N14904

Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,370 hrs · 31,069 cycles

PILOT REPORTED AN ODD ODOR IN THE COCKPIT. PERFORMED A GENERAL ODOR INSPECTION, NO FAULTS FOUND, COULD NOT DUPLICATE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,928 hrs · 28,367 cycles

DURING ROUTINE MAINTENANCE THE LT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY AND THE NR 1 EMERGENCY BATTERY. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,553 hrs · 28,078 cycles

THE CREW REPORTED THAT THE EXIT SIGN ON THE CEILING BACKSIDE LIGHT BULB WAS INOPERATIVE. MAINTENANCE R & R THE AFFECTED EXIT SIGN INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — DISCONNECTED (ZONE 100) · airframe 34,773 hrs · 26,654 cycles

THE CREW REPORTED THAT THEY HAD CABIN AND COCKPIT SMOKE IN FLIGHT FOR ABOUT 2 MINUTES COMING FROM AIR CONDITIONING VENTS, THE SMOKE WAS VISIBLE AND ODOR STRONG AND NOTICEABLE. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND PLACED THE BLEEDS ON MEL 36-11-05-1 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSPECTED THE ACFT, PERFORMED FIM 72-00-00-990-086 WITH NO DEFECTS; FOUND A BLEED TUBE DISCONNECTED FROM HE NR 1 RECIRC FAN CAUSING "FOGGY AIR" IN THE CABIN, THE DUCT WAS RECONNECTED, OPS CHECKS PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL VALVE — FAULTY (BRAKES) · airframe 34,133 hrs · 26,149 cycles

CREW REPORTED A BRAKE DEGRADED MESSAGE ON EICAS DURING LANDING FOLLOWED BY LT OTBD AND INBD OVERHEAT. A REDUCED EFFECTIVENESS OF BRAKING ON LANDING ROLL ALONG WITH ASSYMETRICAL BRAKING NOTED. MAINTENANCE R & R THE INBD BRAKE CONTROL VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,567 hrs · 25,699 cycles

DURING ROUTINE MAINTENANCE THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AFT CEILING LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: TORQUE BOX — DAMAGED (RT WING TE FLAP) · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, RT WING LOWER INBD BOLT HOLE HAS INTERNAL DAMAGE AT TORQUE BOX, NR 1. MAINTENANCE COMPLETED AND PERFORMED REPAIR TO RT WING SPAR III TORQUE BOX LOWER INBD NR 1 BOLT HOLE IAW EC5710-01236. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 100) · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, FRAME 61 IS CRACKED BETWEEN STRINGER 15R-16R. MAINTENANCE COMPLETED AND PERFORMED REPAIR OF FRAME 61 BETWEEN STRINGERS 15R-16R IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TORQUE BOX — DAMAGED (RT WING TE FLAP) · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, RT INBD FLAP TORQUE BOX UPPER MOUNT BOLT HOLE DAMAGED. MAINTENANCE COMPLETED AND PERFORMED REPAIR TO RT INBD FLAP TORQUE BOX INBD NR 2 BOLT HOLE UPPER IAW EC5710-01235. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, NR 2 ENGINE FORWARD LOWER YOKE CRACK STOP DRILL REQUIRES FINAL REPAIR AT 5000 FC OR NEXT C-CHECK. MAINTENANCE PERFORMED TEMPORARY REPAIR IAW EC5450-01123. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, BAGGAGE DOOR CUTOUT CENTER SILL HAS CORROSION, LOCAL LEVEL 2, FRAMES 65-68. MAINTENANCE PERFORMED AND COMPLETED REPAIR OF CARGO DOOR LOWER SILL AND EDGE SEALED CORNERS AND APPLIED FINISH PAINT IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 32,854 hrs · 25,136 cycles

DURING C-CHECK, CARGO DOOR OUTER FRAME AT FWD AND AFT SECTION CORRODED. MAINTENANCE PERFORMED AND COMPLETED REPAIRS TO CARGO DOOR FWD AND AFT FRAMES IAW EC5230-01352. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (CONTROL VALVE) · airframe 31,131 hrs · 23,788 cycles

