N13988

Part: ACM — FROZEN (NR 1) · airframe 44,298 hrs · 33,809 cycles

DFW - FLIGHT 3999 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PLANE AND PLACED THE NUMBER ONE PACK ON MEL 21-51-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 12/02/18 IAH 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: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 43,278 hrs · 32,999 cycles

PILOT REPORTED AN ODOR, CABIN LIGHT WAS GETTING TOO HOT. MX PERFORMED AN INSPECTION OF THE CABIN LIGHTING AND FOUND CABIN LIGHTING CONTROL MODULE AND 1A LIGHT BALLAST BAD. REMOVED AND REPLACED LIGHT CONTROL MODULE AND BALLAST, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRANSDUCER — FAULTY (WHEEL SPEED) · airframe 43,191 hrs · 32,938 cycles

CREW REPORTED BRAKES WERE SLOW TO REPOND ON LANDING ROLLOUT FOR LANDING. BRAKING WAS NORMAL ON BOTH SIDES ON TAXI TO GATE. REMOVED AND REPLACED THE NR 3 WHEEL SPEED TRANDSDUCER IAW MM 32-41-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (BRAKES) · airframe 35,013 hrs · 26,582 cycles

PILOT REPORTED BRAKES ARE NOT EFFECTIVE AT HIGH SPEEDS, FINE AT IDLE SPEED. LITTLE OR NO BRAKING ACTION ON LANDING. MX REMOVED AND REPLACED THE BRAKE CONTROL UNIT AND OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (FRAME 75) · airframe 41,025 hrs · 31,145 cycles

CRACK ON LT REAR STRINGER 2L AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, ITEM 3, FIG 202.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 41,025 hrs · 31,145 cycles

SERVICE DOOR FRAME FORWARD SILL CUT OUT CORRODED. SILL REPLACED AS PER SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 75) · airframe 41,025 hrs · 31,145 cycles

LEFT REAR FUSELAGE SKIN CRACKED AT TWO PLACES AT FRAME 75, STRINGER 21L. REPAIRED THE SKIN IAW SRM 53-31-01, PARA 11, FIG 219, SHEET 2.

Part: TRUNNION — CORRODED (RT MLG) · airframe 41,025 hrs · 31,145 cycles

RIGHT MLG FORWARD LOWER TRUNNION CAP CORRODED. THE TRUNNION CAP WAS REPLACED IAW CARD 57-26-00-220-C02-A00.

Part: BEARING RACE — CORRODED (RT MLG TRUNNION) · airframe 41,025 hrs · 31,145 cycles

CORROSION FOUND ON THE RT MLG FWD UPPER TRUNNION BEARING RACE. THE CORROSION WAS BLENDED OUT IAW 51-10-03 AND ETD2017-145-032710. NDT INSPECTION PERFORMED WITH NO FAULTS.

Part: SUPPORT — CORRODED · airframe 41,025 hrs · 31,145 cycles

RIGHT OTBD LAVATORY SUPPORT CORRODED. THE SUPPORT REPLACED IAW SRM 51-40-02

Part: SKIN — CORRODED (FRAMES 65-68) · airframe 41,025 hrs · 31,145 cycles

AFT FUSELAGE FRAMES 65 AND 68 CORRODED UNDER RADIO ALTIMETER ANTENNA. CORROOSION REMOVED IAW ETD2017-145-032887.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 41,025 hrs · 31,145 cycles

CARGO DOOR LOWER BEAM CORRODED. CARGO DOOR ENTRY LOWER BEAM REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 65) · airframe 41,025 hrs · 31,145 cycles

AFT FUSELAGE SKIN CRACKED AT FRAME 65, AFT RADIO ALTIMETER ANTENNA MOUNT HOLES. REPAIRED IAW ETD2017-145-032887.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,025 hrs · 31,145 cycles

CABIN LT OTBD SEAT TRACK NR 6 CORRODED. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06-400-801-A.

