD KNUCKLE CRACKED. MX R & R THE FWD LOWER YOKE IAW EC 5450-01028, REV A. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF ALL CHECKS.

Part: BRACKET — WORN (RT AILERON) · airframe 23,238 hrs · 18,472 cycles

RT AILERON MOST OTBD PCA ATTACHMENT POINT HAS NO INTERFERANCE FIT BETWEEN HAT BUSHING AND HOLE. R & R AILERON PCA BRACKET.

Part: SKIN — GOUGED (FUSELAGE) · airframe 22,207 hrs · 17,666 cycles

TWO GOUGES AFT OF MAIN CABIN DOOR. CUT OUT DAMAGED SKIN, FABRICATED, PRIMED, PAINTED AND INSTALLED PATCH. LEAK CHECKED GOOD.

Part: SHUTTLE VALVE — LEAKING (BRAKES) · airframe 21,817 hrs · 17,347 cycles

THE CREW REPORTED THE NR 1 HYDRAULIC SYS WENT INTO THE AMBER RANGE IN FLIGHT. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 BRAKE SHUTTLE VALVE AND THE NR 4 BRAKE ASSY. OPS CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE.

Part: FIRE LOOP — FAULTY (ZONE 400) · airframe 19,585 hrs · 15,647 cycles

FLT 4401, REPORTED E2 FIRE DET FAIL MESSAGE ON EICAS. MX REMOVED AND REPLACED NR 2 ENGINE FIRE DETECTION LOOP IAW AMM 26-11-01 WITH OPS CHECKED SUCCESSFUL. ACFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 18,364 hrs · 14,626 cycles

FLIGHT 3073 - FLIGHT CREW REPORTED ELECTRICAL BURNING SMELL IN COCKPIT. EWR MX REMOVED AND REPLACED NR 2 W/S HEAT CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AILERON) · airframe 18,340 hrs · 14,605 cycles

TYS - A/C WAS ON APPROACH WHEN THE CREW REPORTED THAT THE AILERONS FELT HEAVY. MAINTENANCE PERFORMED A DVI ON FORWARD AILERON QUADRANTS AT BOTH LEFT AND RIGHT PCA'S IAW EMB 145AMM-57-11-00. NO DEFECTS NOTED AND WAS RELEASED.

Part: FITTING — WORN (AILERON) · airframe 18,240 hrs · 14,533 cycles

LT AILERON PCA OUTBOARD FITTING OUTBOARD HAT BUSHING FITTING DAMAGE (ELONGATED). REMOVED AND REPLACED PCA FITTING IAW EC5750-01177.

Part: FRAME — CRACKED (FUSELAGE) · airframe 18,235 hrs · 14,258 cycles

RT FRAME 10 IS CRACKED AT DV WINDOW. REMOVED AND REPLACED FRAME 10 IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,863 hrs · 14,218 cycles

ORD FLT 6023 - THE CREW REPORTED AN ELECTRICAL BURNING SMELL FROM THE CLOSET AREA WHILE SITTING AT THE GATE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE OR SMELL ANY ELECTRICAL BURNING SMELL. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 17,509 hrs · 13,923 cycles

THE CREW REPORTED NR 2 ENGINE HAD A SLIGHT FUEL SMELL. MAINTENANCE INSPECTED AND RAN NR 2 ENGINE. NO FUEL ODORS OR LEAKS WERE NOTED.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 17,426 hrs · 13,846 cycles

ORD FLT 5991 - THE CREW REPORTED THE EMERGENCY FLASHLIGHT BEHIND THE CAPTAIN SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BULB. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERHEATED (NR 2) · airframe 16,173 hrs · 12,670 cycles

BHM FLT 6992 THE CREW REPORTED A BATTERY 2 OVERTEMP INDICATION. AIRCRAFT WAS DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BATTERY AND OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 16,092 hrs · 12,591 cycles

IND FLT 5686 THE CREW REPORTED A LOSS OF CABIN PRESSURIZATION INDICATIONS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 15,739 hrs · 12,254 cycles

PRESSURIZATION CABIN RATE ERRATIC FROM 10000FT TO SURFACE AUTO MODE PRESSURIZING BELOW FIELD ELEVATION AND MANUAL PRESSURIZATION MODE INOP. REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW EMB 145AMM 21-31-04, OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,648 hrs · 12,167 cycles

DURING ROUTINE MAINTENANCE THE AFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 15,315 hrs · 11,858 cycles

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FUSE ON NR 4 EMERGENCY BATTERY TRAY IAW RADIANT POWER CORP CMM25-60-83, OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 14,945 hrs · 11,539 cycles

IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHT STRIP AT ROW 19 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (LT AILERON) · airframe 13,528 hrs · 10,376 cycles

SHV - DURING C-CHECK LEFT AILERON UPPER SHROUD BONDING PLATE CORRODED. MX REPAIRED LT AILERON UPPER SHROUD BONDING PLATE IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 10,347 hrs · 8,167 cycles

EWR LOG SQUAWK LAV SMOKE INFLIGHT. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB145 AMM26-14-01. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE RT AND LT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.