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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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-SDR 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 TSDR 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 COMPARTMENSDR 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 REWORKESDR 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 SDR 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 CLEASDR 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 25-33-44SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR VNAA202209249992Floorbeam · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.SDR VNAA2022092499910Stringer · corrodedCORROSION ON STRINGER 27 BTW FS 349.00 TO FS 353.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.SDR VNAA202209249999Stringer Splice · corrodedCORROSION WAS FOUND ON STRINGER SPLICE FS 333.00 ON STRINGER 23RH AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.SDR VNAA202209249991Stringer Clip · crackedCRACK ON STRINGER ATTACHED ANGLE ON STGR 7LH FS1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE.SDR VNAA202209229997Stringer · corrodedCORROSION ON STRINGER 24RH BTW FS 333.00 TO FS 364.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURESDR VNAA202209249993Frame · corrodedCORROSION ON FRAME AT STGR 26LH & FS1031.00 AT AFT BAGGAGE BAY.SDR VNAA202209229995Strip · corrodedCORROSION ON METALIC STRIP (1EA) AT FORWARD UNDERWING FAIRNG 193AB.SDR VNAA2022092499911Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS863 - FS969SDR VNAA202209249994Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS 581 - FS 661SDR VNAA202209229994Seat Track · corrodedCORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS708+5 - FS 761.00SDR VNAA202209249997Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS581.40 - FS677.0SDR VNAA202209249996Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS485.0 - FS581.0SDR VNAA202209249995Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS349.0 - FS485.SDR VNAA202210119993None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17LHSDR VNAA202210119992None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17RHSDR 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 WELLSDR VNAA2022092499912Intercostal · corrodedCORROSION WAS FOUND ON INTERCOSTAL AT STRINGER 20R, BTW FS 310.00 AND FS 319.70 ON MAIN AVIONICS COMPARTMENTSDR VNAA202209249998None · corrodedCORROSION WAS FOUND ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00SDR VNAA202209229993Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS847+5 - FS967 ON STRINGER 15RHSDR VNAA202209229992Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS785+4 - FS847+15 ON STRINGER 15RHSDR VNAA202209229991Seat Track · corrodedCORROSION AT SEAT RAIL BETWEEN FS708+4 - FS761 ON STRINGER 15RHSDR VNAA202209209991Floorbeam · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.SDR VNAA202209229998Stringer · corrodedCORROSION ON STRINGER 22RH BTW FS 333.00 TO FS 349.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURESDR VNAA202209229996None · crackedCRACK ON AFT BACKING OF REFUEL DUCT SUPPORT STRUCTURE ON FS 679.00, BTW STGR 22RH AND 21RH.SDR VNAA202210119994None · crackedCRACKS ON LOWER PRESSURE SEAL RETAINER BOTH CORNERS AT FWD BAGGAGE BAY DOORSDR 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 DELSDR 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 NOTEDSDR 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 TSDR 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-4025SDR 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.SDR 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.SDR 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.SDR 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 51-42-13SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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