N14558

Part: WIRE — DAMAGED (FIRE DETECTOR) · airframe 40,295 hrs · 31 cycles

CREW REPORTED E2 FIREDET FAIL EICAS MESSAGE AFTER TAKEOFF. RETURN TO BASE AND EICAS MESSAGE EXTINGUISHED ON SHORT FINAL. MX TROUBLESHOT TO DAMAGED WIRE W102-1396-24 IN WIRE HARNESS 102. REPAIRED WIRE, OPS TESTED AIRCRAFT IN GROUND AND IN AIR CONFIG ALL OPS TESTS GOOD.

Part: WIRE HARNESS — DAMAGED (FIRE DETECTION) · airframe 40,295 hrs · 31,269 cycles

CREW REPORTED DURING TAKEOFF WE RECEIVED A E2 FIREDET FAIL MESSAGE THEN IT WENT AWAY. THE MESSAGE CAME BACK LATER AND WE RAN THE QRH AND THEN THE MESSAGE REMAINED UNTIL WE WERE SHORT FINAL AND TURNED THE APU FOR A RETURN TO BASE. MX TROUBLESHOT TO BAD ENGINE WIRE HARNESS W407. R & R WIRE HARNESS, OPS TESTED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRMS 57-61 BL0) · corrosion level 2

CORROSION FOUND ON FLOOR SUPPORT BEAM BL0 BETWEEN FR 57 AND FR 61.

Part: TRUNNION — CORRODED (LT MLG)

LH FWD MLG TRUNNION HAS CORROSION ON THE BEARING RACES WITH DAMAGE ON THE FWD FACE REPAIRS COMPLETED IAW ETD2022-145-028349

Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2

LH AFT MLG TRUNNION HAS CORROSION ON THE BEARING RACES WITH DAMAGE ON THE AFT FACE REPAIRS COMPLETED IAW ETD2022-145-028349

Part: CASE — CRACKED (NR 2 ENGINE) · airframe 39,031 hrs · 30,218 cycles

THE CREW REPORTED ON DESCENT CABIN SMELLED LIKE BURNT FEET. MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,565 hrs · 37,565 cycles

DURING C CHECK INSPECTION FOUND CARGO COMPARTMENT DOOR FRAME LOWER BEAM CORRODED AROUND SEVERAL FASTNERS. MAINTENANCE REPLACED CARGO DOOR FRAME LOWER BEAM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,162 hrs · 28,698 cycles

DURING AN INSPECTION, THE FORWARD EMERGENCY LIGHT STRIP WOULD NOT ILLUMINATE. R & R THE BATTERY AND CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 37,152 hrs · 28,689 cycles

FLIGHT ATTENDANT CONTROL PANEL, CABIN LIGHTS INOPERATIVE, SMELLED ELECTRICAL SMOKE. MX REMOVED AND REPLACED PSU LIGHT CONTROL MODULE, AND 1A BALLAST, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,152 hrs · 28,689 cycles

DURING A MX INSPECTION, THE NR 2 EMERGENCY LIGHT BATTERY WAS INOPERATIVE. MX REMOVED AND REPLACED THE BATTERY. OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,033 hrs · 28,598 cycles

EMERGENCY LIGHTS INOPERATIVE FROM GALLEY TO THE EXIT ROW. REMOVED AND REPLACED THE NR 2 AND 3 BATTERY PACKS IAW AMM 33-50-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOPERATIVE FROM GALLEY TO THE EXIT ROW. REMOVED AND REPLACED THE NR 2 AND 3 BATTERY PACKS IAW AMM 33-50-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,751 hrs · 28,374 cycles

DURING MX INSPECTION, THE FORWARD EMERGENCY LIGHTS DID NOT ILLUMINATE. MX R & R THE NR 2 BATTERY POWER SUPPLY, OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 36,362 hrs · 28,050 cycles

IAH - DURING MAINTENANCE INSPECTION EMERGENCY LIGHT STRIPS 1, 2, & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO (2) EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 36,236 hrs · 27,945 cycles