Part: ANGLE — CRACKED (FRAME 10) · airframe 41,025 hrs · 31,145 cycles

COCKPIT LT FRAME 10, UPPER ANGLE CRACKED. THE FRAME ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: PIN — CORRODED (HORIZONTAL STAB) · airframe 41,025 hrs · 31,145 cycles

HORIZONTAL STAB RT PIN CORRODED. PIN REPLACED IAW MM 55-10-01

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,025 hrs · 31,145 cycles

CABIN RT OUTBOARD SEAT TRACK 3 CORRODED. SEAT TRACKED 3 REPLACED IAW AMM 53-01-06-400-801-A

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,025 hrs · 31,145 cycles

CABIN RT OUTBOARD SEAT TRACK NR 4 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801-A.

Part: DOUBLER — CORRODED (WATER FILL PORT) · airframe 41,025 hrs · 31,145 cycles

RIGHT CENTER FUSELAGE CORROSION AROUND POTABLE WATER HEATED NIPPLE. DOUBLER BLENDED IAW SRM 51-10-05

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,025 hrs · 31,145 cycles

FRAME 80 LT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 41,025 hrs · 31,145 cycles

HORIZONTAL STAB LT PIN BUSHING CORRODED. BUSHING REPLACED IAW MM 55-10-01.

Part: FRAME — CRACKED (FRM 10) · airframe 41,025 hrs · 31,145 cycles

COCKPIT RT FRAME 10 CRACKED. THE FRAME WAS REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,025 hrs · 31,145 cycles

RT CABIN SEAT TRACK NR 1 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801A

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 41,025 hrs · 31,145 cycles

SERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 41,025 hrs · 31,145 cycles

HORIZONTAL STAB RT PIN BUSHING CORRODED. PIN BUSHING REPLACED.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,025 hrs · 31,145 cycles

FRAME 80 RT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02

Part: CROSSBEAM — CRACKED (NLG BAY) · airframe 41,025 hrs · 31,145 cycles

NLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.

Part: CROSSBEAM — CRACKED (NLG BAY) · airframe 41,025 hrs · 31,145 cycles

NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.

Part: FLAPPER VALVE — LEAKING (RIGHT WING) · airframe 39,809 hrs · 30,208 cycles

THE CREW REPORTED FUEL STREAMING FROM THE LEFT WING INFLIGHT. MAINTENANCE INSPECTED AND FOUND RIGHT WING FLAPPER VALVE DAMAGED. REPLACED THE FLAPPER VALVE AND OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,192 hrs · 25,737 cycles

THE CREW REPORTED AN EMERGENCY LIGHTS NOT ARMED EICAS MESSAGE IN FLIGHT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE OVERHEAD LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,197 hrs · 25,740 cycles

DURING CRUISE, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE EMERGENCY LIGHTS WERE NOT ARMED. MAINTENANCE R & R THE F/A LIGHTING CONTROL PANEL. THE EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — STUCK (NR 1 ENGINE.) · airframe 33,025 hrs · 24,863 cycles

AIRCRAFT MADE AN AIR RETURN WHEN THE ENGINE NR 1 SHOWED THAT THE ENGINE 1 BLEED VALVE WAS CLOSED. MAINTENANCE R & R THE NR 1 ENGINE BLEED VALVE REF AMM 36-11-05 AND IPC REF 36-11-05, FIGURE 1A ITEM. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 32,431 hrs · 24,395 cycles

THE CREW REPORTED A NR 1 WINDSHIELD FAILED IN FLIGHT ALONG WITH A ELECTRICAL BURNING SMELL. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD. OPS CHECKS WERE GOOD. THEY ALSO REPLACED THE NR 1 HEAT CONTROLLER AND THE NR 1 WINDSHIELD HEAT CONTACTOR.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,419 hrs · 24,385 cycles

THE CREW REPORTED A ELECTRICAL BURNING ODOR AFTER WINDSHIELD NR 1 FAIL INFLIGHT. MX INSPECTED AND FOUND NO ELECTRICAL BURNING ODOR. PERFORMED OPS CHECK OF WINDSHIELD HEAT AND NO DEFECTS WERE FOUND. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — FAULTY (WINDSHIELD HEAT) · airframe 32,410 hrs · 24,377 cycles

THE CREW REPORTED A BURNING SMELL WHEN WINDSHIELD HEAT NR 2 IS ON. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD.

