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 C2XA11IA090Connector · burnedIAH - POST FLIGHT 2812, THE CREW REPORTED ELECTRICAL SMOKE IN THE CABIN AND COCKPIT, AND SEEMED TO BE STRONGEST AROUND ROWS 8 & 9. IAH MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT CONNECTOR AT ROW 10 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED TMay 7, 2011 · N15941 · Emb EMB145EP · Light System WiringSDR C2XA11IA083Display · shortedXNA - FLIGHT 2619 THE CREW REPORTED A SMOKE SMELL FOLLOWED BY THE CAPTAINS PFD CIRCUIT BREAKER POPPING. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE CAPTMay 6, 2011 · N14945 · Emb EMB145EP · Central DisplaySDR RAIA20110504001Arm · bentMAINTENANCE INSPECTED AND FOUND THE PASSENGER DOOR STEP ROLLER ARM BENT. MAINTENANCE REMOVED AND REPLACED THE ROLLER ARM. DOOR OPS CHECKED GOOD.May 4, 2011 · N805HK · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA201105030001Fan · malfunctionedDURING CRUISE THE FLIGHT CREW GOT A NR 1 AHRS OVERHEAT FAIL MESSAGE ON THE EICAS. AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 1 AHRS FAN. SYSTEM OPS CHECKED GOOD.May 3, 2011 · N804HK · Emb EMB145EP · Integrated Flight SystemSDR C2XA11IA081Acm · seizedXNA - FLIGHT 3099, THE CREW REPORTED A BURNING SMELL AND SMOKE FROM THE LEFT COCKPIT VENT AT THE WINDOW WITH A PACK 1 OVERHEAT MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WHERE PACK TWO WAS CHECKED USING BOTH ENGINES WITH NO DEFECTS, AND PACK ONE WAS PLACED ONMay 3, 2011 · N16927 · Emb EMB145EP · Cabin Cooling SystemSDR RAIA201105010005Light · out of positionDURING FLIGHT THE GALLEY CEILING EMERGENCY EXIT LIGHT FELL OFF. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE GALLEY EMERGENCY EXIT LIGHT. SYSTEM OPS CHECKED GOOD.May 1, 2011 · N804HK · Emb EMB145EP · Emergency LightingSDR C2XA11IA078Computer · faultyIAH - FLIGHT 3127, THE CREW REPORTED THAT AHRS NR 1 FAILED IN FLIGHT TWICE FOR 30 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AMay 1, 2011 · N14939 · Emb EMB145EP · Integrated Flight SystemSDR RAIA201104250003Roller · lack of lubeDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND CLEANED AND LUBBED THE PASSENGER DOOR ROLLERS. DOOR OPS CHECKED GOOD.Apr 25, 2011 · N807HK · Emb EMB145EP · Passenger/Crew DoorsSDR C2XA11IA074Blade · brokenFLIGHT 2031, CREW REPORTED NR 2 ENG LP VIBRATIONS EXCEEDED LIMITS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE NR 2 ENGINE, OPS AND LEAK CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETUApr 21, 2011 · N15948 · Emb EMB145EP · Turbine SectionSDR CHQA201100132Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE CENTER FUSELAGE 1 SKIN BETWEEN FRAMES 19 AND 20 THAT WAS BEYOND LIMITS. THE DENT MEASURED 3 INCHES WIDE, BY 2.8 INCHES LONG AND 0.064 INCHES DEEP. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CRACApr 13, 2011 · N978RP · Emb EMB145EP · Fuselage Main, Plate/SkinSDR CHQA201100147Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR CENTER FUSELAGE I ANGLE UNDER CARBON POST AT FRAME 18 ON LEFT OMEGA BEAM ANGLE. MAINTENANCE REPLACED THE CENTER FUSELAGE UNDER CARBON POST FRAME 18 ON LEFT OMEGA BEAM WITH NO FURTHER DEFECTS NOTED.Apr 12, 2011 · N978RP · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201100146Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE DOOR SURROUND STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE DOOR SURROUND LOWER BEAM WITH NO FURTHER DEFECTS NOTED. THE CARGO FLOOR STRUCTURE DOOR SURROUND STRUCTURE Apr 12, 2011 · N978RP · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA201104110001Coupling · leakingDURING FLIGHT THE NR 2 AIR CONDITIONING PACK HAD AN OVER LOAD MESSAGE. AIRCRAFT RETURNED TO ORD AND MAINTENANCE INSPECTED AND REMOVED AND REPLACED COUPLINGS ON THE PACK VALVE AND TEMP CONTROL VALVE. SYSTEM OPS CHECKED GOOD.Apr 11, 2011 · N803HK · Emb EMB145EP · Cabin Cooling SystemSDR RAIA2011041100003Coupling · defectiveDURING CLIMB, THE CREW REPORTED RECEIVING A PACK 2 OVERLOAD