N583NN
Service difficulty reports · 38
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 = 'N583NN' 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 = 'N583NN' 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 VNAA2026031014206Actuator · faultedCAUTION RUDDER LIMITER MSG IN FLIGHT. / REMOVED THE (LH) RTLA 1 FROM STEPS 4A (5) THROUGH COMPLETION AND REPLACED LH RTLA 1 IAW CRJ900 AMM 27-25-03-000/400-801-A04. ALL OPS CHECKED GOOD.SDR VNAA2025042811102Fuel Cap · unsecureRIGHT HAND OVERWING FUELING CAP CAME OPEN IN FLIGHT / INSPECTED RH WING GRAVITY FUEL FILLER CAP IAW CRJ900 AMM 28-11-16-210-801 NO DAMAGE NOTED. INSPECTED RH WING SKIN AROUND FILLER CAP RECEPTICLE NO DAMAGE NOTED. SUMPED RH WING TANK IAW CRJ900 AMM 12-11-28-75SDR VNAA2025021911102Wire Harness · damagedL WING A/I CAUTION MSG. DURING CLIMB OUT OF CLT. / REMOVED AND REPLACED LH OUTBOARD TELESCOPIC HARNESS IAW CRJ 900 AMM 30-11-10-000/400-802. OPS CHECK GOOD. NO FURTHER FAULTS FOUND AT THIS TIME.SDR VNAA2025011311103Spoiler Sys · abnormalOB SPOILERONS AND OB FLT SPOILERS CAUTION MSG IN FLIGHT. / C/W SYSTEM RESET 5.1.18 PER MIPM AND PERFORMED OPERATIONAL TEST OF THE MFS IAW 900 AMM 27ˆ’62ˆ’01ˆ’710ˆ’801SDR VNAA202407020003Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER (REO) 670-53-11-509 REV-E.SDR VNAA202407030008Floor Support · corrodedCORROSION ON RH SILL AND DRAIN DISBONDED ON SILL BTW FS 280.00 TO FS295. RH SILL WAS REPAIRED AND DRAIN WAS BONDED ON SILL BTW FS 280.00 TO FS295.00 PER CRJ/900 SRM 53-21-43-201-002-A01SDR VNAA202407030006Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1770 REV -.SDR VNAA202407030010Strut · corrodedAFTER REMOVAL OF MLG PISTON AXLE//CORROSION AT LH MLG CYLINDER THREADS. THE MLG OUTER CYLINDER GLAND NUT THREADS WERE REPAIRED PER REO670-32-11-221 REV.G.SDR VNAA202407020013Floorbeam · corrodedCORROSION ON FS280 FLOOR PANEL SUPPORT ANGLE. CORROSION ON FS280 FLOOR PANEL SUPPORT ANGLE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED IS OUT LIMITS THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-0SDR VNAA202407020012Bracket · corrodedCORROSION ON MACHINED BRACKETS (6 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. DUE TO NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE, BRACKET MACHINED (6 EAS) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT WERE REPLACED PER SRM 53-32-58-101-0SDR VNAA202407030003Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS AT RBL 9.00 FROM FS 349.00 TO FS473.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN. DUE TO EXCESIVE DAMAGE SEAT RAILS AT RBL 9.00 FROM FS 349.00 TO FS473.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRMSDR VNAA202407030012Lug · corrodedAFTER BUSHING REMOVAL IN REF CARDTRFKE00BN3Q8:271500-RH-PSA, SCRATCHES ON LUG R5, LUG R6 ON AILERON RH. SCRATCHES ON LUG R5, LUG R6 ON AILERON RH WERE REPAIRED PER REO 670-57-61-237 REV - -SDR VNAA202407030011Lug · corrodedAFTER BUSHING REMOVAL IN REF CARD TRFKE00BN30R:271500-LH-PSA, WEAR ON LUG L2, LUG L5 ON AILERON LH. CORROSION AND WEAR ON LUG L2, LUG L5 ON AILERON LH WERE REPAIRED PER REO 670-57-61-237 REV - - & REO 690-57-61-327 REV. - -SDR VNAA202407030009Floorbeam · crackedCRACK ON FLOORBEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR SDR VNAA202407030007Hinge · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.SDR VNAA202407030005Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS AT LBL 27.00 FROM FS 349.00 TO FS 581.00 AT PASSENGER CABIN. FLOOR SEAT RAILS AT LBL 27.00 FROM FS 349.00 TO FS 581.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND SRM 53-21-49-101-001-ASDR VNAA202407030002Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFISDR VNAA202407030001Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND WERE REPLACED PERSDR VNAA202407020015Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA202407020011Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATSDR VNAA202407020010Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM SDR VNAA202407020009Seat Track · corrodedCORROSION ON LEFT SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). LEFT SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WESDR VNAA202407020008Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-355 REV.