N13989

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,824 hrs · 33,004 cycles

DURING MX INSPECTION THE AFT EMERGENCY LIGHTS AND OVER WING LIGHTS WERE FOUND NOT TO ILLUMINATE. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,818 hrs · 32,184 cycles

FLOOR EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 3 IAW AMM 33-50-04 AND IPC 33-50-04 ITEM 30 FIG 01. OPS CHECKED GOOD.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 41,742 hrs · 32,125 cycles

IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 41,742 hrs · 32,125 cycles

IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,284 hrs · 30,203 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHTS WERE INOPERATVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES NR 2, 3, AND 4 ALONG WITH INVERTER NR 6. OPS CHECKED GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 39,156 hrs · 30,103 cycles

THE AFT CABIN EMERGENCY EXIT OVERHEAD LIGHT INOPERATIVE. INSTALLED A LOOSE WIRE ON INTERIOR EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,140 hrs · 30,093 cycles

EXIT SIGN IN CABIN WOULD NOT ILLUMINATE IN EMERGENCY LGT MODE. MAINTNENACE REPLACED THE EXIT SIGN ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,361 hrs · 29,453 cycles

THE CREW REPORTED THE EMERGENCY LIGHT MID SECTION CEILING LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT ROW FORWARD EMERGENCY LIGHT. OPS CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN ROW 18) · airframe 38,044 hrs · 29,192 cycles

THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 18 WAS INOPERATIVE. THE SYSTEM WAS RESET AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 36,901 hrs · 28,276 cycles

THE CREW REPORTED EXIT LIGHT ABOVE EXIT ROW WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS. OPS CHECKS WERE GOOD.

Part: FITTING — CRACKED (NR 1 ENGINE) · airframe 36,030 hrs · 27,568 cycles

DURING C-CK NR 1 ENGINE FWD LOWER YOKE FITTING CRACKED. R & R NR 1 ENGINE FWD LOWER YOKE FITTING IAW EC5450-01142. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOORWAY) · airframe 36,030 hrs · 19,890 cycles

DURING C-CK. CARGO DOOR LOWER CUTOUT STRUCTURE IS CORRODED. R & R CARGO DOOR LOWER STRUCTURE IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · airframe 36,030 hrs · 27,568 cycles

DURING C-CK. RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EC5320-02031. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 36,030 hrs · 27,568 cycles

DURING C-CHECK. FRAME 10 CRACKED UNDER RT DV WINDOW. REPAIRED FRAME 10 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,361 hrs · 25,444 cycles

DURING MX INSPECTION, THE NR 1 EMERGENCY LIGHT INVERTER WAS DISCOVERED INOPERATIVE. MX R & R NR 1 INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 31,195 hrs · 23,773 cycles

DURING C-CHECK, FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-3R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR OF FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-3R IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 31,195 hrs · 23,773 cycles

DURING C-CHECK CARGO DOOR FWD LWR INTERNAL CUTOUT CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUTOUT FWD SHEAR CLIP AT FRAME 65 IAW EC5320-01494. FOUND TO BE MAJOR REPAIR IAW EC5320-01494. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,195 hrs · 23,773 cycles

DURING C-CHECK CARGO CUTOUT LOWER BEAM HAS CORROSION (LOCAL LEVEL 2) BETWEEN FRAMES 65-66. MX R & R CARGO LOWER CUTOUT BEAM AT FRAME 65-68 IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 31,195 hrs · 23,773 cycles

DURING C-CHECK FUSELAGE SKIN FRAMES 15-16 STRINGER 3R-4R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAMES 15-16 STRINGERS 3R-4R IAW SRM 53-23-01 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,032 hrs · 23,644 cycles

DURING ROUTINE MX, THE EMERGENCY AISLE PATH LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,351 hrs · 22,291 cycles

EMERGENCY DOME LIGHT AFT OF OVER-WING CEILING EXIT INOPERATIVE. REPLACED BULB OPS CHECK GOOD ACFT, RELEASED AND RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,222 hrs · 21,376 cycles

DURING ROUTINE MX, THE NR 2 EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 26,734 hrs · 20,247 cycles

STL - FLIGHT 3150, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT POWER OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND ALL SWITCHES TO BE SET CORRECTLY, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 26,689 hrs · 20,213 cycles

