N12163

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 44,769 hrs · 31,201 cycles

RH FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH FWD EMERGENCY LIGHT ASSEMBLY. OPS CHECK FAILED. REMOVED AND REPLACED BATTERY SUPPLY #2. OPS CHECK SAT.

Part: CONNECTOR — LOOSE (ZONE 200) · airframe 44,545 hrs · 30,997 cycles

RH OVERWING EMERGENCY EXIT IDENTIFIER SIGN INOPERATIVE. UPON REMOVAL, FOUND LOOSE CONNECTION, RESECURED ELECTRICAL CONNECTIONS. OPS CHECK SAT

Part: INVERTER — INOPERATIVE (ZONE 800) · airframe 43,221 hrs · 29,708 cycles

ROW 18 AFT AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED #4 EMERGENCY LIGHT INVERTER. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CRACKS SUSPECTED (6X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. AFTER NDT INVESTIGATION, 5 CRACKS FOUND. SKIN REPAIRED WITH DOUBLER AND BUSHINGS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, EXT DENT FOUND ON LH MAIN DOOR SKIN JUST BELOW STR 15L ON LOWER EDGE OF DOOR SKIN. DENT ACCEPTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, EXT DENT FOUND ON LH MAIN DOOR SKIN JUST BELOW STR 12L ON FWD EDGE OF DOOR SKIN. DENT ACCEPTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

FWD FUSE 2, LH OVERHEAD SIDE FRAME ABOVE COCKPIT POST FOUND CRACKED. FRAME REPAIRED WITH A SPLICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, ANGLE FOUND CRACKED ON LH AFT MAIN DOOR SURROUND STRUCTURE FR 19A STR 13L. REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

NLG W/WELL, CRACK FOUND ON NLG UP-LOCK AFT CROSS BEAM. REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, FRAME 15, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. SHEAR CLIP REMOVED AND REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,663 hrs · 28,237 cycles

AT RF1, LH ENTRANCE GUSSET BTW FR 65-68 ON FLOOR STRUCTURE FOUND CORRODED. AT RF1, LH ENTRANCE GUSSET BTW FR 65-68 REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,663 hrs · 28,237 cycles

CF1, LH SILL #1 BTW FR 18-24 FOUND CORRODED. LH SILL #1 BTW FR 18-24 REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, 2X ANGLES FOUND CRACKED ON LH BEAM AND 2X ANGLE CRACKED ON MID OMEGA BEAM AT FWD AND AFT DIGITAL PLATE JUNCTION. ANGLE REMOVED AND REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

IN RH ENGINE PYLON, RH PRECOOLER FWD STRUCTURE BRACKET IS CRACKED. BRACKET REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, CRACK FOUND ON FWD ANGLE UNDER MIDDLE GUSSET BTW FR 20-21 ON FLOOR STRUCTURE AREA. PART REMOVED AND REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

CF1, CRACK FOUND ON MIDDLE STEP FRAME ON FLOOR STRUCTURE MIDDLE OMEGA BEAM BTW FR 18-20. REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

IN LH ENGINE PYLON, LH PRECOOLER FWD STRUCTURE BRACKET IS CRACKED. BRACKET REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,663 hrs · 28,237 cycles

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

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

AT RF1, CRACK FOUND ON LH SHEAR CLIP AT FR 71 BTW STR 17L-18L. AT RF1, LH SHEAR CLIP AT FR71 BTW STR 17L-18L REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 28,237 cycles

