N11539

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 40,396 hrs · 31,145 cycles

DURING MX INSPECTION THE FIRST 3 SETS OF INTERIOR EMERGENCY LIGHTS AND RH LOWER EXTERIOR EMERGENCY LIGHT TURNS ON AND FADES OFF. MX REMOVED AND REPLACED #2 EMERGENCY BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 396,889 hrs · 30,741 cycles

IAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR TO THE FUSELAGE SKIN AT FR21-22 STR 10L-11L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 39,687 hrs · 30,592 cycles

PILOT REPORTED THE EMERGENCY LIGHT INSIDE EXIT ROW WAS NOT ILLUMINATING. MX PREFORMED A SYSTEM RESET AND PERFORMED OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,228 hrs · 30,218 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT COME ON WITH THE F/A CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL MODULE, OPS CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL MODULE — MALFUNCTIONED (CABIN) · airframe 39,247 hrs · 30,235 cycles

GRK - THE CREW REPORTED A BURNING SMELL ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED A LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS OR SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — FAILED (NLG) · airframe 35,145 hrs · 26,958 cycles

NOSE GEAR WOULDN'T RETRACT AFTER TAKEOFF AND RETURNED TO DEPARTURE. FOUND THE NLG UPLOCK BOX AND NLG PROXIMITY SWITCHED BAD. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX AND PROXIMITY SWITCHES IAW AMM 32-33-07; 32-61-01; IPC32-33-07 PAGE 1, ITEM 30A, FIGURE 1. OPS AND LEAK CHECKED GOOD AND THE LDG EXTENSIONS AND RETRACTION WERE DONE IAW 32-30-00;OPS CHECKED GOOD AND RELEASED TO SERVICE.

Part: BRACKET — CRACKED (COCKPIT) · airframe 38,345 hrs · 29,530 cycles

A 2 INCH LONG CRACK WAS FOUND ON THE UPPER LATERAL BRACKET IN THE COCKPIT OVERHEAD. CUTOUT DAMAGED SECTION, SPLICED IN A NEW SECTION, FABRICATED AND INSTALLED DOUBLER. AIRCRAFT STILL IN C-CHECK.

Part: O-RING — LEAKING (NR 1 ENGINE)

NR 1 ENGINE PRODUCED SMOKE ON EXHAUST DURING WALK AROUND. REPLACE LPT SHAFT PLUG O-RING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (FIRE DETECTOR) · airframe 37,565 hrs · 28,894 cycles

FLIGHT 4189 THE CREW REPORTED AN ENGINE ONE FIRE DET FAIL MESSAGE ON EICAS DURING CLIMB AND DESCENT. THE AIRCRAFT LANDED IN JAN WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,687 hrs · 28,216 cycles

CREW REPORTED ONE FLOOR EMERGENCY LIGHT STRIP OUT BETWEEN ROWS 8 & 9. REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSECURE (CONTROL PANEL) · airframe 35,882 hrs · 27,593 cycles

PILOT REPORTED UNABLE TO OPERATE EMERGENCY LIGHTS FROM THE FA PANEL. MX FOUND CONNECTOR ON F/A'S LIGHT CONTROL PANEL LOOSE. SECURED THE CONNECTER AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 32,932 hrs · 25,176 cycles

THE RT OTBD FLAP HAS A CRACK ON THE INBD ROOT FITTING. REPAIRED USING PRINCIPALES OF TECH INSTRUCTIONS TI-145-13-200, REV U. GENERATED A DMI TO PERFORM AN INTERNAL AND EXTERNAL DVI AT A 2C OR 10,000 FLT HRS WHICHEVER OCCURES FIRST.

Part: FLAPPER VALVE — LEAKING (RIGHT WING) · airframe 30,672 hrs · 23,421 cycles

THE CREW REPORTED FUEL VENTING FROM RT WING ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RT WING FLAPPER VALVE. OPS CHECKS WERE GOOD.

Part: SKIN — CRACKED (FRAME 75) · airframe 29,477 hrs · 22,542 cycles

DURING A-CHECK INSPECTION, LEFT FUSELAGE SKIN WAS FOUND TO HAVE A FREE FLOATING HORIZONTAL CRACK MEASURING 9.07 MM, 0.35", WITH A 3.47 MM, 0.13", CRACK TRAVELING UP FROM IT AT FRAME 75 ABOVE STRINGER 2L. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A TRIPLER REPAIR IAW EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROFILE — CRACKED (FRAME 76) · airframe 29,477 hrs · 22,542 cycles

DURING A-CHECK INSPECTION, LEFT L-PROFILE, DRAG ANGLE WAS FOUIND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R PROFILE, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 29,477 hrs · 22,542 cycles

DURING A-CHECK INSPECTION, RT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED FRAME 75 BELOW STRINGER 2R. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 29,110 hrs · 22,235 cycles

CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM COFFEEMAKER WHEN TURNED ON, ODOR WENT AWAY WHEN TURNED OFF. MX PERFORMED OPS CHECK OF THE COFFEEMAKER WITH NO FAULTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (NR 2 ENGINE) · airframe 28,277 hrs · 21,592 cycles

