N16927

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,118 hrs · 30,800 cycles

DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT (SIGN) WAS NOT ILLUMINATING. MX INSPECTED THE ACFT, R & R THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,827 hrs · 30,513 cycles

DURING 5A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED BELOW STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,827 hrs · 30,513 cycles

DURING 5A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED ABOVE STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 31,528 hrs · 30,214 cycles

DURING `A` CHECK INSPECTION, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 31,528 hrs · 30,214 cycles

DURING `A` CHECK INSPECTION, EMERGENCY LIGHT AT 12C WAS FOUND TO BE INOPERATIVE. MX PERFORMED OPS CHECKS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED (EMERGENCY LIGHT) · airframe 31,290 hrs · 29,974 cycles

THE CREW REPORTED THAT DURING LANDING, A BURNING ODOR AND LIGHT LAYER OF SMOKE WAS NOTED IN THE CABIN. THE SMOKE DISSIPATED AFTER LANDING, HOWEVER THE ODOR REMAINED. THE ACFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT WHERE MX FOUND 2 LATERAL LIGHTS TO BE BURNED AND ARCING AT ROW 14. THE AFFECTED LIGHTS WERE REPLACED, OPS CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: PRESSURE SWITCH — INOPERATIVE (BRAKES) · airframe 30,973 hrs · 29,663 cycles

THE CREW REPORTED BRAKE DEGRADE ON LANDING WITH VERY LITTLE BRAKE PRESSURE, ALSO HAD CMC MESSAGE BRAKE WHEEL SPEED TRANSDUCER 3 FAIL OCCURRED 3 TIMES. THE ACFT LANDED WITHOUT INCIDENT AND MX INSPECTED THE ACFT AND PLACED IT ON MEL 32-41-08, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 12-29, MX R & R THE NR 3 BRAKE PRESSURE SWITCH, OPS TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,357 hrs · 29,045 cycles

DURING MX INSPECTION THE AISLE PATH LIGHT AT ROWS 3 THRU 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,315 hrs · 29,001 cycles

DURING MX INSPECTION, THE AISLE PATH LIGHT STRIP AT ROW 10-11 WAS FOUND INOPERATIVE. MX INSPECTED THE ACFT AND REPAIRED THE WIRE ON THE LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BROKEN (LT OVERWING) · airframe 30,085 hrs · 28,776 cycles

DURING MX INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO HAVE THE BULB OUT OF ITS SOCKET. MX R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,345 hrs · 28,062 cycles

DURING MX INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (MLG) · airframe 29,316 hrs · 28,032 cycles

AFTER TAKEOFF, CREW REPORTED THAT AFTER RETRACTING THE LANDING GEAR, HEARD SEVERAL LOUD BANGS FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. INSPECTED ACFT AND FOUND THE NLG DOORS HAD CLOSED WHILE NLG STILL EXTENDED, CAUSING MAJOR DAMAGE TO DOORS, AND FUSELAGE STRUCTURE AROUND THE NLG DOOR CUTOUT. ALL DAMAGE WAS REPAIRED, AND R & R THE NLG DOOR SOLENOID VALVE. OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 29,244 hrs · 27,967 cycles

THE CREW REPORTED THAT THE NLG DOOR OPENED IN FLIGHT. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE LANDING GEAR CONTROL LEVER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAULTED (ZONE 200) · airframe 28,836 hrs · 27,567 cycles

THE CREW REPORTED THAT DURING CLIMB OUT AT 3000 FEET THERE WAS A TEMPORARY LOSS OF POWER ON ENG NR 1, N1 APPROX 70%. A FEW MINUTES LATER, A SECOND LOSS OF POWER ON ENGINE NR 1, THIS TIME TO APPROX 60% N1. BOTH TIMES THRUST LEVERS WERE IN THE DETENT / CLIMB SETTING. THE AIRCRAFT RETURNED WITHOUT INCIDENT WHERE MAINTENANCE REPLACED RELAYS K0401 - K0403 - K0405 - K0407. AN OPERATIONAL CHECK FLIGHT AND SYSTEM CHECKS WERE SUCCESSFUL AND THE DISCREPANCY WAS CLEARED.

