N14945

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,870 hrs · 25,825 cycles

AIRCRAFT SUSTAINED GROUND DAMAGE TO THE RT REAR FUSELAGE BETWEEN FRAMES 63 AND 68. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED FILLERS AND DOUBLERS. REPLACED FRAME 66 INTERNAL SKIN SPLICE BETWEEN STRINGERS 8R & 9R AND 14R & 15R. GENERATED TWO DMI'S. 1 FOR DETAILED VISUAL INSPECTION AT 500 FLIGHT CYCLE INTERVAL AND 1 FOR THIS TEMPORARY REPAIR UNTIL A DETAILED STRUCTURAL ANALYSIS CAN BE MADE BY EMBRAER. THIS REPAIR IS VALID FOR 12 MONTHS FROM SEPT. 23RD 2011 OR UNTIL THE SUBSTANTIATION IS CONCLUDED, WHICHEVER COMES FIRST.

Part: DISPLAY — SHORTED (COCKPIT) · airframe 26,101 hrs · 25,017 cycles

XNA - FLIGHT 2619 THE CREW REPORTED A SMOKE SMELL FOLLOWED BY THE CAPTAINS PFD CIRCUIT BREAKER POPPING. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE CAPTAINS PFD, OPERATIONALLY CHECKED WITH NO DEFECTS OR SMELLS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,610 hrs · 24,502 cycles

IAH - THE CREW REPORTED THAT THE COCKPIT SMELLED LIKE BURNING ELECTRICAL WIRE. MAINTENANCE INSPECTED THE AIRCRAFT POWERED UP THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOUSING — DAMAGED (VERTICAL STAB) · airframe 24,980 hrs · 23,856 cycles

SHV - DURING C-CHECK VERTICAL STABILIZER RT SPERICAL BEARING HOUSING FOUND TO BE OUT OF LIMITS. MAINTENANCE PERFORMED REPAIR ON RT SPERICAL BEARING HOUSING IAW ETD 2010-145/084787. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (RUDDER) · airframe 24,980 hrs · 23,856 cycles

SHV - DURING C-CHECK 2 OBLONG HOLES IN RUDDER II SKIN, LT SIDE, ABOUT 1/2 WAY UP. MAINTENANCE PERFORMED REPAIR TO RUDDER II SKIN, LT SIDE, HALFWAY UP IAW EC5540-01141. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 900) · corrosion level 2 · airframe 24,980 hrs · 23,856 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) FRAMES 19 TO 23. MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM AT FRAME 18-24 IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — BURNED (CABIN) · airframe 24,982 hrs · 23,858 cycles

IAH - FLIGHT 2012, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN BEFORE BOARDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIDEWALL LIGHT ASSY AT SEAT 1A TO HAVE A BURNED CONNECTOR. MAINTENANCE PLACED THE LIGHT ASSY ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL LIGHT ASSEMBLY AT SEAT 1A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED SYS) · airframe 24,524 hrs · 23,380 cycles

FLT 2213 DIVERT - E1 BLEED LK MSG-E1 COMMANDED SHUTDOWN INFLT. MAINTENANCE DOWNLOADED DFDR AND CMC - NO FAULTS FOUND, RAN AC, NO LEAKS. PERFORMED BLEED OPERATIONAL CHECKS IAW EMB-145 AMM 36-00-00 AND 36-11-09, ALL OPERATIONAL CHECKS GOOD. TEST FLIGHT GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,102 hrs · 22,939 cycles

IAH - FLIGHT 2820, DURING POST FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,069 hrs · 22,903 cycles

SHV - GALLEY EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,811 hrs · 20,510 cycles

FLIGHT 2195 MOB - IAH. THE CREW REPORTED A BURNING PLASTIC SMELL AT PASSENGER SEAT ROWS 9 THROUGH 11. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE PASSENGER CABIN. ALL CONDITIONS WERE FOUND TO BE NORMAL AND THERE WERE NOT ANY INDICATIONS OF BURNING, SMOKE OR COMPONENT OVERHEATING.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

