N13553

Part: SKIN — DENTED (FRAMES 68-70) · airframe 41,535 hrs · 32,346 cycles

TYS A/C WAS FOUND WITH GROUND DAMAGE TO THE FUSELAGE AT FRAME 68 THRU 70 AND STRINGER 16L AND 17L.MAINTENANCE CUT OUT THE DAMAGE AREA AND SPLICED A INTERNAL DOUBLER AND REPLACED THE NEW SKIN IAW ETD 2019-145-159935.ALL WORK ACCOMPLISHED AND WILL BE RELEASED WHEN A/C HAS A SERVICE CHECK.

Part: SLEEVE — LOOSE (NR 1 ACM) · airframe 41,447 hrs · 32,163 cycles

IAH - THE CREW REPORTED IN FLIGHT CREW AND PAX REPORTED A CHEMICAL SMELL AND LOUD WHINEIN CABIN ON LEFT (CA SIDE) OF AIRCRAFT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURRED A LOOSE SLEEVE ON THE NUMBER ONE ACM. OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROPVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ZONE 400) · airframe 33,128 hrs · 25,545 cycles

DURING C-CHECK, THE LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE YOKE FITTING IAW EC5450-01182. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (RT ENGINE) · airframe 33,128 hrs · 25,545 cycles

DURING C-CHECK, THE RT ENGINE LOWER FORWARD YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01182. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,402 hrs · 21,062 cycles

THE CREW REPORTED ON TAKEOFF, STRONG ODOR OF RAW FUEL IS NOTED COMING THRU THE ENVIROMENTAL SYS. REPORTED THIS ON ALL THREE FLIGHTS THAT DAY. OPEN

Part: UNKNOWN — ODOR (CABIN) · airframe 27,356 hrs · 21,026 cycles

THE CREW REPORTED A FUEL SMELL ON TAKEOFF ROLL. APU ON, PACKS ON. INSPECTED AND SIMULATED TAKOFF WITH APU ON AND PACKS ON. NO DISCREPANCY OR FUEL ODOR WAS NOTED. ACFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,355 hrs · 21,024 cycles

THE CREW REPORTED A STRONG FUEL ODOR IN CABIN DURING TAKEOFF. APU-ON, PACKS-ON. MX INSPECTED RAN ENGINES AND APU WITH PACKS ON AND NO DEFECTS WERE FOUND. THE ACFT WAS RELEASED FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,897 hrs · 18,221 cycles

DURING SCHEDULED MX INSPECTION, THE MAIN DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (LANDING GEAR) · airframe 21,473 hrs · 16,354 cycles

LANDING GEAR FAIL AFTER ROTATION. REPAIRED BROKEN WIRE W109-0003-22 AT PIN C OF CONNECTOR P2834 IAW EMB145 SWPM 20-21-00 OPS CHECK GOOD IAW EMB 145 AMM 32-32-00. TEST FLIGHT SATISFACTORY. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 21,470 hrs · 16,348 cycles

LANDING GEAR WOULD NOT RETRACT, AIR GROUND FAIL. REMOVED AND REPLACED LGEU IAW EMB145 AMM 32-52-01 AND REMOVED AND REPLACED RELAY IAW EMB 145 AMM 20-13-02. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: CONTROL LEVER — BROKEN (COCKPIT) · airframe 21,468 hrs · 16,347 cycles

LANDING GEAR AIR/GRND FAIL MSG AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,825 hrs · 15,079 cycles

THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT STRIP AT SEAT 8A AND 9A WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 18,870 hrs · 14,384 cycles

TYS A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND NICKS IN THE SKIN WHERE THE UPPER TCAS ANTENNA MOUNTS. MAINTENANCE REPAIRED THE SKIN BY INSTALLING A DOUBLER REPAIR IAW EC 5330-02084. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BUSHING — MIGRATED (SERVICE DOOR) · airframe 18,870 hrs · 14,384 cycles

TYS A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE SERVICE DOOR SWING ARM BUSHINGS MIGRATED. MAINTENANCE REPAIRED THE SWING ARM WITH NEW BUSHINGS IAW EMB 145EC5240-01036. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,871 hrs · 14,384 cycles

THE LT RAMP ANGLE IS CORRODED. REPLACED RAMP ANGLE IAW SRM 51-40-02.