PILOT REPORTED AFTER TAKEOFF, NR PACK OVERHEAT EICAS MESSAGE, ACCOMPANIED WITH BURNING ODOR. MX INSPECTED AND FOUND A LOOSE CLAMP ON THE NR 2 DUAL TEMP CONTROL VALVE. RAN NR 2 PACK WITH NO FAULTS NOTED. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — ARCED (LAVATORY LIGHT) · airframe 30,468 hrs · 23,304 cycles

DIVERTED, CREW REPORTED SMOKE IN CABIN LAVATORY AREA. LANDED SAFELY. CONTRACT MAINTENANCE FOUND SMOKE/ODOR TO BE COMING FROM LIGHT ASSEMBLY LAVATORY ABOVE TOILET. ISOLATED LIGHT ASSY AND PLACED ON NEF. ON 1/5/14. MX R & R BULB AND RESET BALLAST WITH OPS CHECK GOOD AND NO FAULTS NOTED AT THIS TIME. ACFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,081 hrs · 21,487 cycles

RIGHT SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,081 hrs · 21,487 cycles

FRAME 65, LOWER EXTERNAL SURFACE HAS 2 AREAS OF CORROSION ADJACENT TO LOWER BAGGAGE DOOR GUIDE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER.

Part: BEAM — CORRODED (CENTER FUSELAGE) · airframe 28,081 hrs · 21,487 cycles

DURING C-CHECK, CORROSION FOUND ON BEAM AT FRAME 19A. MX R & R BEAM IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FRAME) · airframe 28,081 hrs · 21,487 cycles

DURING C-CHECK, CORROSION FOUND IN CENTER GUSSET AFT OF FRAME 59 AROUND SCREW HOLES. MX R & R GUSSET IAW SRM 51-40-02.

Part: BULB — SMOKE (CABIN LIGHTS) · airframe 26,758 hrs · 20,388 cycles

CREW REPORTED SMOKE FROM 4C SIDEWALL LIGHTS. MX REMOVED BULB. OPEN

Part: CONTROL VALVE — WORN (AC PACK) · airframe 23,752 hrs · 18,067 cycles

CLT- BURNING SMELL WHILE RUNNING BOTH PACKS OFF OF APU AT GATE. REMOVED AND REPLACED NR 1 PACK DUAL TEMP CONTROL VALVE RUBBER CONNECTIONS. OPS CHECK GOOD.

Part: DUCT — DISCONNECTED (CABIN) · airframe 23,752 hrs · 18,067 cycles

CLT- BURNT PLASTIC SMELL IN CABIN. FOUND DISCONNECTED DUCT ON AIR DISTRIBUTION VALVE. RE-SECURED DUCT IAW 21-22-01. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,676 hrs · 18,009 cycles

FLIGHT 2594 - EWR - FLIGHT CREW REPORTED BURNING SMELL IN CABIN AFTER DOOR CLOSED FOR PUSHBACK. F/A WAS USING PA WHEN SHE NOTICED THE BURNING SMELL. EWR MX RUN PACKS FOR 30 MIN WHILE OPERATING BOTH FWD AND REAR PA'S, NO BURNING SMELL WAS NOTICED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACM — INOPERATIVE (AC BAY) · airframe 23,259 hrs · 17,714 cycles

IAH - FLIGHT 2733 BHM TO IAH, THE CREW REPORTED A LITE HAZY SMOKE IN THE COCKPIT DURING CRUISE THAT DISSIPATED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (RT MLG) · airframe 23,195 hrs · 17,664 cycles

CLE - THE CREW REPORTED A BANGING NOISE WHEN THE STEERING TILLER WAS ENGAGED AND TURNING LEFT WITH RIGHT BRAKE APPLIED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR AFT DOWNLOCK PROXIMITY SWITCH AND CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,174 hrs · 17,649 cycles

EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB145 AMM 33-50-12 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,096 hrs · 17,582 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,096 hrs · 17,582 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 23. REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 22,844 hrs · 17,394 cycles