BTR - FLIGHT 2010, THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION. THE ACFT DIVERTED TO BETWEEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BULB — FAULTY (EMERGENCY LIGHTS)

DURING ROUTINE MAINTENANCE THE AFT OVERHEAD WHITE EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AFT OVERHEAD WHITE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. (S)

Part: BALLAST — DEFECTIVE (CABIN) · airframe 20,846 hrs · 19,575 cycles

FLIGHT 2404 - EWR - FLIGHT CREW REPORTED SIDE LIGHTS AT 2A AND 3A INOPERATIVE WITH BURNING SMELL COMING FROM BALLAST. EWR MX REMOVED AND REPLACED BALLAST IAW WMB 145 AMM 33-21-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 20,846 hrs · 19,575 cycles

FLIGHT 2404 - EWR - FLIGHT CREW REPORTED COFFEEMAKERS EMITTING BURNING SMELL WHEN TURNED ON. EWR MX PERFORMED OPERATIONAL CHECK OF BOTH COFFEEMAKERS IAW EMB 145 VCMM 25-30-39 SUCCESSFULLY AND COULD NOT DUPLICATE BURNING SMELL. NO ABNORMALITIES WERE FOUND. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 20,368 hrs · 19,119 cycles

YQB FLIGHT 3072 - THE CREW REPORTED AFTER TAKEOFF A LOUD CLUNK ALONG WITH VIBRATION FELT IN FLIGHT CONTROLS. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR UPLOCK PROXIMITY SWITCH "A" OPEN. THE PROXIMITY SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,183 hrs · 18,935 cycles

SHV - DURING C-CHECK FRAME 65 HAS CORROSION AT STR 17L. MX REPAIRED FR 65 STR 17 IAW EC 5310-01432. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: NOZZLE — DIRTY (A/C PACK) · airframe 20,185 hrs · 18,937 cycles

IAH - FLIGHT 2818, THE CREW REPORTED FOG DENSE IN COCKPIT DURING TAKEOFF ROLL, NO BURNING SMELL JUST FOGGED ALL WINDOWS. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CLEANED WATER SPRAY NOZZLE ON NR 1 PACK IAW EMB145 AMM 21-51-13, OPERATIONALLY CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 20,183 hrs · 18,935 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SECTION HAS VARIOUS ARES OF CORROSION. MX REMOVED AND REPLACED LOWER BEAM AT CARGO DOOR CUTOUT FR 65-68 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 20,183 hrs · 18,935 cycles

SHV - DURING C-CHECK SHEAR CLIP AT FR 65 HAS CORROSION. MX REPAIRED FR 65 SHEAR CLIP IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CONNECTOR — BURNED (CABIN) · airframe 19,468 hrs · 18,177 cycles

IAH FLT 2302, MX WORKING MEL 33-20-001/C PLASTIC BURNT SMELL IN AIRCRAFT. MAINTENANCE REMOVED AND REPLACED CONNECTOR TO OVERHEAD LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: NOZZLE — CLOGGED (LT A/C PACK) · airframe 18,957 hrs · 17,667 cycles

FLIGHT 2553 - CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN WHEN THE AIR CONDITIONING PACKS WERE SELECTED TO MANUAL. MAINTENANCE CLEANED THE LEFT AIR CONDITIONING PACK SPRAY NOZZLE, OPERATIONALLY CHECKED THE SYSTEM AND CLEARED THE DISCREPANCY.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 16,435 hrs · 14,844 cycles

IAH - FLIGHT 2537, DURING DESCENT INTO IAH, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 15,743 hrs · 14,026 cycles

SHV - DURING C-CHECK, MAINTENANCE FOUND FS 68 CARGO DOOR ROD SUPPORT BRACKET(AFT SECTION) CRACKED. MAINTENANCE REPAIRED FS 68 (AFT SECTION) OF CARGO DOOR SUPPORT BRACKET IAW EC 5230-01123. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GOUGED (TE FLAP) · airframe 15,743 hrs · 14,026 cycles