FLIGHT 2517 - MHT - FLIGHT CREW REPORTED LAV SMOKE DETECT SYSTEM WOULD NOT TEST. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,256 hrs · 19,859 cycles

CORROSION ON INTERIOR SKIN BETWEEN FRAMES 14-15, STRINGER 21L-19R. REMOVED AND REPLACED SKIN PANEL IAW EC5330-02440.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,256 hrs · 19,859 cycles

AFT FUSELAGE HAS CORROSION ON FRAME 80 UNDER THE APU GENERATOR "L" BAR GROUNDING ATTACHMENT POINT. BLENDED OUT DAMAGE, PERFORMED NDT- NO DEFECTS NOTED. CONTINUED ON WITH REPAIR IAW EC5310-01544.

Part: GUIDE — WORN (FUSELAGE) · airframe 26,256 hrs · 18,859 cycles

TYS - A/C IN FOR C-CHECK WHEN INSPECTION FOUND THE RIGHT O/B ELEVATOR CABLE AND RIGHT I/B RUDDER CABLES CHAFING AGAINST THE TEFLON GUIDE AT FR39, STR 19R-21R. MAINTENANCE CHANGED OUT THEN CABLES AND TELFON GUIDE IAW EC5320--01463. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,255 hrs · 19,859 cycles

CARGO DOOR CORRODED ON STRUCTURE FRAME 64 ADJACENT TO CUTOUT. INSTALLED DOUBLER IAW EC5320-01479 REPAIR 3.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 25,647 hrs · 19,411 cycles

LT ELEVATOR L/E SKIN HAD A TEAR/CRACK OF 9MM FOUND IN UPPER TIP SKIN AT YH=3022. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW ETD2011-145/02568.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,060 hrs · 19,717 cycles

LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145AMM 33-50-10, OPS CHECK GOOD.

Part: ADC — FAULTY (NR 1) · airframe 23,904 hrs · 18,028 cycles

FLIGHT 2734 - DURING CRUISE AT 36,000 FEET THE CAPTAIN'S AIRSPEED INDICATION STUCK AT 215 KIAS FOR 10 TO 15 MINUTES. AT THAT TIME THE STANDBY AND FIRST OFFICER'S AIRSPEED INDICATIONS WERE OPERATING NORMALLY. UPON DESCENT THE CREW LOST THE CAPTAINS AND FIRST OFFICER'S AIRSPEED INDICATIONS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE DRAINED WATER FROM THE NR 1 AND NR 2 PITOT SYSTEMS AND REPLACED THE NR 1 AIR DATA COMPUTER.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,044 hrs · 16,640 cycles

CLE FLIGHT 2915 THE CREW REPORTED THE LEFT OVERWING EMERGENCY EXIT LIGHT BECOMES ILLUMINATED AFTER NORMAL AIRCRAFT SHUT DOWN. AFTER 7TH POWER DOWN THE LIGHT SEEMED TO OPERATE NORMALLY. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHTS AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK DENTS (2) BETWEEN FRAMES 19-20 STRINGER 14L-13L. MAINTENANCE PERFORMED REPAIR IAW IC2009-145/0556. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK LT OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 WIDESPREAD) AT FRAME 64-69. MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED REPAIR AT AFFECTED AREAS ON LT OMEGA BEAM BUTTSTRAP FRAMES 64-69 IAW EMB-145 EC5320-01137 AND SRM 51-10-03. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 61-66 HAS CORROSION (LEVEL 2 WIDESPREAD) ON SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED REPAIR ON AFFECTED AREAS ON RT FLOOR SILL AT FRAME 61-66 IAW EMB-145 EC5320-01131 REV ORIG AND SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 71. MAINTENANCE COMPLETED THE REMOVAL AND INSTALLATION OF NEW CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 61-71 IAW EMB-145 SRM 53-31-10 AND EC5320-01137 REV ORIG. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK SERVICE DOOR FORWARD SILL HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR FORWARD SILL IAW SRM 51-10-03 AND CPM 51-20-06. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK CROSSBEAM L-BRACKET AT FRAME 23 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM L-BRACKET AT FRAME 23 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 69-73 HAS VARIOUS AREAS OF CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED REPAIR ON RT FLOOR SILL AT FRAME 69-73 AFFECTED AREAS IAW EMB-145 EC5320-01137 REV ORIG AND SRM 51-10-05. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK RT CARGO FRAME 61 CORRODED (LEVEL 2 LOCAL) AT 15R BEHIND CARBON BEAM. MAINTENANCE PERFORMED REPAIR IAW IC2009-145/05601. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR IAW EMB-145 SRM 51-10-03 AND CPM 51-20-06. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK DENTS (3) FRAME 19-20 STRINGER 12L-11L. MAINTENANCE PERFORMED REPAIR IAW IC2009-145/05556. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORRODED NUT PLATES AT FRAMES 20-22. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL NUT PLATES IAW EMB-145 SRM 51-40-09 AND CPM 51-21-07. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK SHELL PLATE AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK CROSSBEAM BETWEEN LT AND CENTER OMEGA BEAM AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM AT FRAME 20 IAW EC5320-01024 REV B AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK SHELL PLATE AT FRAME 22 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK RT FLOOR SILL FRAME 42-47 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT FLOOR SILL AT FRAME 42-47 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP FRAMES 20-22 HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BUTTSTRAP AT FRAME 20-22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 21,817 hrs · 16,472 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT BEAM CORRODED (LEVEL 2 WIDESPREAD) IN SEVERAL AREAS. MAINTENANCE PERFORMED AND COMPLETED INSTALLATION OF CARGO DOOR LOWER CUTOUT BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: RELAY — DEFECTIVE (ELECTRICAL SYS) · airframe 21,774 hrs · 16,441 cycles