AT RF1, CRACK FOUND ON LH SHEAR CLIP AT FR 73 BTW STR 16L-17L. LH SHEAR CLIP AT FR 73 BTW STR 16L-17L REPLACED

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 41,549 hrs · 28,134 cycles

PTIM MAIN INOPERATIVE, BACKUP PITCH TRIM INOPERATIVE EICAS DISPLAYED IMMEDIATELY AFTER T/O. R & R HORZ STAB CTL UNIT. REMOVED HAS UPPER BOLTS. C/W MOVEMENT OF STAB UP/DOWN, NO DEFECTS NOTED. NO DAMAGE OF CORROSION NOTED ON PIVOT BEARING. REINSTALLED HAS UPPER BOLTS. COMPLIED WITH STABILIZER BACKLASH CHECK, WITHIN LIMITS. VERIFIED MAIN & BACKUP PITCH TRIM SWITCHES DO NOT STICK. PERFORMED LOCKOUT LOGIC TEST. OPS CHECK GOOD. VERIFIED BONDING RESISTANCE SATIS ON GROUND STUDS. PERFORMED VOLTAGE, CONTINUITY, & MEGOHM CHECKS ON MAIN PITCH TRIM SYS. INSPECTED & CLEANED TRIM PANEL, HSCU, & HSA CONNECTORS. PERFORMED HORIZONTAL STAB ELECTRICAL OPS CHECK. R & R SPC. OPS CHECK GOOD. R & R HSA. OPS CHECK GOOD.

Part: ACTUATOR — INOPERATIVE · airframe 40,778 hrs · 27,443 cycles

PITCH TRIM MAIN INOPERATIVE EICAS MESSAGE BOTH CAPT AND FO SIDE INOPERATIVE. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,636 hrs · 27,317 cycles

SEAT 18A EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 18A EMERGENCY LIGHT. OPS CHECK SAT

Part: UNKNOWN — ODOR (CABIN) · airframe 40,337 hrs · 27,049 cycles

WHEN SELECTING ENGINE BLEEDS RUBBER SMELL NOTED. TURNED OFF BLEEDS, SMELL DISSIPATED. ON TAXI OUT AND UNTIL 1000 THEY WERE ON APU BLEEDS. AT 1300 GOING TO 3000 TURNED ON ENGINE BLEEDS, CAPTAIN AND FO NOTED RUBBER SMELL COMING FROM THE DUCTS. TURNED OFF BLEEDS AND SMELL WENT AWAY AND WENT BACK ON APU BLEED. PERFORMED ENGINE POWER RUN AND CYCLED PACKS AND ENGINE BLEEDS IN ALL POSSIBLE COMBINATIONS. NO FAULTS NOTED. PERFORMED INLET INSPECTION FOR BOTH ENGINES INSPECTING FAN BLADES AND CORE VANE FOR OIL LEAKAGE OR DAMAGE. NO DEFECTS NOTED. REMOVED FLOORBOARDS AND INSPECTED PACKS AND ASSOCIATED DUCT WORK FOR HEAT DAMAGE. NO DEFECTS NOTE. INSPECTED FLASHLIGHTS FOR ABNORMALITIES. NO DEFECTS NOTED. INSPECTED RELAYS FOR ABNORMALITIES. NO DEFECTS NOTED

Part: NONE — INOPERATIVE · airframe 40,197 hrs · 26,917 cycles

AFT SIDE OF EXIT LOCATING SIGN ASSEMBLY AT ROW 18 IS INOPERATIVE. REMOVED AND REPLACED AFT SIDE OF EXIT LOCATING SIGN ASSEMBLY AT ROW 18. OPS CHECK SAT

Part: LAMP — INOPERATIVE · airframe 40,188 hrs · 26,909 cycles

RH EMERGENCY LIGHT FWD OF WING ON FUSELAGE INOPERATIVE. REMOVED AND REPLACED RH EMERGENCY LIGHT LAMP. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE · airframe 40,188 hrs · 26,909 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT. OPS CHECK GOOD.

Part: NONE — NONE · airframe 39,684 hrs · 26,447 cycles

HAD AN ELECTRICAL BURNING SMELL IN THE FLIGHT DECK WHILE FLYING THROUGH HEAVY RAIN WITH BOTH ENGINE IGNITERS ON. SMELL WENT AWAY AFTER LANDING. COMPLIED WITH FIM. GROUND RAN ENGINE 1 AND 2. NO DEFECTS OR SMELL NOTED. COMPLIED WITH WINDSHIELD HEAT CONTROLLER INSPECTION. NO DEFECTS OR SMELL NOTED.