SHV - DURING C-CHECK, MAINTENANCE FOUND LT I/B FLAP O/B BUSHING GOUGED (ON FLAP). MAINTENANCE REMOVED AND REPLACED LT I/B FLAP O/B BUSHING (ON FLAP) IAW EMB 145 EC5710-01096. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU BAY) · airframe 15,743 hrs · 14,026 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND AFT LOWER SIDE OF APU FIREWALL RIVET HEAD WITH DAMAGE. MAINTENANCE REPAIRED APU LOWER FIREWALL SKIN DAMAGE I/A/W EC 5330-01521. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 13,740 hrs · 11,744 cycles

IAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTIONING. THE CREW ALSO REPORTED CONTROLLABILITY ISSUES ABOVE 240KTS WITH ROLLING 20 DEGREES TO EITHER SIDE, WITH CONTROL RETURNING BELOW 240KTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU) TO BE BAD. MAINTENANCE REMOVED AND REPLACED THAT HSCU, OPERATIONALLY CHECKED IN ACCORDANCE WITH EMB-145 MM 27-40-01 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DEACTIVATED (CABIN)

CREW REPORTED, NR 2 EMERGENCY LIGHT STRIP IN CABIN INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00, OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: CONTROL PANEL — CONTAMINATED (EMERGENCY LIGHTS)

DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTION AT THE FLIGHT ATTENDANTS LIGHTING CONTROL PANEL, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.

Part: LIGHT — MALFUNCTIONED (CABIN)

CLE FLIGHT NR 2115 THE CREW REPORTED TWO EMERGENCY AISLE LIGHTS OUT OF SERVICE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF AISLE PATH EMERGENCY LIGHTS OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLIGHT 2573 - THE FORWARD SECTION OF EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,626 hrs · 9,450 cycles

EWR---CO2573, CREW REPORTED DURING PREFLIGHT, EMERGENCY LIGHTS WERE INOPERATIVE......MAINTENANCE REMOVED AND REPLACED BATTERY AND REPAIRED BROKEN WIRE. (IAW EMB145 MM NR 33-50-01) OPS.CHECKED SYSTEM GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

EWR FLIGHT NR 2568 THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE STARTING FROM ROW 8. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

THE CREW REPORTED FLOOR EMERGENCY LIGHTS BURNED OUT IN TWO SECTIONS. MAINTENANCE RESECURED LOOSE WIRE ON EMERGENCY LIGHT STRIP.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SQUAT SWITCH — FAILED (MLG) · airframe 11,193 hrs · 9,031 cycles

DURING TEST FLIGHT 3160 A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. PILOT USED DOWNLOCK RELEASE BUTTON TO RAISE AND LOWER GEAR. THE AIRCRAFT COMPLETED FLIGHT WITH NO OTHER INCIDENTS. MAINTENANCE ADJUSTED LEFT HAND MAIN LANDING GEAR WOW SWITCH IAW EMB 145 AMM 32-63-05. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM HAS CORROSION UNDER THE COMPOSITE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

SHV DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION AT RAMP SUPPORT ANGLE BETWEEN FRAMES 19 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR ON AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STOP — CRACKED (CARGO DOOR) · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE CARGO DOOR STOP LIP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED STOP IAW EMB 145 SRM 52-30-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 11,193 hrs · 9,031 cycles

SHV - DURING TEST FLIGHT 3160, A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. THE PILOT USED THE DOWNLOCK RELEASE TO CYCLE THE GEAR. THE AIRCRAFT COMPLETED THE TEST FLIGHT AND RETURNED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR PROXIMITY SWITCH AND OPERATIONAL CHECKED GOOD IN ACCORDANCE WITH EMB-145 MM 32-63-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (THRESHOLD) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE FORWARD PASSANGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (CARGO RAMP) · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE LOWER ATTACH ANGLE FOR THE CARGO RAMP AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