Part: CONTROLLER — FAULTY (WINDSHIELD HEAT) · airframe 32,410 hrs · 24,377 cycles

THE CREW REPORTED BURNING ODOR WITH WINDSHIELD HEAT NR 1 ON. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD HEAT CONTROLLER. OPS CHECKED GOOD.

Part: DUCT — LOOSE · airframe 32,054 hrs · 24,093 cycles

CREW REPORTED PACK NR 2 VALVE CLOSED ON EICAS MESSAGE IN FLIGHT WHICH RESULTED IN LOSS OF BOTH AIR CONDITIONING PACKS AND PRESSURIZATION DUE TO NR 1 PACK BEING ON MEL. MX PERFORMED SERVERAL OPERATIONAL CHECKS OF THE PACK NR 2 SYS SUCCESSFUL WITH NO MESSAGES NOTED ON THE EICAS. MX ALSO RESECURED A BLOWN OFF DUCT AND CLAMPS ON THE NR 1 PACK. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,618 hrs · 2,372 cycles

DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 2R AT FR75. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,618 hrs · 23,742 cycles

DURING A-CK INSPECTION THE AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 6L ON FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,618 hrs · 23,742 cycles

DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 8R AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,618 hrs · 23,742 cycles

DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET EBLOW STR 8L AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,618 hrs · 23,742 cycles

DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STRINGER 4R AT FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 31,565 hrs · 23,699 cycles

MX REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. REPLACED RELAY K0275. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

SERVICE DOOR CUT-OUT HAS CORROSION BEYOND LIMITS AFTER BLEND-OUT. R & R REINFORCEMENT STRUCTURE.

Part: GUSSET — CORRODED (FUELAGE) · airframe 31,113 hrs · 23,338 cycles

CORROSION BEYOND LIMITS AFTER BLEND-OUT AT SCREW HOLES IN CENTER OMEGA BEAM GUSSET. R & R GUSSET.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

LOWER CORNER OF SERVICE DOOR CUT-OUT REINFORCMENT STRUCTURE IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SERVICE DOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

OMEGA BEAM AT FRM 20 HAS AREAS OF CORROSION BEYOND LIMITS AFTER BLEND-OUT. CUT-OUT DAMAGE, FABRICATED AND INSTALLED.

Part: FRAME — CORRODED (REAR FUSELAGE 1) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND UNDER THE LWR FWD CHAFED PLATE AT CARGO DOOR FRAME 65,STRINGER 17L. MX CUT OUT DAMAGE AREA AND INSTALL A NEW REPAIR ON THE FRAME REF SRM 53-31-04. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CROSSBEAM — CORRODED (CENTER FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE CROSS-MEMBER AT FRAME 20. MX REMOVED THE CORROSION AND INSTALLED A NEW PART AT FRAME 20 SRM 51-40-02 AND 51-40-03. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN A FLOOR SUPPORT ANGLE BETWEEN FRAMES 23 AND 24. MX R & R THE FLOOR SUPPORT ANGLE REF SRM 51-40-02; 51-40-03 AND CPM 51-23-04. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FRAME — CORRODED (PAX DOOR) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE INTERNAL SIDE OF THE MAIN PAX DOOR ALONG LOWER FRAME AT STR 14L. MX R & R THE AFT AND FWD FRAMES WITH NEW FRAMES REF SRM 51-40-02. ALL WORK COMPLIED WITH AND WILL BE RELEASED AT END OF THE CHECK.