Part: LAMP — INOPERATIVE · airframe 38,982 hrs · 25,833 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB. OPS CHECK SAT

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 37,317 hrs · 25,233 cycles

LANDING GEAR HANDLE CANNOT MOVE. LFG WILL NOT RETRACT. L AIR/GND FAIL ON EICAS DURING CLIMB OUT. TROUBLESHOT LG WILL NOT RETRACT WITH L AIR/GND FAIL MESSAGE ON EICAS. DETERMINED LGEU TO BE AT FAULT. R&R LGEU. OPS CHECK GOOD AT THIS TIME.

Part: SKIN — CORRODED (FRMS 68-70) · airframe 38,283 hrs · 25,199 cycles

CORROSION ON LOWER REAR FUSE 1 SKIN, BTW FR 66-70 AND BTW STR 21L-21R, UNDER ANTENNA RADIO ALTIMETER. RADIO ALT. ANTENA 2 AFT EXT DOUBLER REMOVED FOR ACCESS TO CORROSION. DAMAGED SECTION OF FUSE SKIN REMOVED. ON LOWER REAR FUSE 1 SKIN BTW FR 68-70 AND BTW STR 21L-21R UNDER ANTENNA RADIO ALTIMETER 2, CORROSION REPAIRED.

Part: YOKE — CRACKED (RT ENGINE) · airframe 38,283 hrs · 25,199 cycles

FOLLOWING NDT INSPECTION ON TASK 54-50-00-250-803-A00, 2X CRACKS FOUND ON PYLON YOKES UPPER FLANGE 2X HOLE LOCATION. FOLLOWING NDT INSPECTION, PYLON YOKES UPPER FLANGE HOLES X2 OPENED AT SECOND PERMISSIBLE OVERSIZE (10,668MM). 4X BUSING LOCALLY FABRICATED. 2X BUSHINGS FLUSH PYLON AND 2X BUSHINGS PYLON. CRACKS 2X ON LH AND RH PYLON YOKES UPPER FLANGE FWD AREA REPAIRED. LH AND RH PYLON YOKES UPPER FLANGE REPAIRED. NR # 54-2247

Part: STRUCTURE — CRACKED (FRAME 78 S5-7L) · airframe 38,283 hrs · 25,199 cycles

SUSPECTED CRACK, EXTERNAL FUSE LH, FR 78 BTW STRG 5L-7L. CRACK REPAIRED.

Part: ACCESS PANEL — DAMAGED (LT WING TE FLAP) · airframe 38,283 hrs · 25,199 cycles

LH WING FLAP ACCESS 571AB HOLE ELONGATED AND SURFACE CORROSION. HOLE REPAIRED. NR #57-2130

Part: SKIN — DENTED (FRAME 15) · airframe 38,283 hrs · 25,199 cycles

DENT FOUND ON SKIN UNDER GROUND CONNECTOR AT STR 15 BTW FR 7-8 LH. ON FUSE SKIN, UNDER GROUND CONNECTOR AT STR 15 BTW FR 7-8 (LH), DAMAGE CUT OUT PERFORMED AND RIVET PATTERN DRILLED. REPAIR PARTS LOCALLY FABRICATED AND INSTALLED.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 38,283 hrs · 25,199 cycles

PAINT DAMAGES ON BAGGAGE DOOR SKIN, BTW STA X22364.2 - X22540.2 AND BTW BEAM #1-2. ON BAGGAGE DOOR SKIN, BTW STA X22364.2 - X22540.2 AND BTW BEAM #1-2, PAINT STRIPPED FOR DENT INVESTIGATION. DAMAGE ON BAGGAGE DOOR FOUND OUT OF LIMITS. ON BAGGAGE DOOR, BTW STR X22364.2 - X22540.2 AND BTW BEAM #1-2 DENT WITH BLEND SENT FOR ENGINEERING REVIEW. PATCH REMOVED AND FASTENER PITCH DRAWN FOR REVIEW. BAGGAGE DOOR SKIN DAMAGE BTW STA X22364.2 - X22540.2 AND BTW BEA, #1-2 REPAIRED.