SHV-DURING C-CHECK THE SUPPORT RAMP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE LOWER CROSSBEAM ANGLE FROM THE CENTER BEAM TO THE RIGHT HAND BEAM AT FRAME 23 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: SUPPORT — CORRODED (THRESHOLD) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE LT HAND SILL AT FRAME 61 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: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE DOUBLER ON THE RIGHT HAND FLOORBEAM AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE AFT DIGITAL BUTTSTRAP 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: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 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: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,193 hrs · 9,031 cycles

DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 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: FRAME — DENTED (FUSELAGE) · airframe 11,193 hrs · 9,024 cycles

SHV DURING C-CHECK A DENT WAS FOUND AT FRAME 67 STRINGER 15 RIGHT. MAINTENANCE REMOVED DAMAGE AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (BAGGAGE DOOR) · corrosion level 2 · airframe 11,193 hrs · 9,024 cycles

SHV DURING C-CHECK THE LOWER BAGGAGE DOOR CUTOUT BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 53-31-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHT)

THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING AT ROW 7-12 WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTAINENCE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE AT ROW/SEATS 6. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT FLOOR STRIP. OPERATIONAL CHECKS GOOD

Part: ACTUATOR — SLOW (NOSE GEAR)

CVG FLIGHT#2695 THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT CLOSE ON CLIMBOUT.THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INTERMITTENT

BDL---CO2578, CREW REPORTED, "EMERGENCY AISLE PATH LIGHTING INTERMITTENT". MAINTENANCE PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM IAW EMB145 AMM #33-50-00. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.Original Control number was incomplete. Corrected 9/4/02

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3297 THE CREW REPORTED THE EMERGENCY EXIT ROW LIGHT ABOVE FA SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 3015 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR AT THE SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 3021 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE FLIGHT ATTENDANT JUMP SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — FAULTY (PASSENGER CABIN)

EWR---CO3431, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE (REAR SECTION ONLY)....MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FILTER — LEAKING (TAIL)

CLE FLIGHT# 3130 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AND COCKPIT AFTER APU START.MAINTENACE INSPECTED AND PLACED ON MEL.ON 1/22/01 MAINTENANCE REPLACED THE APU FUEL FILTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: VALVE — DIRTY (APU)

CLE FLIGHT#3024 THE CREW REPORTED THE APU STARTED ON THE GROUND WITH STRONG FUEL SMELL FILLING THE CABIN.MAINTENANCE PLACED THE APU ON MEL 49-00-00.MAINTENANCE REPLACED THE START FUEL CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — DIRTY (APU)

CLE FLIGHT 3075 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND PLACED THE APU ON MEL. MAINTENANCE CLEANED COMBUSTOR DRAIN CHECK VALVE. OPERATIONAL CHECKS OF APU WERE GOOD. NO FUEL SMELL WAS NOTED IN CABIN OR COCKPIT.

Part: CONTROLLER — INOPERATIVE (COCKPIT)

IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT NOT ARMED MESSAGE APPEARED ON THE EICAS DISPLAY. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE PIN — CORRODED (ELEVATOR) · airframe 7,097 hrs · 5,238 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND ELEVATOR HINGE PIN WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE PIN IN ACCORDANCE WITH EMB-145 M/M 55-10-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — CORRODED (ELEVATOR) · airframe 7,097 hrs · 5,238 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND ELEVATOR SPHERICAL BEARINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPHERICAL BEARINGS IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING AUTHORIZATION EA5510-01016, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — FAULTY (TAIL)

EWR - FLT 3605 - CREW REPORTED, STRONG ODOR OF FUEL IN COCKPIT AND CABIN DURING APU START IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE APU. OPS CHECKED GOOD. NO SMELL OF FUEL NOTED. AIRCRAFT MEL CLEARED AND RETURNED TO SERVICE. (M)

