N13978

Part: ACM — FAILED (NR 2) · airframe 46,309 hrs · 35,117 cycles

FLIGHT 4390 THE CREW REPORTED THAT A BANG WAS HEARD BY A PASSENGER NEAR ROW 8-9 AND THE CABIN FILLED WITH A FOG TYPE OF SMOKE THAT NEVER REACHED THE COCKPIT. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO (#2) ACM AND ACM EXHAUST DUCT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — DENTED (FUSELAGE) · airframe 44,787 hrs · 34,207 cycles

BETWEEN FRAME 23 AND 24 STRINGER 19R AND 20R DENTED. REMOVED AND REPLACED A SECTION OF STRINGER 19R AT FRAME 23 TO 25. AIRCRAFT STILL IN C CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,014 hrs · 34,079 cycles

FOUND THE FLOOR LIGHTS AT ROWS 7 THRU 18, AND ALL EXIT SIGNS AT ROW 18 WERE OUT. MAINTENANCE R & R THE EMERGENCY BATTERY NR 3 IAW 33-50-04. R & R THE NR 5 INVERTER IAW 33-50-11. OPS CHECK GOOD AND WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 45,006 hrs · 34,072 cycles

A/C WAS IN FOR AN A-CHECK WHEN INSPECTION FOUND THE EXIT ROW EMERGENCY LIGHT PROXIMITY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #3 LIGHT BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD AND WAS RELEASED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,869 hrs · 33,962 cycles

DURING MX INSPECTION THE FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT 8A THROUGH 11A WAS INOP. MX REMOVED AND REPLACED THE NR 3 BATTERY PACK WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 44,631 hrs · 33,780 cycles

DURING MAINTENANCE INSPECTION, AN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,554 hrs · 33,721 cycles

EMERGENCY LIGHTS OVER THE DOORS WOULD NOT LIGHT UP. MX REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,515 hrs · 33,687 cycles

EMERGENCY LIGHT WAS REPORTED INOPERATIVE. MX REMOVED AND REPLACED THE BATTEYR PACK, OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,512 hrs · 32,877 cycles

PILOT REPORTED 3RD & 4TH EMERGENCY LIGHTS IN CABIN CEILING ARE INOP. MX REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY ASSY RELAMPED #3 & #4 ZONAL LAMPS WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (ROW 18D) · airframe 42,664 hrs · 32,188 cycles

PILOT REPORTED EMERGENCY ROW WINDOW LIGHT 18D INOPERATIVE. MX REMOVED AND REPLACED THE ROW SIGN AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — SHORTED (CABIN LIGHTS) · airframe 41,089 hrs · 30,952 cycles

PILOT REPORTED THE LAVATORY CIRCUIT BREAKER TRIPPED FOLLOWED BY ELECTRICAL ODOR. REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST AND OPS CHECKED GOOD. APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (ENGINE) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK. LT FWD LOWER ENGINE MOUNT CRACKED. REMOVED AND REPLACED ENGINE MOUNT IAW EC5450-01211. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK, LT MLG AFT TRUNNION CRACKED. REMOVED AND REPLACED THE TRUNNION IAW EC5750-01766. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK. FOUND THE FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. REPAIRED THE SKIN IAW EC5330-03120. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK. THE FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 75 STRINGER 2L. REPAIRED THE SKIN IAW EC5330-03119. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK, CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — SHORTED (CABIN LIGHTS) · airframe 40,574 hrs · 30,539 cycles

CREW REPORTED BURNING ODOR IN CABIN. MAINTENANCE PERFORMED GVI OF CABIN AND FOUND ODOR COMING FROM SEAT 1A OVERHEAD AREA. R & R LIGHT CONTROL MODULE UNIT WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (LEFT) · airframe 38,258 hrs · 28,677 cycles

THE CREW REPORTED THAT PACK 2 OVERLOADED MULTIPLE TIMES IN FLIGHT, THE PACK WAS DESELECTED IAW THE QRH AND THE COCKPIT AND CABIN FILLED WITH SMOKE AFTER 2 MINUTES. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND PLACED THE LT PACK ON MEL21-51-00-2 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT LANDED, WHERE MAINTENANCE R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRANSDUCER — FAULTY (WHEEL SPEED) · airframe 37,527 hrs · 28,102 cycles