SHV - DURING C-CHECK, BURNING SMELL AFTER TAKEOFF. REMOVED AND REPLACED RELAY K0642 IAW EMB 145 AMM 20-13-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — FAULTY (NR 4 BRAKE)

CLE FLIGHT 2311 - THE CREW REPORTED A NR 4 BRAKE OVERTEMP MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 4 BRAKE TEMP SENSOR CONNECTOR. OPERATIONAL CHECKS WERE GOOD. (S)

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,715 hrs · 14,213 cycles

TYS - DURING A SERVICE ROUTINE, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY BATTERY NR 4 IAW EMB 145 MM 33-50-04. OPS CHECK GOOD. A/C RELEASED TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 18,314 hrs · 13,925 cycles

FLIGHT - 2303 - SYR - CREW REPORTED SMOKE ODOR IN CABIN COMING FROM OVERHEAD PANEL ABOVE SEAT 1A. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX FOUND ODOR AT THIRD BALLAST AFT MX REMOVED AND REPLACED BALLAST IAW EMB145 AMM 33-21-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BALLAST — FAULTY (CABIN) · airframe 18,314 hrs · 13,926 cycles

BDL FLIGHT 2303 - CREW REPORTED SMOKE ODOR IN CABIN AND DIVERTED FLIGHT TO SYR AND LANDED WITHOUT INCIDENT. SYR MAINTENANCE FOUND STRONG ODOR AT THIRD AFT LIGHTING BALLAST IN CABIN AND DISCONNECTED IT. PLACED ON MEL. FLIGHT CONTINUED ON TO CLE FROM SYR. CLE MAINTENANCE REMOVED AND REPLACED THE THIRD AFT LIGHTING BALLAST. OPERATIONAL CHECKS WERE GOOD.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 18,040 hrs · 13,723 cycles

FLT 2486 EWR - CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX RE-SECURED MAIN CABIN DOOR HANDLE IAW EMB145 AMM 52-18-05 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 17,653 hrs · 13,433 cycles

CLE FLIGHT 2266 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE FORWARD LOCK BOX CABLE. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 16,816 hrs · 12,797 cycles

OMA - FLIGHT 2748, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL INDICATION ON CLIMB. THE AIRCRAFT RETURNED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO MCI WHERE MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG) · airframe 16,536 hrs · 12,585 cycles

CLE FLIGHT 2863, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE JUST AFTER ROTATION FOLLOWED BY ENG REV DISAGREE. ENG REV DISAGREE WENT AWAY AFTER LANDING GEAR WAS EXTENDED. THE AIR/GROUND FAIL MESSAGE WENT AWAY AFTER NOSE WHEEL TOUCHED THE GROUND ON LANDING. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. FOR PERCAUTIONARY PURPOSES THE NOSE LANDING GEAR WOW PROX SWITCH WAS REPLACED ALONG WITH HARNESS. THE NOSE GEAR WAS SERVICED AND THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,465 hrs · 11,747 cycles