Part: BEAM — CORRODED (FRMS 59-61) · airframe 38,283 hrs · 25,199 cycles

LH BEAM CORRODED UNDERNEATH ANCHOR NUT BTW FR 59-61. CF4, LH BEAM UNDERNEATH ANCHOR NUT BTW FR 67-71, GUSSET RENOVED FOR ACCESS TO CORROSION. CF4, LH BEAM UNDERNEATH ANCHOR NUT BTW FR 67-71 CORROSION BLENDED OUT OFF LIMITS. AT CF4, LH BEAM AT FR 67-71, CORROSION REPAIRED AND REINSTALLED.

Part: STRUCTURE — CORRODED (FRAME 65) · airframe 38,283 hrs · 25,199 cycles

CORROSION ON LH REAR FUSE 1 FRAME 65, ON FWD L-SHAPE BTW STR 15L-16L. ON LH REAR FUSE FR65, ON FWD BTW STR 15L-16L L-SHAPE IS OUT OF LIMIT. REMOVED AND REPAIRED.

Part: STRUT — DISCHARGED (NLG) · airframe 38,229 hrs · 25,153 cycles

LG AIR/GND FAIL MESSAGE AFTER TAKE OFF GEAR WOLD NOT RETRACT. SERVICED NOSE LANDING GEAR STRUT. PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK GOOD. PERFORMED MLH PROXIMITY SWITCH CLEARANCE GAP ADJUSTMENT CLEANED MLG PROXIMITY SWITCHES. PERFORMED LANDING GEAR EXTENSION AND RETRACTION ADJUSTMENT TEST. NO DEFECTS NOTED.

Part: SEAT FRAME — CRACKED (SEAT 5A) · airframe 37,991 hrs · 24,932 cycles

PASSENGER SEATS 5A AND 9A HAVE CRACKS IN SEAT FRAME BELOW AISLE ARMREST. R&R SEAT 5A AND 9A. NO FURTHER DEFECTS NOTED.

Part: SKIN — DENTED (RT WING LE) · airframe 43,625 hrs · 27,407 cycles

DENT WITH CREASE ON RT WING LEADING EDGE 2 BETWEEN RIB 1-2. RT WING LEADING EDGE 2 REMOVED. RT WING LEADING EDGE 2 PN 145-65200-402 SN SA1259 HAS BEEN DECLARED UNREPAIRABLE BY MANUFACTURER. RT WING LEADING EDGE 2 INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,625 hrs · 27,407 cycles

DENT ON RT FWD FUSE SKIN 2, 0.30" AFT OF FR 10 AND 1.80" ABOVE STR 17R. DENT ON RT FUSE SKIN 2, 0.0300" AFT OF FR 10 AND 1.8" ABOVE STR 17R REPAIRED.

Part: SEAL — TORN (CARGO DOOR) · airframe 37,112 hrs · 24,095 cycles

PLANE WILL NOT PRESSURIZE. FOUND CARGO DOOR SEAL TORN. R&R CARGO DOOR SEAL. PERFORMED PRESSURE CHECK. OPS AND LEAK CHECK SAT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,762 hrs · 23,792 cycles

RH OVER WING EMERGENCY LIGHT INOPERATIVE. R&R RH OVER WING EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,652 hrs · 23,704 cycles

RIGHT SIDE EXTERNAL EMERGENCY LIGHT OVER WING INOPERATIVE. REMOVED AND REPLACED RIGHT SIDE EXTERNAL OVER WING EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,856 hrs · 23,039 cycles

DURING MX INSPECTION THE RH OVERWING EXIT MARKER WAS INOP. MX R/R INVERTER #4 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,856 hrs · 23,039 cycles

DURING MX INSPECTION THE RH OVERWING EXIT MARKER WAS INOP. MX R/R INVERTER #4 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 35,610 hrs · 22,868 cycles