Part: ENGINE — LEAKING (NR 2) · airframe 18,396 hrs · 14,036 cycles

IAH - FLIGHT 2379, THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS WITH AN ASSOCIATED SMOKE SMELL ON CLIMBOUT. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 18,380 hrs · 14,027 cycles

FLIGHT 2940 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION AFTER T/O WITH NO SMOKE OR HEAT NOTED. SYSTEM WAS RESET SUCCESSFULLY. ACFT APPROVED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,975 hrs · 12,962 cycles

FLIGHT 4932, DURING POST FLIGHT INSP THE CREW REPORTED THE ROW 19 AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAULTY (NR 2) · airframe 16,488 hrs · 12,598 cycles

FLIGHT 2337 - CLT - FLIGHT CREW REPORTED FUEL SMELL IN THE COCKPIT AND ENGINE NR 2 LOCKED UP. MX REMOVED AND REPLACED ENGINE NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT NR 2927 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE BY THE EXIT ROW. MX REPLACED THE AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER)

FLIGHT CREW REPORTED ENG 1 T/R DISAGREE ON TAKEOFF ROLL TWICE AND ON THE SECOND ATTEMPT, MX PERSONNEL RESET CYCLED T/R. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,966 hrs

AUS - DURING MAINTENANCE INSPECTION THE FORWARD SIDE OF THE CEILING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,185 hrs · 10,885 cycles

ONT - FLIGHT 125, DURING POST FLIGHT INSPECTION THE LT EMERGENCY EXIT LIGHT FWD OF WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,571 hrs · 9,777 cycles

MCI - FLIGHT 530, DURING POST-FLIGHT INSPECTION THE EXTERIOR UPPER OVERWING EMERGENCY LIGHT AND FWD SIDE CEILING OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — MISSING (LT WING) · airframe 12,342 hrs · 9,616 cycles

FLT 41 - GEG TO GEG - FUEL LEAKING FROM LEFT WING DURING CLIMB. MX REPO'D 568 FROM ONT WITH MX PERSONAL AND PARTS. MX INSPECTED FUEL TANK AND FOUND MOST O/B FLAPPER VALVE MISSING ON LEFT WING. MX INSTALLED NEW LEFT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: FLAPPER VALVE — MISSING (LT WING) · airframe 12,342 hrs · 9,616 cycles

FLT 41 - GEG TO GEG - FUEL COMING FROM LT WING DURING CLIMBING - REPO'D 568 FROM ONT WITH MX PERSONAL AND PERTS. MX INSPECTED FUEL TANK AND FOUND MOST OUTBOARD FLAPPER VALVE MISSING. MX INSTALLED NEW LT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: STRUCTURE — MISDRILLED (FUSELAGE) · airframe 12,051 hrs · 9,416 cycles

TYS - DISCREPANCY- MISSDRILLED HOLES ON RIGHT SIDE OF CARGO BETWEEN FRAME 62 AND 62A. INSTALLED REINFORCEMENT AT FRAME 62 AND 62A BETWEEN 11R AND 12R IAW EMB 145 EC5310-01407.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 11,520 hrs · 9,015 cycles

EWR FLT 1206 DURING ROUTINE INSPECTION FOUND LT WING FUSELAGE FRONT FAIRING AND AISLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY NR 1 POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.

Part: FIRE LOOP — FAILED (NR 1 ENGINE) · airframe 9,799 hrs · 7,686 cycles

SDF- DISCREPANCY- E1 FIRE DET FAIL EICAS MESSAGE IN FLIGHT. QRC PROCEDURES WERE PERFORMED. NO FIRE/OVERHEAT SUSPECTED. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR IAW EMB 145 AMM 26-11-01 OPS CHECK GOOD.

Part: FIREWALL — CRACKED (AFT FUSELAGE) · airframe 8,632 hrs · 6,757 cycles

DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED ON THE INSIDE, BETWEEN STRINGERS 9R AND 10R AT THE 3 O'CLOCK POSITION. MAINTENANCE INSTALLED REPAIR DOUBLER ON APU FIREWALL IAW SRM 53-32-13 FIG 204. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FIREWALL — CRACKED (AFT FUSELAGE) · airframe 8,632 hrs · 6,757 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT THE RIGHT HAND LOWER MOUNT. MAINTENANCE INSTALLED DOUBLER ON THE APU FIREWALL AT THE RIGHT HAND LOWER MOUNT IAW EMB SRM 53-32-13. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (AFT FUSELAGE) · airframe 8,632 hrs · 6,757 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT MID RIGHT HAND SECTION (INSIDE). MAINTENANCE INSTALLED REPAIR DOUBLER ON APU FIREWALL AT MID RIGHT HAND SECTION IAW EMB 145 SRM 53-32-13 FIG 204. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,978 hrs · 5,464 cycles