PILOT REPORTED AN INTERMITTENT LOSS OF BRAKES ON LANDING WITH BRAKES DEGRADED EICAS MESSAGE. MX R & R NR 3 WHEEL SPEED TRANSDUCER WITH OPS CHECK GOOD. AC WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FRAMES 42-49) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK AFTER REMOVAL OF NR 3 RT WALL SEAT TRACK FOUND SUPPORT CORRODED BETWEEN FRAMES 42-49. MAINTENANCE REMOVED CORROSION ON RT WALL SEAT TRACK FOUND SUPPORT BETWEEN FRAMES 42-49, OUT OF LIMITS SRM 53-00-11. R & R SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FRAME 41-46) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, MULTIPLE AREAS OF CORROSION IN LT SIDEWALL SEAT TRACK FRAMES 41-46. MAINTENANCE REMOVED CORROSION ON LT SIDEWALL SEAT TRACK AND IS OUT OF LIMITS SRM 53-00-11. R & R SEAT TRACK IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, FOUND A CRACK IN UPPER AFT CORNER OF SUPPORT BRACKET FOR INTERNAL HANDLE ON PAX DOOR. MAINTENANCE REMOVED CRACKED PAX DOOR HANDLE SUPPORT BRACKET, LOCATED, DRILLED, ALODINED, AND INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-02, 51-20-03 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK CARGO DOOR CUTOUT STRUCTURE FWD FRAME LOWER CORNER CORRODED. MAINTENANCE R & R CORRODED SHEAR TIE AT CARGO DOOR FWD FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, CORROSION FOUND AROUND AFT TWO NUTPLATES ON INSIDE AND OUTSIDE OF PAX DOOR BOTTOM FRAME. MAINTENANCE R & R PAX DOOR BOTTOM AFT FRAME WITH NEW FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 36,276 hrs · 27,135 cycles

THE F/A REPORTED A BURNING ODOR IN THE CABIN ASSOCIATED WITH THE F/O'S SIDE FLOOR AND WALL LIGHTING FLICKERING. MAINTENANCE INSPECTED THE ACFT AND R & R THE AFFECTED WALL LIGHTS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 48-52) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 48 AND 52. MAINTENANCE REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 52-53) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 52 AND 53, WITH-IN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 36-41) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, MULTIPLE AREAS OF CORROSION ON LT SIDEWALL SEAT TRACK SUPPORT FROM FRAME 41-36. MAINTENANCE REMOVED CORROSION AND WAS FOUND OUT OF LIMITS SRM 53-00-11, R & R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 36-41) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, FOUND SEAT TRACK SUPPORT CORRODED BETWEEN FRAMES 36-41. REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (FRAME 81) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 11, RT END ANGLE IS CRACKED AT APU FIREWALL. MAINTENANCE R & R END ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (FRAME 81) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 10, RT END CLIP IS CRACKED AT APU FIREWALL. MAINTENANCE R & R FRAME 81, STRINGER 10, RT END CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, LT FLOOR SUPPORT BETWEEN FRAMES 18 AND 23 CHAFED AND CORRODED. MAINTENANCE REMOVED CORROSION IAW SRM 53-21-10. FOUND OUT OF LIMITS IAW SRM 53-21-10. REMOVED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — GOUGED (FR 61) · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK THE FRAME CHANNEL AT FRAME 61 BETWEEN STRINGERS 16L-17L WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED OUT THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01959. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

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

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 36,272 hrs · 27,131 cycles

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

Part: TRANSDUCER — FAULTY (BRAKE PRESSURE) · airframe 35,795 hrs · 26,785 cycles

PILOT REPORTED A BRAKE DEGRADED MESSAGE ON EICAS WHEN GEAR WAS LOWERED AND BRAKES FELT LESS EFFECTIVE AND UNEVEN ON LANDING. MAINTENANCE R & R THE NR 4 BRAKE PRESSURE TRANSDUCER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,476 hrs · 25,781 cycles

PILOT REPORTED A STRONG FUEL ODOR DURING TAKEOFF, WHILE APU POWERED THE PACKS. MAINTENANCE PERFORMED OPS CHECK, CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAILED (LEFT) · airframe 31,369 hrs · 23,364 cycles

