N11127

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 3 · airframe 43,493 hrs · 26,557 cycles

MOUNTING PLATE FOR THE RA #2 AFT ANTENNA ON AFT FUSELAGE SEPARATING FROM FUSELAGE. CLEANED SKIN AND FOUND NO CORROSION ON FUSELAGE ONLY RA MOUNTING BRACKET. NO MATERIAL REMOVED. CRACKS FOUND AROUND RIVET HOLES. SUPPLIMENTAL INFORMATION: FOUND CORROSION OF FUSELAGE SKIN UNDER AFT #2 RA ANTENNA MOUNT DURING REMOVAL OF ANTENNA. REPAIRED FUSELAGE SKIN UNDER AFT #2 RA ANTENNA MOUNT IAW EO-EMB145-53-066-O.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 3 · airframe 43,493 hrs · 26,557 cycles

MOUNTING PLATE FOR RADIO ALTIMETER #2 FWD ANTENNA ON AFT FUSELAGE IS SEPARATING FROM THE AIRCRAFT. CORROSION FOUND BETWEEN MOUNTING PLATE AND SKIN OF FUSELAGE. NO CORROSION FOUND ON THE FUSELAGE ONLY MOUNTING PLATE. AFTER CLEANING CRACKS WERE FOUND ON THE FUSELAGE SPIDER WEBBING FROM THE RIVET HOLES, WITH LONGEST ONE BEING 0.3 INCHES IN LENGTH. SUPPLIMENTAL INFORMATION: REAR FUSELAGE LOWER SKIN CRACK AND CORROSION BETWEEN FR65-66 AND STR 21R-21L. REPAIRED LOWER SKIN BETWEEN FR65-66 AND STR 21R-21L IAW EO-EMB145-53-065-R1.

Part: ACCESS DOOR — CRACKED (EXTERNAL POWER) · airframe 41,817 hrs · 25,258 cycles

EXT POWER ACCESS DOOR IS CRACKED... REOMEVED AND REPLACED EXTERNAL POWER DOOR

Part: SUPPORT BRACKET — GOUGED (LT BLEED) · airframe 41,817 hrs · 25,258 cycles

L/H BLEED SYSTEM SUPPORT BRACKET IS GOUGED... REOMOVED AND REPLACED SUPPORT BRACKET...

Part: FLOOR SUPPORT — DAMAGED (FRAME 60) · airframe 41,817 hrs · 25,258 cycles

LAV L/H FLOOR SUPPORT ASSY AT FR 60 IS DAMAGED... REMOVED AND REPLACED DAMAGED SUPPORT...

Part: GUSSET — CORRODED (FRAMES 59-61) · airframe 41,817 hrs · 25,258 cycles

L/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET...

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 41,817 hrs · 25,258 cycles

LOWER CARGO ENTRY BEAM BETWEEN FR 65-68 IS CORRODED AROUND FASTNER HOLES... REMOVED AND REPLACED CARGO ENTRY BEAM...

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 41,817 hrs · 25,258 cycles

BAGGAGE DOOR HOLD OPEN ROD SUPPORT IS CRACKED ON FR 68... REMOVED AND REPLACED BAGGAGE DOOR HOLD OPEN ROD SUPPORT...

Part: DOOR FRAME — CRACKED (CARGO) · airframe 41,817 hrs · 25,258 cycles

BAGGAGE DOOR FRAME AFT EXT FLANGE IS CRACKED AT BOTTOM END... REPAIRED BAGGAGE DOOR IAW ETD2018-145-129196

Part: GUSSET — CORRODED (FRAMES 59-61) · airframe 41,817 hrs · 25,258 cycles

R/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET...

Part: PROFILE — BENT (FRAME 66) · airframe 41,817 hrs · 25,258 cycles

FWD "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE...

Part: PROFILE — BENT (FRAME 66) · airframe 41,817 hrs · 25,258 cycles

AFT "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE...

Part: STRUCTURE — CORRODED (FRAMES 18-19) · airframe 41,817 hrs · 25,258 cycles

AFT "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE

Part: STRUCTURE — CORRODED (FRAMES 18-19) · airframe 41,817 hrs · 25,258 cycles

FWD "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 41,179 hrs · 24,721 cycles

F/O DV WINDOW W/N CLOSE. ADJUSTED FO'S DV WINDOW AND PERFORMED OPS CHECK. OPS CHECK GOOD AND NO DEFECTS NOTED AT THIS TIME.

