Embraer EMB-145LR

Service difficulty reports · 36,799

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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 = 'EMB145LR'
  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 SIMA20130109012Battery · dischargedDURING MAINTENANCE INSPECTION THE FOLLOWING EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK: FLOOR PROXIMITY LIGHTS NR 6, 7 AND 8 AISLE LIGHTS 3 AND 4 OVERWING EXIT LOCATOR (FWD),(LT AFT) EXTERIOR OVERWING LIGHT AND (RT AFT) EXTERIOR OVJan 9, 2013 · N925AE · Emb EMB145LR · Emergency LightingSDR SIMA20130109011Seal · tornDURING B INSPECTION FOUND THE RIGHT EMERGENCY EXIT AFT SEAL TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EMERGENCY EXIT AFT SEAL IAW EMB145 AMM 52-21-01. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 9, 2013 · N925AE · Emb EMB145LR · Emergency ExitsSDR SIMA20130109010Holder · defectiveDURING MAINTENANCE INSPECTION FOUND THE BATTERY HOLDER ASSEMBLY FAILED THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY HOLDER ASSEMBLY P/N 2013-1A S/N 68832. THE OPERATIONAL CHECK WAS Jan 9, 2013 · N925AE · Emb EMB145LR · Emergency LightingSDR CHQA20130109010Cover · missingCREW REPORTED THAT DURING FLIGHT, THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC OR MANUAL MODES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERNAL GROUND CONNECTION VALVE COVER TO BE MISSING AND DEFERRED THE ITEM. THE DJan 9, 2013 · N277SK · Emb EMB145LR · Air Distribution SystemSDR CHQA20130109009O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 1 LEAK MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINTS 17, 19, 23, AND 26 IN THE BLEED SYSTEM. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEJan 9, 2013 · N274SK · Emb EMB145LR · Pneumatic Distribution SystemSDR SIMA20130109008Display · failedON FLIGHT 2842 THE CREW REPORTED THE CAPTAIN’S MFD FAILED IN FLIGHT (WENT COMPLETELY BLANK SUDDENLY) DURING APPROACH MFD CAME BACK UP, BUT WITH AN ACRID ODOR. PULLED MFD 1 CB, ODOR CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM Jan 9, 2013 · N629AE · Emb EMB145LR · Central DisplaySDR SIMA20130109006Inverter · inoperativeDURING MAINTENANCE INSPECTION FOUND THE NR 5 EMERGENCY LIGHT INVERTER WOULD NOT ILLUMINATE RIGHT EMERGENCY EXIT SHROUD "EXIT" SIGN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC/DC POWER INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAJan 9, 2013 · N618AE · Emb EMB145LR · Emergency LightingSDR SIMA20130109005Connector · unsecureDURING MAINTENANCE INSPECTION FOUND THE NR 3 EMERGENCY LIGHT INVERTER WOULD NOT POWER EMERGENCY FLOOR STRIP SECTIONS 2 AND 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR P8528 NOT FULLY SECURE. TIGHTENED CONNECTOR AND PERFORMED OPS CHECK OF EMERGJan 9, 2013 · N618AE · Emb EMB145LR · Light System WiringSDR ASOA20130109218Angle · corrodedDURING A C-CHECK, CORROSION FOUND AROUND NUTPLATED AT THE BAGGAGE DOOR. MX R & R THE BAGGAGE DOOR INBD ANGLE IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Cargo/Baggage DoorsSDR ASOA20130109217Seat Track · corrodedDURING C-CHECK INSPECTION, RT OTBD SEAT TRACK SUPPORT FOUND CORRODED AT FR 55. MX REMOVED THE RIVETS AND FABRICATED A NEW SUPPORT AND INSTALL IAW SRM 51-40-02 AND SRM 53-00-11. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130109216Channel · corrodedDURING C-CHECK, LEFT CHANNEL CROSSBEAM AT FRAME 18 WAS FOUND CORRODED. MX BLENDED CORROSION IAW SRM 51-10-03, PERFORMED HFEC, NO CRACKS FOUND AND WAS WITHIN LIMITS IAW SRM 53-21-10. ALL WORK ACCOMPLISHED AND WILL BE RELEASED A THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130109214Skin · dentedACFT WAS HAVING A BIRD STRIKE INSPECTION WHEN MX FOUND A DENT FWD OF F/O WINSHIELD. MX REPAIRED THE SKIN PANEL IAW EC 5300-01033. ALL WO ACCOMPLISHED AND WAS RELEASED.Jan 9, 2013 · N12957 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20130108002Smoke Detector · dirtyCREW REPORTED INTERMITTENT LAVATORY SMOKE ON EICAS WITH NO SMOKE OR ANY FIRE NOTED IN LAVATORY BY F/A. MX CLEANED THE LAVATORY SMOKE SENSOR AND R & R THE SMOKE DETECTOR PANEL, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 8, 2013 · N13979 · Emb EMB145LR · Smoke DetectionSDR SIMA20130108003Support · corrodedDURING MAINTENANCE INSPECTION FOUND THE RIGHT OUTBOARD SEAT TRACK SUPPORT CORRDED AT FRAME 50. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED REPAIR ACCORDING TO THE EO EM-53-MR-2059. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 8, 2013 · N935AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20130108002Holder · brokenFOR FLIGHT 4078 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 8, 2013 · N620AE · Emb EMB145LR · Emergency EquipmentSDR ASOA20130109213Gusset · corrodedC-CHECK, GUSSET AT FR 17 WAS FOUND WITH MINOR CORROSION AROUND NUTPLATE. MX BLENDED CORROSION LEAVING REMAINING MATERIAL TO BE WITHIN LIMITS IAW SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130109212TFrame · corrodedC-CHECK, CORROSION FOUND AT FRAME 65 AT THE THRESHOLD. MX R & R THE LOWER SECTION OF FRAME 65IAW ETD 2012-145-018140. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20130108211Support · corrodedACFT IN FOR A C-CHECK, CHECK WHEN THE LT WALL SUPPORT HAD CORROSION ON THE LOWER SIDE OF SUPPORT AT FRAME 60. MX R & R THE LT WALL SUPPORT IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130108210Beam · corrodedACFT IN FOR A C-CHECK, CHECK WHEN THE CARGO DOOR CUTOUT WAS FOUND. CORRODED ON THE THRESHOLD BETWEEN FRAMES 65 AND 68. MX BLENDED THE CORROSION IAW SRM 51-10-03. R & R THE AREAS OUT OF LIMITS WITH FABRICATED PARTS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AJan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20130108209Seat Track · corrodedACFT IN FOR A C-CHECK, WHEN THE NR 4 LT SEAT TRACK WAS FOUND CORRODED IN SEVERAL PLACES. BLENDED AREAS IAW SRM 51-10-03, THE OUT OF LIMIT AREAS IAW SRM 53-00-11 WERE CUT OUT AND FABBED PARTS WERE INSTALL IN THE SEAT TRACK SECTION IAW SRM 53-00-11. ALL WORK WJan 8, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20130107019Handle · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE COCKPIT GRAB HANDLE STRUCTURE. THE COCKPIT GRAB HANDLE STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-000584.Jan 7, 2013 · N573RP · Emb EMB145LR · Flight Compartment EquipmentSDR CHQA20130107018Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 7, 2013 · N573RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130107017Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 7, 2013 · N573RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130107016Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 16R AND 17R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 7, 2013 · N573RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130107015Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 15R AND 16R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 7, 2013 · N573RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130107014Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 67 BETWEEN STINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 7, 2013 · N573RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130107002Skin · dentedFOUR DENTS LOCATED BETWEEN FR22/FR23 AND STRINGER 12L/14L. MX REPARIED FUSELAGE SKIN IAW ETD2013-145-000362-C AND SRM 53-21-01, TYPE A1. (1 DOUBLER) FIG 202 USING 3 RIVET ROWS. ACFT RELEASED FOR SERVICE.Jan 7, 2013 · N13914 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20130107008Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHT FLOOR PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE AT ROW 8. MAINTENANCE REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 7, 2013 · N283SK · Emb EMB145LR · Emergency LightingSDR SIMA20130107006Acm · faultyON FLIGHT 2977 THE CREW REPORTED AN OCCASIONAL STRONG OIL SMELL APPARENT IN THE COCKPIT AND GALLEY AREA AND OCCURS AT RANDOM TIMES AND DOES NOT SEEM ASSOCIATED WITH ANT PARTICULAR THRUST OR BLEED SETTINGS. THE PILOT STATED HE BELIEVES THE SMELL TO BE COMING FJan 7, 2013 · N928AE · Emb EMB145LR · Cabin Cooling SystemSDR SIMA20130107005Flashlight · defectiveDURING MAINTENANCE INSPECTION FOUND THE CAPT'S