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 RAIA201310020004Beam · corrodedDOUBLER ON BEAM Y 479 AT FR 22 CORRODED. MAINTENANCE REPLACED DOUBLER, OPS CHECK GOOD.Oct 2, 2013 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR RAIA201310020003Doubler · corrodedDOUBLER ON BEAM Y 479 AT FRAME 20 CORRODED. MX REPLACED DOUBLER.Oct 2, 2013 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201310020002Gusset · corrodedGUSSET ON BEAM Y 0.0 FR 18-23 CORRODED. MX REPLACED GUSSET, OPS CHECK GOOD.Oct 2, 2013 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR RAIA201310020001Insert · corroded1 LAVATORY FLOOR TOILET INSERT CORRODED. MX REPLACED INSERT, OPS CHECK GOOD.Oct 2, 2013 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR ASOA20131001182Light · shortedCREW REPORTED COCKPIT READING LIGHT CIRCUIT BREAKER TRIPPED WITH A BURNING ODOR. MX INSPECTED AND R & R F/O'S READING LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 1, 2013 · N16944 · Emb EMB145EP · Flight Compartment LightingSDR ASOA20130930179Wire · looseDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXIT SIGN ABOVE F/A`S HEAD WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RESECURRED THE WIRING ON THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICSep 30, 2013 · N14925 · Emb EMB145EP · Light System WiringSDR ASOA201309300178Flapper Valve · leakingTHE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE FLAPPER VALVE ON THE RT WING RIB 19, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2013 · N14933 · Emb EMB145EP · Fuel StorageSDR RAIA201309290002Bulb · inoperativeMX INSPECTED AND FOUND CEILING EMERGENCY EXIT LIGHT AT PASSENGER DOOR ENTRANCE INOP. REPLACED CEILING EMERGENCY EXIT LIGHT AND OPS CHECK GOOD.Sep 29, 2013 · N806HK · Emb EMB145EP · Emergency LightingSDR RAIA201309290001Bulb · inoperativeMX INSPECTED AND FOUND EMERGENCY LIGHT OVER F/A'S SEAT INOPERATIVE. REPLACED EMERGENCY LIGHT AND OPS CHECK.Sep 29, 2013 · N806HK · Emb EMB145EP · Emergency LightingSDR RAIA201309220001Terminal · unsecureBURNING ODOR COMING FROM F/O WINDSHIELD AREA AND SMOKE COMING FROM LT LOWER CORNER, DURING CLIMB. MX INSPECTED AND FOUND POWER TERMINAL LOOSE ON F/O'S WINDSHIELD. SECURED TERMINAL AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER, OPS CHECKED GOOD.Sep 22, 2013 · N806HK · Emb EMB145EP · Ice/Rain Protection System WiringSDR ASOA20130921170Smoke Detector · inoperativeAFTER TAKEOFF, CREW REPORTED A LAVATORY SMOKE INDICATION. RAN QRH ITEMS AND MESSAGE WENT AWAY, NO SMOKE NOTED. ACFT LANDED WITHOUT INCIDENT. MX R & R LAVATORY SMOKE DETECTOR, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.Sep 21, 2013 · N14945 · Emb EMB145EP · Smoke DetectionSDR ASOA20130923375Skin · crackedFUSELAGE SKIN BETWEEN THE CAPT WINDOW CUTOUT FRAME FWD TOP CORNER AND CAPT LT WINDSHIELD CUTOUT FRAME TOP OTBD CORNER CRACKED. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED 2 SHIMS AND A DOUBLER IAW ETD2013-145-041246. ACFT RELEASED TO SERVICE.Sep 19, 2013 · N15926 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130915168Light · inoperativeDURING TESTING, NR 3 EMERGENCY LIGHT FAILED TO ILLUMINATE. MX REPLACED THE LIGHT STRIP, OPS TESTED THE SYS AND CLEARED THE DISCREPANCY.Sep 15, 2013 · N15948 · Emb EMB145EP · Emergency LightingSDR RAIA201309090001Seal · leakingBLEED NR 1 LEAK DURING CLIMB, RETURN FROM FLIGHT. MX INSPECTED AND FOUND LEAKS AT COUPLINGS 7 AND 9, REPLACED THE SEALS AT THOSE LOCATIONS AND OPS CHECK GOOD.Sep 9, 2013 · N808HK · Emb EMB145EP · Pneumatic Distribution SystemSDR RAIA201309040002Connector · corrodedSPOILER FAIL MESSAGE IN FLIGHT, SPOILERS SHOW OPEN ON GROUND. MX REPLACED CONNECTOR AT RT