N568NN
Service difficulty reports · 43
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 = 'N568NN' 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 = 'N568NN' 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 VNAA2025112411102Light · sparksCA SIDE READING LIGHT SPARKED AND SMOKED. / REMOVED AND REPLACED CA SIDE MAP READING LIGHT IAW AMM 33-13-03-000/400-801. OPS TEST GOOD.SDR VNAA2025091111101Fmu · faultedL FADEC MSG IN FLIGHT. / REMOVED AND REPLACED R FADEC IAW AMM 73-21-01-000/400-801. REMOVED AND REPLACED LH ENGINE FMU IAW CRJ 900 AMM 73-21-03-000/400-801.OPS CHECK AND LEAK CHECK GOOD. PERFORMED HIGH POWER RUN IAW CRJ 900 AMM 71-00-00-866-806-A02-PSA. ALL PSDR VNAA2024071511101Actuator · unserviceableFLAPS FAIL ON FINAL. FLAPS STUCK AT 45 / PERFORMED ELECTRICAL RIGGING OF RH FLAP IAW CRJ 900 AMM 27-52-00-820-802, RIGGING OUT OF TOLERANCES AND ADJUSTED. ON OPS CHECK OF FLAPS NOTED SQUEALING NOISE FROM FLAP PDU AND TORQUE TUBES ATTEMPTING TO GO FURTHER THAN SDR VNAA202404170002Skin · gougedFWD CARGO DOOR HAS GOUGES AT THE DOOR SKIN EDGE COMMON TO THE LOWER FORWARD AND AFT CORNERS WITHIN SRM REPAIR LIMITS.SDR VNAA202404170001Fitting · gougedGOUGE DAMAGE TO LH WING TRAILING EDGE MACHINED FITTINGS AT WS199.40, WS202.67 AND WS231.23) CAUSED BY INCORRECT HARDWARE ORIENTATION. DAMAGE CLASSIFIED AND REPAIRED IAW MHIRJ REO 690-57-51-332 REV --.SDR VNAA202404160014Skin · gougedNUMEROUS NICKS, GOUGES AND DENTS ON FUSELAGE SKIN BETWEEN FS1031.00 - FS1051.30 AND STR22R - STR25R. DAMAGE CAUSED BY LP PNEUMATIC DUCT PLUG TETHERED BY LANYARD COMING LOOSE IN FLIGHT AND IMPACTING AGAINST THE FUSELAGE REPEATEDLY. CLASSIFIED AND REPAIRED IAW SDR VNAA202404160012Shelf · crackedSHELF THAT SECURES JB-6 HAS A CRACK IN THE FORWARD RH OUTBOARD CORNER APPROX. 1/4 INCH IN LENGTHSDR VNAA202404160008Skin Panel · burnedLIGHTNING STRIKE DAMAGE (SMALL HOLE IN SKIN PANEL) AT APPROXIMATELY FS 440.0 AND STGR 3R, CLASSIFIED IN MHIRJ REO 690-53-21-1744SDR VNAA202404160007Skin · scratchedSCRATCH IN FUSELAGE SKIN AT APPROXIMATELY FS 310.0 AND STGR 25L. DAMAGE WITHIN SRM ALLOWABLE LIMITS PER 53-21-01-101-002-A04SDR VNAA202404160005Seat Track · corrodedFWD CABIN RH I/B SEAT TRACK P/N SH690-33407-1 HAS CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0SDR VNAA202404160004Seat Track · corrodedFWD CABIN RH I/B SEAT TRACK P/N BA690-31111-1 AND HAS CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0SDR VNAA202404160003Seat Track · corrodedFWD CABIN RH I/B SEAT TRACKS P/N SH670-32159-1, BA690-31111-1 AND SH690-33407-1 HAVE CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0SDR VNAA202404170004Bearing · wornRUDDER FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 1 & 2 PER CRJ 900 AMM TASK 27-21-00-720-803. MAXIMUM ALLOWABLE BACKLASH ON HYDRAULIC SYSTEM 1 IS 0.250". HIGHEST TESTED VALUE WAS 0.395". MAX ALLOWABLE BEARING BACKLASH VALUE IS 0.120", MEASURED VALUE WAS 0.132"SDR VNAA202404170003Bearing · wornRUDDER FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 1 & 2 PER CRJ 900 AMM TASK 27-21-00-720-803. MAXIMUM ALLOWABLE BACKLASH ON HYDRAULIC SYSTEM 1 IS 0.250". HIGHEST TESTED VALUE WAS 0.395". MAX ALLOWABLE BEARING BACKLASH VALUE IS 0.120", MEASURED VALUE WAS 0.132"SDR VNAA202404160010Cowling · dentedRH NACELLE, I/B SIDE, FAN COWL PANEL (442AB), TOP EDGE OF PANEL DAMAGED (2 DENTS) APPROX. 