N15986

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,357 hrs · 34,778 cycles

IAH - FLIGHT 4090, DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ABOVE THE FWD HANDSET WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE.

Part: SPAR — CRACKED (LT WING) · airframe 45,229 hrs · 34,669 cycles

TYS A/C WAS FOUND WITH THE LEFT WING SPAR CRACKED AT APPROXIMATELY RIB 9 AREA OF SPAR ONE UNDER THE FAIL SAFE STRAP AND LEAKING FUEL. MAINTENANCE REPAIRED THE L/H WING SPAR AT RIB 9 CRACKED WITH A PERMANENT REPAIR IAW ETD 2019-145-121498. ALL WORK WAS ACCOMPLISHED AND LEAK CHECKS GOOD AND RELEASED BACK TO SERVICE.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 15,127 hrs · 34,625 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND 3 SMALL DENTS BENEATH THE CAPTAINS SEAT ON FUSELAGE. MAINTENANCE RECONTOURED 2 OF THE DENTS AND PERFORMED A SMALL REPAIR ON THE UPPER DENY IAW ETD 2015-145-07 REVISION A. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT END OF THE CHECK.

Part: COOLING DUCT — DISCONNECTED (APU BAY) · airframe 44,957 hrs · 34,438 cycles

THE CREW REPORTED STRONG FUEL SMELL IN FLIGHT DECK IN CRUISE PRIOR TO DESLECTING LOW 2 TO EVEN OUT FUEL. MAINTENANCE INSPECTED AND REINSTALLED STARTER GENERATOR COOLING DUCT IN APU COMPARTMENT. RAN APU AND ENGINES AND NO FUEL SMELL WAS NOTED.

Part: RIB — CRACKED (RT WING) · airframe 44,745 hrs · 34,266 cycles

A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT WING AT RIB 21 CRACKED. MAINTENANCE REPAIRED THE AREA BY TRIMMING OUT THE CRACKED FLANGE, FABRICATED A DOUBLER AND SHIM IAW 145SRM 57-20-07 FIGURE 203. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED BATTERY, OPERATIONAL CHECK WAS SATISFACTORY IAW AMM 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,249 hrs · 29,958 cycles

THE CREW REPORTED THAT THE NR 3 & NR 4 EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHTS) · airframe 38,983 hrs · 29,743 cycles

THE CREW REPORTED THE EMERGENCY LIGHT ARMING ON AND OFF. OVERHEAD CABIN LIGHTS ALSO FLICKERING. MAINTENANCE INSPECTED AND REPLACED THE F/A CONTROL PANEL. OPS CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,386 hrs · 29,268 cycles

ACFT HAD A STRONG BURNING ODOR IN ACFT IN THE FLIGHT DECK AND CABIN. EMERGENCY DECLARED AIR RETURN. ODOR STARTED AFTER TAKEOFF. MAINTENANCE PLACED ON DMI, OPERATE IAW MEL 21-1-00-1, CAT C. PLACARD INSTALLED.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 36,804 hrs · 28,041 cycles

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

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 36,804 hrs · 28,041 cycles

DURING C-CHECK, THE SHEAR CLIP AT FRAME 65, STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04, FIGURE 215. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 36,804 hrs · 28,041 cycles

DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16L-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04, FIGURE 212. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 36,804 hrs · 28,041 cycles

DURING C-CHECK, THE SERVICE DOOR CENTER 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: FITTING — CRACKED (RT WING TE FLAP) · airframe 36,804 hrs · 28,041 cycles

DURING C-CHECK, THE RT OTBD FLAP INBD TORQUE BOX FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01696. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,938 hrs · 27,357 cycles

DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE MIDDLE CABIN CEILING EMERGENCY LIGHT TO BE OUT. MAINTENANCE R & R THE EXIT ROW LIGHT INVERTER, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 35,806 hrs · 27,261 cycles

DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY EXIT LOCATOR AT THE OVERWING EXIT CEILING PANEL WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE ACFT AND SECURED THE CONNECTOR ON THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — INOPERATIVE (NR 2) · airframe 35,205 hrs · 26,768 cycles

CREW REPORTED SMOKE IN CABIN, FOLLOWED BY A POP, THEN BURNING ODOR. ODOR AND SMOKE DISAPATED WHEN NR 2 PACK WAS DESELECTED. ACFT PERFORMED AN AIR RETURN WITHOUT INCIDENT. INSPECTED AND FOUND NR 2 PACK TO BE INOPERATIVE. NR 2 AIR CYCLE MACHINE WAS R & R WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (OVERWING) · airframe 34,213 hrs · 26,003 cycles

PILOT REPORTED THE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,032 hrs · 24,299 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN CEILING WAS INOPERATIVE. THE CREW RESET SYS AND OPS CHECKS WERE GOOD. THE ACFT RETURNED TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

SHEAR TIE CRACKED. R & R SHEAR TIE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

CRACK AT FITTING. REMOVED AND REPLACED FITTING.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

CORROSION BEYOND LIMITS ON RT FLOOR SUPPORT BETWEEN FRAMES 48 THRU 53. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (CENTER FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

CORROSION BEYOND LIMITS ON FRAME 16 LT OF LEFT OMEGA BEAM. REMOVED AND REPLACED CROSSBEAM.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

CORROSION BEYOND LIMITS ON SILL AROUND SCREW HOLE. REMOVED AND REPLACED SILL.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 31,912 hrs · 24,204 cycles

CORROSION BEYOND LIMITS ON RT FLOOR SILL FRAME 18. REMOVED AND REPLACED SILL.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

CORROSION BEYOND LIMITS AT FOUR NUT PLATES ON CENTER OMEGA BEAM. R & R CENTER STRAP.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,912 hrs · 24,204 cycles

RIGHT OMEGA BEAM ANGLES OVER-WING BOX CRACKED INBD AND OTBD SIDES OF FRAME 47. R & R OMEGA BEAM ANGLES, PN'S 140-04213-601, 603, 607,& 609.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,296 hrs · 23,708 cycles

DURING A-CHECK INSPECTION, THE FUSELAGE SKIN ADJACENT TO FR 75 STR 02R WAS FOUND TO BE CRACKED. MX INSTALLED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,958 hrs · 21,782 cycles

OVERHEAD EMERGENCY EXIT SIGN IN GALLEY INOPERATIVE. R & R EMERGENCY LIGHT NR 2 INVERTER. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,881 hrs · 21,686 cycles

THE CREW REPORTED AN EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS INOPERATIVE. MX INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 28,489 hrs · 21,438 cycles

DURING ROUTINE MX THE AFT EMERGENCY EXIT LIGHT AT SEAT 17 WAS INOPERATIVE. MX INSPECTED AND RESET THE EMERGENCY LIGHT SYS AND OPS CHECKS WERE GOOD.

Part: CONTROL PANEL — SMOKE (HYD SYSTEM) · airframe 27,835 hrs · 20,944 cycles

FLT 6161,ON GROUND, CREW REPORTED NR 2 HYDRAULIC PUMP SWITCH FAILED ASSOCIATED WITH SMOKE IN THE COCKPIT. MX REMOVED AND REPLACED HYDRAULIC CONTROL PANEL IAW AMM 20-10-10, OPS CHECKED SUCCESSFUL. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 27,184 hrs · 20,386 cycles

A/C N15986 FLIGHT NUMBER 2038 FROM EWR HAD GRINDING NOISE COMING FROM NOSE LANDING GEAR DURING TAXI, MINOR VARIATIONS IN STEERING, NOSE WHEEL OFF ABOUT 12 DEGREES FROM CENTER WHEN TILLER IS IN NEUTRAL POSITION. MAINTENANCE REMOVED NOSE LANDING GEAR ASSY AND RE-SHIMMED LANDING GEAR LEG THEN REPLACED NOSE LANDING GEAR ASSY IAW EMB-145 AMM 32-20-01. RE-CHECKED NOSE WHEEL ALIGNMENT IAW EMB-145 AMM 32-50-00, ALIGNMENT GOOD. PERFORMED OPERATIONAL CHECK AND TAXI CHECK IAW EMB-145 AMM 32-50-00, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,007 hrs · 20,263 cycles

