N12924

Part: PACKING — TORN (NR 1 ENGINE) · airframe 36,263 hrs · 28,141 cycles

THE CREW REPORTED THAT THE ACFT HAD A VERY STRONG ODOR ASSOCIATED WITH THE PACKS. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, R & R THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAMES 77-78) · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 4 FASTENERS BETWEEN FRAMES 77-78, STRINGERS 3L-4L. MAINTENANCE PERFORMED 4 BUSHING REPAIRS TO THE SKIN IAW EC5330-03018. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-00-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (MAIN PAX DOOR) · corrosion level 2 · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK THE MAIN CABIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01348. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAMES 78-79) · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 3 FASTENERS BETWEEN FRAMES 78-79, STRINGERS 2R-5R. MAINTENANCE PERFORMED 3 BUSHING REPAIRS TO THE SKIN IAW EC 5330-03018. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-02044. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CANNING (FRAME 81) · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK THE APU FIREWALL AT FRAME 81 WAS FOUND TO BE OIL-CANNING BY THE LT SIDE STIFFENER BELOW THE BLEED DUCT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 36,227 hrs · 28,112 cycles

DURING C-CHECK THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03019. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,928 hrs · 24,817 cycles

DURING MX INSPECTION THE AISLE FLOOR EMERGENCY LIGHT AT ROW 16 WAS DISCOVERED INOPERATIVE. MX R & R LIGHT, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 31,498 hrs · 24,488 cycles

CREW REPORTED SMOKE IN COCKPIT AND CABIN IN FLIGHT. MX PERFORMED ABNORMAL SMOKE INSPECTION OF CABIN & COCKPIT AND FOUND NR 1 ACM DAMAGED. R & R NR 1 ACM WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER BEARING — LEAKING (ZONE 600) · airframe 31,365 hrs · 24,384 cycles

DURING CLIMB, THE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO AIRPORT WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE OTBD FLAPPER VALVE IN THE RT WING AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 29,677 hrs · 23,036 cycles

DURING ROUTINE MX, AFT ASILE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE BATTERY POWER SUPPLY CHARGER. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,583 hrs · 22,961 cycles

DURING ROUTINE MX, THE REAR INTERIOR AND EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,421 hrs · 22,829 cycles

DURING MX INSPECTION, FOUND NR 4 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. MX R & R NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,185 hrs · 22,646 cycles

DURING MX INSPECTION, THE LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 BATTERY CHARGING TRAY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 26,163 hrs · 20,244 cycles

FLIGHT 5790 - ORF - FLIGHT CREW REPORTED PRESSURIZATION FAIL IN AUTO AND MANUAL MODE. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT DUPLICATE FAIL. MX REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 26,162 hrs · 20,243 cycles

FLIGHT 6165 - IAD - FLIGHT CREW REPORTED AUTO PRESS ERRACTIC. IAD MX MEL`ED THE SYSTEM. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT DUPLICATE FAIL. MX REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (SDR # C2XA11RI090)

Part: FLOW DIVIDER — LEAKING (APU FUEL) · airframe 26,058 hrs · 20,153 cycles

FLIGHT 2557 FROM IND THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT DURING TAKEOFF. THE AIRCRAFT CONTINUED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE APU FLOW DIVIDER, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DETERIORATED (BLEED AIR SYS) · airframe 23,858 hrs · 18,196 cycles

THE CREW REPORTED A "BLEED 1 LEAK" MESSAGE ON CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT O-RINGS AT JOINT 17 AND 25 OF THE BLEED SYSTEM. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,248 hrs · 17,626 cycles

TYS - EMERGENCY LIGHT ABOVE RT PACK PANEL INOP. REMOVED AND REPLACED BULB.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,077 hrs · 17,510 cycles

FLIGHT 3073 - EWR - FLIGHT CREW REPORTED STRONG SMELL NOTICEABLE IN PAST HALF OF ACFT CABIN. EWR MX PERFORMED OPERATIONAL CHECK OF THE PACKS AND PERFORMED CABIN CONTAMINATION TROUBLESHOOTING CHART SUCCESSFULLY - NO SMELL NOTED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 21,992 hrs · 16,683 cycles

FRM 75 UPPER FITTING HAS OVERSIZED HOLE ON RT O/B HOLE. REMOVED, REPAIRED AND INSTALLED FITTING IAW EC5530-01187, EMB 145 SRM 51-40-02 AND EC5310-01317.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 21,992 hrs · 16,683 cycles

FRETTING AT FRM 75 STR 1R AT FUSELAGE TO STAB ATTACH BRACKET AS MARKED. REMOVED FITTING AT FRM 75, BLENDED CORROSION, PERFORMED DYE-PEN, REPAIRED FITTING AND INSTALLED IAW EC5310-01480, EMB 145 SRM 51-40-02 AND EC5310-01317.

