N531EG

Service difficulty reports · 89

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 = 'N531EG' 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 VNAA2026030913501Unknown · odorSTRONG FUMES AFTER APU START AFT LANDING THROUGHOUT THE WHOLE CABIN. / TROUBLESHOT SMELL PER CRJ7 FIM 22-21-00-810-806. NO SMELL OBSERVED. COULDN€™T REPLICATE FAULT AT THIS TIME.Mar 7, 2026 · N531EG · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2026022813001Pcb · failedL VIB FAULT, R VIB FAULT, STATUS MESSAGE AT FL230. REMOVED AND REPLACED JB2, PCB2 IAW CRJ 700 AMM 24-01-05-000/400-801-A01. OPS CHECK GOOD AT THIS TIME.Feb 24, 2026 · N531EG · Cndair CL6002C10 · Engine Indicating SystemSDR VNAA20251025001Hinge · gougedPAX DOOR HINGE HAS SEVERAL LUGS GOUGED ON BOTH HINGES. REMOVED AND REPLACED PAX DOOR FUSELAGE SIDE HINGE IAW CRJ 700 SRMS 53-21-23-201-007-A01 AND 51-42-21-001-001-A01.Oct 25, 2025 · N531EG · Cndair CL6002C10 · Fuselage, Door HingeSDR VNA202310091005Fitting · damagedPERFORM PERMANENT REPAIR TO NOSE FUSELAGE JACKING PAD HELICOIL INSERT.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNA202310092004Web · corrodedPAX DOOR FWD SIDE INTERCOSTAL DD7 BRACKET FOUND TO BE CRACKED IN THE RADIUS.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNA202310092003Floorbeam · corrodedFOUND CORROSION ON RH FS 280 FLOOR BEAM PN# CC670-34094-2.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNA20231009001Web · crackedPAX DOOR STAIR FWD WEB HAS MULTIPLE CRACKS AT STEP CORNER LOCATIONS, CORROSION AT STAIR FASTENER ATTACH POINTS AND PREVIOUS REPAIRS THAT INTERFERE WITH INTEGRATION OF MODSUM IS67052110210. REQUIRES REPLACEMENT.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNA2023F00005Fitting · damagedPERFORM PERMANENT REPAIR TO NOSE FUSELAGE JACKING PAD HELICOIL INSERT.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, StructureSDR VNA2023F00004Web · corrodedPAX DOOR FWD SIDE INTERCOSTAL DD7 BRACKET FOUND TO BE CRACKED IN THE RADIUS.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNA2023F00003Floorbeam · corrodedFOUND CORROSION ON RH FS 280 FLOOR BEAM PN# CC670-34094-2.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNA2023F00002Floorbeam · corrodedFOUND CORROSION ON FS 280 L/H FLOOR BEAM ON FWD PN# CC670-34094-1.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202310090004Skin · dentedTHE FWD LH FUSELAGE SKIN IS DENTED BELOW THE ADG FS 177-185, STR 23.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNA2023F00001Web · crackedPAX DOOR STAIR FWD WEB HAS MULTIPLE CRACKS AT STEP CORNER LOCATIONS, CORROSION AT STAIR FASTENER ATTACH POINTS AND PREVIOUS REPAIRS THAT INTERFERE WITH INTEGRATION OF MODSUM IS67052110210. REQUIRES REPLACEMENT.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202310090002Former · corrodedPAX DOOR FWD FORMER CORRODED.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202310090001Stringer · corrodedSTRINGER 24L IS CORRODED BETWEEN FS 953.00 AND 969.00.Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202303131111Windshield · burnedCA WINDSHIELD CRACKED AND CAUGHT FIRE ALONG UPPER EDGE CRACKED ABOUT 18 INCHES. REMOVED AND REPLACED LH WINDSHIELD IAW CRJ7 AMM 56-11-01-000/400-801-A01-PSA.Mar 9, 2023 · N531EG · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA202301181111Handle · out of positionPAX DOOR INNER HANDLE MOVED OUT OF LOCKED POSITION MULTIPLE TIMES DURING FLIGHT. PERFORMED GVI OF INTERNAL PAX DOOR IAW CRJ 700 AMM 52-11-00-210-803. PERFORMED FUNCTIONAL TEST MULTIPLE TIMES IAW AMM 52-11-00-720-802. NO DEFECTS NOTED AT THIS TIME AND OPS Jan 16, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2022090399914Fitting · corrodedL/H JACK FITTING WEB IS CORRODED/CRACKED. REMOVED AND REPLACED NOSE JACK FITTING AND LH + RH INTERCOSTALS IAW CRJ-700 SRM 51--42-06-001-001-A01 AND 51-42-21-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA2022090399913Angle · corrodedPAX DOOR SILL ANGLE HAS AREAS OF CORROSION ON THE UNDERSIDE. : INSTALLED NEW SERVICEABLE PAX DOOR SILL ANGLE AND ATTACHMENT PARTS IAW CRJ700 SRM 51--42-06-001-001-A01 AND CRJ700 SRM 51-42-06--001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15 · DoorsSDR VNAA2022090399912Skin · damagedLEFT HAND SIDE EXTERNAL FUSELAGE AT APPROX FS360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR HAS LIGHT SCRATCHES VISIBLE. L/H SIDE EXTERNAL FUSELAGE AT APPROX. F.S360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR LIGHT SSep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA2022090399911Frame · corrodedFRAME CORRODED AT FS 969.00 BETWEEN STGR 25L AND 26R. REPAIRED CORROSION FRAME 969.00 STGR 25L - 26R IAW EA 22-C7-53-0968 REV IR DATED 08/09/2022. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IN ACCORDANCE WSep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039999Intercostal · corrodedAVI BAY DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO 26R. INSTALLED NEW INTERCOSTAL AT STGR 27 - 26R FWD ON AVI BAY DOOR IAW CRJ700 SRM 51--42-06-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039998Intercostal · corrodedL/H AVI DOOR INTERCOSTAL BETWEEN STGR 27 TO STGR 26L IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT LH AVI DOOR BETWEEN STGR 27 AND STGR 26L IAW CRJ700 SRM 51-42–06-001-001-A01 AND SRM 51-42-21-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039997Frame · corrodedFRAME AT F.S 319 IS CORRODED BETWEEN STR 23R TO STR 25L. FRAME @ F.S. 319 WAS REPAIRED AS REQUIRED IAW CRJ 700 SRM 53-00-06-201-- 006-A01.Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039996Frame · corrodedFRAME AT F.S 295.00 FOUND IS CORRODED. REPAIRED FS295 AS REQUIRED IAW CRJ700 SRM 53-00-06-201-006-A01. NO FURTHER DEFECT NOTEDSep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039995Frame · corroded"F.S 349 FRAME IS CORRODED BETWEEN STGR 25R TO 25L. FS 349 FRAME BETWEEN STR23L TOSTR22R WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039994Seat Track · corrodedLH SIDE SEAT RAIL STRUCTURE TRIM RETAINER AT FS 797.00 IS CORRODED. REPLACED SIDE SEAT TRACK AND NEW TRIM RETAINER IAW CRJ700 AMM 53-00-49-400-801-A03Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039993None · crackedWHILE PERFORMING LOWER WING PLANK SB 670BA-57-020C NDT FOUND 5EA HOLES TO HAVE INDICATIONSSep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039992Angle · crackedFOUND LIGHTENING DIVERTER SUPPORT CHANNEL BETWEEN FRAME STATION 333 AND 349 TO BE CRACKED. INSTALLED NEW CLIPS AND ANGLE IAW CRJ 700 SRM 51-42-13-001-001-A01.Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/StructuresSDR VNAA202209039991Intercostal · corrodedSERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 333 TO F.S. 349 AT STGR 20R. REPLACED CORRODED SERVICE DOOR INTERCOSTAL BETWEEN FS 333 TO FS 349 AT STGR 20R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21--001-001-A01.Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Electrical/Electronic Compartment DoorsSDR VNAA202206271112Fuel Sys · warning messageJUST AFTER T/O RAPID FUEL IMBALANCE WITH RH TANK WHILE LH TANK STAYED LEVEL PROBLEM FIXED ITSELF DURING DECENT / PERFORMED OPS TEST OF GRAVITY XFLOW SOV IAW CRJ 700 AMM 28-13-16-710-803-A01, OPS CHECK GOOD. PERFORMED OPS TEST OF FUEL QTY GAUGING COMPUTER IAW AJun 24, 2022 · N531EG · Cndair CL6002C10 · Fuel Quantity IndicatorSDR VNAA202206101111Adhesive · odorBURNING SMELL COMING FROM FWD CLOSET / T/S BURNING SMELL CHECKED CLOSET LT,GALLEY HEATER/FAN, PACKS,AVIONICS FANS,RECIRC FANS,APU AND WIFI IAW CRJ FIM 21-22-00-810-806-A01 FOUND NO DEFECTS FOR LISTED ITEMS SMELL STILL PRESENT SEE NEXT ITEM FOR FURTHER MX. CONTJun 8, 2022 · N531EG · Cndair CL6002C10 · Cabin Equipment/FurnishingsSDR VNAA202111301111Transmitter · unserviceableIN FLIGHT AT APPROX 8000FT, WE NOTICED RH OIL PRESS INDICATION OF ZERO, RAN QRC/QRH FOR NON MSG LOW OIL PRESSURE. OIL PRESSURE REMAINED AT ZERO, OIL TEMP INCREASING QRH DROVE US TO TO SHUT DOWN RH ENGINE; DID NOT RECEIVED THE RH ENG OIL PRESSURE WARNING MSG, ONov 30, 2021 · N531EG · Cndair CL6002C10 · Engine Oil Indicating SystemSDR 2021F00355Transmitter · unserviceableIN FLIGHT AT APPROX 8000FT, WE NOTICED RH OIL PRESS INDICATION OF ZERO, RAN QRC/QRH FOR NON MSG LOW OIL PRESSURE. OIL PRESSURE REMAINED AT ZERO, OIL TEMP INCREASING QRH DROVE US TO TO SHUT DOWN RH ENGINE; DID NOT RECEIVED THE RH ENG OIL PRESSURE WARNING MSG, ONov 26, 2021 · N531EG · Cndair CL6002C10 · Engine Integrated Instrument SystemSDR VNAA202110131111Keelbeam · corrodedDURING SCHEDULED MAINTENANCE AT THE GREENVILLE-SPARTANBURG INTERNATIONAL AIRPORT (GSP) FACILITIES IN GREER, SC, THE MAINTENANCE TEAM FOUND MULTIPLE AREAS OF CORROSION DAMAGE AS FOLLOWS: / CORROSION DAMAGE FOUND IN THREE (3) AREAS (Ï¿½AÏ¿½, Ï¿½BÏ¿½, AND Ï¿½CÏ¿½Oct 10, 2021 · N531EG · Cndair CL6002C10 · Fuselage Main, KeelSDR VNAA201911121102Connector · disconnectedMAINTENANCE FOUND FWD EMERGENCY EXIT SIGN AT THE PASSENGER WIND SCREEN INOP. RECONNECTED PLUG AND THE SIGN OPS CHECKED GOOD.Nov 10, 2019 · N531EG · Cndair CL6002C10 · Light System WiringSDR SIMA2019102304005Floorbeam · corrodedRH FLOOR CROSS BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE WHERE IT IS LAYERED BETWEEN DRIP TRAY AND THE UPPER L ANGLE OF BULKHEAD WALL.-C/A-REMOVED AND REPLACED RH CROSSBEAM 280.00 IAW SRM 51-42-06 AND 51-42-10.Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201910154004Floorbeam · crackedLH CENTER COCKPIT FLOOR BEAM BL 12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00 . COMPLETED INSTALLATION OF LH CENTER COCKPIT FLOOR BEAM AT BL12.00 / IAW SRM 53-11-43.Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201910140002Angle · crackedRH CENTER COCKPIT FLOORBEAM BL 12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00 -C/A-COMPLETED REPAIR AT RH CENTER COCKPIT FLOOR BEAM BL 12.00 LOCATED JUST FWD OF FLOOR BEAM FS280.00 IAW SRM 53-11-43.Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201910140003Floorbeam · corrodedLH FLOOR CROSS BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE WHERE IT IS LAYERED BETWEEN DRIP TRAY AND THE UPPER L ANGLE OF BULKHEAD WALL.-C/A-COMPLETED REPAIR OF THE LH FLOOR CROSSBEAM AT FS280.00 IAW SRM 51-42-06, 51-42-10 AND 53-11-41.Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201908198002Unknown · odorSMELL OF FUMES ON FLT DECK DURING FLIGHT, SMELLED LIKE POPCORN, FA 1 & FA 2 SMELLED STRONG SMELL BY THE EMERGENCY EXIT. SMELL LASTED 20 MIN THEN SUBSIDED BOTH PACKS ON & RECIR FAN, TURN FAN OFF SMELLED POPCORN BURNING REMAINED. UPON MTX ARRIVAL FOUND POPCORNAug 18, 2019 · N531EG · Cndair CL6002C10 · Air Distribution SystemSDR SIMA201906173006Flashlight · inoperativeFA FLASHLIGHT INOP-C/A-REPLACED FLASHLIGHT AS REQ OPC GOOD IAW CRJ-700 AMM 25-61-00Jun 13, 2019 · N531EG · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20190511002Flashlight · inoperativeSUPPLEMENTAL AFT FA FLASHLIGHT INOP. C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT MEL 2514 AUTH #050031 MOC #680993. REMOVED AND REPLACED AFT FA FLASHLIGHT AND CRADLE IAW AMM 25-61-02. OPC GOOD. MEL ITEM RESTORED.May 11, 2019 · N531EG · Cndair CL6002C10 · Emergency LightingSDR SIMA2019040329008Module · failedSEE ITEM 2 THIS LOG PAGE, STEERING INOP MSG FOR THE SECOND TIME WHILE TAXIING TO THE RUNWAY.-C/A-REMOVED AND REPLACED STEERING MANIFOLD OPC LK CK GOOD AMM 32-51-50Mar 29, 2019 · N531EG · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA2018121211003Compressor · contaminatedDURING CLIMB THROUGH APPROXIMATELY 9,000FT VMC AIRCRAFT CLEAN CONFIG NO ICING. M.W. FOR AFT LAV SMOKE ILLUMINATED. PAX AND CREW NOTICED ODOR. ALERT EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE OR SO. ODOR LIKENED TO BURNING EXHAUST. LDG WT UNDER 64,000 #'S.-C/A-NDec 11, 2018 · N531EG · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SIMA201810098004Warning System · activatedOB FLT SPLR & OB SPOILERONS CAUTION MESSAGE WHEN APPROACHING MCI EMERGENVY DECLARED. -C/A-INTERROGATED MDC R OB MFSPCU JAM MDC MESSAGE B1-007920 PERFORMED SPOST1 RESET PERFORMED OPS CK IAW ETN-CR-27-093 OPS CHEK GOOD FIRST OCCURANCE THIS AC.Oct 8, 2018 · N531EG · Cndair CL6002C10 · Drag Control SystemSDR SIMA20180716002Insert · defectiveL BLEED DUCT WARNING MESSAGE ON EICAS WHILE CLIMBING THROUGH 1500 FEET. R ENG BLEED ALSO CLOSED. NO BLEED SOURCE AVAILABLE-C/A-INTERROGATED MDC, FOUND CORRELATED CODE B1-349536. T/S PER FIM 36-21-01. LRU TEST INDICATES MT137 - 100%. REMOVED AND REPLACED CERAMIJul 16, 2018 · N531EG · Cndair CL6002C10 · Pneumatic Indicating SystemSDR SIMA201804040004Bulb · failedSMOKE COMING FROM WIRES IN THE LAVATORY SERVICE PANEL. ELECTRICAL SMOKE ODOR. WASTE SYSTEM CIRCUIT BREAKER TRIPPED. FOUND FLUID LEVEL LIGHT BULB BURNED OUT WHICH WAS THE CAUSE OF THE SMOKE IN THE AREA. RESET THE CIRCUIT BREAKER CB2-M9. REMOVED AND REPLACEMar 22, 2018 · N531EG · Cndair CL6002C10 · Water/Waste System WiringSDR SIMA20180302003Slat System · malfunctionedSLATS FAIL CAUTION ON APPROACH. INTERROGATED MDC, FOUND SLAT ACTUATOR SYSTEM, MECHANICAL BINDING MESSAGE B1-007772. PERFORMED ETN-CR-27-084. FOUND THE RTWING NR 2 AND 3 ACTUATORS TRIPPED. PERFORMED OPS TEST OF SLAT SYSTEM IAW AMM 27-50-00. OPS CHECK FAILEMar 2, 2018 · N531EG · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR SIMA20170418004Web · crackedLEFT FORWARD EQUIPMENT BAY FLOOR WEB HAS A 1/8" CRACK. COMPLETED A REPAIR TO LT FWD EQUIPMENT COMPARTMENT FLOOR IAW ETN-CR-53-099.Apr 18, 2017 · N531EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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