SHV - DURING C-CK - FUSELAGE SKIN CRACKS AROUND RIVETS FR 77-79 STR 5R-9R. REPAIRED SKIN IAW EC5330-02434. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,007 hrs · 20,263 cycles

SHV - DURING C-CK - FUSELAGE SKIN CRACKS AROUND RIVETS FR 77-79 STR 5L-9L. REPAIRED SKIN IAW EC5330-02434. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,007 hrs · 20,263 cycles

SHV - DURING C-CK - LT OMEGA BEAM CORRODED AT FR 20. REMOVED AND REPLACED OMEGA BEAM IAW EC5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,007 hrs · 20,263 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSERVICEABLE (LANDING GEAR) · airframe 26,984 hrs · 20,247 cycles

AFTER EXTENDING THE GEAR THE CREW REPORTED A RIGHT MAIN GEAR RED POSITION INDICATION WITH THE GEAR SELECTOR IN THE DOWN POSITION. THE AIRCRAFT LANDED IN ICT WITHOUT INCIDENT WHERE UPON INSPECTION THE RIGHT MAIN LANDING GEAR DOWN-LOCK PROXIMITY SWITCH CONNECTOR WAS FOUND TO BE UNSERVICEABLE. THE AIRCRAFT WAS FLOWN UNDER A SPECIAL FLIGHT PERMIT TO IAH WHERE THE CONNECTOR WAS REPLACED, OPERATIONAL CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: CONTROL PANEL — CONTAMINATED (CABIN) · airframe 25,671 hrs · 19,247 cycles

FLIGHT 3081 - EWR - FLIGHT CREW REPORTED F/A EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED MOISTURE/WATER FROM F/A ENVIRONMENTAL CONTROL PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,090 hrs · 18,046 cycles

CLE FLT 2690 THE CREW REPORTED THE EXIT LIGHT IN THE CEILING WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BULBS AND OPERATIONAL CHECKS WERE GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 23,969 hrs · 17,961 cycles

FLIGHT 2571 - EWR - DURING CLIMB, FLIGHT CREW REPORTED NR 1 HYDRAULIC LOW QUANTITY MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT WITHOUT ANY INCIDENT. EWR MX SERVICED NR 1 HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SEALANT — DAMAGED (RT WING) · airframe 23,848 hrs · 17,866 cycles

IAH - FLIGHT 2012, THE CREW REPORTED A RT WING FUEL LEAK IN FLIGHT ON THE O/B SIDE OF THE O/B SPOILER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REPAIRED THE FILLET SEALANT AT RIB 5, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 23,001 hrs · 17,243 cycles

IAH - FLIGHT 2276, THE CREW REPORTED THAT THE MAIN PITCH TRIM FAILED DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT, (HSCU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 22,300 hrs · 16,702 cycles

FLIGHT 2150 - EWR - FLIGHT CREW REPORTED "AIR GROUND FAIL" MESSAGE ON EICAS WITH MULTIPLE STICK SHAKE AND PUSHER ACTUATIONS, ALSO SPS 1 FAIL, IC2 WOW INOP, SPOILER FAIL AND E2 IDLE STOP FAIL INDICATIONS. EWR MX REMOVED AND REPLACED NOSE WOW A/G PROX SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 22,185 hrs · 16,606 cycles

DURING C-CHECK. CENTER OMEGA BEAM HAS CORROSION BTW FR 20-23. REMOVED AND REPLACED CENTER OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 22,185 hrs · 16,606 cycles

DURING C-CHECK. CENTER OMEGA BEAM HAS CORROSION BTW FR 24-25. REPAIRED CENTER OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (LANDING GEAR) · airframe 20,934 hrs · 15,686 cycles