REJECTED TAKEOFF DUE TO ENGINE NR 1 AUTO SHUTDOWN ON TAKEOFF ROLL. MX DETERMINED LOW N1 AND E1 EXCEEDANCE AND R & R NR 1 ENGINE IAW TASK CARD 6271001 WITH OPS AND LEAK CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NOSE GEAR) · airframe 29,456 hrs · 21,862 cycles

THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON ROTATION. MX INSPECTED AND PERFORMED FUNCTIONAL CHECKS OF THE PROXIMITY SWITCHES. REPLACED THE NOSE GEAR WOW PROXIMITY SWITCH. OPS CHECKED GOOD.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 29,386 hrs · 21,808 cycles

FLT 4394, THE CREW REPORTED AFTER TAKEOFF THEY RECEIVED AN AIR/ROUND FAIL MESSAGE AND WAS UNABLE TO RETRACT THE LANDING GEAR. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER AND THE LANDING GEAR ELECTRONIC UNIT. ALSO ADJUSTED THE RT GEAR PROXIMITY SWITCH. OPS CHECKED WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 29,187 hrs · 21,652 cycles

CLE FLT 5815 THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND WAS UNABLE TO RAISE GEAR ON DEPARTURE. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR WOW PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 28,947 hrs · 21,462 cycles

LG/AIR GROUND FAIL, HANDLE UNMOVABLE. REMOVED AND REPLACED LGEU IAW EMB 145 AMM 32-32-01. IPC REF 32-32-01 ITEM 1D. OPS CHECK GOOD AIRCRAFT RELEASE AND RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 28,914 hrs · 21,435 cycles

ORD FLT 6062 ON TAKEOFF CREW GOT AN AIR GROUND WARNING, AND THE GEAR WOULD NOT COME UP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 28,785 hrs · 21,341 cycles

MCI - FLIGHT 2437, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS WITH THE GEAR IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE APPROVED A FERRY FLIGHT TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (NR 1 WOW) · airframe 28,622 hrs · 21,210 cycles

ORD FLT 5872 THE CREW REPORTED JUST AFTER TAKEOFF RECEIVED A AIR/GROUND FAIL MESSAGE AND THE GEAR LEVER WOULD NOT GO UP. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTOR ON NR 1 WOW PROXIMITY SWITCH. TIGHTENED CONNECTOR AND OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 28,385 hrs · 21,018 cycles

IAH - FLIGHT 2873, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL EICAS MESSAGE AFTER TAKEOFF, AND THE GEAR HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED AITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ADC — INOPERATIVE (NR 2) · airframe 28,151 hrs · 20,854 cycles

MEM - FLIGHT 2725, THE CREW REPORTED AN ADC MISCOMPARE/LT-ENG, ADC/DATA SYS MESSAGES. THE AIRCRAFT DIVERTED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ADC COMPUTER, OPERATIONALLY TESTED BOTH THE NUMBER NR 1 AND NR 2 ADCS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MONITOR — DEFECTIVE (VIBRATION SYS) · airframe 27,916 hrs · 20,683 cycles

FLIGHT 6135 - RIC - FLIGHT CREW REPORTED E1 ABNORMAL VIBRATION, LP NR 1 LP INDICATION MAXED - NO VIBRATION FELT. CREW SHUT DOWN THE ENGINE AND PROCEED WITH EMERGENCY LANDING. ACFT LANDED UNEVENTFULLY. RIC MX REMOVED AND REPLACED VIBRATION MONITOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 27,347 hrs · 20,220 cycles

FLIGHT 2419 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL IN COCKPIT AND FORWARD CABIN WITH PACK NR 1 ON AND USING APU BLEED. EWR MX RUN APU AND PACK NR 1 BUT NO SMELL WAS DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRAKE ASSY — LOCKED (NR 1) · airframe 27,238 hrs · 20,147 cycles