Part: GUSSET — CORRODED (CENTER FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE GUSSET AT THE CENTER OMEGA BEAM AT FRAME 59 THRU 61. MX R & R THE CENTER OMEGA BEAM GUSSET AT FRAME 59 THRU 61 IN REF SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED · airframe 31,113 hrs · 23,338 cycles

ACFT IN IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE LT SILL AT SCREW HOLES AT FRAMES 19 AND 20. MX REMOVED THE DAMAGED PART, DRILLED AND INSTALL A NEW SILL RE SRM 51-40-02 AND 51-40-03. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK THE CENTER OMEGA BEAM AT FRAME 18 TO FRAME 23 WAS FOUND CORRODED AND OUT OF LIMITS. MX R & R A NEW OMEGA BEAM REFERENCING SRM 51-40-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: STRUCTURE — CORRODED (REAR FUSELAGE) · airframe 31,113 hrs · 23,338 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LAV DUMP HOUSING EXTERNAL SIDE AT DUMP CHUTE. MX R & R THE LAV DUMP CHUTE IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,853 hrs · 22,361 cycles

CABIN EMERGENCY EXIT LIGHTS FOR AISLE INOPERATIVE AT ROW 12 AND AFT. R & R EMERGENCY LIGHT INVERTER NR 6 AND R & R FLOOR PROXIMITY LIGHT NR 8. OPS CHECKED GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: BLEED AIR SYS — MULTIPLE FAIL · airframe 29,443 hrs · 22,021 cycles

ACFT DIVERTED WITH A BLEED LEAK ISSUE. MX RETORQUED NR 2 ENGINE BLEED VALVE AND THE Y DUCT. RETORQUED SEVERAL NR 2 SYSTEMS PACT DUCTS. OPS AND LEAK CHECKED GOOD IAW CHRONIC WORKSHEET,CONTROL NR 594620. BLEED LEAK TASK CARD 6836001 ON NR 2 SIDE ONLY. ACFT WAS RELEASED BACK TO SERVICE. NO PARTS INVOLVED.

Part: LATCH — FAULTY (OXYGEN MASK) · airframe 28,769 hrs · 21,487 cycles

DURING ROUTINE MX, OXYGEN MASK WOULD NOT DEPLOY AT SEAT 16BC. MX INSPECTED AND REPLACED THE OXYGEN DOOR ELECTRICAL LATCH. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,752 hrs · 20,689 cycles

FLT 5864 PWM CREW REPORTED A BIRD STRIKE ON TAKEOFF AND PERFORMED AN AIR RETURN BACK TO PWM WITHOUT INCIDENT. NORTHEAST AVIATION MX PERFORMED BIRD STRIKE INSPECTION IAW EMB145 AMM 05-50-08 WITH DAMAGE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 27,366 hrs · 20,377 cycles

IAH - FLIGHT 2688, THE CREW REPORTED THAT THE MAIN AND BACKUP PITCH TRIMS WERE INOPERATIVE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT (HSCU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROCESSOR — INOPERATIVE (COCKPIT) · airframe 27,210 hrs · 20,563 cycles

FLIGHT 3065 - EWR - FLIGHT CREW REPORTED CAPT AIR SPEED INOP IN FLIGHT DURING CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVES AND REPLACED AIR DATA PROCESSOR UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 26,130 hrs · 19,468 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER SUPPORT CORRODED. REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 53-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 26,130 hrs · 19,468 cycles

SHV - DURING C-CHECK SERVICE DOOR LOWER AFT CUTOUT HAS CORROSION AT STR 12R. REPAIRED SERVICE DOOR LOWER AFT CUTOUT IAW EC5310-01373. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 25,888 hrs · 19,291 cycles

PRESSURIZATION FAILED IN FLIGHT AT FL290. REMOVED AND REPLACED DIGITAL PRESURIZATION CONTROLLER IAW EMB 145 AMM 21-31-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,546 hrs · 19,030 cycles