--SDR VNAA202407020007Support · crackedCRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-020 REV.--SDR VNAA202407020006Seal · wornSTRIKER SEAL OF CENTER CARGO DOOR CUT OUT FWD FRAME WITHIN 3525.55 FH (BEFORE 19,015.45 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. STRIKER SEAL OF CENTER CARGO DOOR CUT OUT FWD FRAME WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A0SDR VNAA202407020005Fireshield · wornRIGHT FWD CORE COWL FIRE SHIELD ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. R/H FWD CORE COWL FIRE SHIELD WAS REPAIRED PER REO N° 690-54-23-382 REV.--SDR VNAA202407020014Skin · corrodedCORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 25 LH. CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 26 LH WAS REPAIRED PER REO 690-53-21-1782 REV -- AND BAY BTW STGR 25LH TO STGR 26LH WAS CLEANED PER CRJ900 SRM SDR VNAA202407020002Skin · wornWEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-476 REV.SDR VNAA202407020001Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-475 REV.--SDR VNAA202407020004Skin · nickedPERM REPAIR BEFORE 19,159.54 FH - DISPOSITION FOR TRIMMED NICK DAMAGE ON SLAT TRAILING EDGE BETWEEN SS341.66 - TRACK2-3, LHS THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 800 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV-. SLAT TRAILING EDSDR VNAA202407030004Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS AT LBL 9.00 FROM FS 374.00 TO FS485.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN. FLOOR SEAT RAILS AT LBL 9.00 FROM FS 374.00 TO FS485.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN WERE REPLACED PER CRJ900 AMM 53-00-49.SDR VNAA202307011111Pin · unserviceable""HIGH VIBE FAN IN FLIGHT LH ENGINE / REMOVED AND REPLACED ALL FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000-801, 72-21-02-400-801-A01-PSA. PREFORMED ENGINE VIBRATION CHECK IAW CRJ 900 AMM 71-00-00-720-806. N1 91.5 VIBE .3 / VIBRATION CHECK GOOD AT THIS TIMESDR VNAA202202161111None · unserviceableLH ENG VIBE OUT OF LIMITS ON CLIMBOUT AT LEVEL OFF WE WERE UNABLE TO KEEP VIBE IN LIMITS, VIBE INCREASED WHEN POWER REDUCED, SHUT DOWN L ENGINE / REMOVED AND REPLACED LH ENGINE FAN BLADE RETAINING PINS IAW CRJ900 AMM 72-21-02-000/400-801. PERFORMED VIBE CHECK SDR VNAA2020102311101Battery Pack · dischargedEMERGENCY LIGHT AFT OF WING INOPERABLE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, IAW CRJ 900 AMM 33-51-17-000/400-801. OPERATIONS CHECK.SDR VNAA2020082011102Window · crackedFO SIDE WINDOW CRACKED. WHILE IN CRUISE, THE FO SIDE WINDOW SHOWED SIGNS OF CRACKING. AN EMERGENCY WAS DECLARED AND THE FLIGHT DESCENDED TO A LOWER ALTITUDE. FLIGHT CONTINUED ON AND LANDED IN PHL SAFELY. TRUCKS WERE ROLLED AS A PRECAUTION BUT WERE CALLED OFF WSDR VNAA2019102401101Acm · failedR PACK AUTO FAIL DUE TO HIGH OUTPUT TEMP. SMELL PRESENT IN CABIN. DEFERRED WITH CREW. MX GAINED ACCESS TO THE AIR CYCLE MACHINES TURBINES TO CONFIRM THAT THEY ARE SEIZED AND CAN'T TURN. MX REPLACED RH AIR CYCLE MACHINE. OPS CHECK GOOD.SDR VNAA2019091311101Bonding Jumper · brokenDURING APPROACH TO LAND FLIGHT SPOILERS AND SPOILERONS MESSAGE CAME ON. THE CREW FOLLOWED THE QRH AND DECLARED AND EMERGENCY FOR LANDING. NO EMERGENCY EQUIPMENT RESPONDED. FLIGHT LANDED WITHOUT ISSUE AND TAXIED TO THE GATE. MX INSPECTED AIRCRAFT FOUND ELECTRICSDR VNAA2016042500024Sensor · damagedBIRD STRIKE LT L/E OTBD FOLLOWED BY FLAPS HALFSPEED AND SLAT STATUS MESSAGES. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LT OTBD SLAT DISCONNECT SENSOR, AND DEFERED THE FLAP SUB SYS IAW MEL. MAINTENANCE CL
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