Embraer EMB-145ER

Service difficulty reports · 1,266

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'EMB145ER'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA03BT039Battery Pack · looseEWR ON PREFLT FOUND MAIN CABIN DOOR EMERGENCY LIGHTS INOP. RERACKED EMERGENCY BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD.Mar 14, 2003 · N16944 · Emb EMB145ER · Emergency LightingSDR C2XA03CL066Lever · intermittentCLE FLIGHT 2846 THE CREW REPORTED AFTER GEAR RETRACTION RECEIVED A MASTER WARNING AND LANDING GEAR LEVER DISAGREE MESSAGE. THE MESSAGE CLEARED WITHIN 10 SECONDS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOODMar 10, 2003 · N17507 · Emb EMB145ER · Landing Gear SelectorSDR C2XA03IA031Lamp · inoperativeDuring postflight inspection the mid cabin emergency exit light would not illuminate. Maintenance removed and replaced the exit light bulb. The system tested good and the aircraft was returned to service.Mar 7, 2003 · N15941 · Emb EMB145ER · Emergency LightingSDR C2XA03CL067Light · inoperativeCLE FLIGHT 2123 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON MID CABIN WALL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Mar 7, 2003 · N15941 · Emb EMB145ER · Emergency LightingSDR C2XA03CL063Actuator · slowCVG 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.Mar 4, 2003 · N14945 · Emb EMB145ER · Landing Gear Door Retract SectionSDR C2XA03SH033Stop · crackedSHV- DURING C-CHECK THE FOWARD EXTERNAL FRAME ON CARGO DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 1, 2003 · N13936 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA03SH032Bracket · crackedSHV-DURING C CHECK THE BRACKET SUPPORTING THE ELEVATOR PULLEYS WAS FOUND CRACKED AND DEFORMED LOCATED IN VERTICAL STABILIZER BY PANEL 325LR. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERFeb 27, 2003 · N13936 · Emb EMB145ER · Flight Control SystemSDR C2XA03SH030Floorbeam · crackedSHV- DURING C-CHECK A RAMP ANGLE WAS FOUND CRACKED ON LEFT HAND FLOORBEAM FOWARD OF FRAME 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED AND ANGLE REPAIR IAW EMB SRM 51-30-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Feb 27, 2003 · N13936 · Emb EMB145ER · Fuselage Main, Floor BeamSDR C2XA03CL060Light · inoperativeCLE FLIGHT 2101 THE CREW REPORTED HALF OF THE EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED NR 2 AND NR 3 EMERGENCY AISLE PATH LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD.Feb 26, 2003 · N17928 · Emb EMB145ER · Emergency LightingSDR C2XA03TY030Sill · corrodedDURING A SCHEDULED 3C INSPECTION THERE WAS EVIDENCE OF CORROSION UNDER THE CARGO DOOR SILL PROTECTIVE PLATE. MAINTENANCE DRILL OUT THE RIVETS IN SILL, REMOVED CORRODED PARTS, FAB NEW BRACKETS AND INSTALL ALONG WITH A NEW CARGO SILL IAW EMB 135/145 SRM 51-40-0Feb 26, 2003 · N14938 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA03SH023Beam · corrodedSHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-21-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH024Beam · corrodedSHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH025Beam · corrodedSHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 24.MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH026Beam · corrodedSHV-DURING C-CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-06.