FLIGHT 2736 - EWR - FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN GALLEY WHEN COFFEE POTS TURNED ON. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 24,719 hrs · 18,416 cycles

IAH - FLIGHT 2751, THE CREW REPORTED A BATT TWO OVERTEMP INDICATION. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 21,738 hrs · 16,208 cycles

FLIGHT 2331 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET AIR GROUND CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RUDDER ACTUATOR) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK HYDRAULIC SYSTEM 1 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INLET — CORRODED (LT ENGINE) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK LT ENG INLET HAS CORRODED BOLT HOLE. MAINTENANCE REPAIRED LT ENGINE INLET MOUNTING ATTACHMENT FLANGE BOLT HOLE IAW EC5420-01158. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV B. PERFORMED BACKLASHES IAW EMB-145 AMM 27-11-00 AND DEFLECTIONS IAW EMB-145 AMM 27-10-00-700-801-A. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK FRM 65 SHEAR CLIP CORRODED AT LWR BEAM. MAINTENANCE REPAIRED FRM 65 SHEAR CLIP AT LOWER BEAM IAW EC5330-01458. ALODINE, PRIMED AND PAINTED IAW EMB 145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RUDDER ACTUATOR) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK HYD SYSTEM 2 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER 1 ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — WORN (LT AILERON) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 AND COMPLETED OPS CHECKS IAW EMB 145 AMM 27-11-00 AND AMM 27-10-00-700-801-A. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,372 hrs · 15,940 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. MAINTENANCE INSTALLED NEW SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

FLIGHT CREW REPORTED AUTO PRESSURIZATION FAILED DURING TAXI OUT. MX REMOVED AND REPLACED PRESSURIZATION MANUAL CONTROLLER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE, MX FOUND SEAT 12 BC OVERHEAD SQUARE EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K)

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT)

IAH FLIGHT 2312 DURING POST FLIGHT INSPECTION THE GALLEY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE GALLEY EMERGENCY LIGHT BALLAST, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 16,860 hrs · 12,735 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER FRAME HAS CORROSION. MX REMOVED AND REPLACED LOWER FRAME OF CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,860 hrs · 12,735 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: STRUT — LOW (NLG) · airframe 16,777 hrs · 12,673 cycles

IAH - FLIGHT 2887, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON TAKEOFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE SERVICED THE NOSE LANDING GEAR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 16,637 hrs · 12,556 cycles

DURING ROUTINE MAINTENANCE, MX FOUND LT FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO FLIGHT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,478 hrs · 12,432 cycles

RIC - MX DURING SCHEDULE ROUTINE MAINTENANACE, MX FOUND 02 EMERGENCY AISLE LIGHTS INOP. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,423 hrs · 12,390 cycles

EWR LOG SQUAWK FLT 2325 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,371 hrs · 12,355 cycles

MAF - FLIGHT 2760, DURING PREFLIGHT THE CREW REPORTED THE AFT THREE EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. THE CREW CHARGED THE EMERGENCY LIGHTS SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,114 hrs · 12,153 cycles

IAH - FLIGHT 2642, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE AFT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESET THE AFT EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 16,099 hrs · 12,141 cycles

CLE FLIGHT 2913 THE CREW REPORTED A LAV SMOKE INDICATION INFLIGHT. NO FIRE OR SMOKE WAS PRESENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: ROLLER — SEIZED (CABIN DOOR) · airframe 16,064 hrs · 12,111 cycles

CLE FLIGHT NR 2816, THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE AFT UPPER ROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,904 hrs · 11,981 cycles

DURING A POST FLIGHT INSPECTION THE AFT EMERGENCY LIGHT AISLE PATH LIGHTING STRIP WAS INOPERATIVE. THE NR 4 EMERGENCY BATTERY PACK WAS REPLACED, THE LIGHTING SYSTEM TESTED AND THE DISCREPANCY CLEARED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,330 hrs · 11,529 cycles