PILOT REPORTED THE EMERGENCY LIGHTS CAME ON WHEN F/A TURNS SIDEWALL LIGHTS FROM BRIGHT TO DIM. MX REMOVED AND REPLACED FLIGHT ATTENDANT LIGHT CONTROL PANEL WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 35,558 hrs · 22,832 cycles

DURING MX INSPECTION THE ROW 1 CEILING EMERGENCY EXIT WAS FOUND INOP. MX RE-SECURED CONNECTOR P8525 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,432 hrs · 22,741 cycles

CREW REPORTED A BURNING ELECTRICAL ODOR FROM COFFEE POT NR 2. MX PERFORMED VISUAL INSPECTION. NO ODOR NOTICED. NO WIRING BURNED. PERFORMED OPS CHECK OF COFFEE POT NR 2 OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 35,034 hrs · 22,450 cycles

IAH - THE CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP NEAR THE EQUIPMENT CLOSET WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURRED THE AFFECTED STRIP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 34,802 hrs · 22,271 cycles

TYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTORS FOUND THE NR 2 ENG. FORWARD LOWER YOLK CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE LOWER FORWARD YOLK IAW ECTC EA 26-2014-063-01. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: LIGHT — SMOKE (CABIN) · airframe 39,095 hrs · 23,228 cycles

IAH - FLIGHT 4163 THE CREW REPORTED SMOKE IN THE CABIN COMING FROM THE LT NR 3 SIDEWALL LIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TERMINAL — BURNED (WINDSHIELD)

THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LUG FOR THE WINDSHIELD HEAT ON THE FLIGHT OFFICERS WINDSHIELD BURNED AND REPAIRED THE ELECTRICAL CONNECTOR. OPS CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 32,205 hrs · 20,456 cycles

THE CREW REPORTED AN ENGINE OIL ODOR IN THE COCKPIT DURING TAKEOFF WITH BLEED NR 1 ON, NR 1 PACK ON . ODOR WENT AWAY WITH ENGINE BLEED OFF APU BLEED ON AND THE NR 1 PACK ON. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPS CHECKED GOOD.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 31,794 hrs · 20,189 cycles

THE CREW REPORTED A RAPID CABIN DEPRESSURIZATION DURING DESCENT AT FL 240. EMERGENCY DECLARED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND MISSING 12 INCH SECTION OF DOOR SEAL. REPLACED THE CARGO DOOR SEAL AND PERFORMED PRESSURIZATION CHECK. T HE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — ARCED (CABIN) · airframe 31,690 hrs · 20,117 cycles

IT WAS REPORTED THE LEFT LAST CEILING LIGHT ARCING. MX REMOVED AND REPLACED LEFT LAST ROW CEILING LIGHT HARNESS ASSY WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,320 hrs · 19,851 cycles

DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #1 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ARCED (CABIN) · airframe 30,909 hrs · 19,580 cycles

CREW REPORTED VISIBLE SMOKE AND FUMES FROM OVERHEAD PANEL ABOVE SEAT 6D. CONTRACT MX FOUND LOOSE SIDEWALL LIGHT ARCING CAUSING PLASTIC TERMINAL TO BURN AND CAUSE SMOKE. DISCONNECTED AND PLACED ON MEL 33-20-00-2. REMOVED AND REPLACED SIDEWALL LIGHT ASSY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 29,227 hrs · 18,421 cycles

DURING C-CHECK THE LAV WASTE DRAIN SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 29,227 hrs · 18,421 cycles

DURING C-CHECK THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — ARCED (CABIN LIGHT) · airframe 27,643 hrs · 17,303 cycles

F/A REPORTED A BURNING SMELL, ZONE 3, SEAT 7/8. MAINTENANCE R & R SIDEWALL LIGHT BULBS AT SEATS 7A AND 8A, OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — UNKNOWN · airframe 26,936 hrs · 16,833 cycles

ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL QTY. R & R O-RING FOR OIL RESERVOIR TANK. PERORMED HIGH SPEED ENGINE RUNS. NO LEAKS NOTED. ACFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 25,635 hrs · 15,963 cycles