NUMEROUS EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,030 hrs · 27,785 cycles

DURING PREFLIGHT INSPECTION, THE FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 35,040 hrs · 26,993 cycles

SUSPECTED NOSE GEAR DOOR OPENED IN FLIGHT. REMOVED AND REPLACED NLG DOOR SEQUENCE PROX SWITCH. OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,915 hrs · 26,891 cycles

PILOT REPORTED FORWARD EMERGENCY EXIT LIGHTS COME ON THEN FADE OUT. CONTRACT MX REMOVED NEW BATTERY PACK AND REINSTALLED BATTERY PACK WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,820 hrs · 26,817 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED NUMEROUS EMERGENCY LIGHTS INOP. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — FAILED (CABIN) · airframe 34,446 hrs · 26,537 cycles

RT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. R & R THE NR 2 EMERGENCY LIGHT AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: DRIVE ASSY — BROKEN (RT WING TE FLAP) · airframe 32,110 hrs · 24,716 cycles

THE CREW REPORTED A FLAP FAIL MESSAGE AFTER TAKEOFF DURING FLAP RETRACTION. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RT OTBD FLAP DAMAGED FROM THE INBD FLAP SHROUD DRIVER BROKEN. THE RT OTBD FLAP WAS REPLACED ALONG WITH THE FLAP SHROUD. OPS CHECKS WERE GOOD.

Part: CONTROL VALVE — FAULTY (BRAKE) · airframe 30,989 hrs · 23,800 cycles

PILOT REPORTED AFTER LANDING AT 120 KTS THE BRAKE EFFECTIVENESS WAS REDUCED BY HALF. INBD BRAKE INDICATION REMAINED COLD AND OTBD BRAKES IN THE YELLOW. MX R & R THE INBD BRAKE CONTROL VALVE AND NR 3 WHEEL SPEED TRANSDUCER WITH TAXI AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CABIN PRESSURE — INOPERATIVE · airframe 28,156 hrs · 21,578 cycles

NO PRESSURIZATION WITH EITHER MANUAL OR AUTOMATIC CONTROL.

Part: ACM — SMOKE (LEFT) · airframe 27,829 hrs · 21,342 cycles

ACFT WAS DESCENDING WHEN THE CREW DETECTED AN ODOR OF ELECTRICAL SMOKE AND THEN BECAME VISUAL IN COCKPIT. AFTER LANDING, MAINTENANCE TROUBLESHOOTING IAW FIM 72-00-00-810-814. MAINTENANCE R & R THE LT PACK ACM IAW AMM 21-51-03. PERFORMED BLEED 1 SYSTEM CLEANSING IAW AMM 21-20-00. OPS CHECKED GOOD AND ACFT WAS RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN /COCKPIT) · airframe 26,794 hrs · 20,568 cycles

PACKS 1 AND 2 WERE REPORTED AS HAVING A BURNED OIL ODOR IN COCKPIT AND CABIN WHEN ON BLEED FROM ENGINES AND APU. MAINTENANCE INSPECTED AND PERFORMED FIM 72-00-00-810-808A AND TASK 21-20-00-100-805 WITH NO BURNED OIL ODOR WHEN OPERATING OFF OF ENGINE OR APU BLEEDS, AND ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,370 hrs · 18,596 cycles

CORROSION ON FUSELAGE SKIN FR 14, 15, STR 18R IN BELLY. BLENDED CORROSION, CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION, NO FURTHER DEFECTS. PERFORMED A SINGLE EXTERNAL DOUBLER REPAIR, ALODINED, PRIMED AND INSTALLED WET. RESTORED EXTERNAL FINISH OF REPAIRED AREA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,370 hrs · 18,596 cycles

FRAME 80 CORRODED ADJACENT TO APU SHUNT CONNECTION AREA. BLENDED OUT CORROSION, FOUND TO BE WITHIN LIMITS. ELECTRICAL BONDING TEST GOOD.