MCI - DURING MAINTENANCE INSPECTION, THE AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSLEAGE) · airframe 15,207 hrs · 11,547 cycles

TYS DUE TO A GROUND DAMAGE FRAME 72 WAS DENTED AT STR 15R. MAINTENANCE PERFORMED NDU ON FR 72 AT STR 15 AND FOUND TO BE CRACKED. CUT THE FRAME BETWEEN STR 17 AND STR 18 AND PREPARED NEW PART FOR SPLICE. INSTALL NEW SPLICE. INSTALL NEW FRAME AND SPLICE IAW EMB 145 SRM 51-40-02; 52-00-04; EC 5330-01643. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AFTER LEAK AND PRESSURE CHECKS WERE GOOD.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 12,797 hrs · 9,697 cycles

CREW REPORTED, "ELECTRICAL SMELL IN COCKPIT". MAINTENANCE FOUND BURNED WIRE TERMINALS AT THE NR 1 WINDSHIELD ASSEMBLY. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSEMBLY IAW EMB145 AMM NR 6-10-01. OPS AND LEAK CHECK GOOD. NO SMELL NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: B-NUT — LOOSE (NR 2 ENGINE) · airframe 12,174 hrs · 9,201 cycles

CLE - FLIGHT NR 2275, THE CREW REPORTED A HYDRAULIC SYSTEM NR 2 FAIL IN FLIGHT. THE AIRCRAFT DIVERTED INTO BUF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED LOOSE "B" NUT ON THE NR 2 ENGINE HYDRAULIC PUMP. SERVICED THE NR 2 HYDRAULIC SYSTEM AND OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 11,522 hrs · 8,699 cycles

IAH - DURING TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERTAIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (APU FIRE DETECT) · airframe 9,919 hrs · 7,444 cycles

CREW REPORTED, (APU FIRE INDICATION DURING FLIGHT. PERFORMED QRH WITHOUT EXTINGUISHING HALON FIRE BOTTLE.) AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND PLACED THE APU ON MEL FOR FOLLOWUP. EWR MAINTENANCE PERFORMED FOLLOWUP AND TROUBLESHOT APU FIRE DETECTOR AND PERFORMED OPERATIONAL TEST ON APU FIRE DETECTOR SYSTEM IAW MM NR 26-12-00-810-802-A. NO PROBLEMS DETECTED AND OPS CHECKED GOOD. MEL PLACARD REMOVED AND CLEARED, AND AIRCRAFT RETURNED TO SERVICE -SDR CLOSED-

Part: SIGN — INOPERATIVE (CABIN)

CLE FLIGHT NR 2004 THE CREW REPORTED THE EMERGENCY LIGHT NEAR THE GALLEY DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT THE GALLEY DOOR.OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE AREA UNDER THE BAGGAGE DOOR LOWER TRIM WAS CORRODED. MAINT R&R THE CARGO DOORWAY LOWER BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: TRIM PANEL — CORRODED (CARGO BAY) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTIONTHE AREA UNDER THE BAGGAGE DOOR LOWER TRIM PIECE SHOWS SIGNS OF CORROSION. MAINT R&R THE CARGO DOORWAY LOWER BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: SEAL — CORRODED (LAVATORY) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE LEFT SEAL IN LAV WAS FOUND CORRODED AROUNDN NUT PLATE. MAINT R&R A NEW LEFT LAV SEAL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: WIRE — BROKEN (CABIN) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE NR 5 PROXIMITY LIGHTING STRIP HAD A BROKEN WIRE. MAINTENANCE REPAIRED THE BROKEN WIRE AND OPS CHECKED GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: WIRE — BROKEN (CABIN) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE NR 4 PROXIMITY LIGHTING STRIP WIRE WAS FOUND BROKEN. MAINT REPAIRED THE BROKEN WIRE AND OPS CHECK GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE RT LAV FLOORBEAM WAS CORRODED. MAINT R&R THE RT FLOORBEAM SEAL IAW EMB135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: HOUSING — CORRODED (VERTICAL STAB) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND VERTICAL STAB SPHERICAL BEARING HOUSING. MAINTENANCE CLEANED AND REPAIRED THE HOUSING IAW EXPRESS JET EC 5510-01061 AND EMB MM 51-50-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK RW3 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK RW4 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF6 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF5 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF4 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK LF2 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,541 hrs · 5,578 cycles