SDF - LT FWD FAIRING EMERGENCY LIGHT, AISLE 1 EMERGENCY LIGHT, AND COCKPIT FLOOD EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,224 hrs · 11,449 cycles

FWD EMERGENCY LIGHT LT SIDE INOP. REPLACED FUSE AT NR 1 EMERGENCY LIGHT BATTERY CRADLE IAW EMB-145 VCMM 25-60-03. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 15,224 hrs · 11,449 cycles

EMERGENCY LIGHT AT TOP OF COCKPIT CEILING INOP. REPLACED FUSE AT NR 1 EMERGENCY BATTERY CRADLE IAW EMB 145 VCMM 25-60-03. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 14,992 hrs · 11,272 cycles

CLE FLIGHT 2098 THE CREW REPORTED THE OUTER LOWER LEFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FUSE ON THE NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,736 hrs · 11,063 cycles

DURING POSTFLIGHT, CREW REPORTED LEFT FAIRING EMERGENCY LIGHT NOT OPERATING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER IAW EMB145 AMM NR 33-50-04, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,901 hrs · 10,434 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LEFT FORWARD EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: CONNECTOR — SHORTED (ENGINE) · airframe 12,838 hrs · 9,580 cycles

THE CREW REPORTED THE AIRCRAFT WOULD NOT ACCEPT CLIMB MODE UNTIL APPROX 7000FT, NORMAL AFTER THAT. ON APPROACH AT 3000 FT. SELECTED T/O MODE AND AIRCRAFT STUCK IN T/O RESERVE UNTIL LANDING. MAINTENANCE INSPECTED AND REPLACED CONNECTOR 10584 FOR NR 2 ENGINE RESISTOR MODULE. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,310 hrs · 9,157 cycles

IAH - FLIGHT 2553, DURING PREFLIGHT INSPECTION, THE NR 2 EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AFFECTED LIGHT STRIP ON MEL 3350-00/2 CAT C CONTROL NUMBER 057514, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOP SERVICE. THE AIRCRAFT LANDED IN CRP WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,310 hrs · 9,157 cycles

CRP - DURING MAINTENANCE INSPECTION, THE NUMBER THREE EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,278 hrs · 9,135 cycles

STL - DURING MX INSPECTION, THE EMERGENCY LIGHT BY THE LEFT EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 12,269 hrs · 9,129 cycles

CLE FLIGHT NR2715 - THE CREW REPORTED THE MID CABIN EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL CHECKS WERE GOOD.

Part: LEVER — BENT (MAIN CABIN DOOR) · airframe 12,063 hrs · 8,973 cycles

CREW REPORTED MAIN CABIN DOOR DIFFICULT TO SHUT AND NOT INDICATING CLOSED. MX INSPECTED AND REPLACED SPRING LEVER ON FOLDING FLAP ACTUATING CAM. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — FAULTY (FUSELAGE) · airframe 11,463 hrs · 8,501 cycles

DURING 4A INSPECTION IN BTV, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT SIGN AT SEAT 12A AREA TO BE NOT OPERATING. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT 12A AREA IAW EMB145 MM 33-50-14. OPS CHECKED GOOD.

Part: LIGHT — BURNED OUT (CABIN)