IAH - DURING MAINTENANCE INSPECTION MAINTENANCE REPORTED THAT WITH ENGINE ONE BLEED ON, BOTH PACKS FILLED THE CABIN WITH SMOKE. MAINTENANCE PREFORMED PACK SYSTEM OPERATIONAL CHECKS WITH ENGINE 1 BLEED WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — FAULTY (NR 1 PYLON) · airframe 22,460 hrs · 17,087 cycles

CLE - FLT 2519 THE CREW REPORTED DURING CLIMB RECEIVED A "BLEED 1 OVERTEMP" ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 FAN AIR THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — FAULTY (CABIN) · airframe 21,270 hrs · 16,150 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 3BC DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 20,430 hrs · 15,546 cycles

ROC FLT 2516 THE CREW REPORTED WHILE DESCENDING THROUGH FL200 AURAL WARNING "CABIN" ACCOMPANIED BY INCREASE CABIN ALT AND DECREASE DELTA P ON EICAS, MANUAL WORKED FINE. A/C REL IAW MEL 21-30-00/1,CTA"C", CTL NUMBER 185425, C/W "M" PROCEDURES PER DDP. MAINTENANCE REPLACED THE DIGITAL CONTROLLER ON 1/15/2010 AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,050 hrs · 14,485 cycles

THE CREW REPORTED THE EMERGENCY LIGHT STRIP WAS INOPERATIVE AT ROW 8A / 9A. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 18,511 hrs · 14,067 cycles

SHV DURING C-CHECK. LT OMEGA BEAM HAS CORROSION AT FR 43-44. REPAIRED LT OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 18,511 hrs · 14,067 cycles

SHV DURING C-CHECK. LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED LT OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK (FR 26) LT OMEGA BEAM I/B FLANGE HAS CORROSION AT NUTPLATE. MAINTENANCE REMOVED AND REPLACED NUTPLATE AT FR 26 LT OMEGA BEAM I/B FLANGE IAW EC5320-01137 AND ALODINED, PRIMED AND PAINTED BLENDED AREA ON LT OMEGA BEAM I/B FLANGE NUTPLATE FR 26 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK BAGGAGE DOOR CUT-OUT LOWER BEAM HAS CORROSION. MAINTENANCE REMOVED AND INSTALLED NEW BAGGAGE DOOR CUTOUT LWR BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK CORROSION AROUND RIVETS AT FR 61 STR 16L-15L. MAINTENANCE REMOVED CORROSION IAW EMB-145 CPM 51-21-04 AND CPM 51-21-05. MAINTENACE COMPLETED INSTALLATION OF CARBON SUPPORT DOUBLER AT FR 61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK CENTER OMEGA BEAM AT FR 25 HAS CORROSION AT NUTPLATE. MAINTENANCE REMOVED CORROSION AND CLEANED, ALODINED, PREPPED, PRIMED AND TOPCOATED CENTER OMEGA BEAM AT FR 23-26 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK CENTER OMEGA BEAM (FR 25-29) HAS PITTING ON I/B FLANGE. MAINTENANCE REMOVED PITTING CORROSION, ALODINED, PRIMED AND PAINTED BLENDED AREA ON CENTER OMEGA BEAM FR 25-29 ON I/B FLANGE IAW CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,511 hrs · 14,067 cycles

SHV-DURING C-CHECK LT OMEGA BEAM I/B FLANGE HAS PITTING (FR 30-31). MAINTENANCE REMOVED CORROSION AND ALODINED, PRIMED AND PAINTED BLENDED AREA ON LT OMEGA BEAM I/B FLANGE FR 30-31 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT FRAME — CRACKED (CABIN) · airframe 18,516 hrs · 14,070 cycles

