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 C2XA02SH005Wire · brokenSHV - DURING C-CHECK INSPECTION, THE NUMBER THREE EMERGENCY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES.May 1, 2002 · N17928 · Emb EMB145ER · Light System WiringSDR C2XA02BT018Smoke · detectedCREW REPORTED, DECLARED EMERGENCY FOR SMOKE IN CABIN, SEEMED TO BE COMING FROM NR 2 PACK. MAINTENANCE RAN NR 2 PACK IAW EMB145 MM 21-51-00, NO SMOKE DETECTED. REPEATED PROCESS SEVERAL TIMES, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.Apr 30, 2002 · N13935 · Emb EMB145ER · Air Distribution SystemSDR RAIA00204132Controller · inoperative5258-PIT- BOTH WINDSHIELD WIPERS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WINDSHIELD WIPER CONTROLLER.Apr 21, 2002 · N808HK · Emb EMB145ER · Windshield/Door Rain/Ice RemovalSDR C2XA02SH004Spring · corrodedSHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD AND OUTBOARD LOWER FLAP SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 19, 2002 · N17928 · Emb EMB145ER · Trailing Edge Flap Control SystemSDR C2XA02SH003Spring · corrodedSHV - DURING C-CHECK INSPECTION, THE RIGHT HAND INBOARD AND OUTBOARD FLAP LOWER SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 19, 2002 · N17928 · Emb EMB145ER · Flight Control SystemSDR C2XA02IA094Acm · inoperativeIAH- PACK #1 GIVES SMOKE WHEN OPERATING ON APU BLEED. IAH- MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 ACM. PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS Apr 19, 2002 · N13936 · Emb EMB145ER · Cabin Cooling SystemSDR C2XA02SH006Cowling · crackedSHV - DURING C-CHECK INSPECTION, THE LOWER RIGHT HAND APU COWLING MOUNT OPENING WAS FOUNDS TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK, AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPRApr 16, 2002 · N17928 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA02CL098Bolt · looseCLE FLIGHT#3157 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN.MAINTENANCE INSPECTED AND TIGHTENED THE INNER DOOR HANDLE ASSEMBLY BOLT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 8, 2002 · N15948 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA02CL096Light · inoperativeCLE 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.Apr 2, 2002 · N14945 · Emb EMB145ER · Emergency LightingSDR RAIA00203109Starter · failed5316-PIT-RIGHT ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED RIGHT STARTER, OPS CK OK.Mar 27, 2002 · N808HK · Emb EMB145ER · Engine StarterSDR C2XA02IA081Apu · leakingDURING APPROACH FLIGHT 3649, THE CREW NOTED THAT THE APU FAILED ON APPROACH/STRONG FUEL ODOR IN CABIN AND COCKPIT. IAH- MAINTENANCE INSPECTED THE APU, AND, THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIMar 25, 2002 · N17928 · Emb EMB145ER · Airborne Auxiliary Power Unit (APU) SystemSDR C2XA02CL078Charger · inoperativeDURING ROUTINE MAINTENANCE FOUND STRIPS 2 AND 3 OF THE EMERGENCY AISLE PATH LIGHTING, AND THE CABIN SERVICE DOOR EXTERIOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASMar 17, 2002 · N14938 · Emb EMB145ER · Emergency LightingSDR C2XA02TY054Floorbeam · corrodedTYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL, AFT OF THE COCKPIT DOOR WAS FOUND CORRODED.Mar 16, 2002 · N13929 · Emb EMB145ER · Fuselage Main, Floor BeamSDR C2XA02TY053Angle · corrodedTYS, During a scheduled inspection the ramp angle on center omega beam has corrosion. Maintenance removed and replaced the ramp angle. I/A/W-EMB135/14SRM-51-40-02, 51-20-03, 51-40-06 and 51-40-02. Repair procedures where satisfactory and the aircraft will be rMar 16, 2002 · N13929 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA02TY052Manifold · chafedTYS, DURING A SCHEDULED INSPECTION THE APU FIRE EXTINGUISHER HEAD MANIFOLD WAS FOUND CHAFED AT B-NUT. MAINTENANCE REMOVED AND REPLACED THE MANIFOLD IAW-EMB135/145MM-20-10-03 AND 26-23-05. REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASEDMar 16, 2002 · N13929 · Emb EMB145ER · Extinguishing SystemSDR C2XA02TY051Tube · kinkedTYS, During a scheduled inspection the right APU fire extinguisher tube was found damaged. Maintenance removed and replaced the tube. I/A/W-EMB145MM-20-10-03 and 26-23-05. Repair procedures where satisfactory and the aircraft will be released upon complection Mar 16, 2002 · N13929 · Emb EMB145ER · Extinguishing SystemSDR C2XA02TY050Beam · corrodedTYS, During a scheduled inspection the center omega beam between FR18 and FR24 was found corroded. Maintenance removed and replaced the omega beam. I/A/W-EMB-SRM-51-40-02 and 51-21-02. Repair procedures where satisfactory and the aircraft will be released uponMar 16, 2002 · N13929 · Emb EMB145ER · Fuselage Main, Floor BeamSDR C2XA02TY049Gusset · corrodedTYS, During a