Part: RELAY — FAULTED (ZONE 200) · airframe 28,836 hrs · 27,567 cycles

CREW REPORTED DURING CLIMB OUT AT 3000 FT, THERE WAS A TEMPORARY LOSS OF POWER ON NR 1 ENGINE, N1 APPROX 70 PERCENT. A FEW MINUTES LATER, A SECOND LOSS OF POWER ON NR 1 ENGINE, THIS TIME TO APPROX 60 PERCENT N1. BOTH TIMES THRUST LEVERS WERE IN CLIMB DETENT SETTING. THE ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. MX REPLACED RELAYS K0401 - K0403 - K0405 - K0407. AN OPS CHECK FLIGHT AND SYS CHECKS WERE SUCCESSFUL AND THE DISCREPANCY WAS CLEARED.

Part: FADEC — FAILED (ZONE 200) · airframe 28,770 hrs · 27,500 cycles

THE CREW REPORTED THAT AFTER ROTATION THE ACFT YAWED AND THE F/O CALLED POWER LOSS. THE POWER LEVERS WERE PUSHED FULL FORWARD AND THE N1 ON THE LT ENGINE WAS AROUND REMAINED AROUND 24 PERCENT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACED THE THE NR1 FADEC. ENGINE RUNS WERE SUCCESSFUL AND THE ACFT RETURNED TO SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 27,602 hrs · 26,294 cycles

XNA - FLIGHT 3099, THE CREW REPORTED A BURNING SMELL AND SMOKE FROM THE LEFT COCKPIT VENT AT THE WINDOW WITH A PACK 1 OVERHEAT MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WHERE PACK TWO WAS CHECKED USING BOTH ENGINES WITH NO DEFECTS, AND PACK ONE WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,946 hrs · 25,632 cycles

IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,946 hrs · 25,632 cycles

IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 26,870 hrs · 25,553 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR AT SEAT 6A. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT AT SEAT 6A ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT BALLAST AT ROW 6A, OPERATIONALLY TESTED WITH NO DEFECTS OR BURNING ODOR, REMOVED MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 26,870 hrs · 25,553 cycles

FLIGHT 2634, A PASSENGER AND F/A NOTICED AN ELECTRICAL BURNING ODOR IN MID CABIN DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT BALLAST AT ROW 10 ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 12/08/10 SHV MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST AT ROW 10A, OPERATIONALLY TESTED WITH NO DEFECTS OR ODOR, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 26,843 hrs · 25,522 cycles

TUL - FLIGHT 2972, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A SMOKE SMELL AND FLICKERING CABIN LIGHTING. MAINTENANCE INSPECTED THE LIGHTING AND PLACED THE LIGHT AT SEAT 7A ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 12/01/10 IAH MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 7A, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 26,251 hrs · 24,904 cycles

LEFT BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 25,737 hrs · 24,385 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BETWEEN THE CAPTAINS DV WINDOW AND WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,463 hrs · 24,109 cycles

IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, GROUND RAN BOTH ENGINES AND PACKS ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,463 hrs · 24,109 cycles

IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, AND GROUND RAN BOTH ENGINES, AND PACKS, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,822 hrs · 23,436 cycles