SDF - LT AND RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT ASSY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4 AND NR 4 CHARGER. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. BATTERY P/N 2013-BR, CHARGER P/N 11-0049, EMERGENCY LIGHT ASSY P/N 30-2510-3.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 6,814 hrs · 5,339 cycles

DURING RON MAINTENANCE FOUND EMERGENCY LIGHTS OUT AFT OF EMERGENCY EXIT ROW OF SEATS. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSEMBLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 6,385 hrs · 5,011 cycles

GSO - PILOT REPORTED AIR/GROUND FAIL INDICATION MESSAGE ILLUMINATED CAUSING THE LANDING GEAR NOT TO RETRACT. THE AIRCRAFT RETURNED TO GSO AND LANDED WITHOUT INCIDENT. UPON LANDING THE AIR/GROUND FAIL MESSAGE CLEARED ITSELF. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAIL MESSAGE AND PERFORMED A PRECAUTIONARY SYSTEM RESET WITHOUT FURTHER FAILURE INDICATIONS BEING NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,501 hrs · 4,330 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB IN THE EMERGENCY LIGHT. ALL OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,501 hrs · 4,330 cycles

DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW THREE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 4,234 hrs · 3,365 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOORBEAM RAMP ANGLE. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,234 hrs · 3,365 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CHARGER — OVERHEATED (FLASHLIGHT)

CREW REPORTED SMELL IN FORWARD CABIN AREA, INSPECTED FORWARD CABIN AREA AND FOUND FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT CHARGER OVERHEATING. PLACED FORWARD EMERGENCY FLASHLIGHT AND HOLDER ON MEL 25-60-05 CONTROL 037554 CATEGORY-C (CIRCUIT BREAKER FOR FLIGHT ATTENDANTS FLASHLIGHT PULLED). MAINTENANCE REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT UNIT. OPS CHECKED GOOD IAW EMB145 AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: LEVER — INTERMITTENT (MLG)

SYR FLIGHT 3181 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE CREW CYCLED THE GEAR AND CONTINUED AS NORMAL. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: STRUT — UNDERSERVICED (NLG)

IAH- FLIGHT 2538, THE CREW NOTED AFTER TAKEOFF THAT THE LANDING GEAR WOULD NOT RETRACT, AIR/GROUND SENSOR FAILURE ON EICAS. FOLLOWED QRH. THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SERVICED THE NOSE LANDING GEAR SHOCK ABSORBER IAW EMB 145 AMM 32-20-01,PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION, AND, RETRACTION IAW EMB145 AMM 32-30-00, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (LT MLG WW)

ELP- FLIGHT 2833, DURING CLIMB THE CREW NOTED THAT THE LANDING GEAR DISAGREE MESSAGE APPEARED. THE CREW RETURNED THE AIRCRAFT TO ELP AND LANDED WITHOUT INCIDENT. ELP- MAINTENANCE RESET THE UPLOCK HOOK ON THE LEFT MLG UPLOCK BOX IAW EMB-145 MM 32-32-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — DEFECTIVE (MLG)

IAH- FLIGHT 2833, DURING LANDING THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE MESSAGE ILLUMINATED. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB-145 MM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLOCK — FAULTY · airframe 1,817 hrs · 1,447 cycles

EWR---CO2297, CREW REPORTED, "ON CLIMB AFTER TAKEOFF, WE GOT A LANDING GEAR DISAGREEMENT MESSAGE ON EICAS MESSAGE WITH LANDING GEAR INDICATION SHOWING UP IN RED. GEAR WAS UP AND CAME DOWN NORMALLY WITH THE LANDING GEAR LEVER." MAINTENANCE FOUND BAD GROUND TO PINS 1,5,9,AND 10 AT LANDING GEAR LEVER GROUND BLOCK. REMOVED AND REPLACED LANDING GEAR LEVER GROUND TERMINAL BLOCK IAW EMB145 MM #20-13-05 AND EMB145 WM #32-33-50. OPS.CHECKED OF LANDING GEAR IAW EMB145 MM #32-30-00. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SELECTOR — DEFECTIVE (MLG)

IAH FLIGHT 2732 THE CREW REPORTED A LANDING GEAR AURAL WARNING WHEN THE GEAR WAS SELECTED UP. NO WARNING WHEN GEAR WAS DOWN. MAINTENANCE REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD.

Part: SENSE LINE — BROKEN (NR 1 ENGINE)

CLE FLIGHT 3421 THE CREW REPORTED A NR 1 ENGINE BLEED LEAK WARNING MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED DUCT PRESSURE SENSE LINE. OPERATIONAL CHECKS WERE GOOD.