scheduled inspection the aft gusset was found corroded. Maintenance removed and replaced the aft gusset. I/A/W-EMB-SRM-51-40-02 and CMP-51-04-00. Repair procedures where satisfactory and the aircraft will be released upon complection of inspectioMar 16, 2002 · N13929 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA02TY047Attach Fitting · chafedDURING A SCHEDULED 1-C INSPECTION THE LOWER RUDDER 1 STABILIZER ATTACH POINT HAS DISPLACED METAL ON RT SIDE NEAR BUSHING.Mar 11, 2002 · N13929 · Emb EMB145ER · Rudder StructureSDR C2XA02CL070Inverter · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 12 TO ROW 19.MAINTENANCE REPLACED THE EMERGENCY LIGHT DC/AC INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Mar 8, 2002 · N14942 · Emb EMB145ER · Emergency LightingSDR C2XA02CL069Bulb · inoperativeDURING ROUTINE MAINTENANCE CHECK MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE LEFT AND RIGHT OVERWING LIGHTS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Mar 8, 2002 · N14942 · Emb EMB145ER · Emergency LightingSDR C2XA02CL066Proximity Switch · faultyCLE FLIGHT#3848 THE CREW REPORTED THE LEFT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR UPLOCK PROXIMITY SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASMar 7, 2002 · N13936 · Emb EMB145ER · Landing Gear Door Retract SectionSDR C2XA02CL061Control Handle · failedCLE FLIGHT 3284 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT AFTER TAKEOFF. THE CREW RECYCLED THE GEAR HANDLE AND THE GEAR DID RETRACT ON THE SECOND ATTEMPT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPEFeb 28, 2002 · N14943 · Emb EMB145ER · Landing Gear SelectorSDR C2XA02TY058Fitting · corrodedTYS, During a scheduled inspection the aft galley inboard floor fitting was found corroded, Maintance removed and replaced the fitting. I/A/W-C & D Aerospace VCMM-25-31-45. The replacement was satisfactory and the aircraft will be released upon complection of Feb 23, 2002 · N13929 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA02IA040Acm · failedIAH- THE CREW NOTED WHITE SMOKE IN THE COCKPIT DURING PARKING WITH NR 1 ENGINE AND APU RUNNING, (NO WARNINGS). MAINTENANCE REMOVED AND REPLACED NR 1 ACM, PERFORMED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVFeb 22, 2002 · N17928 · Emb EMB145ER · Cabin Cooling SystemSDR C2XA02BT004Inverter · faultyEWR---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.Feb 22, 2002 · N14945 · Emb EMB145ER · Emergency LightingSDR C2XA02CL058Fire Warning · malfunctionedCLE FLIGHT 3234 THE CREW REPORTED A APU FIRE WARNING IN FLIGHT AFTER START. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE WAS EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED APU AND FOUND NO EVIDENCE OF FIRE OR NO DEFECTS. THEFeb 21, 2002 · N12934 · Emb EMB145ER · Fire DetectionSDR C2XA02CL055Bleed Valve · wornCLE FLIGHT 3040 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WITH APU RUNNING WITH BLEEDS ON. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 19, 2002 · N16944 · Emb EMB145ER · APU Bleed Air SystemSDR C2XA02IA037Floorbeam · corrodedIAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE RIGHT OUTBOARD FLOORBEAM DIGITAL RECESS WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON RELEASE FROM C-CHECK.Feb 18, 2002 · N15926 · Emb EMB145ER · Fuselage Main, Floor BeamSDR C2XA02IA036Floorbeam · corrodedIAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE CENTER FLOORBEAM GUSSET WAS CORRODED BETWEEN FRAMES 58 AND 60. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON RELEASE FROM C-CHECK.Feb 18, 2002 · N15926 · Emb EMB145ER · Fuselage Main, Floor BeamSDR C2XA02CL054Check Valve · stickingCLE FLIGHT# 3020 THE CREW REPORTED A STRONG FUEL SMELL WHEN THE APU WAS STARTED ON THE GROUND.MAINTENANCE INSPECTED AND REPLACED THE APU COMBUSTION DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 18, 2002 · N14939 · Emb EMB145ER · APU Core EngineSDR C2XA02CL053Check Valve · stickingCLE FLIGHT# 3157 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN AFTER APU START.MAINTENANCE INSPECTED AND STRAIGHTENED A KINKED DRAIN HOSE AND REPLACED THE COMBUSTOR DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SFeb 18, 2002 · N16944 · Emb EMB145ER · APU Core EngineSDR C2XA02CL051Odor · detectedCLE FLIGHT 3151 THE CREW REPORTED A FUEL ODOR IN THE CABIN DURING APU START. MAINTENANCE PERFORMED OPERATIONAL CHECKS GOOD. NO FUEL SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 14, 2002 · N16944 · Emb EMB145ER · Air Distribution SystemSDR C2XA02CL050Switch · lack of lubeDURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT DOOR DID NOT INDICATE A OPEN MESSAGE ON THE EICAS WHEN THE DOOR WAS OPEN. MAINTENANCE INSPECTED AND FOUND THE MICROSWITCH ACTUATION PIN TO BE STICKING. THE PIN WAS LUBRICATED AND OPERATIONAL CHECKS Feb 13, 2002 · N14939 · Emb EMB145ER · Door Warning SystemSDR C2XA02CL048Bulb · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE.MAINTENANCE REPLACED EMERGENCY EXIT LIGHT BULB.OPERATIONAL CHECKS WERE GOOD.Feb 13, 2002 · N14939 · Emb EMB145ER · Emergency LightingSDR C2XA02CL046Wire · damagedCLE FLIGHT 3021 THE CREW REPORTED THE EMERGENCY LIGHTS WERE OUT AT ROWS 3-7. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 7. ALSO REPAIRED WIRING AT ROW 7 FOR THE LIGHT STRIP. MAINTENANCE ALSO REPLACED THE EMERGENCY LIGHT BFeb 10, 2002 · N14943 · Emb EMB145ER · Light System WiringSDR C2XA02CL037Odor · detectedCLE FLIGHT 3015 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AND COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 8, 2002 · N16944 · Emb EMB145ER · Air Distribution SystemSDR C2XA02IA034Crease Beam · corrodedIAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 22 and 23 WAS CORRODED AROUND THE NUT PLATES, IAH- MAINTENANCE REMOVED and REPLACED THE CREASE BEAM, AND, THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE, WHEN RELEASED FRFeb 6, 2002 · N15926 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA02IA033Crease Beam · corrodedIAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 18 and 20 WAS CORRODED AROUND THE NUT PLATES. IAH- MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FFeb 6, 2002 · N15926 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA02TY025Bushing · out of positionTYS, DURING A SCHEDULED 1C INSPECTION, THE MAIN CABIN DOOR HOLD OPEN LATCH BUSHING MIGRATING. MAINTENANCE REINSTALLED BUSHING IAW-EMB-GST-1682/01, REPAIR PROCEDURES ARE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Feb 6, 2002 · N14930 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA02CL035Check Valve · stickingCLE FLIGHT# 4065 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WHEN THE APU WAS STARTED.MAINTENANCE REPLACED THE APU START FUEL CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 6, 2002 · N16944 · Emb EMB145ER · Airborne Auxiliary Power Unit (APU) SystemSDR C2XA02TY029Track · wornTYS, During a scheduled 1C inspection, the right outboard flap, outbd. track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedurFeb 6, 2002 · N14930 · Emb EMB145ER · Trailing Edge FlapsSDR C2XA02TY028Track · wornTYS, During a scheduled 1C inspection, the right outboard flap, inbd. track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedureFeb 6, 2002 · N14930 · Emb EMB145ER · Trailing Edge FlapsSDR C2XA02TY027Track · wornTYS, During a scheduled 1C inspection, the right inboard flap, outbd track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair proceduresFeb 6, 2002 · N14930 · Emb EMB145ER · Trailing Edge FlapsSDR C2XA02TY026Track · wornTYS, During a scheduled 1C inspection, the right inboard flap track was found worn by roolers at normal flap degree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repair procedures are saFeb 6, 2002 · N14930 · Emb EMB145ER · Trailing Edge FlapsSDR C2XA02TY024Bellcrank · gougedTYS, During a scheduled 1C inspection, the left elevator attach bellcrank was found gouged. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0415/02, repair procedures are satisFeb 6, 2002 · N14930 · Emb EMB145ER · Elevator StructureSDR C2XA02TY023Arm · gougedTYS, During a scheduled 1C inspection, the upper rotation arm on the cabin door was found gouged. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0360/02, repair procedures areFeb 6, 2002 · N14930 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA02TY022Axle · gougedTYS DURING A SCHEDULED 1-C INSPECTION THE NLG AXLES HAD SOME SMALL GOUGES NOTED. A GST WAS ISSUED GST 0389/02 THAT STATED BLEND AREA AND APPLY NDI AND IF NO CRACKS ARE FOUND, RESTORE PROTECTIVE FINISH. NO CRACKS WERE FOUND. ALL WORK WAS ACCOMPLISH AND WILLFeb 5, 2002 · N14930 · Emb EMB145ER · Nose/Tail Landing Gear Strut/AxleSDR C2XA02CL032Receptacle · burnedCLE FLIGHT 3279 THE CREW REPORTED THE LEFT COFFEE POT WARMER DID NOT WORK AND HAD A BURNING SMELL WHEN TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE LT COFFEE POT WARMER RECEPTACLE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SFeb 4, 2002 · N14925 · Emb EMB145ER · Buffet/GalleysSDR C2XA02TY021Bracket · gougedTYS, During a scheduled 1C inspection a gouge was found on the outboard fitting of the left elevator spring tab. Maintenance blended the damage, performed dye penetrant inspection (no defects noted) and restored the protective finish I/A/W-EMB-GST-0361/02, repFeb 2, 2002 · N14930 · Emb EMB145ER · Elevator Tab Control System
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