IAH - FLIGHT 3020, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE NUMBER FIVE AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM IAW EC 5320-01467. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK FRAME 10 SUPPORT BRACKET CRACKED JUST UNDER LEFT DV WINDOW LOWER CUTOUT FRAME. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAME 10 LT IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (LT WING) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LEFT I/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT I/B LEADING EDGE SPLICE SHEAR CLIP IAW SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (PAX DOOR) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK MAIN DOOR LOWER HINGE LOCK PIN HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED MAIN DOOR LOWER HINGE IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (SPOILER) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LT GROUND SPOILER CENTER HINGE O/B FITTING I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER CENTER HINGE IAW EMB-145 AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK PROXIMITY LIGHT 3 AND 4 FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY IAW EMB-145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAME 17-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LT GROUND SPOILER I/B HINGE O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER I/B BRACKET IAW EMB-145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — DAMAGED (SPOILER) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE O/B HOLE OF ATTACHMENT BRACKET ON WING DAMAGED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER HINGE IAW EMB-145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (AILERON) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LT AILERON OUTBOARD HINGE POINT HAS MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE POINT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK CENTER SERVICE DOOR SILL IS CORRODED (LEVEL 2 LOCAL) IN VARIOUS SPOTS. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LT OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) FRAME 46-53. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM BUTTSTRAP FRAME 46-53 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK RT DOUBLER AT FRAME 61 CORRODED (LEVEL 2 LOCAL) AT RIVET HOLES (BEHIND CARBON CROSS BEAM). MAINTENANCE REMOVED AND REPLACED RT DOUBLER AT FRAME 61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (LT WING) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK LEFT O/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT O/B LEADING EDGE SPLICE SHEAR CLIP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 24,392 hrs · 22,961 cycles

SHV - DURING C-CHECK FRAME 10 CRACKED AT STRINGER 13L. MAINTENANCE REMOVED AND REPLACED CHANNEL AT FRAME 10 STRINGER 13L IAW EMB-145 SRM 51-40-02 AND CPM 51-21-05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL HANDLE — INOPERATIVE (COCKPIT) · airframe 24,234 hrs · 22,793 cycles

IAH - FLIGHT 2867, DURING CLIMB 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 HANDLE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,409 hrs · 20,954 cycles

FLIGHT 3029, DURING POST FLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT IDENTIFIER AT AN OVERWING TO BE INOPERATIVE. MAINT INSPECTED THE AC, AND REMOVED AND REPLACED THE NR (3) INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (WING) · airframe 22,161 hrs · 20,713 cycles

WING SKIN CRACK ON LEFT I/B CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01143. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (NLG) · airframe 22,147 hrs · 20,700 cycles

IAH - FLIGHT 2638, THE CREW REPORTED A NOISE COMING FROM UNDER THE CENTER CONSOLE DURING FLIGHT, AND THE CREW SUSPECTED THE NOSE GEAR DOORS TO BE OPEN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPLICE — DAMAGED (BLEED AIR SYS) · airframe 21,566 hrs · 20,114 cycles

SHV - FLIGHT 2249 - DIVERTED INTO SHV DUE TO A BLEED 2 VALVE FAIL MESSAGE ON DEPARTURE. MAINTENANCE REPAIRED SPLICE SP 11183 IAW EMB 145 SWPM 20-21-00. OPS CHECK GOOD IAW EMB 145 AMM II 36-00-00-700-803-A. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SQUAT SWITCH — INOPERATIVE (RT MLG) · airframe 21,134 hrs · 19,650 cycles

IAH - FLIGHT 2845, THE CREW REPORTED A GEAR LEVER AIR/GRND FAIL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE WEIGHT ON WHEELS PROXIMITY DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BURNED (EMERGENCY LIGHT) · airframe 20,711 hrs · 19,197 cycles

IAH FLIGHT 2637, THE CREW REPORTED A BURNING SMELL NEAR SEAT 1A. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BULB SOCKET FOR BURNED. THE CABIN LIGHTING WAS PLACED ON MEL 33-20-00 CAT-C CTL NUMBER 124492, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.THE AIRCRAFT RETURNED TO IAH ON FLIGHT 3141 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERAQTIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,583 hrs · 19,062 cycles

IAH - FLIGHT 2830, THE CREW REPORTED THAT THE READING LIGHT AT SEAT 5A FLICKERED ON AND OFF AND CREATED SMOKE. THE F/A PUSHED THE RESET BUTTON AND THE LIGHT WOULD NOT TURN OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AFFECTED READING LIGHT AND CABIN AREA WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 20,330 hrs · 18,790 cycles

HRL - FLIGHT 2002, DURING PREFLIGHT INSPECTION THE CREW REPORTED A POSSIBLE BURNING SMELL IN THE GALLEY WHEN THE AIRCRAFT WAS POWERED UP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CABIN LIGHT BALLAST A SEAT 1A TO BE BURNT. THE BALLAST WAS DISCONNECTED AND THE CABIN LIGHT PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED BALLAST, OPERATIONALLY CHECKED THE LIGHTING SYSTEM WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — SMOKE (CABIN) · airframe 20,123 hrs · 18,566 cycles