FLASHLIGHT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPT'S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WJan 7, 2013 · N663AR · Emb EMB145LR · Emergency EquipmentSDR SIMA20130107004Flashlight · inoperativeON FLIGHT 3226 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPT'S FLASHLIGHT IAW EMB 145 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 7, 2013 · N622AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20130107002Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS Jan 7, 2013 · N617AE · Emb EMB145LR · Emergency LightingSDR SIMA20130107001Skin · canningDURING MAINTENANCE INSPECTION FOUND OIL CANNING OF FUSELAGE SKIN BETWEEN FRAME 19 AND FRAME 23 STRINGER 11L - 12L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE SKIN IAW AEA EO EM-53MR-2052. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 7, 2013 · N604AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR RAIA201301060001Door · out of adjustDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED AND ADJUSTED THE DOOR RIGGING. DOOR OPS CHECKED GOOD.Jan 6, 2013 · N847HK · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20130106001Cradle · unserviceableON FLIGHT 4033 THE CREW REPORTED THE LOWER CLIP MISSING FROM THE CAPTAIN’S FLASHLIGHT CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT CRADLE IAW EMB MM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS Jan 6, 2013 · N653AE · Emb EMB145LR · Emergency EquipmentSDR ASOA20130107208Light · inoperativeMAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.Jan 6, 2013 · N15983 · Emb EMB145LR · Emergency LightingSDR ASOA20130105207Support · corrodedRT OTBD SEAT TRACK SUPPORT CORRODED ON LOWER FOOT. CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105206Support · corrodedNR 1 LEFT WALL SEAT TRACK SUPPORT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105205Gusset · corrodedGUSSET AT FRAME 65 TO 68 AT Y=-479 IS CORRODED BEYOND LIMITS. R & R GUSSET.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105204Structure · corrodedFRAME 15 DIGITAL IS CORRODED BEYOND LIMITS. R & R DIGITAL.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105203Channel · corrodedPAX DOOR U CHANNEL CORRODED BEYOND LIMITS AFTER BLENDING. R & R U CHANNEL.Jan 4, 2013 · N16981 · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA20130105202Seat Track · corrodedNR 3 LEFT ISLE SEAT TRACK GUSSET IS CORRODED OUT OF LIMITS AFTER BLENDING. R & R GUSSET.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20130104001Seal · lack of lubeFOR FLIGHT 2972 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR SEAL IAW EMB-145 AMM 52-11-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 4, 2013 · N602AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20130103004Light · not seatedDURING MAINTENANCE INSPECTION FOUND THE RIGHT HAND OVER WING EXT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED THE RIGHT HAND EXTERNAL OVERWING EMERGENCY LAMP IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT Jan 3, 2013 · N691AE · Emb EMB145LR · Emergency LightingSDR SIMA20130103002Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY UNABLE TO PROVIDE POWER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMVOED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETJan 3, 2013 · N672AE · Emb EMB145LR · Emergency LightingSDR ASOA20130103201Sill · corrodedRIGHT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103200Angle · corrodedLEFT ANGLE HAS CORROSION THAT IS OUT OF LIMITS AFTER BLEND OUT. R & R LEFT ANGLE.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103199Gusset · corrodedCORROSION AFT LAVATORY LT FLOOR GUSSET CORRODED OUT OF LIMITS AFTER BLENDING. R & R FLOOR GUSSET.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103198Support · corrodedSUPPORT IN THE LAVATORY AREA HAS CORROSION OUT OF LIMITS AFTER BLENDING. REMOVED AND REPLACED DOUBLER.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103197Brace · corrodedRT CROSS BRACE IS CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R BRACE.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous Structure
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