N16911

Part: TURBINE WHEEL — DAMAGED (APU) · airframe 40,299 hrs · 31,025 cycles

CREW REPORTED SMOKE IN COCKPIT AND CABIN WITH APU RUNNING. MX FOUND DAMAGE TO APU TURBINE WHEEL. MX REMOVED AND REPLACED APU WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,943 hrs · 29,935 cycles

THE CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER BEHIND THE F/A COAT CLOSET, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,786 hrs · 29,017 cycles

DURING C-CK. RT MLG AFT UPPER TRUNNION IS CRACKED. REMOVED AND REPLACED RT MLG AFT UPPER TRUNNION IAW ETD216-145-110849 IN EC/TC W/O 482331. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 37,786 hrs · 29,017 cycles

DURING C-CK. LT MLG AFT UPPER TRUNNION IS CRACKED. REMOVED AND REPLACED LT MLG AFT UPPER TRUNNION IAW ETD2016-145-11089 IN ET/EC W/O 4822331. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — DAMAGED (CABIN LIGHTS) · airframe 35,374 hrs · 27,079 cycles

PILOT REPORTED A FUNNY ODOR IN CABIN NEAR MCD. MAINTENANCE R & R CABIN CEILING LIGHT HARNESS AT SEAT 1A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 31,726 hrs · 24,213 cycles

THE CREW REPORTED BURNING ODOR AFTER TAKEOFF BUT NO VISIBLE SMOKE. ODOR DISSIPATED AFTER A FEW MINUTES. MAINTENANCE REPLACED THE F/O FLASHLIGHT BRACKET. OPS CHECKS WERE GOOD.

Part: CRADLE — FAULTY (FLASHLIGHT) · airframe 31,721 hrs · 24,209 cycles

THE CREW REPORTED SMOKE ODOR AFTER TAKEOFF. SMOKE DISIPATED AFTER 5 MINUTES. ALSO REPORTED ODOR ON DESCENT. THEY ALSO NOTED THE LOCALIZER DID NOT WORK ON CAPTAIN`S OR F/O'S SIDE. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT FLASHLIGHT HOLDER/BRACKET ASSEMBLY. OPS CHECKS WERE GOOD. MAINTENANCE ALSO INSPECTED AND PERFORMED LOCALIZER CHECKS AND NO DEFECTS WERE FOUND.

Part: WIRE — UNSECURE (SMOKE DETECTION) · airframe 23,033 hrs · 17,497 cycles

FLIGHT 2369 - EWR - FLIGHT CREW REPORTED BAGG SMOKE LIGHT REMAINS ILLUMINATED AFTER APU FIRE TEST BUTTON IS RELEASED. EWR MX RE-SECURED WIRE TO PLUG AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BAR — FAILED (APU) · airframe 22,974 hrs · 17,450 cycles

IAH - FLIGHT 2129, THE CREW REPORTED A APU CONTACTOR FAIL MESSAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU SHUNT GROUND BAR TO HAVE FAILED CAUSING DAMAGE TO FRAME 80 AND THE ELECTRICAL WIRING ON THE SHUNT. IAH MAINTENANCE REMOVED THE DAMAGED SECTION OF FRAME 80 AND INSTALLED A FILLER REPAIR, REPAIRED THE ELECTRICAL WIRING, REMOVED AND REPLACED THE SHUNT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — LOOSE (AILERON) · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK RT AILERON HAT BUSHING AT DAMPNER ATTACH BRACKET ON AILERON LOOSE. MAINTENANCE REMOVED AND REPLACED RT AILERON DAMPNER ATTACH BRACKET ON AILERON IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK LT UPPPER SEAT TRACK SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 50. MAINTENANCE PERFORMED REPAIR AT LT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EMB-145 EC5320-01522A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (AILERON) · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK RT AILERON HAS 3 MIGRATED HAT BUSHINGS AT PCA ATTACH BRACKET ON AILERON. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET ON AILERON IAW EC5750-01177 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK RT COCKPIT FRAME 10 CRACK BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED RT COCKPIT FRAME 10 BELOW DV WINDOW IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 46. MAINTENANCE PERFORMED REPAIR AT LT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EMB-145 EC5320-01522A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,972 hrs · 17,448 cycles

SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE FRAME 22-23 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER FLANGE FRAME 22-23 IAW EC5320-01570. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 18,096 hrs · 13,781 cycles

CLE FLIGHT 2785 THE CREW REPORTED THE LAV SMOKE WOULD NOT TEST. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR / SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,549 hrs · 14,899 cycles

MCI - DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 19,229 hrs · 14,674 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,821 hrs · 14,373 cycles

FLIGHT 2521 - EWR - FLIGHT CREW REPORTED LAST 3 FLOOR PROXIMITY LIGHT STRIPS NOT WORKING. EWR MX REMOVED AND REPLACED INVERTER NR 6 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,666 hrs · 14,256 cycles

FLT 2077 - FLIGHT CREW REPORTED LIGHT BEHIND CAPTAIN'S CLOCK AND RADIO PANEL WAS FLICKING AND BURNING ODOR WAS DETECTED. EWR MX PERFORMED VISUAL INSPECTION ON CAPTAIN'S CLOCK WIRING HARNESS, PERFORMED OPS CHECK AND FOUND NO DEFECTS. ALSO NO BURNING ODOR WAS DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,236 hrs · 13,949 cycles

THE 1ST FLOOR EMERGENCY PROXIMITY STRIP WILL NOT ILLUMINATE. REMOVED AND REPLACED PROX LIGHT STRIP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. AIRCRAFT STILL IN C CHECK.