INBD SPOILER PROXIMITY SWITCH, OPS CHECK GOOD.Sep 4, 2013 · N809HK · Emb EMB145EP · Flight Control System WiringSDR RAIA201309040001Bulb · inoperativeEMERGENCY LIGHT INOPERATIVE AT LEFT AFT WING-FUSELAGE FAIRING. MX REPLACED BULB AND OPS CHECKED GOOD.Sep 4, 2013 · N802HK · Emb EMB145EP · Emergency LightingSDR ASOA20130902160Bulb · burned outDURING MX INSP, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 2, 2013 · N14933 · Emb EMB145EP · Emergency LightingSDR RAIA201309010001Bulb · inoperativeLT OVERWING EMERGENCY EXIT LIGHT IS INTERMITTENT. MX REPLACED THE EMERGENCY LIGHT BULB AND OPS CHECKED GOOD.Sep 1, 2013 · N802HK · Emb EMB145EP · Emergency LightingSDR ASOA20130830158Gcu · malfunctionedTHE CREW REPORTED AN ELECTRICAL PROBLEM WITH THE MAIN BUSS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL ODOR CAME IN THE COCKPIT) AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING IN BPT WITHOUT INCIDENT. Aug 30, 2013 · N14939 · Emb EMB145EP · AC Generator-AlternatorSDR ASOA20130830157Starter Gen · malfunctionedTHE CREW REPORTED AN ELECTRICAL PROBLEM WITHTHE MAIN BUS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL SMELL CAME IN THE COCKPIT, AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING WITHOUT INCIDENT. MX INSPEAug 30, 2013 · N14939 · Emb EMB145EP · Starter-GeneratorSDR RAIA201308240001Fairing · looseVERY NOTICEABLE VIBRATION ON YOKE ABOVE 220 KIAS. MX FOUND ELEVATOR TRIM FAIRING LOOSE ON ELEVATOR. MX REMOVED FAIRING AND PLACED ON CDL 55-20-3.Aug 24, 2013 · N808HK · Emb EMB145EP · Elevator StructureSDR ASOA20130820154Inverter · inoperativeDURNG MX INSPECTION, SEVERAL FLOOR EMERGENCY LIGHT PROXIMITY STRIPS DID NOT ILLUMINATE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 20, 2013 · N14937 · Emb EMB145EP · Emergency LightingSDR RAIA201308160001Gusset · corrodedCENTER GUSSET FR59 CORRODED BEYOND LIMITS. MX REPLACED CENTER GUSSET AT FR59.Aug 16, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308150002Fitting · looseDURING CLIMB AT 25,000 FT, CREW REPORTED HARD TO CONTROL PRESSURIZATION, NOT ABLE TO PRESSURIZE. RETURNED TO DEPARTURE, MX INSPECTED AND FOUND MANUAL CONTROLLER PRESSURE LINE FITTING LOOSE AND LEAKING, TIGHTENED AND OPS CHECKED GOOD.Aug 15, 2013 · N808HK · Emb EMB145EP · Cabin Pressure Control SystemSDR RAIA201308140012Support Angle · corrodedRAMP SUPPORT ANGLE ON BEAM Y-479.0 IS CORRODED AT FR18. MX REPLACED RAMP SUPPORT ANGLE ON BEAM Y-479.0 AT FR18.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140011Floor Support · corrodedLT FLOOR SUPPORT AT FRAMES 17 - 23 IS CORRODED BEYOND LIMITS. MX REPLACED LT FLOOR SUPPORT.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140010Beam · corrodedDOUBLER ON BEAM Y-479.0 AT FR22 IS CORRODED BEYOND LIMITS. MX REPLACED DOUBLER.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Main, StructureSDR RAIA201308140009Beam · corrodedDOUBLER ON BEAM Y-479.0 AT FR20 IS CORRODED BEYOND LIMITS. MX REPLACED DOUBLER.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Main, StructureSDR RAIA201308140008Profile · corrodedPASSENGER DOOR FRAME U-PROFILES ARE CORRODED BEYOND LIMITS. MX REPLACED PASSENGER DOOR FRAME U-PROFILES.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140007Shear Tie · corrodedSHEAR TIE ON AFT CARGO DOOR FRAME IS CORRODED BEYOND LIMITS. REPLACED DAMAGED PORTION OF SHEAR TIE ON AFT CARGO DOOR FRAME.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Internal Mounting StructureSDR RAIA201308140006Sill · corrodedAFT RT SERVICE DOOR SILL CORRODED BEYOND LIMITS. MX REPLACED AFTER RT SERVICE DOOR SILL.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140005Sill · corrodedFWD RT SERVICE DOOR SILL CORRODED BEYOND LIMITS. MX REPLACED FWD RT SERVICE DOOR SILL.