THE AFT EMERGENCY FLASHLIGHT WAS REPORTED INOPERATIVE. MAINTENANCE R & R THE AFT EMERGENCY FLASHLIGHT BATTERY PACK AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 24,070 hrs · 14,962 cycles

DURING 1A INSPECTION, FUSELAGE SKIN FOUND TO HAVE THREE CRACKS EMINATING FROM A SINGLE RIVET ON FRAME 79 ABOVE STRINGER 6L. REMOVED DAMAGE AND PERFORMED A BUSHING REPAIR IAW ETD2014-145-031313 AND AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

CORROSION BEYOND LIMITS AFTER BLEND-OUT AROUND NUTPLATE GUSSET OTBD OF LT OMEGA BEAM. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CHANNEL — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

CORROSION BEYOND LIMITS AFTER BLEND-OUT AROUND NUTPLATE HOLES IN CENTER OMEGA BEAM. CUT-OUT FWD AND AFT DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS.

Part: SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

CORROSION BEYOND LIMITS AFTER BLEND-OUT AROUND NUTPLATE ON AFT SERVICE DOOR SILL. REMOVED AND REPLACED SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 61) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

LEFT LATERAL FLOOR SUPPORT AT FRAME 61 BETWEEN LT AND CENTER OMEGA BEAMS. CORRODED BEYOND LIMITS AFTER BLEND-OUT.

Part: FLOORBEAM — CORRODED (FRAME 61) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

RT LATERAL FLOOR SUPPORT AT FRAME 61 BETWEEN RT AND CENTER OMEGA BEAM CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.

Part: GUSSET — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

NUTPLATE HOLES CORRODED BEYOND LIMITS ON RT SIDE GUSSET. R & R GUSSET.

Part: GUSSET — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

NUTPLATE HOLES ON LT SIDE OF GUSSET IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: THRESHOLD — CORRODED (FRAME 65-68) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

CARGO DOOR CUTOUT THRESHOLD CORRODED BEYOND LIMITS. R & R THRESHOLD.

Part: BRACKET — CORRODED (FRAME 65) · corrosion level 2 · airframe 23,619 hrs · 14,682 cycles

ANGLE BRACKET AT FORWARD SIDE OF CARGO DOOR FRAME 65 WHICH CONNECTS LT OMEGA BEAM AND FLOOR SILL IS CORRODED BEYOND LIMITS. R & R ANGLE BRACKET.

Part: FLOORBEAM — CORRODED (FRAME 61) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK, CORROSION WAS FOUND ON THE LT OTBD LATERAL FLOORBEAM AT FRAME 61. MAINTENANCE R & R THE NEW FLOORBEAM IAW SRM 53-31-10 AND 51-40-02.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK, CORROSION WAS FOUND ON THE AFT LOWER PAX DOOR CUT-OUT ANGLE. MAINTENANCE REPLACED THE PAX DOOR CUTOUT ANGLE IAW SRM 51-40-02 AND CPM 51-21-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 23,619 hrs · 14,682 cycles

C-CHECK, CORROSION WAS FOUND ON THE RT OTBD LATERAL FLOOR SUPPORT AT FRAME 61. MAINTENANCE R & R THE CORRODED SUPPORT IAW SRM 53-31-1- AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAD MULTIPLE AREAS OF CORROSION FROM FRAME 64-70. MAINTENANCE R & R THE OMEGA BEAM CAP IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CRACKED (FRAMES 16-17) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK, LEFT OMEGA BEAM SPLICE WAS FOUND CRACKED BETWEEN FRAMES 16-17. MAINTENANCE R & R THE DIGITIAL SPLICE IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK. DAMAGE WAS FOUND ON A SHEAR TIE AT FRAME 65, STRINGER 19. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FRAME 18) · airframe 23,619 hrs · 14,682 cycles

DURING C-CHECK, FOUND CORRODED CENTER OMEGA GUSSET AT FRAME 18. MAINTENANCE R & R CENTER OMEGA BEAM IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · airframe 23,619 hrs · 14,682 cycles