GRB FLT 4912 THE CREW REPORTED THE NR 1 BRAKE LOCKED UP DURING TAXI AND THE MAIN WHEEL ASSEMBLY WENT FLAT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY AND MAIN WHEEL. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 60 HAS CORROSION (LEVEL 2 LOCAL) AS SEEN UNDERNEATH AT NUT PLATES. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAME 59-62 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK LT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED LT FRAME 10 BELOW DV WINDOW IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 58-60 NUT PLATE HOLES HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM BUTTSTRAP AT FRAME 58-61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK RT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED RT FRAME 10 BELOW DV WINDOW CUTOUT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON RT OMEGA BEAM AROUND NUT PLATE HOLE AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK BETWEEN FRAMES 51-52 STRINGER 19L. MAINTENANCE REMOVED AND REPLACED STRINGER BETWEEN FRAMES 51-52 STRINGER 19L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 59 HAS CORROSION (LEVEL 2 LOCAL) AS SEEN UNDERNEATH AT NUT PLATE. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAMES 59-62 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (SPEED BRAKE) · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK RT SPEED BRAKE I/B HINGE O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT SPEED BRAKE I/B HINGE FITTING IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK LT OMEGA BEAM "L" FLANGE AT FRAME 40-41 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM "L" FLANGE AT FRAME 40-41 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK RT GROUND SPOILER I/B BRACKET O/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REPLACED RT GROUND SPOILER I/B BRACKET IAW EMB-145 SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. TORQUED BOLTS TO 42 IN LBS IAW EMB-145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,616 hrs · 19,701 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAMES 17-23 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE HAS CORROSION (LEVEL 2 LOCAL) FR 35-36. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM LOWER FLANGE FRAME 35-36 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 26,072 hrs · 19,279 cycles

FLIGHT 2946 - JAX-EWR - FLIGHT CREW DIVERTED FLIGHT TO SAV DUE TO BLEED NR 2 LEAK IN FLIGHT. CREW LANDED ACFT UNEVENTFULLY. EWR MX PERFORMED INSPECTION AND FOUND LEAK AT TEMP CONTROL VALVE HARDWARE. MX REMOVED AND REPLACED HARDWARE (O-RING AND TIE WRAPS) AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SOCKET — BURNED (CABIN) · airframe 25,732 hrs · 19,028 cycles

FLIGHT 2614 - EWR - FLIGHT CREW REPORTED BURNING SMELL ABOVE SEAT 1A. EWR MX FOUND BURNED CEILING LIGHT SOCKET AT SEAT 6A. MX REMOVED AND REPLACED CEILING LIGHT ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — FAULTY (NR 3 BRAKE) · airframe 25,246 hrs · 18,664 cycles

CLE FLT 2883 THE CREW REPORTED A NR 3 BRAKE OVERHEAT MESSAGE DURING APPROACH. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 BRAKE ASSEMBLY AND BRAKE TEMP SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (BRAKE SYSTEM) · airframe 25,246 hrs · 18,664 cycles

BOS FLT 2883 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE DURING TAKEOFF. THE TAKEOFF WAS ABORTED. THE CREW RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD.

Part: BUSHING — WORN (LT AILERON)

ACFT CURRENTLY IN A C-CHECK STATUS WAS FOUND WITH THE LT AILERON PCA BRACKET WITH MIGRATING BUSHINGS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K)

Part: FITTING — WORN (RT AILERON)

RT AILERON PCA FITTING OTBD LUG (ON AILERON) MISSING HAT BUSHING. REMOVED AND REPLACED FITTING IAW EC5750-01177, REV B. AIRCRAFT CURRENTLY IN C-CHECK. (K)

Part: MOUNT — CORRODED (ENGINE)

AC CURRENTLY INA C-CHECK STATUS AND THE NR 2 ENGINE INLET MOUNTING FLANGE BOLT HOLES HAD SEVERAL HOLE`S THAT WERE FOUND CORRODED. MAINT REPAIRED THE INLET BOLTHOLES IAW EC5420-01161. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)

Part: CHECK VALVE — LEAKING (FUEL SYSTEM) · airframe 21,285 hrs · 15,750 cycles

IAH-FLIGHT 2350, THE CREW REPORTED A FUEL LEAK FROM THE RT HAND WING. THE AIRCRAFT LANDED AT ORD WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RT WING NACA INLET FLAPPER CHECK VALVE. LEAK CHECKED WITH NOT DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: ENGINE — LEAKING (NR 2) · airframe 20,320 hrs · 15,062 cycles

IAH - FLIGHT 2156 - AFTER TAKEOFF THE LAVATORY SMOKE INDICATOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE NR 2 ENGINE WAS FOUND TO BE THE SOURCE OF THE SMOKE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, PERFORMED GROUND RUNS AND CLEARED THE DISCREPANCY.