Part: SKIN — DENTED (PAX DOOR) · airframe 24,370 hrs · 18,596 cycles

PAX DOOR HAS PETRUDING DENT BELOW HANDLE. CUT OUT DAMAGE, FABRICATED, ALODINED, PRIMED AND PAINTED DOUBLER AND FILLERS. INSTALLED DOUBLER AND FILLER.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,137 hrs · 16,840 cycles

DURING SCHEDULED MX INSPECTION, BOTH EXTERNAL OVERWING EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE. MX R & R EMERGENCY EXIT BATTERY POWER SUPPLY IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 20,862 hrs · 15,558 cycles

DIVERTED INTO TYS FOR A OVERTEMP BATTERY AND MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD AND WAS RELEASED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 20,362 hrs · 15,484 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. RIC MX REMOVED AND REPLACED NR 4 EMERGENCY BATTERY POWER SUPPLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 20,190 hrs · 15,366 cycles

DURING ROUTINE MX, THE EMERGENCY ISLE PATH LIGHTING WAS FOUND INOPERATIVE. MX REPLACED THE NR2 AND NR3 EMERGENCY LIGHT BATTERIES. OPS CHECKS WERE GOOD.

Part: FAN — SHORTED (E&E BAY) · airframe 20,116 hrs · 15,307 cycles

EWR - FLIGHT 2931 BURNING SMELL IN COCKPIT. REMOVED AND REPLACED NR 2 RECIRCULATION FAN IN FORWARD AVIONICS IAW EMB 145 AMM 21-26-02. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHUNT — BURNED (APU) · airframe 19,297 hrs · 14,680 cycles

FLIGHT 2586 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL SMELL IN AIRCRAFT ON TAXI IN. IT WAS FOUND THAT THE BURNING SMELL WAS COMING FROM APU. EWR MX REMOVES AND REPLACED APU SHUNT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPPROVED TO RETURN TO SERVICE.

Part: SHUNT — OVERHEATED (APU) · airframe 19,277 hrs · 14,664 cycles

FLIGHT 2615, THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE AIRCRAFT DURING TAXI. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE ODOR TO BE COMING FROM THE APU. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE APU SHUNT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRATF WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (ZONE 100) · airframe 18,372 hrs · 13,959 cycles

IAH - FLIGHT 3097, THE CREW REPORTED A BATTERY 2 OVERTEMP INDICATION AT FL360. THE CREW FOLLOWED QRH AND TURNED OFF BATTERY TWO. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CHAFED (FUSELAGE) · airframe 18,136 hrs · 13,763 cycles

FUSELAGE SKIN IS CHAFED INSIDE RT PRE COOLER PYLON AREA PANEL 424DB. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EMB ETD 2010-145/04181.

Part: STRIP — CORRODED (WING) · airframe 18,136 hrs · 13,763 cycles

PANEL 193 AL HAS CORRODED BONDING STRIPS. REPAIRED BONDING STRIPS IAW EMB EC5750-013215 REV F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,136 hrs · 13,763 cycles

TYS - GALLEY CENTER OMEGA BEAM TOP CAP HAS CORROSION AT CARBON FIBER BEAM. REMOVED AND REPLACED GALLEY CENTER OMEGA BEAM TOP CAP.

Part: BATTERY — THERMAL RUNAWAY (NR 2) · airframe 16,242 hrs · 12,349 cycles

IAH - FLIGHT 2203, UPON LANDING THE CREW REPORTED A NUMBER TWO BATTERY OVER TEMP THERMAL RUNAWAY. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NUMBER TWO MAIN BATTERIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 15,822 hrs · 12,027 cycles

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

Part: LOCK — OUT OF ADJUST (PAX DOOR) · airframe 13,889 hrs · 10,644 cycles

FLT 522 - RDU - FLIGHT CREW REPORTED PAX DOOR HARD TO OPEN. MX FERRY FLIGHT TO TYS. MX ADJUSTED HANDLE LOCKING MECHANISM OPERATIONALLY CHECK SATISFACTORY AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE.