IAH - FLIGHT 2372, THE CREW REPORTED AN OVERWHELMING SMELL OF SMOKE IN THE CABIN AND COCKPIT THAT GOT BETTER WITH THE PACKS OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE NUMBER ONE ENGINE HAD SUFFERED A BIRD STRIKE. MAINTENANCE CLEANED THE RESIDUE FROM THE ENGINE, BORESCOPE INSPECTED AND OPERATIONALLY CHECKED WITH NO DEFECTS/SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 20,034 hrs · 18,470 cycles

IAH FLT 2903, THE CREW REPORTED A BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WIT NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 20,014 hrs · 18,449 cycles

IAH - FLIGHT 2811, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. THE CREW DISCHARGED BOTH BAGGAGE FIRE BOTTLES, AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 20,014 hrs · 18,448 cycles

IAH - DURING MAINTENANCE INSPECTION THE BAGGAGE SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 19,906 hrs · 18,324 cycles

MEM - DURING MAINTENANCE INSPECTION THE BAGGAGE FIRE DETECTOR WAS FOUND TO BE INOPERATIVE. THE DETECTOR WAS PLACED ON MEL 26-23-00 CAT C CONTROL NUMBER 115843, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 4930 WHERE MAINTENANCE REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,118 hrs · 17,389 cycles

IAH - DURING A-CHECK INSPECTION, THE LEFT HAND EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — NO INDICATION (CARGO BAY) · airframe 18,739 hrs · 16,930 cycles

SHV-FLT 2384 SHV TO IAH. DURING PREFLIGHT CHECKS THE BAGGAGE SMOKE INDICATOR ON THE EICAS WOULD NOT ILLUMINATE DURING THE OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 BAGGAGE SMOKE DETECTOR IAW EMB 145 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,370 hrs · 16,498 cycles

JAN - FLIGHT 2760, DURING PREFLIGHT INSPECTION ,THE FORWARD SECTION OF EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,370 hrs · 16,498 cycles

JAN - FLIGHT 2760, DURING PREFLIGHT INSPECTION ,THE FORWARD SECTION OF EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LEVER — INTERMITTENT (MLG) · airframe 17,248 hrs · 15,256 cycles

CREW REPORTED, "NOSE GEAR DOOR[S] OPENED DURING CLIMB-OUT AT 15000 FT AND 290 KNOTS." MX R & R LGEU AND NLG ACT PROX SWITCHES 2. A/C TEST FLT FOR VERIFICATION TESTED UNSATISFACTORY ON 8/29/2005 AS CO3475, "MLG INDICATES UP NOSE GEAR DOOR VISUALLY VERIFIED OPEN". MX INSPECTED WIRING PER WIRING MANUAL FOUND HIGH RESISTANCE AT PIN 10 AT LEVER TO GS0255DC AND HIGH RESISTANCE AT PLUG P7123. WHEN LEVER CYCLED DURING L/G RETRACTION TEST WAS INTERMITTENT. R/R`D L/G RETRACTION LEVER IAW EMB145 MM NR 32-32-08 AND GROUNDING BLOCK GS025506 IAW EMB145 WIRING MANUAL NR 20-13-05. MLG RETRACTION TEST GOOD, TEST FLEW A/C SATISFACTORILY. A/C RETURNED TO SERVICE.

Part: SOLENOID VALVE — FAULTY (NLG) · airframe 17,237 hrs · 15,245 cycles

CREW REPORTED, "NOSE GEAR DOORS DID NOT CLOSE ON FIRST RETRACTION CYCLE, CLOSED ON SECOND RETRACTION CYCLE ALL INDICATIONS GOOD." MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR SOLENOID VALVE IAW EMB145 MM NR 32-53-02 AND OPS CHECKED GOOD IAW EMB145 MM NR 32-30-00. NO FAULTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,737 hrs · 13,585 cycles

DURING ROUTINE MAINTENANCE, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY.

