Embraer EMB-145EP

Service difficulty reports · 2,197

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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 = '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 RAIA2013031800001Garlock Seal · wornCREW REPORTED RECEIVING AN ENGINE NR 1 LOW OIL PRESSURE MESSAGE ON THE EICAS DURING APPROACH AND SUBSEQUENTLY PERFORMED A COMMANDED SHUTDOWN OF THE NR 1 ENGINE. MAINTENANCE INSPECTED THE AIRCRAFT/ENGINE AND FOUND A LEAK AT THE NR 3 ENGINE GENERATOR AND THE ENMar 18, 2013 · N802HK · Emb EMB145EP · Turbine Engine Oil SystemSDR RAIA201303170002Light · inoperativeDURING SCHEDULED MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT. SYSTEM OPS CHECKED GOOD.Mar 17, 2013 · N805HK · Emb EMB145EP · Emergency LightingSDR ASOA20130317032Skin · crackedDURING 2A INSP THE LT FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED BELOW STR 1R. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 17, 2013 · N14940 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130317031Skin · crackedDURING 2A CHECK THE FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED, PROTRUDING FROM A PREVIOUS REPAIR BETWEEN STR 00 & 01R. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 17, 2013 · N14940 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130317030Skin · crackedDURING 2A INSPECTION, THE LT SKIN AT FRAME 78 BETWEEN STR 5L AND 6L WAS FOUND TO BE CRACKED. MX PERFORMED A DOUBLER REPAIR AMD THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 17, 2013 · N14940 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA201303150001Connector · dirtyDURING SCHEDULED MAINTENANCE THE AFT SIDEWALL EMERGENCY EXIT LIGHT AT 12A WAS FOUND INOP. MAINTENANCE CLEANED THE LIGHT CONNECTOR. SYSTEM OPS CHECKED GOOD.Mar 15, 2013 · N807HK · Emb EMB145EP · Light System WiringSDR RAIA201303130001Light · inoperativeDURING SCHEDULED MAINTENANCE THE RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CHECKED GOOD.Mar 13, 2013 · N805HK · Emb EMB145EP · Emergency LightingSDR RAIA201303110002Thrust Reverser · malfunctionedDURING CRUISE FLIGHT THE FLIGHT CREW GOT A E1 TR DISAGREE MESSAGE. AIRCRAFT RETURNED TO STL. MAINTENANCE INSPECTED AND DEFERRED THE NR 1 T/R ON DMI #64406 PER MEL 78-34-00.Mar 11, 2013 · N805HK · Emb EMB145EP · Engine Thrust ReverserSDR RAIA201303110001Strut · low pressureDURING FLIGHT THE FLIGHT CREW GOT A L/G AIR GROUND FAIL EICAS MESSAGE. MAINTENANCE INSPECTED AND SERVICED THE NLG STRUT. OPS CHECKED THE LANDING GEAR SYSTEM, SYSTEM OPS CHECKED GOOD.Mar 11, 2013 · N805HK · Emb EMB145EP · Nose/Tail Landing Gear Strut/AxleSDR ASOA20140310037Bulb · burned outDURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 10, 2013 · N14933 · Emb EMB145EP · Emergency LightingSDR RAIA201303090002Flashlight · inoperativeDURING SCHEDULED MAINTENANCE THE AFT CABIN EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT. SYSTEM OPS CHECKED GOOD.Mar 9, 2013 · N807HK · Emb EMB145EP · Emergency EquipmentSDR RAIA201303090001Flashlight · inoperativeDURING SCHEDULED MAINTENANCE THE AFT CABIN FLASHLIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT. SYSTEM OPS CHECKED GOOD.Mar 9, 2013 · N810HK · Emb EMB145EP · Emergency EquipmentSDR RAIA201303080002Connector · dirtyDURING CRUISE FLIGHT THE FLIGHT CREW GOT A BLEED 2 VALVE CLOSED MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND CLEANED AND CHECKED THE SECURITY OF THE CONNECTOR ON THE VALVE. OPS CHECK OF SYSTEM CHECKED GOOD.Mar 8, 2013 · N807HK · Emb EMB145EP · Pneumatic System WiringSDR ASOA20130308287Skin · corrodedACFT IS IN A C-CHECK POSITION WHEN INSPECTION FOUND CORROSION WAS FOUND ON A SKIN PANEL AT FRAME 13 AT STRINGERS 20R AND 19R. MX R & R THE SKIN PANEL IAW SRM 53-00-02. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.Mar 8, 2013 · N14945 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130308206Skin · corrodedACFT IS IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE SKIN AFT OF FRAME 18, BETWEEN STRINGERS 20L AND 19R. MX R & R THE SKIN IAW EMB 145 EC 5330-02715. THE RVSM REMAP WAS GOOD AS WELL AS PRESSURE CHECKS. ACFT WILL BE RELEASED AT THE END OF ALL CHECKS.Mar 8, 2013 · N14945 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA2013030200001Clamp · defectiveDURING CLIMBOUT OF IAD, THE CREW REPORTED A LOUD POP ON ENTERING ICING, A BLEED 2 LEAK MESSAGE ON THE EICAS FOLLOWED BY A BLEED 1 LEAK MESSAGE ON EICAS. AFTER BLEED ISOLATION, THE CREW REPORTED A STRONG BURNING SMELL. MAINTENANCE