TYS DURING A SCHEDULED INSPECTION SEAT TRACK LW6 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FUEL NOZZLE — MALFUNCTIONED (NR 2 ENGINE)

CLE FLIGHT 3299 THE CREW REPORTED A BURNING EXHAUST FUME SMELL DURING ICE TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RELAY — INOPERATIVE

IAH FLIGHT#3785 THE CREW REPORTED A ODER OF GAS FUMES DURING ICE TEST.MAINTENANCE INSPECTED AND REPLACED THE PACK SETDOWN RELAY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE THE EXTERIOR EMERGENCY LIGHT AT THE LEFT WING WAS FOUND INOPERATIVE.MAINTENANCE REPLACED THE BULB ON THE EXTERIOR EMERGENCY LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INLET — GOUGED (RT ENGINE) · airframe 3,417 hrs · 2,354 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE INLET GUIDE PIN HOLE FOR COWLING WAS FOUND TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 3178/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,417 hrs · 2,354 cycles

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

Part: FIRE LOOP — CHAFED (RT ENGINE) · airframe 3,417 hrs · 2,354 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE FIRE DETECTION LOOP WAS FOUND CHAFED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FIRE DETECTION LOOP IAW EMB-145 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANTENNA — CORRODED · airframe 3,417 hrs · 2,354 cycles

TYS During a schedule inspection, corrosion was found on the lower TCAS 2 antenna. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-145-AMM-34-43-03, operational checked good. The repair was satisfactory and the aircraft will be released upon complection of the inspection.

Part: CAP — GOUGED (NLG) · airframe 3,417 hrs · 2,354 cycles

TYS DURING A SCHEDULED INSPECTION, A GOUGE WAS FOUND ON THE BEARING CAP SURFACE OF THE LEFT HAND TOP BEARING CAP OF THE NOSE GEAR. MAINTENANCE REWORKED THE LEFT UPPER HALF TOP BEARING CAP SURFACE OF NOSE LANDING GEAR IAW-EMB-GST-3164/01. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: SWITCH — FAILED (CABIN) · airframe 3,417 hrs · 2,354 cycles

TYS DURING A SCHEDULED INSPECTION, THE ALTITUDE SENSING SWITCH FOR PASSENGER OXYGEN FAILED OPS CHECK. MAINTENANCE REMOVED AND REPLACED THE ALTITUDE SENSING SWITCH IAW-EMB-145-AMM-35-20-03, OPERATIONAL CHECKED GOOD. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,417 hrs · 2,354 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD TOP CAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE AREAS OF MINOR CORROSION AND GOUGED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: APU — FAILED (TAIL)

BNA FLT 4046, THE CREW REPORTED APU AUTOSHUT DOWN CAUSING SMOKE IN AIRCRAFT. MAINTENANCE REPLACED APU. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: APU — ODOR (APU BAY)

LIT - FLIGHT 4047, THE CREW REPORTED A STRONG FUEL ODOR AT FL350 WITH BOTH BLEEDS AND PACKS SELECTED. THE AIRCRAFT LANDED AT LIT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. PERFORMED OPERATIONAL TESTS WITH BOTH ENGINES RUNNING, AND NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 4367 WHERE MAINTENANCE FOUND THE FUEL ODOR TO BE COMING FROM THE APU. MAINTENANCE PLACED THE APU ON MEL 49-00-00 CAT C CONTROL NUMBER 011493, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — VIBRATION (LT ENGINE) · airframe 1,870 hrs · 1,272 cycles

IAH FLIGHT 3977. CREW ABORTED TAKEOFF DUE TO THE LEFT HAND ENGINE VIBRATION REACHING THE AMBER RANGE. THE AIRCRAFT WAS FERRIED TO TYS AFTER EXTENSIVE TROUBLESHOOTING BY MAINTENANCE. THE LEFT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001. THE OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.