FLIGHT 2866 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE WHEN GEAR IS IN TRANSIT DOWN. EWR MX REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,238 hrs · 15,196 cycles

IAH - DURING MAINTENANCE INSPECTION THE SECOND AND THIRD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,287 hrs · 15,232 cycles

MCI - DURING MAINTENANCE INSPECTION THE SECOND AND THIRD AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: ACTUATOR — DEFECTIVE (NLG DOOR) · airframe 19,249 hrs · 14,527 cycles

FLIGHT 3053 - EWR - CREW REPORTED LANDING GEAR AIR/GRND WARNING MESSAGE DURING GEAR TRANSITION TO EXTEND. EWR MX REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATORS IAW EMB 145 AMM 32-30-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. THIS SDR WAS FILED FOR THE RIGHT HAND ACTUATOR. SDR C2XA08RI030 WAS FILED FOR THE LEFT HAND ACTUATOR.

Part: ACTUATOR — DEFECTIVE (NLG DOOR) · airframe 19,249 hrs · 14,527 cycles

FLIGHT 3053 - EWR - CREW REPORTED LANDING GEAR AIR/GRND WARNING MESSAGE DURING GEAR TRANSITION TO EXTEND. EWR MX REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATORS IAW EMB 145 AMM 32-30-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. THIS SDR WAS FILED FOR THE LEFT HAND ACTUATOR. SDR C2XA08RI031 WAS FILED FOR THE RIGHT HAND ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,342 hrs · 18,947 cycles

TYS - DURING ROUTINE MX THE EMERGENCY LIGHTS AT ROW 7 AND 12 INOP. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB 145 AMM 33-50-08, OPS CHECK GOOD. A/C WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 18,945 hrs · 14,314 cycles

TYS - DURING AN A-CHECK INSPECTION A CRACK IN THE UPPER LT WING SKIN FWD OF THE I/B SPOILER CENTER HINGE POINT. THE SKIN WAS INSPECTED AND PLACED ON DMI FOR 500FC WITH A REINSPECT EVERY 50FC IAW IC2008-145/00965. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — FAILED (NR 1 ENGINE) · airframe 17,575 hrs · 13,365 cycles

FLT 2497 CREW REPORTED ENGINE NR 1 UNCOMMANDED IN-FLIGHT SHUTDOWN ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX PERFORMED TROUBLESHOOTING AND DETERMINED ENGINE NR 1 NEEDS REMOVED AND REPLACED. 10-9-07 ENGINE WAS SENT TO ROLLS ROYCE FOR REPAIR. DURING ENGINE REPAIR, IT WAS FOUND THAT THE HCF FAILURE OF HPT1 BLADE, P/N 23076976, DUE TO VANE BURN THROUGH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,470 hrs · 13,286 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION BETWEEN FRAMES 23 & 25. MAINTENANCE REPAIRED DAMAGE AREA ON CENTER OMEGA BEAM AT FRAME 23 & 25 IAW EMB 145 SRM 53-00-10 FIG 203. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,470 hrs · 13,286 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM AT FRAME 60 WITH CORROSION AROUND NUT PLATE. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 60 AROUND NUT PLATE USING REPAIR PROCEDURES DESCRIBED ON THE EMB 145 SRM 53-21-10 ITEM 3 FIG 202 IAW EC 5320-01373 REV ORIG. AIRCRAFT APPROVED TO RETURN TO SERVICE.

Part: SHUTOFF VALVE — INOPERATIVE (BRAKES) · airframe 17,218 hrs · 13,099 cycles

FLT 2616 - EWR - CREW REPORTED INBOARD BRAKE FAIL MESSAGE ON EICAS IN FLIGHT. CREW DECLARED EMERGENCY, BUT ACFT LANDED WITHOUT ANY INCIDENTS. EWR MX REMOVED AND REPLACED INBOARD LEFT BRAKE SHUTOFF VALVE IAW EMB-145 AMM 32-41-05. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,265 hrs · 12,364 cycles

BNA - STRONG ODOR IN COCKPIT AT CRUISE. FOUND FORWARD ELECTRICAL COMPARTMENT FAN INOP IAW MEL 21-26-00, CATAGORY C, CONTROL 113884. VERIFIED NORMAL OPERATION OF ELECTRONIC COMPARTMENT VENTALATION SYSTEM. OPS CHECK GOOD.