Part: ROD — LOOSE (SERVICE DOOR) · airframe 10,644 hrs · 13,889 cycles

FLT 0543 - MCI - FLIGHT CREW REPORTED SERVICE DOOR WILL NOT OPEN FROM INSIDE. MX SECURED LOOSE HARDWARE AT DOOR OPEN ROD. OPERATIONALLY CHECK SATISFACTORY AIRCRAFT RELEASED TO RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,095 hrs · 8,689 cycles

RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND FWD NR 1 EMERGENCY LIGHT INOP. AFTER TROUBLESHOOTING THE SYSTEM, IT WAS FOUND EMERGENCY LIGHT BATTERY POWER SUPPLY INOP. MX REMOVED AND REPLACED POWER SUPPLY NR 1. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 8,513 hrs · 6,661 cycles

SHV - DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 7,775 hrs · 6,064 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,750 hrs · 6,041 cycles

DURING ROUTINE MAINTENANCE THE EXTERNAL WING EMERGENCY AFT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY BATTERY CHARGER ASEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — INOPERATIVE (VERTICAL STAB) · airframe 7,182 hrs · 5,599 cycles

CLT - FLIGHT 3268, THE CREW REPORTED THE PITCH TRIM ONE INOP AND ASSOCIATED AUTO TRIM FAIL MESSAGES IN CRUISE FLIGHT, AND THE INABILITY TO USE PITCH TRIM WITH PRIMARY OR BACKUP TRIM. THE AIRCRAFT LANDED AT CLT WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 7,062 hrs · 5,512 cycles

SDF, DURING A SCHEDULED ROUTINE CHECK THE AFT FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER, OPERATIONAL CHECKED GOOD IAW EMB-145 MM 33-50-04.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 6,942 hrs · 5,418 cycles

CLE FLIGHT NR 2634 , THE CREW REPORTED BOTH AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 6,930 hrs · 5,410 cycles

IAH - THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED WINDSHIELD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,610 hrs · 5,175 cycles

SDF - FWD FRONT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT STRIP, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: TUBE — LOOSE (NR 1 ENGINE) · airframe 4,141 hrs · 3,268 cycles

TYS DURING CLIMBOUT THE CREW GOT A INDICATION THAT THE NR 1 ENG HAD A BLEED LEAK AND RETURNED TO THE BLOCK. MAINT FOUND A LOOSE BURST DETECT LINE ON THE LT LEADING EDGE. TIGHTENED IAW EMB135/145 MM 20-10-03. PERFORMED AIRBLEED OPS CHECK IAW 145 AMM 36-00-00-700-803A, PERFORMED ANTI-ICE TEST IAW EMB 145 AMM 30-00-00-700-802A, PERFORMED COOLING PACK TEST IAW EMB 145 MM 21-51-00-700-802A. ALL WORK WAS ACCOMPLISHED AND ALL CHECKS WERE POSITIVE AND WAS RELEASED FOR TEST FLIGHT AND TEST FLIGHT WAS GOOD. ALL RECORDED ON LOG PG 919465 AND 602 NR 743788 FOR CORRECTIVE ACTION. A/C WAS RELEASED FOR REVENUE SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,141 hrs · 3,268 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND UNDER THE CARGO DOOR PROTECTIVE PLATE. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-145 SRM 51-40-02 AND AMM-21-31-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,141 hrs · 3,268 cycles

TYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD CENTER DIGITAL PLATE AT THE FORWARD NUT PLATE HOLE. MAINTENANCE REPAIRED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-145 SRM 51-21-01 AND CMP-51-21 04/05/06.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,141 hrs · 3,268 cycles

TYS DURING A SCHEDULED 1C INSPECTION THE FWD AND AFT PAX DOOR THRESHOLD SUPPORT BRACKETS WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE THRESHOLD SUPPORT BRACKETS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,141 hrs · 3,268 cycles

TYS DURING A SCHEDULED 1C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 20. MAINT CUT OUT THE CORRODED AREA, FABBED A NEW FILLER, SHIM AND DOUBLER, INSTALLED. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.