Part: SHUTOFF VALVE — LEAKING (NR 2 BLEED SYS) · airframe 39,355 hrs · 23,178 cycles

NR 2 BLEED LEAK EICAS MESSAGE. SECURED LEAK AT PRSOV VALVE, OPS CHECKED GOOD.

Part: CONTAINER — TORN (LIFE VEST) · airframe 39,314 hrs · 23,137 cycles

CAPTAIN`S LIFE VEST POUCH TORN. R & R THE LIFE VEST.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 39,314 hrs · 23,137 cycles

FIRST OFFICER`S FLASHLIGHT WAS INOPERATIVE. R & R THE FLASHLIGHT. OPS CHECKED GOOD.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 37,880 hrs · 21,904 cycles

OIL PRESSURE WENT INTO RED ON FINAL APPROACH. OIL ON NR 1 COWLING. R & R NR 1 ENGINE GENERATOR IAW AMM 24-31-01 AND CORRESPONDING CARBON SEAL WAS R & R IAW MM 72-63-10. NO LEAKS NOTED AT THIS TIME. OPS CHECKED GOOD.

Part: SKIN — DENTED (FRAMES 23-24) · airframe 36,846 hrs · 21,031 cycles

DENT IN ACFT SKIN FORWARD OF SERVICE DOOR AT FRAME 18, STR 11R AND AFT OF SERVICE DOOR BETWEEN FRAMES 23, 24 AND STR 12R, 13R. CUTOUT THE CREASES, FABRICATED AND INSTALLED FILLER AND EXTERNAL DOUBLER IAW EC5320-02092.

Part: ACM — SMOKE (NR 1) · airframe 36,670 hrs · 20,904 cycles

SMOKE WAS REPORTED IN COCKPIT. ACFT RETURNED TO GATE AND NR 1 PACK WAS PLACED ON MEL. MAINTENANCE R & R NR 1 ACM WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 34,386 hrs · 19,345 cycles

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

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,106 hrs · 18,525 cycles

THE CREW REPORTED A STRONG OIL AND DIRTY PACK ODORS IN THE COCKPIT DURING DESCENT AND LANDING. LANDED WITHOUT INCIDENT, MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,996 hrs · 15,934 cycles

DURING C-CHECK CENTER OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR OF CENTER OMEGA BEAM AT FRAME 59 IAW SRM 51-40-02 AND EC5310-01473. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,996 hrs · 15,934 cycles

DURING C-CHECK RT OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR AND INSTALLED DOUBLER REPAIR AT RT OMEGA BEAM AT FRAME 60 IAW SRM 51-40-02 AND EC 5310-01473, REV ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 28,996 hrs · 15,934 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,813 hrs · 15,828 cycles

DURING MX INSPECTION, THE EMERGENCY EXIT LIGHT AT SEAT 2B WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK WITH OPS CHECKS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (RIGHT) · airframe 28,392 hrs · 15,548 cycles

THE CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH SMOKE IN THE CABIN SEEMING TO COME FROM THE LIGHTS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE NR 2 ENGINE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AUDIO PANEL — FAILED (ZONE 200) · airframe 25,494 hrs · 13,723 cycles

POST-FLIGHT CREW REPORTED CAPTAINS AUDIO PANEL INOPERATIVE AND THEN POPPED CIRCUIT BREAKER WITH ELECTRICAL ODOR IN COCKPIT. MX PERFORMED GVI AT CAPTAINS AUDIO PANEL WIRING AND R & R CAPTAINS DIGITAL AUDIO PANEL WITH OPS CHECK SUCCESSFUL AND NO FURTHER ELECTRICAL ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — FAILED (RECIRCULATION) · airframe 25,257 hrs · 13,590 cycles

DURING DESCENT THE CREW REPORTED SMOKE IN THE COCKPIT AND DECLARED AN EMERGENCY LANDING, WITHOUT INCIDENT. UPON INSPECTION, MX DETERMINED THE SOURCE OF SMOKE TO BE THE COCKPIT RECIRCULATION FAN. THE FAN WAS REPLACED, OPS CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 25,194 hrs · 13,554 cycles

DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION WARNING HOWEVER NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT DIVERTED TO ICT AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. THE AIRCRAFT WAS FLOWN UNDER A FERRY PERMIT TO IAH WHERE THE NR 2 ENGINE WAS REPLACED, OPERATIONAL CHECKS PERFORMED AND THE DISCREPANCY CLEARED. ***SDR FILED OPEN PENDING ENGINE TEARDOWN REPORT***

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,015 hrs · 12,839 cycles

SHV - DURING C-CK - LT SKIN HAS CRACKS AROUND 4 RIVETS. REPAIRED SKIN IAW EC5330-02432. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 23,917 hrs · 12,780 cycles

TYS - A/C EN ROUTE FROM CLT TO IAH WHEN SMOKE WAS SEEN IN THE CABIN, CREW RETURN TO CLT WITHOUT INCIDENT OR INJURY. MAINTENANCE RAN A/C ON THE GROUND PER FIM 21-20-00-810-803-A. NO SMOKE OR FUMES DETECTED. OPS CHECK WAS GOOD AND WAS RELEASED BACK TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 23,912 hrs · 12,779 cycles

SMOKE IN CABIN DURING CLIMBOUT. AIR RETURN. C/W FIM TASK CARDS. NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 23,900 hrs · 12,772 cycles

FLIGHT 2143 - GSP - FLIGHT CREW REPORTED THAT APPEARED TO BE A LEAK OF FUEL ON LEFT WING, CONFIRMED BY TOWER IN FLT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT WING FLAPPER VALVE AT NACA VENT AND PERFORMED OPERATIONAL CHECK SUCCESSFUULY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 20,160 hrs · 10,740 cycles

IAH - FLIGHT 2878, THE CREW REPORTED COMING OUT OF PIT THAT THE GEAR WOULD NOT RETRACT WHEN COMMANDED, AND RECEIVED EICAS WARNING LG/LEVER DISAGREE. THE GEAR EVENTUALLY RAISED AND THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EXTENSION/RETRACTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL LINE — LEAKING (APU) · airframe 19,558 hrs · 10,427 cycles

IAH - FLIGHT 2337, THE CREW REPORTED, SMELLED FUEL AFTER T/O WITH THE APU RUNNING BLEEDS AND AGAIN AFTER STARTING THE APU UPON PARKING AT IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL LINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (SPOILER) · airframe 19,361 hrs · 10,327 cycles

FLIGHT 2484 - EWR - FLIGHT CREW REPORTED SPOILER FAILURE INDICATION ON EICAS DURING LANDING. CREW ABORTED APPROACH. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT INBOARD SPOILER PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,172 hrs · 10,220 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — WORN (ZONE 200) · airframe 19,172 hrs · 10,220 cycles

SHV - DURING C-CHECK SMOKING RIVETS AT LT FRAME 78. MAINTENANCE PERFORMED REPAIR ON FRAME 78 STRINGER 6L IAW EC5330-02011. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,172 hrs · 10,220 cycles

SHV - DURING C-CHECK RT FRAME 78 HAS VISUAL EVIDENCE OF CRACKS AROUND RIVETS. MAINTENANCE PERFORMED REPAIR ON RT FRAME 78 STRINGER 6R IAW EC5330-02011. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (ZONE 100) · airframe 19,172 hrs · 10,220 cycles

SHV - DURING C-CHECK CARGO DOOR FWD TRIANGLE BRACKET IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE BLENDED AND EVALUATED THE CORROSION ON THE CARGO DOOR FWD TRIANGLE BRACKET IAW EC5320-01479 REV ORIG. CORRODED AREAS FOUND TO BE WITHIN LIMITS WITH .006 MATERIAL LOSS. PREPPED, PRIMED AND PAINTED IAW EMB-145 XR CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (LAV WASTE) · airframe 19,172 hrs · 10,220 cycles

SHV - DURING C-CHECK, TOILET WASTE DRAIN VALVE CORRODED. REMOVED AND REPLACED TOILET WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,143 hrs · 10,201 cycles

FLIGHT 2353 - YQM - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CREW DOWN POWERED ACFT AND MESSAGE DISAPPEAR. ACFT RETURNED TO SERVICE.