REMOVED AND REPLACED A BLEEDMar 2, 2013 · N806HK · Emb EMB145EP · Pneumatic Distribution SystemSDR ASOA20130226025HSkin · crackedDURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A .2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, ANFeb 26, 2013 · N14938 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA201302260001Step · out of adjustDURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE AIRSTAIRS ARE NOT FULLY DEPLOYING WHEN THE DOOR IS OPENED. MAINTENANCE INSPECTED ADJUSTED BOTTOM STEP. DOOR OPS CHECKED GOOD.Feb 26, 2013 · N806HK · Emb EMB145EP · Passenger/Crew DoorsSDR ASOA20130225024Inverter · inoperativeDURING MX INSPECTION, THE PASSENGER CABIN FWD EMERGENCY EXIT LOCATING SIGN ON 253CLC FAILED TO ILLUMINATE. MX R & R THE AFFECTED SIGN EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 25, 2013 · N14930 · Emb EMB145EP · Emergency LightingSDR ASOA20130219020Connector · disconnectedTHE CREW REPORTED THE EXIT SIGN OVERWING EXIT WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RECONNECTED THE SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 19, 2013 · N14930 · Emb EMB145EP · Light System WiringSDR ASOA20130212013Charger · inoperativeDURING SCHEDULED MX, THE EMERGENCY FLOOR STIP LIGHTING AT POSITIONS 1,2,3 AND SERVICE DOOR EMERGENCY LIGHTING WERE FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.Feb 12, 2013 · N14925 · Emb EMB145EP · Emergency LightingSDR ASOA20130211014HLamp · burnedTHE CREW REPORTED THAT DURING LANDING, A BURNING ODOR AND LIGHT LAYER OF SMOKE WAS NOTED IN THE CABIN. THE SMOKE DISSIPATED AFTER LANDING, HOWEVER THE ODOR REMAINED. THE ACFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT WHERE MX FOUND 2 LATERAL LIGHTS TO BE BFeb 11, 2013 · N16927 · Emb EMB145EP · Emergency LightingSDR ASOA20130210012Skin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2R. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130210011Skin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130209010HSkin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.Feb 9, 2013 · N14939 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130209009HLight · inoperativeDURING SCHEDULED MX, THE PASSENGER DOOR BOTTOM EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.Feb 9, 2013 · N17928 · Emb EMB145EP · Emergency LightingSDR ASOA20130130007HLight · inoperativeDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 3 TO ROW 6 WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 30, 2013 · N14925 · Emb EMB145EP · Emergency LightingSDR RAIA201301160001Pressure Switch · malfunctionedDURING CLIMB THE AIRCREW GOT A WING ANTI-ICE FAIL MESSAGE. AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPECTED, TROUBLESHOT THE SYSTEMS, AND HAD AIRCRAFT FLY A TEST FLIGHT DURING WHICH EQUIPMENT WAS CONNECTED TO TEST THE ANTI-ICE SYSTEMS IN FLIGHT. MAINTENANCE Jan 16, 2013 · N806HK · Emb EMB145EP · Airfoil Anti/De-ice SystemSDR RAIA201301140001Fire Warning · false activationDURING CLIMBOUT OF BDL AIRCREW GOT AN APU FIRE WARNING EICAS MESSAGE. AIRCREW DECLARED AN EMERGENCY AND RETURNED TO BDL WITHOUT AN INCIDENT. MAINTENANCE INSPECTED AND FOUND NO INDICATION OF FIRE. THE APU WAS DEFERRED DUE TO ERRONEOUS FIRE WARNING MESSAGE ANJan 14, 2013 · N808HK · Emb EMB145EP · Fire DetectionSDR RAIA201301120001Pressure Switch · malfunctionedDURING CLIMB THE FLIGHT CREW GAT A WING ANTI-ICE FAIL MESSAGE. AIRCRAFT RETURNED TO ORD. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 2 LOW PRESSURE SWITCH. SYSTEM OPS CHECKED GOOD.Jan 12, 2013 · N806HK · Emb EMB145EP · Airfoil Anti/De-ice SystemSDR ASOA20130106003Charger · inoperativeTHE CREW REPORTED THAT THE LT AND RT EXTERNAL OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 6, 2013 · N12934 · Emb EMB145EP · Emergency LightingSDR ASOA20130102002Bulb · burned outDURING A-CHECK INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFCTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 2, 2013 · N14940 · Emb EMB145EP · Emergency LightingSDR RAIA201212300002Light · inoperativeDURING SCHEDULED MAINTENANCE THE CEILING EMERGENCY EXIT LIGHT AT ROW 16 IS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CHECKED GOOD.Dec 30, 2012 · N808HK · Emb EMB145EP · Emergency LightingSDR ASOA201212226001Pressure Switch · inoperativeTHE CREW REPORTED BRAKE DEGRADE ON LANDING WITH VERY LITTLE BRAKE PRESSURE, ALSO HAD CMC MESSAGE BRAKE WHEEL SPEED TRANSDUCER 3 FAIL OCCURRED 3 TIMES. THE ACFT LANDED WITHOUT INCIDENT AND MX INSPECTED THE ACFT AND PLACED IT ON MEL 32-41-08, AND THE ACFT WAS ADec 26, 2012 · N16927 · Emb EMB145EP · Landing Gear Brake SystemSDR RAIA201212240001Tube · leakingDURING CRUISE FLIGHT THE WING ANTI-ICING FAIL IN ICING CONDITIONS. AIRCRAFT MADE AN UNSCHEDULED LANDING AT DAY. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 LOW PRESSURE SWITCH AND NR 2 WING ANTI-ICING DISTRIBUTION TUBE BETWEEN THE NR 2 WING ANTI-ICINDec 24, 2012 · N802HK · Emb EMB145EP · Airfoil Anti/De-ice SystemSDR RAIA201212220001Detection Sys · malfunctionedDURING CLIMB THE FLIGHT CREW GOT AN APU FIRE INDICATION. AIRCRAFT RETURNED TO STL. MAINTENANCE PERFORMED AN APU FIRE INSPECTION. NO EVIDENCE OF FIRE WAS NOTED. INSPECTED APU COWLING AND NO DAMAGE WAS NOTED. MAINTENANCE DEFERRED THE APU FIRE DETECTION SYSTDec 22, 2012 · N808HK · Emb EMB145EP · Fire DetectionSDR ASOA20121217159Skin · crackedDURING SCHEDULED MX THE RT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.Dec 17, 2012 · N14925 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20121217158Skin · crackedDURING SCHEDULED MX THE LT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.Dec 17, 2012 · N14925 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA201212140002Light · inoperativeDURING SCHEDULED MAINTENANCE THE GALLEY EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD.Dec 14, 2012 · N807HK · Emb EMB145EP · Emergency LightingSDR RAIA201212140001Light · inoperativeDURING SCHEDULED MAINTENANCE THE RIGHT WING FORWARD EMERGENCY OVERWING LIGHT WAS FOUND INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD.Dec 14, 2012 · N805HK · Emb EMB145EP · Emergency LightingSDR RAIA201212130002Light · inoperativeDURING SCHEDULED MAINTENANCE THE LEFT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT NR 5 FAILED TO ILLUMINATE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULB. SYSTEM OPS CHECKED GOOD.Dec 13, 2012 · N805HK · Emb EMB145EP · Emergency LightingSDR RAIA201212130001Battery · dischargedDURING SCHEDULED MAINTENANCE THE AFT CEILING EMERGENCY EXIT LOCATOR FAILED TO ILLUMINATE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY. SYSTEM OPS CHECKED GOOD.Dec 13, 2012 · N805HK · Emb EMB145EP · Emergency LightingSDR ASOA20121210156Firewall · crackedDURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 1.25" TOTAL LENGTH AT THE 9 O'CLOCK POSITION WITH A RIVET IN THE MIDDLE. MAINTENANCE PEFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 10, 2012 · N17928 · Emb EMB145EP · APU Cowling/ContainmentSDR ASOA20121209166Inverter · inoperativeGALLEY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.Dec 9, 2012 · N13929 · Emb EMB145EP · Emergency LightingSDR ASOA20121208155Skin · crackedSUPPLEMENTAL, DURING A-CHECK INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 5 SEPARATE CRACKS AT 3 DIFFERENT RIVETS AT FRAME 75. THESE INCLUDE 2 CRACKS MEASURING .07" AND .25" ON EITHER SIDE OF 1 RIVET DIRECTLY ABOVE STRINGER 2 LT, 2 CRACKS MEASURING .1Dec 8, 2012 · N17928 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20121205153Skin · crackedDURING A-CHECK INSPECTION THE RT WING SKIN WAS FOUND TO HAVE A .70" LOG CRACK AT THE CUT-OUT FOR THE SPOILER CENTER HINGE POINT. INSTALLED A REPAIR DOUBLER TO THE AFFECTED AREA AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 5, 2012 · N15926 · Emb EMB145EP · Wing, Plate/SkinSDR ASOA20121205164Skin · corrodedTHE FORWARD LOWER FUSELAGE INTERNAL SKIN WAS NOTED WITH CORROSION BEYOND LIMITS BETWEEN FRAMES 13 & 14, STRINGER 19L THRU 18R. R & R SKIN PANEL, REMAPPED LT & RT RVSM CRITICAL REGIONS. ACFT STILL IN C-CHECK.Dec 4, 2012 · N14942 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20121201152Skin · crackedDURING A-CHECK INSPECTION, TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN EMINATING FROM THE SAME RIVET AT FRAME 75, STRINGER 2R. MX PERFORMED A DOUBLER REPAIR AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 1, 2012 · N13936 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20121129151Skin · crackedDURING A-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AFT OF A RIVET AT FRAME 75 STRINGER 01 LT. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 29, 2012 · N12946 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA201211290150Skin · crackedDURING A-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR 75 STRINGER 2 RT. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 29, 2012 · N12946 · Emb EMB145EP · Fuselage Main, Plate/Skin
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