Part: ACM — MALFUNCTIONED (NR 2) · airframe 20,143 hrs · 14,945 cycles

FLIGHT 2985 - EWR - CREW REPORTED LAV SMOKE AND SMOKE IN THE CABIN DURING TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 ACM IAW EMB 145 AMM 21-51-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 20,083 hrs · 14,908 cycles

GSP - DURING CLIMB THE CREW HAD A LAV SMOKE INDICATION ON EICAS WITH VISIBLE SMOKE AND SMOKE SMELL. CREW AIR RETURNED TO GSP, MX PERFORMED HIGH POWER ENG RUNS FOR APPROXIMATELY 3 MINUTES AND COULD NOT DUPLICATE DISCREPANCY. A/C WAS RETURNED TO SERVICE.

Part: SKIN — PUNCTURED (FUESLAGE) · airframe 19,498 hrs · 14,509 cycles

DENT AND PUNCTURE UNDERNEATH SERVICE DOOR. REPAIRED DAMAGE TO AIRCRAFT IAW EC 5330-01752. PRESSURE CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,591 hrs · 13,843 cycles

FLT 2072, CREW REPORTED THAT FIRST ENG START HAD BEEN ABORTED DUE TO A HUNG START & A STRONG ODOR OF FUEL, ENGINE DRY MOTORED, & STARTED SUCCESSFULLY OFF OF FADEC B. ACFT LANDED WITHOUT INCIDENT. MX PLACED IGNITION SYSTEM ON MEL 74-20-00 CAT B CTL 125656, & ACFT APPROVED FOR RETURN TO SERVICE. 10-9-07 MX R & R "A" IGNITION EXCITER, OPERATIONALL CHECKED WITH NO DEFECTS, REMOVED MEL, & ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (ELEVATOR) · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE LEFT ELEVATOR UPPER SKIN WAS FOUND TO BE DENTED OUT OF LIMITS DUE TO LENGTH. EDDY CURRENT INSPECTION OF THE AREA REVEALED NO RELEVANT INDICATIONS. SUBMITTED TO ENGINEERING FOR DISPOSITION.

Part: SKIN — DENTED (PAX DOOR) · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE MAIN DOOR WAS FOUND TO BE DENTED FORWARD OF THE WINDOW. DENT WAS FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 52-10-01. EDDY CURRENT INSPECTION OF THE AREA REVEALED NO RELEVANT INDICATIONS. SUBMITTED TO ENGINEERING FOR DISPOSITION.

Part: CASE — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE NUMBER 2 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSTION.

Part: CASE — CORRODED (ZONE 400) · corrosion level 2 · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE NR 1 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSITION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED FROM FR 23-30. AN AREA AT FR 24 WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-00-10 AND EC 5330-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,852 hrs · 12,523 cycles

SHV - DURING C-CHECK THE LEFT OMGEA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FR 23-30. DAMAGE AT FR 24 WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 AND EC 53-00-10, FIG 202 SHT 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — BURNED (FUSELAGE) · airframe 16,785 hrs · 12,469 cycles

THE CREW REPORTED SMOKE COMING FROM LIGHT ASSEMBLY ABOVE SEAT 1A. MAINTENANCE INSPECTED AND REPLACED SEAT 1A LIGHT BRACKET AND HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,429 hrs · 10,634 cycles

MCI - DURING MAINTENANCE INSPECTION, THE RT WING FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,408 hrs · 10,621 cycles

DURING ROUTINE MAINTENANCE THE EXTERIOR RIGHT OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPAIRED WIRE W102-8500-22. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 14,198 hrs · 10,456 cycles

SHV - RON AIRCRAFT GOUGE IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L. MAINTENANCE REPAIRED GOUGES IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L IAW EMB 145 SRM 53-21-01 & IC 2005-145/4770. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,067 hrs · 10,348 cycles

MCI - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT MARKER AT ROW 12BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,084 hrs · 8,855 cycles

DURING C CHECK, THE LEFT OMEGA BEAM SPLICE WAS CORRODED AND CRACKED BETWEEN FRAMES 23 AND 24. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01179. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,084 hrs · 8,855 cycles

DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

THE CREW NOTED DURING PREFLIGHT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE PLACED FLOOR LIGHTING ON DMIDO TO PARTS NOT IN STOCK.THE AIRCRAFT WAS RETURNED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AFTER THE DMI WAS CLEARED.