ACFT WAS ON THE GROUND WHEN CREW SAW VISABLE SMOKE ON THE F/O SIDE OF ACFT. MX R & R THE NR 2 ENGINE FUEL LOW PRESSURE SWITCH IAW AMM 28-45-01, OPS CHECK GOOD IPC REFERENCE EMB 145 28-21-00, FIG 01 ITEM 110A. ACFT RELEASED TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (NR 2 ENGINE) · airframe 28,267 hrs · 21,585 cycles

PILOT REPORTED VISIBLE SMOKE IN COCKPIT ON THE F/O'S SIDE WITH THE FUEL PUMPS ON. MX PERFORMED A DETAILED VISUAL INSPECTION IN THE COCKPIT AND NO SMOKE NOTED. R & R THE NR 2 ENGINE LOW PRESSURE SWITCH WITH OPS CHECK SUCCESSFUL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,084 hrs · 21,436 cycles

DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,084 hrs · 21,436 cycles

DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-01, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,084 hrs · 21,436 cycles

DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 55. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,084 hrs · 21,436 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT CENTER SILL WAS FOUND TO BE CORRODED. BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,084 hrs · 21,436 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (TE FLAP) · airframe 23,936 hrs · 18,116 cycles

ORD FLT 5946 THE CREW REPORTED A FLAP FAIL MESSAGE AT 500 FT ON FINAL APPROACH WITH FLAPS SHOWING 45 DEGREES. MAINTENANCE INSPECTED AND REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR. PERFORMED ZERO RIG OF THE FLAP SYSYTEM. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — FAULTY (TEE HANDLE) · airframe 23,861 hrs · 18,045 cycles

ACFT WAS IN FOR A SERVICE ROUTINE AND ON THE MORNING DEPARTURE CLIMBOUT THE CREW GOT A AURA WARNING OF A FIRE. ACFT RETURNED TO DEPARTURE WHERE MX FOUND THE NR1 ENG FIRE SWITCH WOULD NOT LOCK DOWN INT DOWN POSITION. MX R & R THE ENG FIRE SWITCH IAW MM 31-00-00. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: POTENTIOMETER — FAULTY (NLG STEERING) · airframe 23,480 hrs · 17,734 cycles

ORD FLT 5912 THE CREW REPORTED THE STEERING WAS UNRESPONSIVE WHILE TAXIING. THE AIRCRAFT STARTED PULLING RIGHT AND GRINDING NOISE CAME FROM THE NOSE WHEEL AREA. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR FEEDBACK POTENTIOMETER. ADJUSTED AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 23,050 hrs · 17,402 cycles

IAH - FLIGHT 3051, THE CREW REPORTED THAT AT FULL POWER SETTING DURING CLIMB PACK TWO EMITTED A BURNING SMELL. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ISIS — INOPERATIVE (COCKPIT) · airframe 20,075 hrs · 15,208 cycles

IAH - FLIGHT 2237, THE CREW REPORTED THAT ON LANDING THE ISIS FAILED WITH AN OUT OF ORDER MESSAGE FOLLOWED BY AN ELECTRICAL BURNING SMELL ON THE FLIGHT DECK. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE RESET THE ISIS, OPERATIONALLY TESTED WITH NO DEFECTS OR SMELL NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED MINUS THE SMOKE SMELL ON FLIGHT 2084, WHERE THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ISIS UNIT, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — INOPERATIVE (APU) · airframe 19,464 hrs · 14,767 cycles

FLIGHT 2082 - IND - FLIGHT CREW REPORTED ELECTRIC BURN SMELL IN COCKPIT AND GALLEY FOLLOWED BY APU AUTO SHUTDOWN. MX REMOVED AND REPLACED APU STARTER GENERATOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 19,230 hrs · 14,585 cycles

ABQ - FLIGHT 2728, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT ELECTRICAL AND PNEUMATIC SYSTEMS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

DURING C-CHECK LIGHTNING STRIKE BETWEEN FRAME 23 AND 24 STRINGER 14L (EXTERNAL). MX PERFORMED AND COMPLETED REPAIR IAW SRM 53-21-01 AND IC 2009-145/05374. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L. MAINTENANCE REPAIRED DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L IAW IC2009-145/05429. INSPECTION PERFORMED RVSM CRITICAL REGION INSPECTION. RVSM WAS FOUND TO BE IN LIMITS. NO FURTHER MAINTENANCE ACTION WAS REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK LT OMEGA BEAM I/B SIDE HAS CORROSION FRAME 58-59. MAINTENANCE PERFORMED AND COMPLETED REPAIR OF LT OMEGA BEAM FRM 59 AT CROSSBEAM ATTACHMENT POINT IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK (FR 65/STR 16L) SHEER CLIP AT CARGO DOOR CUTOUT BASE FWD CORNER HAS CORROSION. MAINTENANCE REMOVED CORROSION AND COMPLETED REPAIR AT FRAME 65 CLIP IAW EC5330-01458 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK HAT BUSHING MIGRATED ON LT SPEED BRAKE ACTUATOR ATTACHMENT BRACKET. MAINTENANCE REMOVED, MEASURED AND REINSTALLED HAT BUSHING ON LT SPEED BRAKE ATTACHMENT BRACKET FOR ACTUATOR IAW EMB-145 EC5740-01152 REV B. MEASURED WITHIN LIMITS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (CARGO BAY) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK CORROSION FOUND AT FRAME 65 CLIP. MAINTENANCE PERFORMED AND COMPLETED REPAIR TO FRAME CLIP AT FR 65 IAW EC5330-01458 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK LT HORIZONTAL L/E UPPER AND LOWER SURFACE HAS CORROSION AROUND ALL RIVET HEADS AND SCREW HEADS. MAINTENANCE REMOVED CORROSION BY POLISHING LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SURFACES IAW EC5530-01116. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK SERVICE DOOR CUTOUT AFT STRUCTURE AT FRAME 22 BETWEEN STRINGER 15R AND 16R HAS CORROSION AT BOLT HOLE. MAINTENANCE REPAIRED SERVICE DOOR CUTOUT AFT STRUCTURE AT FRAME 22 BETWEEN STRINGER 15R AND 16R AT BOLT HOLE IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (FUSELAGE) · airframe 18,531 hrs · 14,046 cycles