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH027Butt Strap · corrodedSHV-DURING C-CHECK BUTT STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH028Angle · corrodedSHV-DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH029Butt Strap · corrodedSHV-DURING C-CHECK LEFT HAND BUTT STRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE CORRSION.MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03CL050Selector · malfunctionedROC FLIGHT 2025 THE CREW REPORTED THE LANDING GEAR WOULD NOT FULLY RETRACT AFTER DEPARTURE FORM ROC. THE GEAR WAS RECYCLED AND STILL DID NOT FULLY RETRACT. THE AIRCRAFT RETURNED AND LANDED IN ROC WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED IFeb 24, 2003 · N15941 · Emb EMB145ER · Landing Gear SelectorSDR C2XA03CL049Warning System · false indicationCLE FLIGHT 2201 THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE DURING APPROACH INTO SDF. THE LANDING GEAR WAS RECYCLED AND THE MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED MULTIPLE GEAR OPERATIONAL Feb 22, 2003 · N14930 · Emb EMB145ER · Landing Gear Position and WarningSDR C2XA03CL047Duct · separatedCLE FLIGHT 2032 THE CREW REPORTED ON TAXI RECEIVED A APU BLEED LEAK INDICATION THEN A SMOKE ODOR WAS NOTICED. THE APU WAS SHUTDOWN. MAINTENANCE INSPECTED AND FOUND THE APU BLEED DUCT SEPARATED DOWN STREAM OF THE APU SHUT-OFF VALVE. THE BLEED DUCT ASSEMBLY WFeb 22, 2003 · N13929 · Emb EMB145ER · APU Bleed Air SystemSDR C2XA03SH022Strap · corrodedSHV-DURING C-CHECK THE LEFT HAND STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 53-31-19 AND 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH021Sill · corrodedSHV-DURING C-CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 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.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH020Sill · corrodedSHV-DURING C-CHECK THE RIGHT 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.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH010Sill · corrodedSHV-DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH019Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND SILL AND THE LEFT HAND FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH018Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND AND CENTER FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH017Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND LEFT HAND FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH016Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND RIGHT FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH015Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE RIGHT SILL AND RIGHT FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH014Butt Strap · corrodedSHV-DURING C-CHECK THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-01.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH013Butt Strap · corrodedSHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH012Butt Strap · corrodedSHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH011Butt Strap · corrodedSHV-DURING C-CHECK THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA03SH009Butt Strap · corrodedSHV-DURING C CHECK AFT BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AFT BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Feb 22, 2003 · N13936 · Emb EMB145ER · Fuselage Structure (General)SDR RAIA00302050IgniterLEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED "A" IGNITER AND PLACED ON DEFERRAL THE "B" IGNITER, OPS CK OK.Feb 18, 2003 · N808HK · Emb EMB145ER · Spark Plug/IgniterSDR C2XA03SH007Beam · corrodedDURING C-CHECK THE RIGHT DIGITAL BEAM AFT OF SERVICE DOOR WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 TO 23. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Feb 18, 2003 · N13936 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA03CL040Connector · dirtyCLE FLIGHT#2025 THE CREW REPORTED EMERGENCY LIGHTING OVERHEAD IN FORWARD GALLEY WAS INOPERATIVE.MAINTENANCE INSPECTED AND CLEANED CONNECTOR FOR LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.Feb 14, 2003 · N15941 · Emb EMB145ER · Emergency LightingSDR RAIA00302045Switch · intermittentPIT- EMERGENCY LIGHTS ON STAIRS AND BELOW COCKPIT DOOR FLASH OCCASIONALLY. MAINTENANCE CLEANED SWITCH IN DOOR, OPS CHECK OK.Feb 12, 2003 · N808HK · Emb EMB145ER · Emergency LightingSDR C2XA03CL038Handle · looseSYR FLIGHT#2886 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE.MAINTENANCE INSPECTED AND RESECURED THE INSIDE HANDLE ON THE MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD.Feb 11, 2003 · N15948 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA03BT030Connector · faultyCVG/EWR---CO2547, CREW REPORTED "SMOKE COMING OUT PA PHONE BEHIND CAPTAINS HEAD." CVG MAINTENANCE TROUBLESHOT PROBLEM TO FORWARD PA UNIT. DISABLED PA SYSTEM, PULLED PA AND INTERPHONE CIRCUIT BREAKERS AND FORWARD PA CANNON PLUG CONNECTOR. AIRCRAFT MAINTENANCE Feb 11, 2003 · N15941 · Emb EMB145ER · Communications SystemSDR C2XA03BT026Proximity Switch · faultyEWR---CO 2143, CREW REPORTED, " LANDING GEAR/ GROUND FAILURE MESSAGE ON EICAS WHEN GEAR DOWN IS SELECTED." MAINTENANCE REMOVED AND REPLACED LEFTHAND LANDING GEAR SHOCK ABSORBER PROXIMITY SWITCH, OPS. CHECKED GOOD IAW EMB145 MM #32-63-02. AIRCRAFT RETURNED TO Feb 3, 2003 · N14938 · Emb EMB145ER · Landing Gear SystemSDR C2XA03CL029Ballast · faultyCLE FLIGHT#2267 THE CREW REPORTED A ELECTRICAL BURNING SMELL COMING FROM ABOVE THE FLIGHT ATTENDANT CALL PANEL.MAINTENANCE INSPECTED AND REPLACED THE DIMMING BALLAST FOR THE CEILING LIGHTS ABOVE SEAT 1A.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOFeb 3, 2003 · N14925 · Emb EMB145ER · Passenger Compartment LightingSDR C2XA03CL027Windshield · failedCLE FLIGHT 2067 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAFeb 3, 2003 · N14930 · Emb EMB145ER · Flight Compartment WindowsSDR C2XA03CL024Control Unit · failedCLE FLIGHT 2693 THE CREW REPORTED THE LT MAIN LANDING GEAR REQUIRED 3 CYCLES BEFORE LOCKING IN UP POSITION. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. ALSO REPLACED THE UPLOCK BOX ASSEMBLY ON THE LEFT GEAR. OPERATIONAL CHECKS WERE Jan 31, 2003 · N15926 · Emb EMB145ER · Landing Gear Door ActuatorSDR CA030130001Engine · fire(CAN) TRANS STATE EMBRAER 145ER HAD ON GROUND ENGINE FIRE (NO PAX). AFTER DRY ROTOR, MECHANICS NOTED ENGINE FIRE. WHILE TROUBLESHOOTING THE ENGINE DUE TO INABILITY TO START. FUEL SPRAY NOZZLES HAD JUST BEEN CHANGED, FIRE BOTTLES DISCHARGED AND FIRE DEPT CALL Jan 30, 2003 · Emb EMB145ER · Engine (Reciprocating)SDR C2XA03BT015Light · intermittentBDL---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.Jan 26, 2003 · N14945 · Emb EMB145ER · Emergency LightingSDR C2XA03CL022Charger · inoperativeDURING ROUTINE MAINTENANCE THE FORWARD RIGHT EMERGENCY EXTERIOR WING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Jan 23, 2003 · N14930 · Emb EMB145ER · Emergency LightingSDR C2XA03CL021Wire · brokenMKE FLIGHT#2135 THE CREW REPORTED THE EMERGENCY EXIT AISLE PATH LIGHTING FROM ROW 7 FORWARD WAS INOPERATIVE.THEY ALSO REPORTED THE EXIT LIGHT ON THE FORWARD CABIN PARTITION AND THE LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED Jan 22, 2003 · N15941 · Emb EMB145ER · Emergency LightingSDR C2XA03BT012Windshield · crackedBWI---CO2476, CREW REPORTED FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT AIRCRAFT DIVERTED TO BWI. AIRCRAFT LANDED UNEVENTFULLY. EWR MAINTENANCE WORKING WINDSHIELD CHANGE AT THIS TIME.Jan 20, 2003 · N14933 · Emb EMB145ER · Flight Compartment WindowsSDR C2XA03BT011Stall Warning · faultyCREW REPORTED, TAKEOFF CONFIGURATION WARNING ON TAKEOFF ROLL THROUGH 50 KNOTS, WITH AIRCRAFT IN PROPER CONFIGURATION. TAKEOFF ABORTED AND RETURNED TO GATE. MAINTENANCE PERFORMED TAKEOFF CONFIGURATION CHECK TEST IAW EMB145 AMM 31-51-00. OPS CHECKED GOOD. NOJan 20, 2003 · N14930 · Emb EMB145ER · Elevator Control System
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