N14916

Part: FCU — FAULTY (APU) · airframe 41,183 hrs · 31,849 cycles

HEAVY EXHAUST GAS SMELL AFTER STARTING THE APU. REMOVED AND REPLACED THE APU FUEL SOLENOID VALVE IAW HSMM 49-31-02 AND FCU IAW HSMM 49-32-01. OPS AND LEAK CHECKS WERE SATISFACTORY.

Part: CONNECTOR — BROKEN (COCKPIT) · airframe 40,650 hrs · 31,437 cycles

SHV - FLIGHT 4309 THE CREW REPORTED SMOKE IN THE FLIGHT DECK AND DIVERTED TO SHV. THE AIRCRAFT LANDED IN SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE MAGNETIC COMPASS LIGHTING CONNECTOR ON MEL 33-10-00 CAT C AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT FLEW TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

THE AISLE EMERGENCY LIGHTING BETWEEN SEATS 8 - 18 WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP BY ROW 9 AND 10 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND OPS CHECKS WERE GOOD.

Part: BULB — BURNED (CABIN LIGHTS) · airframe 36,656 hrs · 28,275 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LIGHT BULB AT SEAT 8A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAME 65-68) · corrosion level 2 · airframe 32,352 hrs · 24,860 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: FLOOR SUPPORT — CORRODED (FRAME 38) · corrosion level 2 · airframe 32,352 hrs · 24,860 cycles

DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · corrosion level 2 · airframe 32,352 hrs · 24,860 cycles

DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 43-44) · corrosion level 2 · airframe 32,352 hrs · 24,860 cycles

DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 43-44. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01958. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 33-34) · corrosion level 2 · airframe 32,352 hrs · 24,860 cycles

DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 33-34 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,027 hrs · 22,361 cycles

DURING ROUTINE MX, THE EMERGENCY LIGHT STRIP BY SEATS 1A/ 2A WOULD NOT TURN ON. MX REPLACED THE AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 27,499 hrs · 21,109 cycles

DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL CORRODED FR 65-66. MX R & R CARGO DOOR CUTOUT LOWER SILL BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,612 hrs · 19,559 cycles

THE CREW REPORTED A STRONG JET FUEL ODOR DURING APU START. MX PERFORMED APU OPS CHECKS AND NO FUEL ODOR WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 22,894 hrs · 17,318 cycles

IAH - FLIGHT 2093, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FMU — DEFECTIVE (NR 2 ENGINE) · airframe 22,695 hrs · 17,160 cycles

IAH - FLIGHT 3151, THE CREW REPORTED A LOW N1 MASTER WARNING ON TAKEOFF ROLE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO FPMU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK FRAME 10 STR 10R-9R CRACKED. MAINTENANCE REMOVED AND REPLACED FRM 10 BETWEEN STR 9R-13R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK 2 WORKING RIVETS FRM 78 BETWEEN STR'S 5L-6L. MAINTENANCE PERFORMED REPAIR AT FRM 78 BETWEEN STR'S 5L-6L WORKING RIVETS IAW EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK APU FIREWALL (EXT SKIN) HAS CRACKS FROM RT UPPER MOUNT AT STIFFENER ENDS AND FROM RIVET HEADS TO RT LOWER MOUNT, AND (2) EACH ON LT SIDE AT 9 O'CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL IAW EMB-145 EC 5330-02226. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 22. MAINTENANCE PERFORMED REPAIR AT RT OMEGA BEAM AT FRAME 22 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR AND INSTALLED A DOUBLER ON RT OMEGA BEAM AT FRAME 23 IAW EC5320-01443 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK PAX DOOR BOTTOM 4 NUT PLATE HOLES FOR MAIN LINER CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FOR AFFECTED AREA OF PAX DOORS NUT PLATES FOR MAIN LINERS FOUND TO BE WITHIN LIMITS IAW EC5210-01154. RESTORED ORIGINAL FINISH TO THE AFFECTED AREA OF PAX DOOR IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND APPLIED SEALANT IAW EMB-145 SRM 51-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK FOUND CRACK ON APU FIREWALL AROUND 3 O'CLOCK POSITION. MAINTENANCE REPAIRED CRACKS ON APU FIREWALL 3 O'CLOCK POSITION IAW EMB-145 EC5330-02226. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK 4 WORKING RIVETS FRM 79 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN WORKING RIVETS AT FRM 79 STR'S 3L-8L IAW EMB-145 EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK 7 WORKING RIVETS FRM 79 BETWEEN STR'S 3R-7R. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN FRM 79 STR'S 3R-7R IAW EMB-145 EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND APPLIED SEALANT IAW EMB-145 SRM 51-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK SERVICE DOOR BOTTOM NUT PLATE HOLES CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FROM AFFECTED AREA OF SERVICE DOOR BOTTOM NUT PLATE HOLES FOUND TO BE WITHIN LIMITS IAW EC5210-01154. RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK 10 WORKING RIVETS FRM 77 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR OF WORKING RIVETS AT FRM 77 BETWEEN STR'S 3L-8L IAW EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CRACKED (CARGO BAY) · corrosion level 2 · airframe 22,624 hrs · 17,108 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM HAS CORROSION (LEVEL 2 LOCAL) FRM 65-68. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR CUTOUT LWR BEAM FRM 65-68 AND RESTORED TO ORIG FINISH IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DEFECTIVE (BLEED AIR SYS) · airframe 22,615 hrs · 17,102 cycles

FLIGHT 3085 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN / BLEED NR 1 LEAK WITH APU RUNNING. EWR MX REMOVED AND REPLACED O-RINGS AT JOINTS 25 AND 23. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 21,598 hrs · 16,333 cycles