Part: FRAME — CHAFED (FUSELAGE) · airframe 15,498 hrs · 13,326 cycles

DURING SCHEDULED INSPECTION FRAMES 68 AND 70 AT STRINGER 13R WERE FOUND CHAFED. REPAIRED CHAFED AREAS BY BLENDING THE DAMAGED AREA IAW EC 5310-01292. AIRCRAFT RETURNED TO SERVICE.

Part: STOP — ELONGATED (PAX DOOR)

DURING SCHEDULED INSPECTION THE TWO UPPER COMMON TO MAIN DOOR STOPS AT FRAME 18 AND STRINGER 61 WERE ELONGATED. OVERSIZED HOLES, AND REWORKED PER ED5310-01291. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — FAULTY (CABIN LIGHT)

YUL FLIGHT 2847 THE CREW REPORTED SMOKE IN CABIN FROM PSU 11/12A. MAINTENANCE INSPECTED AND REPLACED THE CABIN LIGHT BALLAST AT 12A. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320-01067 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION THE LEFT HAND SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 60 AND 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IN ACCORDANCE WITH EMB-145 SRM51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320-01067 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH EMB-145 SRM 51-20-03, AND 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION,THE SUPPORT RAMP AND REINFORCING ANGLE WERE FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED THE SUPPORT RAMP AND THE REINFORCING ANGLE IN ACCORDANCE WITH EMB-145 SRM 51-40-02.

Part: CREASE BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION.THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION, THE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSS BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION, THE LEFT, CENTER, AND RIGHT HAND BUTT STRAPS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTIONS OF BUTT STRAPS IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CREASE BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320-01068. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 18. MAINTENANCE REMOVED THA DAMAGED SECTIONS OF BUTTSTRAP, AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,536 hrs · 9,307 cycles

SHV-DURING C-CHECK INSPECTION,THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 22.MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTIONS OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BLOWN (CABIN) · airframe 10,492 hrs · 8,347 cycles

TYS During a scheduled inspection, The emergency light above seat 12A was found not working. Maintenance removed and replaced the light bulb, operational checkes good I.A.W.-EMB-145-MM-33-50-08, Aircraft will be released to service upon complection of inspection.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - FLIGHT 4038, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE EMERGENCY LIGHT SWITCH, AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,500 hrs · 4,688 cycles

TYS DURING A SCHEDULED INSPECTION THE FWD RIGHT HAND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-145 MM 33-50-07, OPEATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OXYGEN MASK — DEPLOYED (CABIN)

BTV - FLT 4218 - CREW REPORTED SEAT 17A OXYGEN MASK DEPLOYED INFLIGHT. MAINTENANCE ADJUSTED LATCHING MECHANISM AND RESECURED THE OXYGEN MASK IAW EMB145 AMM 35-20-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAULTY (E/E BAY)

EWR-CREW REPORTED AFTER TAKEOFF, GEAR WOULD NOT RETRACT. NOSE GEAR DISAGREED WITH MAIN GEAR INDICATION AIRCRAFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT A/C AND FOUND FAULTY LANDING GEAR ELECTRONIC UNIT REMOVED AND REPLACED LGEU GEAR SWUNG AND OPS. CHECKED SYSTEM GOOD IAW EMB 145 32-32-00. A/C RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH-DURING C-CHECK INSPECTION, THE NUMBER 8 EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB145 M/M 33-50-00-700-001A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DAMAGED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT STRIP ON PANEL 251BF WAS FOUND TO HAVE A DAMAGED CONNECTOR. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB145 M/M 33-50-00-700-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — CRACKED (FUSELAGE)

IAH-DURING C-CHECK INSPECTION, THE APU BLEED DUCT WAS FOUND TO BE CRACKED BETWEEN THE AFT PRESSURE BULKHEAD AND THE APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BLEED DUCT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH-DURING C-CHECK INSPECTION, THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY WAS FOUND TO HAVE A BLOWN FUSE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IN ACCORDANCE WITH EMB145 M/M 33-50-00-700-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (FUSELAGE)