12" FROM AFT END OF PANEL. DAMAGE CLASSIFIED IN PSA AIRLINES EA A1-690-54-00024 REV A.SDR VNAA202404160009Fairing · unserviceableRH ENGINE, FWD FAN COWL HINGE LINE FAIRING DAMAGED/BENT BEYOND REPAIR LIMITS. (PANEL 442BB)SDR VNAA202404160011Bracket · crackedSERVICE DOOR STABILIZATION BRACKET (P/N CC670-38380-3), CRACKED (UPPER STABILIZER BAR MOUNT AT ROD ATTACH POINT)SDR VNAA202404170006Bearing · wornLH ELEVATOR FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 3 PER CRJ900 AMM CH. 27-31-00-720-804. MAXIMUM ALLOWABLE BACKLASH IS 0.070", MEASURED VALUE WAS .090". SPHERICAL BALL P3A3211, AND BUSHING B0309008-08-055 AT LH ELEVATOR, PCU #3 WORN BEYOND LIMITS.SDR VNAA202404170005Bushing · wornLH ELEVATOR FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 3 PER CRJ900 AMM CH. 27-31-00-720-804. MAXIMUM ALLOWABLE BACKLASH IS 0.070", MEASURED VALUE WAS .090". SPHERICAL BALL P3A3211, AND BUSHING B0309008-08-055 AT LH ELEVATOR, PCU #3 WORN BEYOND LIMITS.SDR VNAA202404160006Drain · corrodedRH FWD GALLEY SERVICE DOOR AFT DRAIN TUBE ASSEMBLY CORRODED THROUGH.SDR VNAA202404160013Channel · crackedWING/FUSELAGE FAIRING, RH (PANEL 196DR) SUPPORT CHANNEL HAS A 1.33" CRACK, 7.4" FROM FWD END OF CHANNEL. PN:BA690-39311-1.SDR VNAA202404160002Mount Fitting · corrodedG1 GALLEY HAS 2 CORRODED FLOOR FITTING MOUNTS. FWD OUTBD AND AFT INBD LOCATIONS.SDR VNAA202404160001Mount Fitting · unserviceableFWD LAVATORY FWD OUTBOARD FLOOR MOUNT EXFOLIATING CORROSION THROUGH MOUNT.SDR VNAA2023113011102Unknown · unknownDIRTY SOCK SMELL COMING THRU VENTILATION SYSTEM / PERFORMED POST WASH BLEED DRY OUT PROCEDURE ON L & R BLEEDS IAW CRJ-900 AMM 72-00-00-100-803-A01-PSA STEPS H(6) THROUGH SHUTDOWN. NO ABNORMAL ODORS NOTED AFTER EXTENDED VERIFICATION STEP.SDR VNAA202204211111Pressure Valve · departedTHE LOW PRESSURE DOOR WAS LEFT OPEN DEPARTING CLT AND THE LOW PRESSURE VALVE DOOR CAME OFF SOMEWHERE BETWEEN CLT AIRPORT AND JAN AIRPORT. CLT OPS HAS BEEN NOTIFIED OF THE MISSING VALVE COVER AND AIRCRAFT DAMAGE AS WELL. A DENT NEXT TO THE LOW PRESSURE VALVE DOSDR VNAA2020090311101Fan · failedRECIRC FAN FAULT STATUS MESSAGE FOLLOWED BY BURNING RUBBER SMELL. TROUBLE SHOT RECIRC FAN FAULT STATUS MESSAGE "RECIRC FAN 2, FAILED WIRING/LOW FAN SPEED" IAW CRJ 900 FIM 21-22-10-810-802-A02. REMOVED AND REPLACED RT RECIRC FAN IAW CRJ 900 AMM 21-22-10-000/4SDR VNAA202006089998Intercostal · corrodedINTERCOSTALS CORRDED.SDR VNAA202006089997Seat Track · corrodedFLOOR SEAT TRACK CORRODED AT RBL 9.00 BETWEEN FS 485 AND FS 533.00.SDR VNAA202006089996Floorbeam · corrodedFS 280 CROSSBEAM FWD FLOOR SUPPORT ANGLE BETWEEN LBL 12 AND RBL 12 IS CORRODED.SDR VNAA202006089995Seat Track · corrodedFLOOR SEAT TRACK CORRODED AT LBL 27.00 AND BETWEEN FS 364 TO FS 485.00.SDR VNAA202006089994Seat Track · corrodedFLOOR SEAT TRACK AT LBL 9.00 AND BETWEEN FS 374.00 TO FS 483 CORRODED IN SEVERAL LOCATIONS. SEAT TRACK REPLACED.SDR VNAA202006089993Seat Track · corrodedFLOOR SEAT TRACK CORRODED AT RBL 9.00 AND BETWEEN FS 364 TO FS 483.00. REPLACED SEAT TRACK.SDR VNAA202006089992Floor Support · corrodedINTERCOSTALS BELOW FLOOR AT PAX DOOR FROM FS 310.00 TO FS 349.00 ARE CORRODED. REPLACED INTERCOSTALS.SDR VNAA202006089991Intercostal · corrodedL/H AND R/H INTERCOSTALS AT STGR 27 BETWEEN FS 349 AND FS 364 ARE CORRODED. REPLACED INTERCOSTALS.SDR VNAA2019101411101Acm · failedSMOKE IN CABIN. C/W GVI OF AFT EQUIPMENT BAY IAW CRJ 900 AMM 53-60-01-PSA. NO VISUAL DEFECTS NOTED. T/S PER CRJ 900 FIM 21-22-00-810-806 AND FOUND ISSUE TO BE WITH THE RH PACK. MAINTENANCE REMOVED AND REPLACED R/H AIR CYCLE MACHINE OPS CHECK GOOD AT THIS TIMESDR VNAA2019071011103Proximity Sensor · out of adjustIN PREPARATION TO LAND THE CREW RECEIVED A ANTI SKID CAUTION MESSAGE WITH A WOW MESSAGE. THE CREW RAN THE QRH AND WAS NOT ABLE TO RESET THE SYSTEM. THEY DECLARED AN EMERGENCY AND GROUND EMERGENCY EQUIPMENT RESPONDED. THE AIRCRAFT LANDED WITHOUT ISSUE AND WASSDR VNAA2018090711101Warning System · false activationAIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT AND HAD SERVICE DOOR CAUTION LIGHT, THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE / MASKS DID NOT DROP, BUT EQUIPMENT DID ROLL. THE AIRCRAFT TAXIED INTO THE GATE UNDER ITS OWN POWER. MX INSPECTED A/C ANDSDR VNAA2018031111101Unknown · odorAFTER PUSHING OFF THE GATE FAS REPORTED AN ODOR IN THE CABIN, LIKE A BURNING MATCH. RETURNED TO THE GATE. MAINTENANCE INSPECTED. FOUND NO EVIDENCE OF SOURCE OF BURNING ODOR. RAN ENGINES, NO ODOR NOTED.SDR VNAA2017030100002Lens · missingSERVICE DOOR EXIT SIGN LENS IS MISSING. INSTALLED A REPLACEMENT LENS.SDR VNAA2016081200011Cover · missingGALLEY FLOOR EMERGENCY LIGHT COVER MISSING. MAINTENANCE INSTALLED LENS COVER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA2016070500009Circuit Breaker · poppedEMERGENCY LIGHTS ON WITH SWITCH IN ARM POSITION. CREW RESET CIRCUIT BREAKER CBP-2 U3 AND THE ACFT CONTINUED SERVICE.SDR VNAA2015102300021Fan · odorSHORTLY AFTER TAKEOFF, CREW REPORTED SMOKE ODOR WHICH PROGRESSIVELY GOT WORSE DURING CLIMBOUT TO 1,000 FT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. TROUBLESHOT, AND FOUND ODOR COMING FROM FORWARD GALLEY EXHAUST FAN.SDR VNAA2015071400014Probe · failedCREW REPORTED BRAKE OVERHEAT MESSAGE IN CRUISE AND ON APPROACH. INNER LT BRAKE TEMPERATURE MONITORING SYS, BTMS, INDICATOR WENT TO 20 BOTH TIMES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 2 MLG BRAKE TEMPERATURE PROBE AND PERFORMED CHECK
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