Part: LINE — LEAKING (APU)

EWR - FLT 3605 - CREW REPORTED STRONG ODOR OF FUEL IN COCKPIT AND CABIN DURING APU START IN FIGHT. MAINTENANCE INVESTIGATED AND PLACED APU ON NEL NR 49-00-00-C PLACARD NR 009254, AND RELEASED AIRCRAFT TO SERVICE. (M)

Part: LINE — LEAKING (COCKPIT)

EWR - FLT 4254 - CREW REPORTED STRONG ODOR OF GAS IN COCKPIT WHEN APU STARTED IN AIR. NO ODOR WHEN STARTED ON GROUND. MAINTENANCE PERFORMED OPERATIONAL CHECK OF APU REFERENCE TO EMB145 MM 49-00-00. OPS CHECKED GOOD. LEAK CHECKED GOOD. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

MHT - FLT 3978 - CREW REPORTED AIR RETURN FOR GALLEY DOOR INDICATOR AFTER TAKEOFF, LANDING WAS 400 LBS OVERWEIGHT. AIRCRAFT RELEASED IAW MEL NR 52-70-00/1 CONTROL NR 009233. AIRCRAFT FEW TO EWR WHERE MAINTENANCE OPERATIONALLY CHECKED THE GALLEY DOOR, OPS CHECKED AT THIS TIME WAS GOOD IAW EMB145 MM 52-43-00. MAINTENANCE CLEARED THE MEL AND RETURNED THE AIRCRAFT TO SERVICE. (M)

Part: NOZZLE — MALFUNCTIONED (NR 2 ENGINE)

CLE - FLT 4078 - THE CREW REPORTED SMOKE IN CABIN AND COCKPIT WITH ACTIVATION OF THE DE-ICE SYSTEM DURING HIGH POWER SETTINGS. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES IAW MM 73-11-10. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: COMPRESSOR — CONTAMINATED (ENGINE)

BTV - REPORTED SMOKE IN CABIN AFTER TAKEOFF AIRCRAFT RETURNED TO BTV UNEVENTFULLY. MAINTENANCE RAN BOTH ENGINES AND OPS CHECKED SYSTEM GOOD. FOUND THE SMELL TO BE COMPRESSOR WASH FLUID THAT HAD GOTTEN INTO THE BLEED AIR SYSTEM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ECU — FAULTY (MLG)

EWR - FLT 3869 - ON LANDING, CREW REPORTED LANDING GEAR THREE RED ON INDICATIONS. PERFORMED EMERGENCY LANDING. LANDED WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED THE LGEU AND GEAR HANDLE, SWUNG LANDING GEAR OPS CHECKED GOOD AND RETURNED THE AIRCRAFT TO SERVICE (M)

Part: SEAL — FAILED (PAX DOOR)

CLE - FLT 4234 - THE CREW REPORTED THAT THE MAIN CABIN DOOR DEVELOPED A LEAK AND THEY LOST PRESSURE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN MAIN DOOR SEAL IAW EMB145 MM 52-18-04. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ENGINE — FAILED (NR 1)

YUL-CLE - FLT 3995 - THE CREW REPORTED THE NR 1 ENGINE SMOKES ON SHUTDOWN. THE AIRCRAFT WAS AT THE GATE, NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW TASK CARD NR 6271001. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR)

EWR - 4135 - AFTER DEPARTURE LANDING GEAR DID NOT RETRACT. QRH, TRY CYCLING GEAR. GEAR CYCLED DID NOT WORK. APPEARED NOSE GEAR RETRACTED BUT MAINS DID NOT. RETURNED TO EWR UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED LGEU AND OPS CHECKED AIRCRAFT GOOD FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING 1A INSPECTION, THE AFT EMERGENCY AISLE PATH LIGHTSTRIP WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHTSTRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)