Part: BLEED VALVE — STICKING (APU) · airframe 16,153 hrs · 12,276 cycles

CLE FLIGHT 2837 THE CREW REPORTED THE APU CAUSES A SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: FIREWALL — CRACKED (AFT APU) · airframe 12,581 hrs · 9,360 cycles

SHV-DURING C-CHECK CRACKS (2) AT RIVETS FWD SIDE OF APU FIEWALL RT SIDE PLUS UPPER RT SIDE. MAINTENANCE REPAIRED APU FIREWALL CRACK FWD SIDE R/H 3 OCLOCK POSITION IAW EC5330-01477 AND REPAIRED APU RIRE WALL AT UPPER R/H SIDE IAW EMB 145 SRM 53-32-13 AND IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE

Part: FIRE LOOP — DEFECTIVE (NR 2 ENGINE) · airframe 10,326 hrs · 7,595 cycles

NR 2 FIRE DET FAIL. REMOVED AND REPLACED ENG NR 2 FIRE LOOP, OPS CHECK GOOD.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

SHV-DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 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: SKIN — DAMAGED (VERTICAL STAB LE) · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK THE VERTICAL STABILIZER LEADING EDGE WAS FOUND TO HAVE COMPOSITE DAMAGE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 51-70-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK LEFT HAND FLOORBEAM AT FRAME 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 51-30-01 AND 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — SCRATCHED (CARGO DOOR) · airframe 7,926 hrs · 5,675 cycles

SHV DURING C-CHECK CARGO COMPARTMENT LT SILL LIFT AT FRAME 73 WAS FOUND TO HAVE SCRATCHES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK THE RIGHT INBOARD FLAP WAS FOUND TO HAVE DELAMINATION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 IC 20003-14512058. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

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

Part: RIB — GOUGED (NACELLE) · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK NUMBER TWO UPPER COWLING WAS FOUND TO HAVE A GOUGE AT THE AFT RIB. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED RIB IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK THE MAIN DOOR SILL WAS FOUND TO HAVE CORROSION AROUND NUT PLATES. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK THE AFT BUTTSTRAP BETWEEN FRAMES 16 AND 18 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 7,926 hrs · 5,675 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,926 hrs · 5,675 cycles

DURING C-CHECK THE LT HAND BUTTSTRAP BETWEEN FRAMES 14 AND 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01074. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH FLIGHT 2906 THE CREW REPORTED ON PREFLIGHT THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: LEVER — FAULTY (TE FLAPS)

CLE FLIGHT 3081 THE CREW REPORTED A LANDING GEAR AURAL WARNING INDICATION WHEN THE GEAR HANDLE WAS MOVED TO THE UP POSITION. MAINTENANCE REPLACED THE FLAP LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG)

IAH- FLIGHT 3809, L/G / AIR GROUND FAILED AT ROTATION. MAINTENANCE REMOVED AND REPLACED THE WOW PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (COCKPIT)

CLE FLIGHT 3265 THE CREW REPORTED THE FIRST OFFICERS, CONTROL YOKE IS CRACKED. MAINTENANCE REPLACED THE CONTROL YOKE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — SHORTED (COFFEMAKER)

ISP - FLT 1119 - THE CREW REPORTED A SMELL OF BURNING COFFEE AND RUBBER COMING FROM THE CABIN. THE AIRCRAFT LANDED AT ISP WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE GALLEY HOT JUGS ON MEL 25-60-02/3 CONTROL NR 264838, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE HOT JUG CONNECTOR, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)