Part: SKIN — SCRATCHED (PAX DOOR) · airframe 7,863 hrs · 5,527 cycles

SHV - DURING C-CHECK THE PASSENGER DOOR WAS FOUND TO HAVE SEVERAL SCRATCHES ON SKIN. MAINTENANCE REMOVED DAMAGED AREAS AND REPAIRED AFFECTED SECTIONS IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED · airframe 7,863 hrs · 5,527 cycles

SHV DURING C CHECK THE PASSENGER DOOR WAS FOUND TO HAVE A DENT JUST FOWARD OF DOOR'S WINDOW. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — GOUGED · airframe 7,863 hrs · 5,527 cycles

SHV DURING C CHECK FUSELAGE SKIN WAS FOUND GOUGED JUST AFT OF LOWER AFT CORNER OF SERVICE DOOR CUT OUT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01209. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 7,863 hrs · 5,527 cycles

SHV - DURING C-CHECK HOLES ON FRAME 15 WHERE COCKPIT TO CABIN LEFT FORWARD PORTION ATTACHES WERE FOUND ELONGATED. MAINTENANCE REPAIRED ELONGATED HOLES IAW CONTINENTAL EXPRESS EC 5340-01050. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED · airframe 7,863 hrs · 5,527 cycles

SHV-DURING C CHECK THE T REINFORCEMENT ON STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND REPLACED AFFECTED RAMP ANGLE. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (NR 2 COWLING) · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK NUMBER TWO LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND PLACED AFFECTED EDGE MEMBER IAW EMB SRM 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK FOWARD DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 14 AND 19. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED FOWARD DIGITAL BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK FLOORBOARD ANGLE CROSS BEAM JUST AFT OF FRAME 23 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C CHECK SILL BY SERVICE DOOR FOUND TO HAVE CORRSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED SILL IAW EMB SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20-23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED OMEGA BEAM IAW EMB SRM 145 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C CHECK NUMBER ONE LOWER COWLING AFT STIFFENER WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV - DURING C-CHECK LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION ON DOUBLER INBOARD AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOUBLER — CORRODED (CABIN) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C CHECK TWO DOUBLERS WERE FOUND TO HAVE CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C CHECK NUMBER ONE COWLING STIFFENER AT STATION 2180 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — GOUGED (NR 1 COWLING) · airframe 7,863 hrs · 5,527 cycles

SHV - DURING C-CHECK NUMBER 1 LOWER COWLING OUTBOARD EDGE MEMBER WAS GOUGED BETWEEN STATIONS XN=2905.0 AND XN=3167.5. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,863 hrs · 5,527 cycles

SHV- DURING C-CHECK BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: B-NUT — LOOSE (NR 2 ENGINE)

IAH- DURING TAKEOFF THE CREW NOTED THAT E2 ATTCS NO MARGIN, REJECTED TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOUND A LOOSE B-NUT ON THE START CONTROL VALVE. MAINTENANCE TIGHTENED THE B-NUT AND PERFORMED A ENGINE RUN ON THE NR 2 ENGINE. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (ELEVATOR)

LIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY, THE FLIGHT WAS DIVERTED TO LIT, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (ELEVATOR)

LIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY AND THE FLIGHT WAS DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 6,805 hrs · 4,694 cycles

EWR- CREW REPORTED, LAV SMOKE INDICATOR WITH SMELL OF SMOKE, BUT LAV SMOKE INDICATOR EXTINGUISHED AFTER ONE MINUTE AND SMOKE SMELL DISSIPATED. MAINTENANCE RAN ENGINES WITH BOTH PACKS ON, TESTED LAV SMOKE NO SMELL IN CABIN OR COCKPIT, NO FAN SMOKE FAULT IAW EMB 145 MM 26-14-01.