MESSAGE WITH PACK NR 1 ALREADY DEFERRED. MAINTENANCE REMOVED AND REPLACED BLEED DUCT COUPLINGS AND TEMP CONTROL VALVE. FOLLOW-ON OPERATIONAL CHECK WERE GOOD.Apr 11, 2011 · N803HK · Emb EMB145EP · Pneumatic Distribution SystemSDR CHQA201100131Spar · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT WING SPAR I TOP FLANGE CRACKED THRU AT RIB 19. THE CRACK WAS 2.745 INCHES LONG AND 0.001 INCHES WIDE THRU THE MATERIAL. THE DAMAGED AREA WAS REMOVED AND A REINFORCING PATCH WAS INSTALLED PER TI-145-11-095.Apr 10, 2011 · N978RP · Emb EMB145EP · Wing SparSDR CHQA201100135Channel · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE 1 SERVICE DOOR CHANNEL. THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I SERVICE DOOR CHANNEL WAS REPLACED.Apr 7, 2011 · N978RP · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201100134Rib · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM CENTER RIB. MAINTENANCE REPLACED THE MAIN PASSENGER DOOR STRUCTURE BOTTOM CENTER RIB.Apr 4, 2011 · N978RP · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA201104030003Fan · dirtyDURING CLIMB THE AIRCRAFT HAD A AHRS NR 1 OVERHEAT MESSAGE ON THE EICAS. AIRCRAFT RETURNED FROM FLIGHT. MAINTENANCE INSPECTED AND CLEANED AHRS NR 1 FAN. SYSTEM OPS CHECKED GOOD.Apr 3, 2011 · N804HK · Emb EMB145EP · Integrated Flight SystemSDR CHQA201100125O-Ring · leakingCREW REPORTED THAT DURING CLIMB, IN ICING CONDITIONS, RECEIVED A "BLEED 1 LEAK" MESSAGE. THE MESSAGE WENT AWAY AFTER THE BLEED 1 VALVE CLOSED. THE CREW RETURNED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RING AT THE LEFT WING ROOT. OPEMar 31, 2011 · N978RP · Emb EMB145EP · Pneumatic Distribution SystemSDR C2XA11IA060Skin · crackedIAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL ON THE CAPTAINS SIDE WAS FOUND TO BE CRACKED BETWEEN THE CAPTAINS DV WINDOW AND THE CAPTAINS WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVMar 27, 2011 · N14942 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR V0XR20110321001Fitting · corroded(V0XR) FRAME FOOT AT FR 62 AND STR 19-185 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SHEAR CLIP AT FR 62 AND STR 19-185 IAW EMB145 SRM 51-10-02, 51-40-02, 51-20-03. W/C 1069Mar 21, 2011 · N808HK · Emb EMB145EP · Fuselage Main, FrameSDR C2XA11IA059Engine · vibrationIAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT Mar 21, 2011 · N14939 · Emb EMB145EP · Engine (Turbine/Turboprop)SDR CHQA201100068Connector · corrodedCREW REPORTED THAT WHILE ON FINAL APPROACH INTO CAE, HAD WINDSHEAR WARNING DUE TO WEATHER AND ON GEAR RETRACTION, THE NOSE LANDING GEAR RETRACTED NORMALLY, BUT 30 SEC LATER THERE WAS A LANDING GEAR AIR/GROUND FAIL MESSAGE AND BOTH MAINS SHOWED IN TRANSIT. A MMar 19, 2011 · N978RP · Emb EMB145EP · Landing Gear System WiringSDR C2XA11IA055Control Handle · inoperativeIAH - FLIGHT 2544, THE CREW REPORTED THAT THE GEAR WAS SLOW TO RETRACT ON DEPARTURE FROM DAL WITH THE ASSOCIATED WARNINGS. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE, OPERATIONALLYMar 17, 2011 · N15948 · Emb EMB145EP · Landing Gear SelectorSDR C2XA11IA056Element · inoperativeIAH - FLIGHT 2804 THE CREW REPORTED AN E2 FIRE DETECTOR FAIL MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE FIRE DETECTOR ELEMENT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRMar 16, 2011 · N14937 · Emb EMB145EP · Fire DetectionSDR RAIA201103160001Glowstrip · looseDURING POST FLIGHT INSPECTION THE MAINTENANCE FOUND THE PHOTO LUMINESCENT LIGHT STRIP LOOSE AT ROW 1A. MAINTENANCE RE-SECURED THE LIGHT STRIP. SYSTEM OPS CHECKED GOOD.Mar 16, 2011 · N802HK · Emb EMB145EP · Emergency EquipmentSDR RAIA201103150001Power Supply · dischargedDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE OVERWING EMERGENCY EXIT SIGND INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY POWER SUPPLY. SYSTEM OPS CHECKED GOOD.Mar 15, 2011 · N804HK · Emb EMB145EP · Emergency LightingSDR V0XR20110314008Seat Track · corrodedSEAT TRACK RT SIDE POSITION D, STA 17913.2 TO STA 20230.0 CORRODED BETWEEN AND UNDER SCREWS. R & R SEAT TRACK RT SIDE, POSITION D, STA 17913.2 TO STA 20230.0 IAW EMB 53-01-06.