N586NN
Service difficulty reports · 47
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 = 'N586NN' 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 = 'N586NN' 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 VNAA2025050911101Control Unit · faultedFLAP FAIL CAUTION MSG ON TAKE OFF. / REMOVED AND REPLACED SFECU 1 IAW AMM 27-51-05€“000/400-801-A01. PERFORMED OPS TEST OF THE FLAPS/SLATS SYS IAW AMM 27-50-00-710-801-A02 AND SELF-TEST OF THE SFECU IAW AMM 27-51-05-740-801-A01. OPS TEST AND SELF TEST GOOD ATSDR VNAA202411240002Skin · damagedREO 690-53-21-1683-2750FH PERM REPAIR - TEMPORARY DISPOSITION FOR DAMAGED HOLES ON FUSELAGE STRUCTURE FOR LAVATORY WASTE DOOR HINGE AT FS379.00 BTWN STR21R - STR22R PERFORM A PERMANENT REPAIR IAW APPROVED PROCEDURES 2750FH. PERMANENT REPAIR ON DAMAGED HOLES OSDR VNAA202411240031Seat Track · corrodedCORROSION ON BULKHEAD SIDE POST AT LBL 9.00. CORROSION ON BULKHEAD SIDE POST AT LBL 9.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01SDR VNAA202411240030Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (2 EA). EVALUATED,SEAT RAILS OF LBL9 BTW FS693.00 TO FS977.00. (2 EA),THEREFORE IS OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM53-51-49-101-001-A02 AND SEAT RSDR VNAA202411240028Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (4EAS) LOCATED ON FS310.00 LBL 19, FS317.00 RBL 3, FS295.00 RBL 3 AND BTW FS280.00 TO FS295.00 RBL 16 AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (4EAS) LOCATED ON FS310.00 LBL 19, FS317.00 RBL 3, FS295.00 RBL 3 AND BTW FS280.00 TOSDR VNAA202411240027Angle · corrodedCORROSION ON ANGLE BTW FS 1015 AND SGTR-20LH AT AFT CARGO COMPARTMENT. CORROSION ON ANGLE BTW FS 1015 AND SGTR-20LH AT AFT CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CSDR VNAA202411240026Hinge Fitting · excess playAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.B.SDR VNAA202411240019Intercostal · corrodedCORROSION ON RH/LH INTERCOSTALS (2 EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. RH/LH INTERCOSTALS (2 EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-SDR VNAA202411240014Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 RSDR VNAA202411240001Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. REPAIRED PER REO 690-53-11-1876 RESDR VNAA202411240029Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ/900 AMM 53-00-49SDR VNAA202411240025Plate · corrodedIN REF TO: DURING INSPECTION OF THE TASK CARD 53-20-333-JIC IT WAS DETECTED CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CASDR VNAA202411240024Door Sill · corrodedCORROSION ON DOOR SILL BTW FS519.64 TO FS562.36 AT SURROUND STRUCTURE FWD CARGO DOOR. DOOR SILL BTW FS519.64 TO FS562.36 AT SURROUND STRUCTURE FWD CARGO DOOR WAS REPAIRED PER REO 690-53-31-885 REV--SDR VNAA202411240023Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL27 BTW FS 477.40 TO FS 693.00 (1 EA). SEAT RAIL OF LBL27 BTW FS 477.40 TO FS 693.00 (1 EA) IS OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202411240022Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS 477.40 TO FS 693.00 (4 EAS). SEAT RAILS OF LBL9 BTW FS 477.40 TO FS 693.00 (4 EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02. PER CONFIGURATION, NEW SEAT RAILS OSDR VNAA202411240021Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS 477.40 TO FS 693.00 (4 EAS). SEAT RAILS OF RBL9 BTW FS 477.40 TO FS 693.00 (4 EAS) ARE OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONSDR VNAA202411240020Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=349.00 TO FS=477.40 LBL 9 (1EA) / RBL 9(1 EA). FLOOR SEAT RAILS BTW FS=349.00 TO FS=477.40 LBL 9 (1EA) / RBL 9(1 EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 AND SDR VNAA202411240018Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE WAS FOUND OUT OF LIMITS PER CRJ 900 SRM 53-21-43-101-001-A03 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SDR VNAA202411240017Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 (7EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 AT PASSENGER COMPARTMENT. SIDE SEAT RAIL STGR 15 (7EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 AT PASSENGER COMPARTMENT ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101SDR VNAA202411240016Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 (4EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL STGR 15 (4EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40 ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFORE WESDR VNAA202411240015Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-SDR VNAA202411240013Nozzle · dentedDENTS ON NOZZLE ASSY EXHAUST AT LH ENGINE DENTS ON NOZZLE ASSY EXHAUST AT LH ENGINE WERE REPAIRED PER REO 690-54-15-003 REV. - - .SDR VNAA202411240007Cap · corrodedCORROSION ON SILL, MID CAP AND KICK PLATE AT PASSENGER DOOR. CORROSION ON MID CAP AND KICK PLATE AT PASSENGER DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. KICK PLATE WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-001- A02. MID CAP WAS EVALUSDR VNAA202411240012Inlet · dentedDENTS (5 EAS) ON LOWER LH ENGINE NOSE INLET COWL BTW 5/7 O´CLOCK POSITION. DENTS (5 EAS) ON LOWER LH ENGINE NOSE INLET COWL BTW 5/7 O´CLOCK POSITION WERE REPAIRED PER REO 690-54-11-528 REV. - - AND PER REO 670-51-00-085 REV. -A.SDR VNAA202411240011Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.SDR VNAA202411240010Web · crackedCRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ/900 SRM 53-11-43-201-001-A01SDR VNAA202411240009Hinge · corrodedCORROSION ON UPPER HINGE AT ACCESS PANEL 832ET. CORROSION ON UPPER HINGE AT ACCESS PANEL 832ET WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-00-01-101-001-A01 AND REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR VNAA202411240008Panel · corrodedCORROSION ON ACCESS PANEL 832FT AND 832DT. CORROSION ON ACCESS 832DT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 52-11-04-101- 001-A01. ACCESS PANEL 832FT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-11-04-101SDR VNAA202411240006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-495 REV.--SDR VNAA202411240005Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-494 REV.--SDR VNAA202411240004Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACESDR VNAA202411240003Drag Angle · crackedINITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TOSDR VNAA2024100711102Warning System · false indicationDUCTMON FAULT STATUS MSG, A/I ICE DUCT CAUTION MSG, A/I DUCT WARNING MSG, RH WING A/I CAUTION MSG, LH WING A/I CAUTION MSG IN CRUISE FLIGHT EMERGECY DECLARE TO EXIT ICING / PERFORMED BITE TEST OF THE AILC IAW CRJ 900 AMM 30-12-12-740-801-A01. NO FAULTS FOUND SDR VNAA202202151111Windshield · smokeFO WINDSHIELD LOWER HEAT BLOCK BEGAN PRODUCING SMOKE IN FLIGHT. NO FIRE. SMOKE SUBSIDED AFTER ABOUT 10 SECONDS AFTER TURNING OFF WINDHIELD HEAT / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-PSA. OPS CHECK AND LEAK CHECK