C-CHECK, THE LEFT FLOOR SILL AT FRAME 18 WAS FOUND CORRODED. MAINTENANCE R & R THE LT FLOOR SILL AT FRAME 18 IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 62-65) · airframe 23,619 hrs · 14,682 cycles

DURING C CHECK, RT OMEGA BEAM CAP AT FRAME 64 WAS FOUND CORRODED. MAINTENANCE R & R THE OMEGA BEAM CAP AT FRAME 64.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 22,315 hrs · 13,862 cycles

DURING MX INSPECTION, THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. R & R THE NR 2 EMERGENCY LIGHT BATTERY AND OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,553 hrs · 12,734 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — BURNED (CABIN LIGHTS) · airframe 18,193 hrs · 11,182 cycles

DURING PREFLIGHT, CREW REPORTED SMOKE COMING FROM THE UPPER SIDEWALL BETWEEN SEATS 12A & 15A. MX INSPECTED THE ACFT AND FOUND A BURNED RECEPTICLE FOR THE OVERHEAD LIGHT AT SEAT 14A. MX R & R THE LIGHT BULB, RECONNECTED THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ADC — INOPERATIVE (ZONE 100) · airframe 18,094 hrs · 11,125 cycles

THE CREW REPORTED THAT THE ENGINE THRUST SETTING CYCLED UNCOMMANDED ON TAXI. THE ACFT RETURNED TO THE GATE WHERE MX R & R THE NR 1 AIR DATA COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (CARGO DOOR) · airframe 17,867 hrs · 11,006 cycles

CARGO DOOR DENTED IN SEVERAL PLACES BETWEEN FRAMES 65 & 66, STRING 13L & 15L. CUTOUT DAMAGED AREAS, INSTALLED DOUBLER & FILLERS. PRIMED AND PAINTED.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 16,138 hrs · 9,857 cycles

ORD FLT 6104 THE CREW REPORTED A BLEED NR 2 OVERTEMP THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 HIGH TEMPERATURE THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,981 hrs · 9,737 cycles

AIRCRAFT SUSTAINED TWO LIGHTNING STRIKES. REMOVED AND REPLACED O/B STATIC WICK BASE AND DISCHARGER, REMOVED AND REPLACED LT ELEVATOR TIP FAIRING, BLENDED OUT LIGHT DAMAGE ON FUSELAGE ON SKIN AT FRAME 18 AND STR 19R, REPAIRED DAMAGE ON SKIN AT FRM 12 & STR 19R BY DRILLING HOLE AND INSTALLING A RIVET. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,329 hrs · 7,360 cycles

ORD FLT 5707 THE CREW REPORTED A SLIGHT BURNING ODOR IN THE GALLEY DURING FLIGHT. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE OR SMELL ANY BURNING ODOR'S. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BUSHING — MIGRATED (AILERON) · airframe 12,866 hrs · 6,987 cycles

SHV - DURING C-CHECK RT AILERON HAS MIGRATED HAT BUSHING ON O/B PCA ATTACHMENT BRACKET O/B SIDE. MAINTENANCE COMPLETED REPAIR OF RT AILERON O/B PCA ATTACHMENT BRACKET O/B SIDE IAW EC 5740-01152. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,866 hrs · 6,987 cycles

SHV - DURING C-CHECK AFT DIGITAL HAS CORROSION (LEVEL 2 LOCAL) AT NUT PLATES (FR 17 & 18) ON LT OMEGA BEAM. MAINTENANCE REMOVED AND REPAIRED DAMAGED SECTION OF THE AFT DIGITAL AT FRAME 17 & 18 ON LT OMEGA BEAM IAW EC5320-01449. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,866 hrs · 6,987 cycles

SHV - DURING C-CHECK PREVIOUS REPAIR ON LT OMEGA BEAM (FR 20) AT RAMP ANGLE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED PREVIOUS REPAIR AND INSTALLED NEW REPAIR ON LT OMEGA BEAM AT FRAME 20 IAW EMB145XR SRM 51-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,866 hrs · 6,987 cycles