Part: DUCT — DEFECTIVE (PRECOOLER) · airframe 17,755 hrs · 9,466 cycles

FLIGHT 2753 - EWR - FLIGHT CREW REPORTED BLEED OVERTEMP - PACK NR 2 OVERHEAT ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX REMOVED AND REPLACED PRE-COOLER DUCT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,527 hrs · 7,743 cycles

CLE FLIGHT2252 - THE CREW REPORTED CABIN CEILING EMERGENCY LIGHT WAS INOPERATIVE AT THE OVERWING EMERGENCY EXIT. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FITTING — WORN (RT AILERON) · airframe 14,262 hrs · 7,611 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC 5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL SYS — LEAKING (APU) · airframe 11,104 hrs · 5,977 cycles

IAH - FLIGHT 2097, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WITH THE APU ON. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 -C- 116102. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 02/19/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL NOZZLE — UNKNOWN (APU) · airframe 11,080 hrs · 5,965 cycles

IAH - FLIGHT 2041, THE CREW REPORTED A FUEL SMELL IN THE CABIN ON START. MAINTENANCE PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 2891 WHERE MAINTENANCE REMOVED AND REPLACED THE APU FUEL NOZZLES, OPERATIONALLY CHECKED WITH NO DEFECTS. THE MEL WAS REMOVED, AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,036 hrs · 5,936 cycles

EWR LOG SQUAWK FLT NR 2323, STRONG FUEL ODOR ON TAKEOFF ROLL THROUGH 600 FT. INSPECTED AFT COWLING AND FOUND VERY SMALL AMOUNT OF RESIDUAL FUEL AND STRONG SMELL OF FUEL, MEL'D APU IAW MEL 49-00-00. LATER REMOVED AND REPLACED ANTI SURGE VALVE IAW EMB145 MM 49-55-01. OPS CHECK GOOD. ODOR STILL PRESENT. APU REMAINS ON MEL.

Part: BLEED VALVE — FAULTY (APU) · airframe 10,904 hrs · 5,866 cycles

EWR LOG SQUAWK STRONG FUEL ODOR IN COCKPIT DURING TAKEOFF. FOUND WINDSHIELD HEAT NR 2 CONTROLLER POWER TERMINALS MELTED. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER NR 2 IAW EMB145 AMM 30-42-01 AND REPAIRED WIRE TERMINAL TO CONTROLLER IAW EMB145 AMM 20-21-00. OPS CHECK GOOD. *S/D* IAH FLIGHT 2940 THE CREW REPORTED FUEL SMELL ON TAKEOFF GOES AWAY WHEN ENGINE BLEEDS ARE SELECTED AND APU BLEED CLOSED. CLE MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 10,612 hrs · 5,714 cycles

EWR LOG SQUAWK ON LANDING CABIN FILLED WITH SMOKE, GRAY IN COLOR SMELLED LIKE BURNED RUBBER. INSPECTED BOTH ENGINES AND APU FOR SIGNS OF LEAKAGE. CHECKED OIL SERVICE. INSPECTED CABIN FOR SIGNS OF ELECTRICAL SMOKE. NO DEFECTS NOTED. RAN BOTH ENGINES, BOTH PACKS AND APU AT VARIOUS SETTINGS/CONFIGURATIONS. NO SMOKE NOTED ON RUNUP. REF EMB145XR MM 72-00-00 AND 21-20-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,434 hrs · 5,091 cycles

DURING A CURRENT 2C INSPECTION THE FWD EMERGENCY LIGHT ABOVE THE CLOSET ENTRANCE WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECK GOOD AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,434 hrs · 5,091 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM UNDER CABIN FIBER BEAM AT FR19 TO 21. MAINTENANCE CUT OUT THE CORRODED AREA, FABRICATED DOUBLER, PERFORMED DOUBLER REPAIR ON FR19 TP 20. ALODINED PRIMED IAW EMB 145XR-SRM-53-00-10.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 7,490 hrs · 4,070 cycles

IAH - DURING PREFLIGHT INSPECTION THE FORWARD EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 6,101 hrs · 3,319 cycles

DURING "A" CHECK INSP, GALLEY OVERHEAD EMERGENCY EXIT LIGHT FOUND TO BE INOPERATIVE. MX R & R AFFECTED LIGHT BULB. OPS CHECKED WITH NO DEFECTS NOTED. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,846 hrs · 2,638 cycles

DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED AND REPLACED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (MAINS)

DURING TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR LEVER WITH SATISFACTORY RESULTS AND CONTINUED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS FOR THE EXTENSION/RETRACTION SYSTEM IAW EMB-145 AMM 32-30-00 WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1)

CLE FLIGHT NR 2843 THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.