REQUIRED. PESDR VNAA202108031112Acm · unserviceableWHILE ON APPROACH INTO SDF. CREW START NOTICING SMOKE IN THE COCKPIT WHICH STARTED TO GET HEAVY, STARTED BURNING THEIR EYES AND THROAT. THEY THEN GOT A CHIME FROM THE THE CABIN TELLING THEM THAT THEY WERE GETTING THE SMOKE IN THE CABIN. THEY DECLARED AN EMERGESDR VNAA202107289991Rib · crackedLH LEADING EDGE MACHINED RIB AT SS 57.16 0.50" CRACK ON UPPER FLANGESDR VNAA202106309996Seat Track · corrodedSEAT RAIL AT RBL 9 CORRODED BEYOND LIMITSSDR VNAA2020092011101Proximity Sensor · out of adjustGEAR DISAGREE MESSAGE IN FLIGHT WHEN GEAR UP SELECTED. CREW DECLARED EMERGENCY AND DIVERTED TO CAK. INTERROGATED MDC AND FOUND MULTIPLE FAULTS FLAGGING NLG PROXIMITY SENSOR PX22. FOUND PX22 TO BE READING "DEGRADED FAR" IN MDC WITH GEAR UP WHEN IT WAS SUPPOSSDR VNAA2020081411101Acm · failedSTRONG ELEC SMELL IN CABIN. PERFORMED OPS TEST OF AIR COND. SYST. LH PACK CHECK BAD AND OPS CHECK PASS LIGHTS GOOD. REMOVED AND REPLACED LH ACM IAW CRJ900 AMM. ALSO REMOVED AND REPLACED LH WATER EXTRACTOR DUCT. LH PACK OPS CHECKS GOOD AT THIS TIME NO ELECTRICASDR VNAA2020072311101Controller · faultedCREW NOTICED SMALL CRACK IN WINDSHIELD THAT KEPT GROWING AS THEY APPROACHED STL AREA. DECIDED TO DECLARE EMERGENCY AND DIVERT TO EVV. FLIGHT LANDED SAFELY AND WITH NO FURTHER ISSUES. MX REMOVED AND REPLACED CAPTIANS WINDSHIELD AND WINDSHIELD TEMP CONTROLLER.SDR VNAA2019091511102Warning System · false activationON ARRIVAL AT FL160, WHEN FLAPS WERE SELECTED, RECEIVED SPOILERONS AND FLIGHT SPOILERS CAUTION MSG. CREW PUT FLAPS BACK TO 0 AND RAN QRH. DECLARED EMERGENCY AS A PRECAUTION. CABIN DID NOT BRACE. TRUCKS DID ROLL. / FLIGHT LANDED WITH OUT INCIDENT AND WAS ABLSDR VNAA2019031311101Selector Valve · failedLANDING GEAR FAILED TO EXTEND SO THE CREW EXTENDED MANUALLY. THEY DECLARED AND EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. TRUCKS WERE ROLLED BUT THE CABIN WAS NOT BRACED. SUPLEMENTAL INFORMATION MX R&R MLG SELECTOR VALVE. OPS CHECK GOODSDR VNAA20181212111Warning System · false activationTHE CREW REPORTED A NOSE WHEEL STEERING INOP 'C' MSG IN FLIGHT AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT ISSUE AND THE SYSTEM WAS RESET, OPS CHECK GOOD.SDR VNAA2017092711101Warning System · activatedFLIGHT 5564 (AVP-CLT) DECLARED EMERGENCY ON DESCENT INTO CLT FOR RUNWAY 36C. CREW HAD AN INBOARD SPOILER MESSAGE AND OUTBOARD SPOILERON MESSAGE ON APPROACH. CREW FOLLOWED QRH AND CONTINUED INTO CLT AFTER DECLARING EMERGENCY AS PRECAUTION. CREW DID NOT REQUISDR VNAA2017080211101Manifold · defectiveON CLIMBOUT THE CREW RECEIVED A NOSE WHEEL STEERING CAUTION MESSAGE. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND DECLARED EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE STEERING MANIFOLD AND THE ROD END FOSDR VNAA2017073011102Warning Message · false activationAFTER TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING CAUTION MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTINUED TO THEIR DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED MULTIPLE GEAR SWINGS AND OPERATIONAL CHECKED GOOD.SDR VNAA2017073011101Steering Sys · malfunctionedAIRCRAFT EXPERIENCED A NOSE WHEEL STEERING INOPERATIVE MESSAGE. THE CREW CONTINUED TO DESTINATION AND THE TOWER DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. ONCE STOPPED, MAINTENANCE CONTROL WAS ABLE TO RESET THE NOSE WHEEL STEERING WITH THE CR
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