SHV - DURING C-CHECK RT OMEGA BEAM (FR 23) HAS CORROSION (LEVEL 2 LOCAL) AT NUT PLATE. MAINTENANCE FABRICATED AND INSTALLED NEW DOUBLER AT RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 53-21-10 "DOUBLER" AND PREP, PRIMED AND PAINTED IAW EMB-145XR CPM 51-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,866 hrs · 6,987 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FR 20. MAINTENANCE COMPLETED INSTALL OF REPAIR ON CENTER OMEGA BEAM AT FRAME 20 IAW EMB-145XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE, MX FOUND EXIT ROW IDENTIFIER LIGHT OUT AT ROW 12A INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINT, MX FOUND LT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: UNKNOWN — LOOSE (APU FUEL PUMP)

FLT 0210-SMF- FLIGHT CREW REPORTED APU LEAKING FUEL FROM DRAIN. CREW RESET APU MASTER AND FOUND PUMP IN THE ON POSITION. STARTED APU AND SYSTEMS. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: VALVE — INOPERATIVE (BLEED SYSTEM)

FLT 0216 - ONT - FLIGHT CREW REPORTED BLEED 1 AND 2 OVERTEMP IN ICING CLIMBOUT. THRUST TO ELIMINATE MSG, ICING WAS AT 240. ALSO HAD A PACK 2 MEL OVERLOAD-AIR RUSHING IN COCKPIT. MX PERSONNEL REMOVED AND REPLACED PACK 2 OVERTEMP SWITCH AND NR 2 FAN AIR VALVE. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. OVERTEMP SWITCH: P/N 782100-11, S/N 2698, TSN:4807, CSN:2541. FAN AIR VALVE: P/N 816610-2, S/N 2004010117, TSN:12113, CSN:6479. (A)

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT 0050 - ONT - FLIGHT CREW REPORTED AN ELECTRICAL ABNORMAL WARNING/EMERGENCY LIGHT NOT ARM MSG WHEN ARMED. MX RESET EMERGENCY LIGHT SYSTEM. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: PANEL — OPEN (LEFT ENGINE)

FLT 0224 - SMF - FLIGHT CREW HEARD A LOUD "BANG" AFTER TAKE OFF/CLIMB - E1 LOSING POWER AS INCREASING ALTITUDE TO SMF AND DID AN AIR-RETURN AND DID NOT DECLARE AN EMERGENCY. MAINTENANCE FOUND OUTER BYPASS PANEL BLOWN OPEN AT 11 O`CLOCK. MAINTENANCE REINSTALLED OUTER BYPASS PANEL. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: NUT — LOOSE (APU FUEL SYSTEM) · airframe 11,762 hrs · 6,278 cycles

FLT 0318 - ABQ - FLIGHT CREW REPORTED APU LEAKING FUEL WHILE ON THE GROUND. MX TIGHTEN APU FUEL VLV JAM NUT. OPERATIONALLY AND LEAK CHECK SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,874 hrs · 5,806 cycles

MCI - DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,257 hrs · 3,903 cycles

CLE FLIGHT 2252 - THE CREW REPORTED THE EMERGENCY WINDOW EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: TIRE — FAILED (RT MLG) · airframe 884 hrs · 455 cycles

CLE- FLIGHT 2230, CREW REPORTED THAT THE NR 3 MAIN TIRE BLEW ON TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NR 3 TIRE HAD BLOWN AND CAUSED DAMAGE TO THE RIGHT INBOARD FLAP. ALSO FOUND DAMAGE TO THE NR 2 ENGINE INLET GUIDE VANES AT THE 5 O'CLOCK POSITION. APPLIED SPEED TAPE TO THE DAMAGED AREA OF THE RIGHT INBOARD FLAP AND PLACED ON DMI FOR 100FC AS PER EMBRAER FACSIMILE REF IC2004-145/4377. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED BACK TO SERVICE.