Embraer EMB-145EP

Service difficulty reports · 2,197

Newest first. General aviation reporting is voluntary.

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 = 'EMB145EP'
  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 C2XA10SH145Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAME 33 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH144Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH143Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM CARBON CROSSBEAM CUTOUT AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH142Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH141Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 20. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH140Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 25 CARBON CROSSBEAM AREA IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH139Fitting · corrodedSHV - DURING C-CHECK BAGGAGE DOOR CUTOUT HAS CORROSION (LEVEL 2 LOCAL) AT FWD LWR CORNER. MAINTENANCE PERFORMED REPAIR OF FRAME 65 SHEAR CLIP AT BAGGAGE DOOR CUTOUT FWD LWR CORNER IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2010042300002Mechanism · lack of lubeDURING THE GROUND HANDLING, THE CREW REPORTED THAT THE MAIN DOOR MECHANISM HAD BECOME INCREASINGLY DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBED THE DOOR HANDLE MECHANISM AND THE DOOR SEAL. FOLLOW ON OPERATIONAL CHECK OF THE DOOR WAS GOOD.Apr 23, 2010 · N809HK · Emb EMB145EP · Passenger/Crew DoorsSDR C2XA10IA127Ballast · malfunctionedMEM - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL BY ROWS 16-19. MAINTENANCE INSPECTED THE AIRCRAFT AND IDENTIFIED A BAD BALLAST ABOVE ROW 16. THE CABIN LIGHTS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERApr 23, 2010 · N15941 · Emb EMB145EP · Passenger Compartment LightingSDR RAIA2010042300001Unknown · smokeTHE CREW REPORTED SMOKE IN THE CABIN FOLLOWING TAKEOFF. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE CABIN AREAS ABOVE AND BELOW THE FLOORBOARDS FOR SOURCES OF SMOKE. NONE WERE FOUND. ADDITIONALLY, MAINTENANCE INSPECTED THE BLEED LINES AND PNEUMATIC Apr 23, 2010 · N807HK · Emb EMB145EP · Air Distribution SystemSDR C2XA10IA126Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 22, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR RAIA201042100001Bracket · out of adjustTHE CREW REPORTED THAT DURING LANDING APPROACH, A LANDING GEAR DISAGREE MESSAGE APPEARED ON THE EICAS AND THAT THE FREE FALL LEVER WAS USED TO EXTEND THE LANDING GEAR. MAINTENANCE ADJUSTED THE NLG PROXIMITY SWITCH BRACKET FOR THE DOWNLOCK AND PERFORMED SEVERAApr 21, 2010 · N801HK · Emb EMB145EP · Landing Gear Position and WarningSDR RAIA2010042000001Smoke Detector · faultyDURING DESCENT INTO IAD, THE CREW REPORTED RECEIVING A BAG BAY SMOKE MESSAGE ON THE EICAS WITH NO ASSOCIATED SMOKE OR SMELL IN THE CABIN. THE CAPTAIN USED BOTH BAGGAGE BAY FIRE EXTINGUISHERS. MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE BAY SMOKE DETECTORS AApr 20, 2010 · N804HK · Emb EMB145EP · Smoke DetectionSDR C2XA10IA125Battery Pack · dischargedIAH - FLIGHT 2217, THE DURING POST FLIGHT THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFApr 19, 2010 · N14937 · Emb EMB145EP · Emergency LightingSDR C2XA10IA124Lever · defectiveIAH - FLIGHT 2709, THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE ON CLIMBOUT. THE AIRCRAFT LANDED AT ISH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR REApr 19, 2010 · N12946 · Emb EMB145EP · Landing Gear SelectorSDR C2XA10SH137Fitting · crackedSHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT HAS VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE YOKE FWD LOWER PYLON FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 17, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach FittingsSDR RAIA2010041500001Target · faultyDURING CLIMBOUT OF PIT, THE CREW REPORTED RECEIVING A LG AIR/GND FAIL MESSAGE ON THE EICAS AND THAT THE GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE RT FWD MAIN GEAR AIR/GND PROXIMITY SWITCH TARGET. SUBSEQUENT GEAR EXTENSION AND RETRACTION CHApr 15, 2010 · N804HK · Emb EMB145EP · Landing Gear Position and WarningSDR C2XA10IA120Ballast · overheatedIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE BALLAST 2A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 15, 2010 · N13929 · Emb EMB145EP · Lighting SystemSDR C2XA10IA117Controller · inoperativeMEM - FLIGHT 2249, DURING DESCENT THE CREW REPORTED THAT AUTO PRESSURIZATION FAILED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE CREW PLACED THE AUTO PRESSURIZATION ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED ATApr 11, 2010 · N14943 · Emb EMB145EP · Cabin Pressure ControllerSDR RAIA2010040800001Pitot Line · contaminatedWHILE IN CRUISE, THE CREW REPORTED RECEIVING AN AIR SPEED COMPARATOR ERROR, ALTIMETER COMPARATOR ERROR, FOLLOWED BY AN ADC 1 FAIL MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND WATER TO BE IN THE NR 1 PITOT SYSTEM. THE WATER WAS DRAINED FApr 8, 2010 · N808HK · Emb EMB145EP · Pitot/Static SystemSDR RAIA2010040600002Unknown · odorWHILE IN CLIMB, THE CREW REPORTED A STRONG SMELL OF FUEL WITH PACKS RUNNING ON APU BLEED AFTER TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE APU BLEED SYSTEM WITH NO DEFECTS NOTED.Apr 6, 2010 · N809HK · Emb EMB145EP · Air Distribution SystemSDR RAIA2010040600001Connector · disconnectedWHILE IN CRUISE, JUST FOLLOWING TAKEOFF, THE CREW RECEIVED A LND/AIR GROUND MESSAGE ON THE EICAS. PRIOR TO FLIGHT, MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT DOWN LOCK PROXIMITY SWITCH CONNECTOR TO DISCONNECTED. THE CONNECTOR WAS RECONNECTED TO THE Apr 6, 2010 · N804HK · Emb EMB145EP · Landing Gear System WiringSDR RAIA2010040500001Light · inoperativeDURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE MID CABIN CEILING EMERGENCY LIGHT AS BEING INOPERATIVE. PRIOR TO FLIGHT, MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. FOLLOW-ON OPERATIONAL CHECK OF THE LIGHTS WERE GOOD.Apr 5, 2010 · N809HK · Emb EMB145EP · Emergency LightingSDR RAIA2010040200001Bulb · burned outPRIOR TO FLIGHT, THE CREW REPORTED THAT ONE OF THE EMERGENCY LIGHTS AS BEING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB IAW AMM PROCEDURES PRIOR TO FLIGHT. OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS GOOD.Apr 2, 2010 · N808HK · Emb EMB145EP · Emergency LightingSDR RAIA2010033100001A/C Pack · malfunctionedWHILE IN CRUISE, THE CREW REPORTED THAT THE NR 1 PACK SMELLED HOT FOLLOWED BY A PACK NR 1 OVERLOAD. MAINTENANCE DEFERRED THE NR 1 PACK SYSTEM IAW MEL.Mar 31, 2010 · N805HK · Emb EMB145EP · Cabin Cooling SystemSDR RAIA2010033000001Connector · loosePRIOR TO FLIGHT, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT STRIP AS BEING INOPERATIVE. MAINTENANCE RE-SECURED THE CONNECTOR TO THE LIGHT ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.Mar 30, 2010 · N809HK · Emb EMB145EP · Light System WiringSDR V0XR201003300001Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 47-52 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2155.Mar 30, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003390003Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 36-47 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2159.Mar 29, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003390002Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 47-52 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2155.Mar 29, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003390001Seat Track · corrodedLT LOWER SEAT TRACK BETWEEN FR 47-52 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2158.Mar 29, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR C2XA10IA107Skin · crackedIAH - FLIGHT 2820, DURING POST FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 27, 2010 · N14945 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR V0XR201003260009Floor Support · corrodedLT OTBD FWD DIGITAL FR 14-17 IS CORRODED BEYOND LIMITS. R & R DIGITAL. W/C 2102Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003260008Seat Track · corrodedLT LOWER SEAT TRACK BETWEEN FR 18-24 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2167.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003260007Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 24-30 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2164.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003260006Seat Track · corrodedLT LOWER SEAT TRACK BETWEEN FR 24-30 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2163.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003260005Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 30-35 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2149.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003260004Support · corrodedCTR FLOORBOARD SUPPORT AT YO.O AT FR 18-20 IS CORRODED BEYOND LIMITS. R & R SUPPORT. W/C 2096Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003260003Angle · corrodedANGLE AT FRM 14 LY 780 IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1167.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201003260002Sill · corrodedRT SILL AT FRM 53-59 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1121.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003260001Angle · corrodedFLOOR SUPPORT ANGLE LY-479.0 - RT OTBD AT FR 18 IS CORRODED. R & R ANGLE. W/C 1110.Mar 26, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10IA108Skin · crackedCRP - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETMar 25, 2010 · N16944 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR C2XA10IA104Sign · malfunctionedIAH - FLIGHT 2132, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EXIT SIGN AT SEAT 12C TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 25, 2010 · N14943 · Emb EMB145EP · Emergency LightingSDR CHQA201000061Brake Sys · malfunctionedCREW REPORTED THAT ON GEAR EXTENSION, "BRK OUTBD INOP" MESSAGE APPEARED ON EICAS. CREW FOLLOWED QRH AND REPORTED THAT ON LANDING ROLL OUT IT FELT LIKE BRAKES WERE ONLY HALF AS EFFECTIVE. ON TAXI A "BRK OVERHEAT" MESSAGE WAS REPORTED AND MFD INDICATED THE OUTMar 25, 2010 · N978RP · Emb EMB145EP · Landing Gear Brake SystemSDR V0XR201003250008Seat Track · corrodedLT LOWER SEAT TRACK BETWEEN FR 30-35 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2152.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201003250007Floor Support · corrodedFLOOR SUPPORT ANGLE(S) AT LY 479.0 FR 18-20 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 2097.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003250006Floor Support · corrodedFLOOR SUPPORT ANGLE(S) AT LY 479.0 FR 18-20 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 2097.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003250005Beam · corrodedRT BEAM HAT SECTION RY 479.0 FR 17-24 IS CORRODED BEYOND LIMITS. R &R BEAM. W/C 2092.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201003250004Gusset · corrodedCTR GUSSET AT FR 53-59 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1136.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003250003Gusset · corrodedGUSSET AT LY 479.0 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1129.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201003250002Sill · corrodedRT SILL AT FR 24-29 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1069.Mar 25, 2010 · N803HK · Emb EMB145EP · Fuselage Miscellaneous Structure
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