DURING SCHEDULED MAINTENANCE ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WAS FOUND TO BE INOPERATIVE. THE AFFECTED STRIP WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 3230 THE CREW REPORTED THE EMERGENCY OVERHEAD AISLE WING EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY EXIT LAMP. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DELAMINATED (FLAP) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED INSPECTION THE RIGHT INBOARD FLAP LOWER TRAILING EDGE DELAMINATED. MAINTENANCE REPAIRED THE DELAMINATED AREA I/A/W-EC5750-01196, PRIMED AND PAINTED I/A/W-CMP-51-21-03/05/05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM PLATE I/A/W-EMB-135/145-SRM-53-21-10 AND CMP-53-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE CLEANED THE AREA, FILLED WITH EPOXY RESIN, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED A DOUBLER I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-10-02, 51-21-04/05/06 AND GST1927/02A. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (GALLEY SUPPORT) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED INSPECTION THE LEFT WING INBOARD FLAP BOTTOM SIDE HAS TWO AREAS OF DELAMINATION. MAINTENANCE REPAIRED THE DAMAGED AREAS I/A/W-EC5750-01195, EMB-CMP-51-21-03/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED 2C CHECK CORROSION WAS FOUND ON THE SERVICE DOOR SILL, JUST BELOW THE SILL PLATE. MAINT CLEANED CORROSION, FILLED AREA WITH EPOXY RESIN, FABRICATED, ALODINED, PAINTED AND INSTALL REPAIR DOUBLER IAW 135/145 SRM 51-40-02, 51-10-02, CPM 51-21-05-06- AND GST 1927/O2A. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: GUSSET — CORRODED (LAVATORY) · airframe 7,438 hrs · 5,359 cycles

DURING A SCHEDULED 2C INSPECTION THE LAV FLOOR SUPPORT GUSSETS IN ZONE 261DF AND 262CF WERE CORRODED. MAINT INSPECTED AREA, REMOVED AND REPLACED RIVETS ON LT AND RT GUSSETS AS NEEDED. REMOVED AND REPLACED THE CENTER GUSSET, PRIMED AND PAINTED IAW SRM 135/145 51-40-02, EC 2003-145/1150 AND CPM51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (LAV AREA) · airframe 7,438 hrs · 5,359 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE LT FLOOR SILL IN THE LAV AREA HAD SOME CORROSION. MAINT REMOVED AND REPLACED THE LT FLOOR SILL IN THE LAV, REMOVED AND REPLACED LT CARBON FIBER IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

IAH- FLIGHT 2088, LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE, ATTEMPTED TO RECYCLE GEAR TWICE WITH NO CHANGE. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT)

FLIGHT 2910, GEAR DID NOT RETRACT WHEN HANDLE PLACED IN UP POSITION, THIRD TRY SUCCESSFUL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT, OPS TEST GOOD. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — INTERMITTENT (COCKPIT)

CLE FLIGHT#2301 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR EMERGENCY EXTENSION OVERRIDE SWITCH.WIRE SPLICE SP1750 WAS ALSO REPAIRED.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — INTERMITTENT (MLG EMER)

CLE FLIGHT 2301 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR EMERGENCY EXTENSION OVERRIDE SWITCH. WIRE SPLICE SP1750 WAS ALSO REPAIRED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RELAY — FAILED (MLG)

BDL-FLT 2150 CREW REPORTED DURING DESCENT AT 250 KTS, SOUNDED AS THOUGH NOSE GEAR DOORS OPENED, NO OTHER INDICATIONS. MAINTENANCE REMOVED AND REPLACED RELAY K0642 LANDING GEAR CONTROL RELAY, PERFORMED SATISFACTORY OPERATIONAL TESTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — FAULTY

BTV---CO3389, DURING 5A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTS DO NOT COME ON IN AUTO MODE....REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY POWER SUPPLY/CHARGER IAW EMB145 MM 33-50-04. OPS.CHECKED GOOD.

Part: WIRE HARNESS — BURNED (CABIN)

IAH- FLIGHT 4117, DURING CLIMB THE CREW NOTED SMOKE IN THE CABIN AND GOT LAV SMOKE ON THE EICAS. THE CREW RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT SEATS 14A AND 15A. GROUND RAN AIRCRAFT AND FOUND NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL HANDLE — INOPERATIVE (COCKPIT)

IAH - FLIGHT 4196, 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 CONTROL HANDLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LEVER — INOPERATIVE (MLG)

CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. CREW CYCLED LANDING GEAR CONTROL LEVER AND GEAR RETRACTED NORMALLY. A/C LANDED WITHOUT INCIDENT. MX REMOVED/REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM 32-32-02. A/C WAS APPROVED FOR RETURN TO SERVICE.