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR20110314007Seat Track · corrodedSEAT TRACK, RT SIDE POSITION D STA 15506.5 TO STA 17913.2 CORRODED AROUND SCREWS AND BETWEEN SCREWS. R & R RT SIDE SEAT TRACK POSITION D STA 15506.5 TO STA 17913.2 IAW AMM 53-01-06.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR20110314006Seat Track · corrodedSEAT TRACK RT SIDE POSITION C STA 12176.2 TO STA 15506.5 IS CORRODED AROUND SCREWS. R & R SEAT TRACK C AT STA 12176.2 TO STA 15506.5 IAW AMM 53-01-06.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR20110314005Seat Track · corrodedSEAT TRACK, LT SIDE POSITION B STA 12176.2 TO STA 15506.5 CORRODED AROUND SCREWS. R & R SEAT TRACK B AT STA 12176.2 TO STA 15506.5 IAW AMM 53-01-06.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR20110314004Strip · crackedRT UPPER FAIRING STRIP FROM STA 16143.5 TO 17445.0 IS CRACKED. REPLACED RT UPPER FAIRING STRIP FROM STA 16143.5 TO 17445.0 IAW SRM 51-10-02, 51-40-02, 51-20-03.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR20110314003Bracket · crackedBRACKET CRACKED ON FWD END OF RT BLEED AIR PACK CONTROL VALVE IN WING ROOT. REMOVED CRACKED BRACKET, RECEIVED NEW BRACKET, LOCATED TO ACFT, DRILLED AND INSTALLED BRACKET IAW SRM 51-40-02.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR20110314002Frame · corrodedRT BEAM FRM 58-63 IS CORRODED OUT OF LIMITS. R & R RT BEAM FRAME 58-63 IAW SRM 51-10-02, 51-40-02, AND CPM 51-21-05, 51-21-04.Mar 14, 2011 · N808HK · Emb EMB145EP · Fuselage Main, FrameSDR V0XR201103110021Fairing · corrodedCOCKPIT CTR WINDSHIELD UPPER FAIRING IS DAMAGED. R & R FAIRING.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110020Seat Track · corrodedRT SEAT TRACK POSITION C STA 17913.2-20230.0 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110019Seat Track · corrodedLT SEAT TRACK POSITION A STA 17913.2-20230.0 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110018Seat Track · corrodedRT SEAT TRACK POSITION C STA 15506.5-17913.2 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110017Seat Track · corrodedLEFT SEAT TRACK POSITION B STA 15506.5-17913.2 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110016Seat Track · corrodedRT SEAT TRACK POSITION C STA 9814.0-1276.2 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110015Seat Track · corrodedRT SEAT TRACK POSITION C STA 7324.0 - STA 9814.0 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201103110014Support · corrodedCENTER BEAM SUPPORT AT FR 60 IS CORRODED BEYOND LIMITS. R & R CTR BEAM SUPPORT.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110013Gusset · crackedCTR GUSSET AT FR 29-36 IS CORRODED BEYOND LIMITS. R & R GUSSET.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110012Duct · crackedGASPER DUCT ASSY IS CRACKED UNDER FLOOR BETWEEN FR 47-48. R & R DUCT ASSY.Mar 11, 2011 · N808HK · Emb EMB145EP · Air Distribution SystemSDR V0XR201103110011Stand Off · brokenSTANDOFF AT FR 25 BROKEN. R & R STANDOFF.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110010Fitting · brokenSTANDOFF AT FR 20 BROKEN. R & R STANDOFF.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110009Shear Tie · corrodedFRAME FOOT AT FR 60 STA 17R-18R IS CORRODED BEYOND LIMITS. R & R SHEAR CLIP.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Internal Mounting StructureSDR V0XR201103110008Beam · corrodedCTR BEAM AT Y0.0 FR 58-63 IS CORRODED BEYOND LIMITS. R & R BEAM.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201103110007Profile · corrodedRT PROFILE AT 61 IS CORRODED BEYOND LIMITS. R & R PROFILE.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201103110006Gusset · corrodedLEFT GUSSET AT 19-23 IS CORRODED BEYOND LIMITS. R & R GUSSET.Mar 11, 2011 · N808HK · Emb EMB145EP · Fuselage Miscellaneous Structure
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