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140004Beam · corrodedBOTH FWD AND AFT BEAM ASSY NEAR PASSENGER DOOR AT Y-479.0 CORRODED BEYOND LIMITS. MX REPLACED BOTH ANGLES.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Main, StructureSDR RAIA201308140003Support · corrodedAFT ANGLE FOR CENTER RAMP SUPPORT AT Y0.0 HAS CORROSION BEYOND LIMITS. MX REPLACED AFT ANGLE FOR CENTER RAMP SUPPORT.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140002Support · corrodedCENTER RAMP SUPPORT AT Y0.0 HAS CORROSION BEYOND LIMITS. MX REPLACED CENTER RAMP SUPPORT.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308140001Gusset · corrodedFORWARD CENTER "U" GUSSET AT Y 0.0 HAS CORROSION BEYOND LIMITS. REPLACED FWD CENTER "U" GUSSET.Aug 14, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201308130001Channel · corrodedCARGO BAY ZEE CHANNEL CORRODED. MX REPLACED CHANNEL.Aug 13, 2013 · N807HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR ASOA20130810198Fire Detector · defectiveFIRE DETECTION FAIL MESSAGE ON EICAS DURING TAXI. R & R FIRE DETECTOR IAW AMM 26-11-01. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 10, 2013 · N15941 · Emb EMB145EP · Fire DetectionSDR ASOA20130808145Skin · crackedDURING 2A INSPECTION THE LT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FRAME 77 BELOW STRINGER 8L. MX REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVAug 8, 2013 · N14933 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130808144Skin · crackedDURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STR 5R. MC REMOVED THE DAMAGE, AND PERFORMED A FREEZE PLUG REPAIR ISE APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 8, 2013 · N14933 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130808143Skin · crackedDURING 2A INSPECTION, LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN TWO PLACES AT A RIVET ON FRAME 79 BELOW STRINGER 5L. MX REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW IAW APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SAug 8, 2013 · N14933 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719125Skin · crackedDURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRAKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUYBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719132Skin · crackedDURING INSPECTION, LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6L. MX PERFORMED A BUSHING REPAIR IAW ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719131Skin · crackedDURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719130Skin · crackedDURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 4 PLACES AT A SINGLE RIVET ON FRAME 79 BELOW STRINGER 05L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719129Skin · crackedDURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A SINGLE RIVET ON FRAME 77 BELOW STRINGER 8L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719128Skin · crackedDURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/20/2013.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719126Skin · crackedDURING INSPECTION, RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW EA EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130719127Skin · crackedDURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 3R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHNICAL DISPOSITION ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130716124Skin · crackedDURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 17, 2013 · N14938 · Emb EMB145EP · Fuselage Main, Plate/Skin
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