BASE FRAME ASSY (LEG) HAVE BEEN FOUND CRACKED IN THE AREA SURROUNDING ATTACHMENT FROM FRAME TO SEAT. ON THIS PARTICULAR ACFT 10 DOUBLE SEAT BASE FRAME (LEG) ASSEMBLIES WERE FOUND CRACKED. THIS PARTICULAR PART HAS BEEN REMOVED AND REPLACED WITH NEW PART.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVETS AND COMPLETED POLISHING PROCEDURES ON LT LEADING HORIZONTAL EDGE IAW EMB-145 EC5530-01116 REV D - 80 PERCENT MATERIAL THICKNESS REMAINS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 18,511 hrs · 14,067 cycles

SHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE ON HORIZONTAL STABILIZER RT LEADING EDGE WITH POLISHING PROCEDURE IAW EC5530-01116 REV D, 80 PERCENT MATERIAL THICKNESS REMAINS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 18,005 hrs · 13,700 cycles

IAH - DURING MX INSPECTION THE EMERGENCY EXIT OVERHEAD LIGHT AT THE CENTER EXIT WAS FOUND TO BE INOPERATIVE. MX INSPECTED THE ACFT AND RECONNECTED THE EMERGENCY LIGHT, OPS TESTS WERE SATISFACTORY, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,837 hrs · 13,574 cycles

IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (LANDING GEAR) · airframe 15,272 hrs · 11,809 cycles

FLT 2868 - EWR - CREW REPORTED A LOUD NOISE FROM NOSE WHEEL AREA AFTER LANDING GEAR EXTENSION. NORMAL DOWN AND LOCKED INDICATION. NO MESSAGES ON EICAS. ALTHOUGH ALL INDICATIONS WERE NORMAL, CREW PROCEEDED WITH EMERGENCY DESCENT. ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED DOWNLOCK PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 13,795 hrs · 10,748 cycles

CLE FLIGHT 3004 THE CREW REPORTED ON APPROACH WHEN EXTENDING THE LANDING GEAR A LANDING GEAR AIR/GROUND FAIL MESSAGE CAME ON THE EICAS. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT MAIN GEAR PROXIMITY SWITCH 2. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,536 hrs · 9,769 cycles

CLE FLIGHT 2532 - THE CREW REPORTED THE EMERGENCY EXIT LIGHT OVER GALLEY DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED A LOOSE CONNECTION AT THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,682 hrs · 8,324 cycles

DURING ROUTINE MAINTENANCE AN EMERGENCY LIGHT FLOOR STRIP WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE NR 5 INVERTER OPS CHECKED GOOD AND RETURNED THE A/C BACK TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,334 hrs · 8,049 cycles

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE CENTER EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY EXIT) · airframe 9,706 hrs · 7,549 cycles

BNA - DURING MAINTENANCE INSPECTION, THE RIGHT EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 8,949 hrs · 6,940 cycles

SHV - DURING C-CHECK THE APU FIREWALL IS CRACKED AT RT O/B EDGE. MAINTENANCE REPAIRED THE DAMAGE ON THE APU FIREWALL RT O/B IAW EC5330-01473. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU) · airframe 8,949 hrs · 6,940 cycles

DURING C-CHECK, APU FIREWALL HAS SEVERAL CHAFE MARKS AT BOTTOM EDGE. MX REMOVED DAMAGED AREA ON APU FIREWALL BOTTOM EDGE IAW EC 5310-01339. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,949 hrs · 6,940 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FS 23-FS 29. MX REPAIRED LT OMEGA BEAM FS 23-FS 29 I/A/W EC 5320-01249. ACFT APPROVED TO RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 6,958 hrs · 5,375 cycles

EWR LOG SQUAWK OVERHEAD EMERGENCY LIGHT BETWEEN ROW 7 AND 8 OUT. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB IAW EMB MM 33-50-08. OPS CHECK GOOD.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 4,394 hrs · 3,377 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,394 hrs · 3,377 cycles

SHV- DURING C-CHECK, THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 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: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 4,394 hrs · 3,377 cycles

SHV- DURING C-CHECK, THE BAGGAGE DOOR LOWER CUTOUT SILL BETWEEN FRAMES 66 AND 67 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 4,394 hrs · 3,377 cycles

DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.