N589NN
Service difficulty reports · 62
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 = 'N589NN' 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 = 'N589NN' 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 VNAA2026061619002Diode · faultedDC EMERGENCY BUSS CAUTION MSG IN FLIGHT. REMOVED AND REPLACED EMERGENCY BUSS DIODE (CR82) IAW AMM 24-61-01-000-400-801-A01. OPS CHECKED GOOD.SDR VNAA2025072211101Actuator · failedFLAPS FAIL ON TAKE OFF. COMPLETED INSTALL OF LH #3 FLAP ACTUATOR IAW CRJ 900 AMM 27-52-09-400-803 AND LH #4 FLAP ACTUATOR IAW AMM 27-52-09-400-804. OPS CHECK GOOD.SDR VNAA2025070911101Actuator · trippedRTF-FLAPS FAIL CAUTION MSG ON TAKE OFF. / FOUND B1 CODE 006551. CLEARED INHIBITS AND SELF TEST FOR SFECU PASSED IAW CRJ 900 AMM 45-45-00-970-821. FOUND LH OB INB FLAP ACTUATOR TRIPPED. RESET THE TRIPPED ACTUATOR IAW CRJ 900 AMM 27-52-09-610-802. PERFORMED OPS SDR VNAA2025022811103Flap System · malfunctionedON APPROACH TO GPT, PILOTS MOVED THE FLAP LEVER TO 8 AND GOT A STICK SHAKER FOLLOWED BY A STICK PUSHER. PILOTS WERE ABLE TO MANUALLY PULL THE NOSE UP FROM A DIVE DOWN SCENARIO. PILOTS DISCONNECTED THE STICK PUSHER SWITCHES AND BEGAN TO CLIMB PERFORMING A GO ARSDR VNAA202410210034Drip Tray · corrodedCORROSION ON RH TRAY DRIP ASSY. RH TRAY DRIP ASSY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01.SDR VNAA202410210033Lug · corrodedCORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WAS FOUND. CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV-.SDR VNAA202410210032Lug · corroded"DESCRIPTION: CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WAS FOUND. HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--"SDR VNAA202410210031Skin · dented" SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH.WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-580 REV."SDR VNAA202410210030Skin · dented"SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-579 REV."SDR VNAA202410210029Floor Support · cracked"CRACK ON FLOOR SUPPORT RBL12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE, FLOOR SUPPORT RBL 12 TBW FS221.73 TO FS229 FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-1855 REV."SDR VNAA202410210028Seat Track · corrodedCORROSION ON SEAT RAILS FROM STA 847 TO 977 AND LBL9. SEAT RAILS FROM STA 847 TO 977 AND LBL9 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONF (A12)"SDR VNAA202410210027Seat Track · corrodedCORROSION ON SEAT RAILS FROM STA 847 TO 977, RBL9. SEAT RAIL FROM STA 847 TO 977, RBL 9 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 SRM 53-00-49-201-002-A01 AND PER CRJ900 AMM 53-00-49 (CONFIG A12).SDR VNAA202410210026Floor Support · corrodedCORROSION ON FLOOR SUPPORTS FROM STA 1000 TO STA 1069 LBL9 & LBL27 OF FLOOR STRUCTURE (C2). FLOOR SUPPORTS LBL27 ANT LBL9 AT FS1000 TO FS1069 WERE EVALUATED OUT OF LIMITS AND WERE REPAIRED PER CRJ900 SRM 53-61-43-101-001-A02 AND CRJ900 SRM 53-00-41-201-001-A0SDR VNAA202410210025Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT WERE EVALUATED OUT OR LIMITS PER CRJSDR VNAA202410210024Floor Support · corrodedCORROSION ON FLOOR SUPPORT SPLICE LOWER CHORD BTW STA 865-881 AND 9RBL AT FLOOR STRUCTURE OF PASSENGER CABIN (CPAX). FLOOR SUPPORT SPLICE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-43-101-001-A02; FABRICATED PER DWG NO. SH670-32161 REV. NC AND WAS REPLASDR VNAA202410210023Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-381 REV.SDR VNAA202410210022Canister · crackedCRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 LH FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.SDR VNAA202410210021Floorbeam · corroded"AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON LH SIDE FLOOR BEAM AT FS 280.00. LH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-00SDR VNAA202410210020Floorbeam · corroded"AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON RH SIDE FLOOR BEAM AT FS 280.00. RH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-00SDR VNAA2024102100019Rib · cracked"CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE RH WING WAS REPAIRED PER REO 690-57-51-380 REV."SDR VNAA202410210018Hinge Fitting · corroded"AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 Y NO. 3 AT VERTICAL STABILIZER REAR SPAR WERE REPLACED PER RIL #2103 REV. B."SDR VNAA202410210017Seat Track · corroded"DESCRIPTION: CORROSION ON SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847. SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847.00 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 ANDSDR VNAA202410210016Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40. EVALUATED,SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40 DUE TO EXCESIVE DAMAGE, THEREFORE ARE OUT OF LIMITS PER CRJ-900 SRSDR VNAA202410210015Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977. EVALUATED, SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02, CRJ-900 SRM SDR VNAA202410210014Angle · corroded"CORROSION ON MOUNTING ANGLE OF GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. MOUNTING ANGLE WAS EVALAUTED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01"SDR VNAA202410210013Plate · corroded"INITIAL INSPECTION: CORROSION ON KICK PLATE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE. CORROSION WAS REMOVED ON KICK PLATE PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE IS WHITHIN OF LIMITS AND DUE TO EXCESSIVE DAMAGE MID CAP ASDR VNAA202410210012Door Sill · corroded"INITIAL INSPECTION: CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT. EVALUATED, DUE TO EXCESSIVE CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT,THEREFORE OUT OF LIMIT PER CRJ 900 SRM 53-61-23-201-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06SDR VNAA202410210011Stringer · corroded"CORROSION ON STRINGER 21RH FS 319.70 TO FS 333 . STGR21 RH BTW FS319 TO FS333 WAS EVALUATED PER CRJ900 SRM 53-21-03-101-002-A04 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01"SDR VNAA202410210010Crossbeam · cracked"I"INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. WAS REPAIRED PER REO 690-SDR VNAA202410210009Floorbeam · cracked"INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53SDR VNAA202410210008Frame · corroded"CORROSION ON FRAME FS364.00 NEAR STGR 27 BEHIND OF SENSOR PX41 AT MAIN AVIONICS COMPARTMENT. FRAME FS364 WAS RE INSPECTED PER CRJ900 NDTM PART 01 51-20-009-210-A01 AND ONLY NUTPLATE BRACKET WAS FOUND WITH CORROSION, WAS FABRICATED PER DWG SH670-32456 REV. NCSDR VNAA202410210007Intercostal · corroded"INITIAL INSPECTION: CORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. EVALUATED, DUE TO NOT ALLOWED DAMAGE ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT,THEREFORE SDR VNAA202410210006Frame · corroded"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900SDR VNAA202410210005Frame · corroded"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900SDR VNAA202410210004Angle · corroded"CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6 CSDR VNAA202410210003Fitting · corroded" CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFORSDR VNAA202410210002Bracket · corroded"CORROSION ON BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ-900 SRM 5SDR VNAA202410210001Drag Angle · cracked"INITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TR RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TSDR VNAA2024081311101Sensor · unserviceableBRAKE OVHT WARNING MSG IN FLIGHT, LHOB BTMS EICAS INDICATION BOX SHOWED RED, AND INDICATED 20, IN CRUISE FLIGHT / REMOVED AND REPLACED ASCU IAW CRJ900 AMM 32-44-06-000/400-801-A01 AND REMOVED AND REPLACED LH OB BRAKE TEMP SENSOR IAW CRJ900 AMM 32-46-01-000/400SDR VNAA2024050911101Warning Message · false indicationELEVATOR SPLIT CAUTION MSG IN FLT / TROUBLESHOOT AND PERFORMED OPERATIONAL TEST OF THE ELEVATOR CONTROL SYSTEM IAW CRJ 900 FIM 27-31-00-810-803-A02 AND AMM 27-31-00-710-801-A01. OPS CHECK GOOD AT THIS TIME. FAULT CLEARED AND FAULT DID NOT RE-APPEAR.SDR VNAA2023102011101Detector · unserviceableDURING CRUISE, THE CREW NOTICED A FLAPS/STALL FAIL MESSAGE / REMOVED AND REPLACED RIB SKEW DETECTOR MT5 IAW CRJ900 AMM 27-52-45-000/400-802-A01. OPS CHECK GOOD. RIG CHECK GOOD.SDR VNAA2023092911101Pseu · unserviceableNLG DID NOT DEPLOY WHEN LEVER SELECTED DOWN, HAD TO MANUALLY EXTEND PER QRH. REMOVED & REPLACED PSEU I.A.W. CRJ900 AMM 32-61-01-000/400-801. PERFORMED MULTIPLE OPS CHECKS OF LANDING GEAR EXTENSION/RETRACTION I.A.W. CRJ900 AMM 32-30-00-865-801. OPS CHECKS GOOD.SDR VNAA202307121113Manifold · unserviceableSTEERING INOP AFTER TAKE OFF AND GEAR UP / REMOVED AND REPLACED THE STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. OPS CHECK AND LEAK CHECK GOOD.SDR VNAA202306191111Unknown · unknownNOSE WHEEL STEERING INOP CAUTION MESSAGE 10 SECONDS AFTER TAKE OFF. NO MESSAGE SHOWN UPON MEET AND GREET PERFORMED. RESET OF NWS IAW CRJ 900 AMM 32-50-00-810-802. NO DEFECTS NOTEDSDR VNAA202302021111Not Entered · not enteredRH RUDDER SKIN STA136.90 - STA148.86 DENTED. PERFORMED PERMANENT REPAIR IAW EA 23-C9-55-0029-IR_APPROVED.SDR VNAA202212061111Drain Mast · missingAFT FUEL DRAIN MISSING. REMOVED REMAINING PIECE OF THE DRAIN MAST AND SEAL IAW AMM 28-20-03-000-801-A01. NO FURTHER DEFECTS NOTED. A/C OK FOR FERRY FLIGHT. FERRY FLT 9977. REMOVED AND REPLACED AFT FUEL DRAIN MAST IAW AMM 28-20-03-000/400-801-A01.SDR VNAA202207281111Sensor · fault messageMX DIVERSION DUE TO BRAKE OVERHEAT WARNING MESSAGE. CREW FOLLOWED QRH AND DECIDED TO DIVERT TO THE NEAREST SUITABLE AIRPORT. TRUCKS WERE ROLLED IN ATL TO CHECK FOR BRAKE FIRES. CREW DID NOT PERFORM AN OVERWEIGHT LANDING. CREW WAS ABLE TO TAXI TO THE GATE AND MSDR VNAA2022071211211Stiffener · dentedDURING OVERNIGHT MX AT GSP, FOUND 3/4"" CRACK AND 1 1/2"" DENT ON FORWARD BAGGAGE BAY DOOR FORWARD LOWER STABILIZER / PERFORMED PERM REPAIR OF THE FWD BAGGAGE DOOR LOWER FWD STIFFENER IAW REO 690-52-35-298, EA 22-C9-52-0853, CRJ 900 SRM 51-42-06, AND CRJ 900 SSDR VNAA202206301111Acm · unserviceableON DEPARTURE AFT FA IMMEDIATELY SMELLED SMOKE AND CALLED FWD FA. IT WAS DETERMINED THAT THE SMOKE ODOR WAS STRONGER IN THE REAR OF THE AIRCRAFT (ROW 11 BACK TO AFT FA STATION). SLIGHT SMOKY ODOR IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DECIDED TO RETURN SDR VNAA202106309995Seat Track · corrodedSEAT RAIL AT LBL9 CORRODED BEYOND LIMITS
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