Part: SMOKE — DETECTED (LAVATORY)

AMA- FLIGHT 3808 ON TAKEOFF THE CREW NOTED SMOKE IN THE LAV AND RETURNED TO AMA WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LAV FIRE DETECTION SYSTEM AND CHECKED THE LAV FOR SMOKE, NO DEFECTS NOTED. COULD NOT DUPLICATE THE PROBLEM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY)

CLE FLIGHT NR 3323 THE CREW REPORTED SMOKE IN CABIN AND COCKPIT ALONG WITH A LAV SMOKE INDICATION. THE CREW DECLARED A EMERGENCY AND RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM LAV SMOKE DETECTOR. THE DEBRIS WAS LINT AND DUST. OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — FAULTY (COCKPIT)

CREW REPORTED ON TAXI, SMOKE IN COCKPIT ELECTRICAL BURNING SMELL IN COCKPIT ONLY. CONTRACT MAINTENANCE FOUND FAULTY AP PUSHBUTTON SWITCH ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW EMB145 MM 22-11-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION, FRAME NR 80 WAS FOUND TO BE CHAFED BY THE APU FIRE BOTTLE DISCHARGE LINE. MAINTENANCE REPAIRED FRAME NR 80 IAW EMB-GST-0872/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — CHAFED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE INTERNAL SKIN AT FRAMES NR 66 AND 67 WAS FOUND CHAFED BY A BLEED LINE ADEL CLAMP. MAINTENANCE REPAIRED DAMAGED AREA BY INSTALLING A DOUBLER IAW EMB-GST-0869/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION.

Part: FAIRING — CRACKED (APU) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER RIGHT HAND FAIRING WAS FOUND CRACKED ALONG THE ATTACHMENT FLANGE. MAINTENANCE REMOVED AND REPLACED THE FAIRING IAW EMB GST-0835/01 AND EMB-145 CPM-51-21-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FIRE LOOP — CHAFED (LT ENGINE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE FIRE LOOP WAS FOUND CHAFED, ON TOP SECTION OF ENGINE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FIRE LOOP IAW EMB-145 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. P/N 3601-133-500/230C-9.0M.

Part: FIREWALL — GOUGED (APU) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE APU FIRE WALL WAS FOUND GOUGED ADJACENT TO THE BYPASS VALVE. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0429/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ATTACH FITTING — GOUGED (RT AILERON) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND GOUGED AND CHAFED. MAINTENANCE REMOVED AND REPLACED THE ATTACH FITTING IAW EMB GST-0903/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION UNDER THE CARBON FIBER SUPPORT RAIL AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-145 SRM-53-21-10, EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-03,04. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP BETWEEN FRAME 18 AND 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OMEGA BEAM TOP CAP IAW EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-06. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 22. MAINTENANCE REPAIRED THE RIGHT HAND OMEGA BEAM IAW EMB GST-0823/01, REPAIR WAS SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: AXLE — GOUGED (NLG) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR AXLE WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE AXLE IAW EMB GST-0866/01 AND EMB-CPM-51-21-05, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: COWLING — GOUGED (APU) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER PROFILE WAS FOUND TO BE BENT AND GOUGED. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW EMB-GST-0801/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 3,772 hrs · 2,636 cycles

TYS DURING A SCHEDULED INSPECTION THE FLOOR STRUCTURE DIGITAL GUSSET LOCATED JUST AFT OF THE COCKPIT DOORWAY, WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE DIGITAL GUSSET IAW EMB-145 SRM 51-40-03 AND EMB-145 CMP 51-21-06, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FRAME — CHAFED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION, FRAME 64 LOCATED INSIDE OF CARGO BAY WAS FOUND CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0812/01, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA BEAM RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND BENT AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION.

Part: BRACKET — GOUGED (AILERON) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND AILERON ATTACHMENT BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE BRACKET IAW EMB GST-085/01, THE REPAIR WAS FOUND SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — CRACKED (COWLING) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND UPPER COWLING SKIN WAS FOUND CRACKED JUST FORWARD OF THE CENTER HINGE POINT. MAINTENANCE REPAIRED THE SKIN IAW EMB GST-0821/01, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — GOUGED (CARDO DOOR) · airframe 3,772 hrs · 2,536 cycles

TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND GOUGED AT THE CUTOUT FOR THE ACTUATING HANDLE. MAINTENANCE REPAIRED THE SKIN IAW EMB GST-0815/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: O-RING — WORN (CARGO BAY)

CLE-CREW REPORTED A BLEED 2 LEAK MESSAGE ON THE EICAS. CREW FOLLOWED THE QRH AND THE MESSAGE WENT AWAY AFTER ONE AND HALF MINUTES. A/C RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED 0-RINGS ON NR 2 BLEED IN AFT UPPER CARGO BAY IAW CONTINENTAL EXPRESS EC 3610-01032. A/C WAS RELEASED FOR SERVICE.