Part: HINGE BRACKET — CRACKED (HORIZ STAB) · airframe 18,236 hrs · 13,949 cycles

RT HORIZONTAL STAB HINGE PIN RETENTION EAR IS CRACKED. REMOVED AND REPLACED RT HORZ STAB HINGE PIN BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT STILL IN C CHECK.

Part: WIRE — BROKEN (LIGHT STRIP) · airframe 18,236 hrs · 13,949 cycles

NR 1 EMERGENCY LIGHT STRIP ON THE FLOOR HAD BROKEN WIRES. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-12. AIRCRAFT STILL IN C-CHECK.

Part: ACM — FAULTY (AC BAY) · airframe 18,193 hrs · 13,913 cycles

CLE FLIGHT 2368 THE CREW REPORTED SMOKE IN THE CABIN WHILE ON THE GROUND WITH THE APU RUNNING AND PACKS ON. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 16,052 hrs · 12,456 cycles

IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH REINSPECTIONS TO BE MADE AT EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSTALLED A TRIPLER REPAIR IAW EC5740-01148, REMOVED THE DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HUB CAP — UNSECURE (RT MLG WHEEL) · airframe 13,406 hrs · 10,490 cycles

CLE FLIGHT 2098 AFTER TAKEOFF THE RIGHT MAIN GEAR DID NOT INDICATE LOCKED AND THE LANDING GEAR LEVER DISAGREE MESSAGE APPEARED ON THE EICAS. CYCLED GEAR 3 TIMES WITH SAME RESULTS. MAINTENANCE INSPECTED AND FOUND THE NR 3 MAIN WHEEL ASSEMBLY HUBCAP UNSECURED. THE HUBCAP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: WIRE HARNESS — SHORTED (NLG PROX) · airframe 9,949 hrs · 7,778 cycles

FLT NUMBER 2703, LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE ON CLIMB-OUT. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NLG PROXIMITY SENSE HARNESS ASSY. ACFT WAS TEST FLOWN WITH NO DISCREPANCIES NOTED AND SUBSEQUENTLY RELEASED TO SERVICE.

Part: LANDING GEAR — COLLAPSED (NOSE) · airframe 9,946 hrs · 7,775 cycles

CREW REPORTED, "NOSE LANDING GEAR COLLASPED ON PUSH BACK FROM GATE." MAINTENANCE TROUBLESHOOTING AND REPAIRING AIRCRAFT.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 8,234 hrs · 6,428 cycles

IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,234 hrs · 6,428 cycles

IAH- FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 8,234 hrs · 6,428 cycles

IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT) · airframe 5,959 hrs · 4,682 cycles

PILOT REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM 32-32-01. THE OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT)

THE CREW REPORTED DURING CLIMBOUT THE GEAR WOULD NOT RETRACT. THE CREW RECYCLED THE GEAR AND THE GEAR RETRACTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

ROUTINE INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT OVER THE LEFT HAND WING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB AND PERFORMED A SATISFACTORY OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

EWR- ON POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR FAILED TO ILLUMINATE. EWR- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FLT 2380 - DURING POSTFLIGHT INSPECTION THE AFT EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE.

Part: STRINGER — GOUGED · airframe 4,171 hrs · 3,215 cycles

TYS, During a scheduled inspection a gouge was found at stringer 19R center fuselage IV. Maintenance blended, performed dye-pen inspection, fabricated and installed repair angle and shims. I/A/W-EMB-145-SRM-53-24-02, 51-40-02 and CPM-51-21-06. The repair was satisfactory and aircraft was released to service.

Part: SUPPORT — CORRODED (FLOOR) · airframe 4,171 hrs · 3,215 cycles

TYS DURING A SCHEDULED 1C INSPECTION THE TOP CAP ANGLE BEAM WAS CORRODED.MAINT.REPLACED RAMP ANGLE BEAM FOR TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: BEAM — CORRODED (FUSELAGE) · airframe 4,171 hrs · 3,215 cycles

DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE CUT OUT DAMAGED AREA, FAB, ALODINE, PRIME, PAINTED AND INSTALLED REPAIRED DOUBLER, FILLER AND SHIMS IAW EMB 135/145 SRM 53-21-10, 51-40-02;CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: CDU — FAILED (COCKPIT)

PHL FLIGHT#2062 THE CREW REPORTED #1 CDU/FMS FAILED IN FLIGHT.AFTER LANDING A STRONG BURNING/SMOKE ODOR IN COCKPIT AND CABIN WAS NOTICED.MAINTENANCE REPLACED THE #1 CDU AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (GALLEY)

THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — LOOSE (SERVICE DOOR)

CLE FLIGHT#3194 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE GALLEY SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND RESECURED LOOSE WIRE ON THE EMERGENCY EXIT LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — LOOSE

EWR---CO3039, CREW REPORTED, THE GALLEY DOOR EMERGENCY LIGHT WAS INOPERATIVE....MAINTENANCE FOUND A LOOSE CONNECTOR AND RESECURED THE CANNON PLUG. OPS.CHECKED SYSTEM GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT#4368 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE GALLEY DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.