SHV - DURING C-CHECK 3 WORKING RIVETS FOUND AT FRAME 79 STRINGER 3R-6R. MAINTENANCE REMOVED AND REPLACED RIVETS AT FRAME 79 STRINGER 3R-6R IAW EC5330-01941 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,275 hrs · 13,125 cycles

IAH - FLIGHT 2883 THE CREW REPORTED A PITOT 3 HEAT INOP MESSAGE ON EICAS WITH A BURNT ELECTRICAL SMELL COMING FROM THE F/O'S SEATING AREA. IAH MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE PITOT HEAT ALL WITH NO DEFECTS OR ODORS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (A-SYSTEM)

ACFT DIVERTED BACK TO BNA FROM BNA BECAUSE OF A SYSTEM 1 HYD LOW QUANTITY. MX SERVICED THE HYD SYSTEMS AND OPS CHECKS GOOD IAW AMM 12-13-01. ACFT RELEASED BACK TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 16,312 hrs · 12,435 cycles

FLIGHT 2756 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GRD FAIL MESSAGE JUST AFTER LIFT OFF AND GEARS COULD NOT BE RETRACTED. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT L/G TRAILING WOW PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: SENSOR — FAULTY (LT MLG) · airframe 15,851 hrs · 12,114 cycles

CLE FLIGHT NR 2356, THE CREW REPORTED A LANDING GEAR AIR/GND FAIL MESSAGE AFTER TAKEOFF AND GEAR RETRACTION. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT GEAR WOW PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 15,430 hrs · 11,824 cycles

CLE FLIGHT 2600 THE CREW REPORTED A ENGINE 1 FIRE DETECT FAIL ON TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECT LOOP. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL MODULE — MALFUNCTIONED (FIRE DETECTION) · airframe 14,856 hrs · 11,449 cycles

ENGINE 2 FIRE DETECT FAIL. REMOVED AND REPLACED NR 2 FIRE DETECT CONTROL MODULE IAW EMB 145 AMM 26-11-03. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,796 hrs · 10,720 cycles

FLIGHT 2334 - EWR - CREW REPORTED EMERGENCY LIGHT SIGN DOES NOT ILLUMINATE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 6,830 hrs · 5,328 cycles

EWR- CO2686, CREW REPORTED EMERGENCY EXIT SIGN BY THE MAIN CABIN DOOR IS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW EMB 145 AMM NR 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE THE RIGHT CENTER FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY.

Part: RIB — GOUGED (LT COWLING) · airframe 4,317 hrs · 3,368 cycles

SHV-DURING C-CHECK THE LEFT LOWER COWLING CENTER RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 4,317 hrs · 3,368 cycles

SHV-DURING C-CHECK THE FORWARD EMERGENCY FLASHLIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT LAMP IAW DME CORPORATION VCMM 25-60-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (LT NACELLE) · airframe 4,317 hrs · 3,368 cycles

SHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,317 hrs · 3,368 cycles

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

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,317 hrs · 3,368 cycles

SHV-DURING C-CHECK THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED AT AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,317 hrs · 3,368 cycles

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

Part: SOCKET — BURNED (GALLEY) · airframe 2,215 hrs · 1,660 cycles

CREW REPORTED, BURNING ODOR BY GALLEY AREA FOLLOWING LANDING, SMELLS LIKE BURNED POPCORN. MAINTENANCE REMOVED AND REPLACED NR 2 COFFEEMAKER SOCKET IAW EMB145 AMM 25-31-01 AND NR 2 COFFEEMAKER IAW EMB AMM 25-31-01. OPS.CHECKED GOOD. NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (LT MLG)

IAH- DURING FLIGHT 3628, ON APPROACH THE CREW NOTED THAT THE AIR/GND FAIL. THE CREW DECLARED EMERGENCY AND PERFORMED A EMERGENCY DESCENT WHILE ON APPROACH. AFTER LANDING IT WAS NOTED THAT THE SPOILER INOP, LEFT REVERSER INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 WEIGHT ON WHEELS PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.