N542EA

Service difficulty reports · 91

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N542EA' AND registry_match = 'registration'
  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 VNAA20260328005Hinge · corrodedCORROSION ON FWD/ MIDDLE/ AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. CORROSION ON MIDDLE HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND EVAUATED WITHIN LIMITS PER CRJ-700 SRM 53-Mar 9, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA20260328004Drag Angle · crackedDURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TFeb 10, 2026 · N542EA · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous StructureSDR VNAA20260328003Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENFeb 10, 2026 · N542EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260328010Seat Track · corrodedCORROSION SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 AT PAX CABIN. CORROSION ON SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 (PAX CABIN) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REWORKEFeb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260328009Seat Track · corrodedCORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2 SECTIONS) FROM FS785 TO FS953 AT PAX CABIN. CORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2 Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260328007Hinge Fitting · corrodedCORROSION IN THE INNER AREA OF THE BORE LUGS AT AILERON FITTING 1, CENTRAL FITTING (L1, L2, L3, L4, L5, L6) AND FITTING 4 (UPPER AND LOWER) OF LH WING AILERON. BORE LUGS HINGE FITTING NO. 1 & 4 (LOWER) , CENTER HINGE FITTING BORE LUGS L1, L3, L4, L6 WERE CLEAFeb 8, 2026 · N542EA · Bombdr CL6002D15 · AileronsSDR VNAA20260328006Fitting · corrodedWORKSHOP INTERIOR SHEET METAL: CORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-44Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2025090211101Transceiver · fluctuatesIN-FLIGHT AT FL20.0 WE EXPERIENCED THE RA START TO MAKE 25.00FT, 500FT, 100FT CALL OUTS AND FLUCTUATE. / REMOVED AND REPLACED RAD ALT #1 IAW CR7 AMM 34-44-01-000/400-801-A02-PSA. BIT CHECKS GOOD.Aug 29, 2025 · N542EA · Cndair CL6002C10 · Ground Proximity SystemSDR VNAA2025073111102Hose · chafedHYD SYSTEM 2 LOW PRESSURE CAUTION MESSAGE IN FLIGHT WITH 0% QUANTITY. FOUND HYD 2 DAMPENER FLEX HOSE TO BE CHAFED THROUGH BY ADEL CLAMP. REMOVED AND REPLACED HOSE AND CLAMP IAW AMM 29-11-59-000/400-801. OPS CHECK/LEAK CHECK GOOD.Jul 26, 2025 · N542EA · Cndair CL6002C10 · Hydraulic System, MainSDR VNAA2025032411101Steering Sys · malfunctionedSTEERING INOP AFTER TAKEOFF. / PERFORMED OPS CHECK OF THE NOSEWHEEL STEERING IAW CRJ700 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.Mar 21, 2025 · N542EA · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2025021211101Skin · dentedDENT ON LH FUSELAGE AFT OF AFT NLG DOOR. / REPAIRED LH FUSELAGE BETWEEN FS250.00- FS265.00 STR24L-STR23L IAW REO 670-53-11-2096 AND CRJ700 SRM REF 51-42-21.Feb 10, 2025 · N542EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2024110511102Unknown · odorSMOKE CONDITION IN CABIN, CONDITION IMPROVED WHEN PACKS SHUT OFF. / INSPECTED AIRCRAFT IAW CRJ700 FIM 21ˆ’21/22ˆ’00ˆ’810ˆ’806-A01 AND FOUND B1 CODE 211943--RH PACK AUTOFAILED CAUTION MSG DISPLAYED. ISOLATED ISSUE TO THE RH PACK, VENTIALATED AIRCRAFT CABIN Nov 1, 2024 · N542EA · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202209249992Floorbeam · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.Sep 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2022092499910Stringer · corrodedCORROSION ON STRINGER 27 BTW FS 349.00 TO FS 353.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.Sep 13, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209249999Stringer Splice · corrodedCORROSION WAS FOUND ON STRINGER SPLICE FS 333.00 ON STRINGER 23RH AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.Sep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209249991Stringer Clip · crackedCRACK ON STRINGER ATTACHED ANGLE ON STGR 7LH FS1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE.Sep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209229997Stringer · corrodedCORROSION ON STRINGER 24RH BTW FS 333.00 TO FS 364.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURESep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209249993Frame · corrodedCORROSION ON FRAME AT STGR 26LH & FS1031.00 AT AFT BAGGAGE BAY.Sep 5, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202209229995Strip · corrodedCORROSION ON METALIC STRIP (1EA) AT FORWARD UNDERWING FAIRNG 193AB.Sep 4, 2022 · N542EA · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2022092499911Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS863 - FS969Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209249994Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS 581 - FS 661Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209229994Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS708+5 - FS 761.00Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209249997Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS581.40 - FS677.0Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209249996Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS485.0 - FS581.0Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209249995Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS349.0 - FS485.Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202210119993None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17LHAug 14, 2022 · N542EA · Bombdr BD1001A10 · Fuselage Structure (General)SDR VNAA202210119992None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17RHAug 14, 2022 · N542EA · Bombdr BD1001A10 · Fuselage Structure (General)SDR VNAA202210119991None · corrodedCORROSION ON WHEEL BINS ATTACHMENT ANGLES (2 EA) BTW FS 797.00 TO FS 830.40 RBL 16 AND LBL 49 ON MAIN WHEEL WELLAug 14, 2022 · N542EA · Bombdr BD1001A10 · Standard Practices/StructuresSDR VNAA2022092499912Intercostal · corrodedCORROSION WAS FOUND ON INTERCOSTAL AT STRINGER 20R, BTW FS 310.00 AND FS 319.70 ON MAIN AVIONICS COMPARTMENTAug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202209249998None · corrodedCORROSION WAS FOUND ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209229993Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS847+5 - FS967 ON STRINGER 15RHAug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209229992Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS785+4 - FS847+15 ON STRINGER 15RHAug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209229991Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS708+4 - FS761 ON STRINGER 15RHAug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202209209991Floorbeam · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202209229998Stringer · corrodedCORROSION ON STRINGER 22RH BTW FS 333.00 TO FS 349.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTUREAug 12, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202209229996None · crackedCRACK ON AFT BACKING OF REFUEL DUCT SUPPORT STRUCTURE ON FS 679.00, BTW STGR 22RH AND 21RH.Aug 12, 2022 · N542EA · Cndair CL6002C10 · Fuel ServicingSDR VNAA202210119994None · crackedCRACKS ON LOWER PRESSURE SEAL RETAINER BOTH CORNERS AT FWD BAGGAGE BAY DOORAug 2, 2022 · N542EA · Bombdr BD1001A10 · Standard Practices/StructuresSDR VNAA202201071111Gust Lock · false indicationAS PILOT FYING ON SHORT FNAL INTO RWY 16 AT HPN (<500'AGL), GOT A GLD RELATED MASTER CAUTION MSG. DUE TO THE SHORT RUNWAY AND DOWNHILL SLOPE, I COMMENCED A GO-AROUND. MESSAGE EXTINGUISHED DURING THE CLIMB OUT BEFORE I COULD ASCERTAIN THE EXACT MESSAGE. GOT DELJan 5, 2022 · N542EA · Cndair CL6002C10 · Gust Lock Damper SystemSDR VNAA2020080511101Unknown · odorSTRONG BURNING ODOR IN AFT ROWS WHEN AC POWER APPLIED - INSPECTED AFT EQUIP. BAY , AND CAB LIGHTING, CYCLED AC POWER FROM CAT AND APU , AND CYC RH PACK NO DEFECTS NOTED SMELL NOT PRESENT. GVI NO DEFECTS NOTEDAug 3, 2020 · N542EA · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2020062211101Pump · failedHYDRAULICS SYSTEM FAILURE. FLIGHT CREW RAN THE QRH, AND DECLARED AN EMERGENCY. HYD PUMP 3A LOW PRESSURE CAUTION IN FLIGHT. REMOVED AND REPLACED NR 3A HYD ACMP. SERVICED 3A HYD SYS TO 55% AT 49 DEGREES C. PERFORMED OPERATIONAL AND LEAK CHECK. NO LEAKS AT TJun 21, 2020 · N542EA · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), MainSDR SIMA202002065009Skin · damagedEXT. FUSELAGE SKIN HAS AREA OF DAMAGE BETWEEN FS 969.00 AND 985.00 AT STR 27.-C/A-C/W REPAIR IAW ERS-CR-53MR-4025Feb 5, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA202001287001Angle · cracked"L" ANGLE AT BL 26.0 ON RH SIDE IS CRACKED ON LOWER END. -C/A-FOUND STANCHION TO BE CRACKED BEHIND THE RH BULKHEAD. REMOVED AND REPLACED STANCHION BEHIND THE RH BULKHEAD IAW SRM 5-42-12. CHECK NRWC E767449 FOR INSTALLATION OF NEW "L" ANGLE.Jan 27, 2020 · N542EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA202001295006Bulkhead · corrodedRH BULKHEAD WALL AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION AT FLOOR LEVEL-C/A-COMPLETED RH BULKHEAD LOWER WEB REPAIR @ FS280.00 IAW SRM 53-11-10-201-004.Jan 25, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA202002034003Floorbeam · corrodedRH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-REMOVED AND REPLACED RH FLOOR BEAM AT FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.Jan 24, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20200203004Floorbeam · corrodedLH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-RAR'D LH FLOOR BEAM AT FS2800.00 IAW SRM 51-42-06 AND 51-42-13Jan 23, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA202001273002Support Angle · crackedPASSENGER DOOR AFT SIDE HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR. -C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW 52-11-04-201-004-A01.Jan 23, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA2020020412008Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04.Jan 20, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20200203007Skin · crackedPASSENGER DOOR AFT SIDE SKIN HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW SRM 52-11-04-201-004-A01.Jan 20, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA2020020517014Floorbeam · crackedRH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.Jan 17, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA2020020517015Floorbeam · crackedLH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.Jan 17, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
Back to N542EA