IAH-DURING C-CHECK INSPECTION, THE LEFT HAND EMERGENCY LIGHT ON PANEL 191 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IN ACCORDANCE WITH EMB145 M/M 33-50-00-700-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT RAMP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — WORN (COCKPIT)

IAH-DURING C-CHECK INSPECTION, THE CAPTAINS AND FIRST OFFICERS SEAT TRACKS WERE FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACKS IN ACCORDANCE WITH EMB145 SRM 53-01-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: UNKNOWN — SMOKE (CABIN)

YUL - FLT 4009 - CREW REPORTED SMOKE IN AIRCRAFT AFTER TAKEOFF SUSPECT NR 1 PACK. MAINTENANCE DISPATCHED TO YUL, PERFORMED HARD/OVERWEIGHT LANDING INSPECTION AND RELEASED A/C IAW MEL NR 21-51-00 CATERGORY C PLACARD NR 003822. AIRCRAFT RETURNED TO SERVICE. ON NEXT TAKEOFF SMOKE REPORTED IN A/C. AFTER TAKEOFF SUSPECT NR 2 PACK. MAINTENANCE SUSPECTED DE-ICE FLUID IN APU INLET CAUSING SMOKE. TEST FLIGHT OF AIRCRAFT REQUIRED BEFORE RETURN TO SERVICE. AIRCRAFT TEST FLEW SATISFACTORY TO EWR. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PIN — LOOSE (NR 1 RAM AIR)

CLE - FLT 4237 - THE CREW REPORTED THE RAM AIR FAILED DURING FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE SECURED A LOOSE PIN ON THE NR 1 RAM AIR ACTUATOR AND PERFORMED OPERATIONAL CHECKS IAW EMB145 MM 21-25-00, NO DEFECTS WERE NOTED. THE AIRCRAFT RELEASED TO SERVICE. (M)

Part: GENERATOR — FAILED (NR 2)

CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AIR RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M)

Part: GENERATOR — FAILED (NR 3)

CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AIR RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M)

Part: GENERATOR — FAILED (NR 5)

CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AIR RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M)

Part: GENERATOR — FAILED (NR 4)

CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AIR RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M)

Part: GENERATOR — FAILED (NR 1)

CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AIR RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M)

Part: BULB — FAILED (ROW 3)

BTV - FLT 4218 - EMERGENCY LIGHT IN PASSENGER DOOR AND OVERHEAD ROW 3 INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT IN PASSENGER AND OVERHEAD ROW 3, OPS CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (LT/RT EMER EXIT)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (LT/RT EMER EXIT)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ADC — FAILED (COCKPIT)

CLE - FLT 4101 - CREW REPORTED THAT WHILE IN CRUISE FLIGHT, THE NR 2 ADC CAUSED NUMEROUS PROBLEMS WITH AIRSPEED AND ALTITUDE. THE CREW ALSO HAD THE NR 1 ENGINE CONTROL A/B FAIL AND THE NR 2 ENGINE B CONTROL FAIL, WHICH WOULD NOT RESET. AIRCRAFT DIVERTED INTO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ADC IAW EMB-145 MM 34-13-00, 34-15-00 AND 34-15-01. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: CARBON SEAL — DAMAGED (RT ENGINE)

EWR - FLT 4222 - CREW REPORTED THAT WHILE EN ROUTE TO EWR RECEIVED A LOW OIL PRESSURE WARNING ON THE RIGHT ENGINE. THE CREW ACCOMPLISHED A COMMANDED ENGINE SHUT DOWN AND LANDED IN EWR WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT ENGINE AND FOUND THE MAGNETIC CARBON SEAL FOR THE STARTER TO BE DAMAGED AND LEAKING. THE SEAL WAS REMOVED AND REPLACED IAW EMB-145 MM TASK NR 72-63-10-000-802 AND NR 72-63-10-400-802, OPERATIONAL AND LEAK CHECKS WERE GOOD. (M)

Part: BULB — FAILED (CABIN)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND AFT AND LEFT HAND AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AFT AND LEFT HAND AFT EXTERIOR EMERGENCY LIGHT BULBS IAW EMB-145 MM 33-50-07. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)