FLIGHT 2961 - EWR - FLIGHT CREW REPORTED MAIN AND BACK UP PITCH TRIM INOPERATIVE ON CLIMBOUT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,740 hrs · 15,708 cycles

FLIGHT 2543 - EWR - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHT OVERWING EXIT INOPERATIVE. MX REMOVED AND REPLACED AISLE PATH LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,463 hrs · 14,731 cycles

FLIGHT NR 3117, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MX INSPECTED AND REPLACED THE NR3 EMERGENCY LIGHT BATTERY AND CHARGER. OPS CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,463 hrs · 14,731 cycles

YYZ - FLIGHT 3117 - THE CREW REPORTED THE EMERGENCY LIGHTS DID NOT WORK. THE CREW RESET AND OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,974 hrs · 14,241 cycles

RIC - DURING ROUTINE MX, RIC MX FOUND EMERGENCY LIGHT EXIT SIGN AFT GALLEY BULKHEAD INOPERATIVE. MX R&R NR 3 INVERTER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 18,618 hrs · 14,116 cycles

CLE FLT 2345 - THE CREW REPORTED A PITCH TRIM MAIN INOP MESSAGE IN FLIGHT. THE CREW RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,511 hrs · 14,044 cycles

EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP. R&R LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE

Part: SKIN — GOUGED (FUSELAGE)

ACFT CURRENTLY IN A C-CHECK STATUS AND THE LT FUSELAGE WAS FOUND GOUGED AND DENTED AT FR19. MAINTENANCE CUT OUT THE AREA AND FABRICATED A NEW REPAIR IAW EC5330-01824. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (S)

Part: CONTROL UNIT — INOPERATIVE (BRAKES) · airframe 15,527 hrs · 11,920 cycles

IAH - FLIGHT 2802, DURING TAXI THE CREW REPORTED A BRAKE OUTBOARD MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 14,816 hrs · 11,407 cycles

BNA - FLIGHT NR 2175 - AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT AND CYCLE PROCEDURE PER QRC DID NOT WORK AND A/C DIVERTED INTO TYS. TYS REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02-400-801A AND EVERYTHING. OPS CHECKED GOOD IAW EMB 145 AMM 32-30-00-700-801A.

Part: LIGHT — INOPERATIVE (INTERPHONE) · airframe 9,373 hrs · 7,138 cycles

IAH - FLIGHT 2690, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN INTERPHONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CABIN INTERPHONE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING ROUTINE INSPECTION, MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT AND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULBS IAW EMB145 MM 33-50-05 AND 33-50-10. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAULTY

BTV---CO2002, DURING 2A INSPECTION, MAINTENANCE FOUND FLOOR EMERGENCY LIGHT STRIP 2ND FROM THE REAR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED #7 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IAW EMB145 AMM #33-50-12. OPS. CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

BNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE #1 EMERGENCY LIGHT BATTERY WOULD NOT HOLD CHARGE. BNA- MAINTENANCE REMOVED AND REPLACED THE #1 EMERGENCY LIGHT BATTERY,PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,042 hrs · 2,963 cycles

SHV- DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 16 AND 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 4,042 hrs · 2,963 cycles

SHV DURING C CHECK THE RAMP ANGLE SUPPORT ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED RAMP ANGLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,042 hrs · 2,963 cycles

DURING C CHECK, THE LT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAITENACE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PLATE — GOUGED (NR 1 PYLON) · airframe 4,042 hrs · 2,963 cycles

SHV-DURING C CHECK, NR 1 ENGINE, FOWARD PYLON YOKE GUSSET PLATE WAS FOUND TO HAVE A GOUGE BY LOWER ENGINE MOUNT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5420-01038. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,042 hrs · 2,963 cycles

DURING C CHECK, THE CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — FAULTY

EWR---CO3489, CREW REPORTED THAT THERE WAS AN ELECTRICAL SMELL IN THE AFT CABIN (AT SEATS 17A AND 18A) AIRCRAFT PLACED ON MEL #33-20-00 CATEGORY "C" CONTROL NUMBER 031926. ....MAINTENANCE REMOVED AND REPLACED CEILING LIGHT ASSEMBLY AT SEAT 17A AREA. OPS.CHECKED GOOD. MEL ITEM CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

CLE FLT 3274 THE CREW REPORTED THAT DURING LANDING GEAR RETRACTION THE AURAL WARNING LANDING GEAR SOUNDED. NO OTHER INDICATIONS NOTED. AIRCRAFT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE AURAL WARNING UNIT. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED

EWR---CO3419, CREW REPORTED "EMERGENCY LIGHT INOPERATIVE". MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AND RECHARGED EMERGENCY LIGHT BATTERIES. OPS.CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTACLE — BURNED (GALLEY)

CLE FLIGHT 3296 THE CREW REPORTED A BURNING SMELL FROM THE NR 1 COFFEE POT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 COFFEE POT RECEPTACLE. OPERATIONAL CHECKS WERE GOOD.

Part: RECEPTACLE — BURNED (GALLEY)

CLE FLIGHT 4004 THE CREW REPORTED A SMELL OF SMOKE IN THE GALLEY, POSSIBLY FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED THE LEFT COFFEE WARMER RECEPTACLE. OPERATIONAL CHECKS WERE GOOD.

Part: RECEPTACLE — DEFECTIVE (GALLEY)

IAH FLIGHT 3740 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEEMAKER. MAINTENANCE INSPECTED AND REPLACED THE HOT JUG RECEPTACLE. OPERATIONAL CHECKS WERE GOOD.

Part: FIREWALL — CRACKED (FUSELAGE)

CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL WAS CRACKED. THE AIRCRAFT WAS RELEASED IAW EMBRAER AUTHORIZATION GST2711/01. MAINTENANCE REPLACED THE APU FIREWALL. OPERATIONAL CHECKS WERE GOOD.