Part: STRUCTURE — CORRODED (NR 2 INLET) · airframe 21,992 hrs · 16,683 cycles

TYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION IN TWO HOLES ON THE NR 2 ENGINE INLET. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHINGS TO REMOVE THE CORROSION. ALL WORK WAS ACCOMPLISHED IAW EC5420-01158 AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: TUBE — LEAKING (BLEED AIR SYS) · airframe 21,965 hrs · 16,664 cycles

FLIGHT CREW REPORTED ENGINE BLEED NR 2 LEAK AFTER TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 BLEED SYSTEM TUBE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: O-RING — BLOWN (BLEED AIR SYS) · airframe 21,687 hrs · 16,440 cycles

IAH - FLIGHT 2695, THE CREW REPORTED A BLD 2 LK INDICATION ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BLEED DUCT O-RINGS UNDER THE CARGO FLOOR. OPERATIONAL AND LEAK CHECKS PERFORMED SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AHRS — INOPERATIVE (NR 1) · airframe 21,046 hrs · 15,945 cycles

IAH - FLIGHT 2027, THE CREW REPORTED AN AHRS1 FAIL / ATT FAIL 1, AND SPS ADVANCE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ONE AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 17,934 hrs · 13,789 cycles

CLE FLIGHT 2793 - THE CREW REPORTED MULTIPLE WARNINGS DURING CLIMB E1 FUEL LO LEVEL, AMBER DASHES ON FUEL TOTAL + TANK 2 FUEL LEVELS, RMU NR 2 BLANK, APU SHUTOFF VALVE CLOSED, AURAL WARNING FLAP FAIL, AUTO PILOT FAIL. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. ON GROUND, RECEIVED ESS BUS 2 FAIL, STICK SHAKER, AND GUSTLOCK FAIL. MAINTENANCE INSPECTED AND REPLACED CONTACTOR RELAYS KOO80 AND K0016. OPERATIONAL CHECKS OF THE DC DISTRIBUTION WERE GOOD. KO016 P/N 464CC01.

Part: LANDING GEAR — MALFUNCTIONED · airframe 17,474 hrs · 13,489 cycles

FLIGHT 2412 - DGO - IAH, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO DGO AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE LANDING GEAR EXTENSION AND RETRACTION TESTS WERE PERFORMED. THE GEAR RETRACTED AND EXTENDED NORMALLY DURING THE SYSTEM TESTS AND THE DISCREPANCY WAS CLEARED.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,225 hrs · 11,813 cycles

FLT NR 2312 - SMELLED BURNING ODOR 20 MINUTES AND 5 MINUTES BEFORE LANDING. NO SMOKE OBSERVED. FLT ATTENDANT SMELLED IT FIRST IN FWD CABIN. INSP COCKPIT AREA OVERHEAD PANELS, SIDE WALL PANELS UNDER COCKPIT FOORS RAN BOTH ENGINES AT MAX POWER WITH ENGINE BLEEDS ON. INSP LEFT/RIGHT RELAY SUPPORTS AND LEFT/RIGHT WINDSHIELD HEAT CONTROLLERS AND LEFT/RIGHT DISTRIBUTION CONTACTERS BELOW FLIGHT ATTENDANT SEAT. NO FAULT FOUND.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 13,331 hrs · 10,319 cycles

STL - DURING MAINTENANCE INSPECTION BOTH OVERWING EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 9,024 hrs · 7,146 cycles

IAH - FLIGHT 2732, A BURNING SMELL WAS NOTICED IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED TWO LIGHT BALLASTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: STRIP — INOPERATIVE (CABIN) · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE NR 4 AND NR 5 EMERGENCY PROXIMITY AISLE LIGHTS WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 5 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. MAINTENANCE OPERATIONALLY CHECKED ALL LIGHT STRIPS AND WERE FOUND TO BE GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE LEFT HAND RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAME 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 15. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR EMB IC2003-145/4250. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK THE MAIN PASSENGER DOOR SILL SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR SILL SUPPORT IAW EMB 145 IPC 53-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,663 hrs · 5,843 cycles

SHV- DURUNG C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 7,663 hrs · 5,843 cycles

SHV- DURING C-CHECK STRINGER 19L T-REINFORCEMENT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TEE FITTING — GOUGED (LONGERON) · airframe 7,663 hrs · 8,543 cycles

DURING C-CHECK THE TEE REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,833 hrs · 5,871 cycles

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

Part: LAMP — FAULTY

BTV--CO2002, DURING 3A INSPECTION MAINTENANCE FOUND EMERGENCY EXIT LIGHT OVER RIGHTHAND ESCAPE HATCH (WING) TO BE INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AS NECESSARY IAW EMB145 AMM #33-50-07. OPS.CHECKED GOOD.

Part: CHARGER — OPEN (CABIN AREA) · airframe 5,806 hrs · 4,351 cycles

CLE---COCO2351, CREW REPORTED, EMERGENCY EXIT DOOR SIGN LIGHT INOPERATIVE. MAINTENANCE REALIGNED PIN ON CHARGER BASE. OPS.CHECKED GOOD IAW EMB145 AMM #33-50-00. AIRCRAFT RETURNED TO SERVICE.