N590NN
Service difficulty reports · 46
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 = 'N590NN' 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 = 'N590NN' 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 VNAA2025022111101Windshield · crackedCA SIDE WINDSHEILD CRACKED IN FLIGHT. / REMOVED AND REPLACED THE CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD.SDR VNAA20250102028Hinge Fitting · corrodedCORROSION ON CENTER FITTINGS BORE LUG L1,L2,AND L5 AT LH CENTER FITTINGS BORE LUG L1,L2,AND L5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV. -- AND REO 690-57-61-356 REV. --SDR VNAA20250102026Door Sill · corrodedIN REFERENCE TO JOB TRFKE001P2A5:53-30-307-JIC/002: AFTER REMOVAL DOOR SILL, CORROSION ON AFT CHORD INNER AT SURROUND STRUCTURE AFT CARGO DOOR WAS FOUND. EVALUATED, DUE TO DAMAGE IS NOT ALLOWED, AFT INNER CHORD PER CRJ-900 SRM 53-61-23-101-001-A01 AND AFT CHOSDR VNAA20250102029Bushing · damagedHOUSING OF RH AILERON LUG #6 WAS MEASURED AND WAS FOUND OUT LIMITS BY STANDARD (NOMINAL MEASUREMENT). BUSHING OF RH AILERON LUG #6 WAS FABRICATED PER REO 670-57-61-107 REV- BSDR VNAA20250102027Hinge Fitting · corrodedCORROSION ON CENTER FITTINGS BORE LUG R1, R2, R5 AND R4 WAS FOUND AT RH AILERON. CENTER FITTINGS BORE LUG R1,R2,R5 AND R4 WAS FOUND AT RH AILERON WAS REPAIRED PER REO 670-57-61-107 REV - BSDR VNAA20250102015Web · corrodedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER PER CRJ900 SRM 53-11-43-201-001-A01SDR VNAA20250102011Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1893SDR VNAA20250102024Seat Track · corrodedCORROSION ON SEAT RAIL (2 EAS) BTW FS 477.40 TOFS 693.00 ON RBL 9. SEAT RAIL (2 EAS) BTW FS 477.40 TOFS 693.00 ON RBL 9 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG. A12).SDR VNAA202501032023Canister · crackedIN REFERENCE TO JOB CARD 500-08E2-JIC: DURING INSPECTION ON AREA WAS DETECTED CRACK IN CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--SDR VNAA20250102022Floor Support · corrodedCORROSION ON FLOOR SUPPORTS LH (3EAS) BTW FS280.00 TO FS310.00 AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS LH (3EAS) BTW FS280.00 TO FS310.00 AT FUSELAGE FLOOR STRUCTURE WERE FOUND OUT LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ 900 SRM 53-21-43-101-001-A03 THEREFSDR VNAA20250102031Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN. RH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND WERE RSDR VNAA20250102030Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN. LH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 ASDR VNAA20250102010Plate · corrodedCORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF. DRAIN PLATE OF FLOOR PANEL 232BRF WAS REPLACED PER CRJ/900 AMM 53-00-47.SDR VNAA20250102009Angle · corrodedCORROSION ON ANGLE MOUNTING AND ANGLES (4EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLES (4EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATESDR VNAA20250102008Cap · corrodedCORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON KICKPLATE BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01,EVALUATED ON KICKPLATE,SDR VNAA20250102007Hinge · 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 VNAA20250102006Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-SDR VNAA20250102021Floorbeam · corrodedCORROSION ON FLOOR BEAM 9 LBL BTW FS 1000.00 TO FS 1047.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-001-A01 AND NO DAMAGE WAS FOUND ON FLOOR BEAM 9 LBL BTW FS 1000 TO FS 1022 AND BTW FS 1045 TO FS 1051 AND WAS RSDR VNAA20250102020Floorbeam · corrodedCORROSION ON FLOOR BEAM 27 LBL BTW FS 1000.00 TO FS 1047.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. PAINT WAS REMOVED ON FLOORBEAM 27 LBL BTW FS 1000.00 TO FS 1005 AND BTW FS 1038 TO FS 1051 PER CRJ900 SRM 51-26-01-001-001-A01 AND NO DAMAGE WAS FOUND AND WSDR VNAA20250102019Seat 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 WERE REPLACED PER CRJ900 AMM 53-0SDR VNAA20250102018Seat Track · corrodedINITIAL INSPECTION: CORROSION ON RH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (7EA). RH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (7EA) 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 CRJ900 AMSDR VNAA20250102017Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (6EA). LH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONFIG.A1SDR VNA2025F00000Hinge · corrodedCRACK AND CORROSION ON FWD/MID/AFT HINGES, DEGRADED PAINT AND MISSING DECAL ON STEP PLATE AT AFT BAGGAGE BAY. DUE TO EXCESSIVE DAMAGE, FWD/MID/AFT HINGES ON STEP PLATE AT AFT BAGGAGE BAY WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01, REPLASDR VNAA20250102005Stringer · corrodedSTRINGER 26R IN STA. FS= 333 TO FS=349 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-42-21-001-001-A01.SDR VNAA20250102004Stringer · corrodedCORROSION ON STRINGER 26RH IN STA. FS= 333 TO FS=349 AT MAIN AVIONICS COMPARTMENT. STRINGER R/H 26RH IN STA. FS= 333 TO FS=349 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-SDR VNAA20250102025Floor Support · crackedCRACK ON FLOOR SUPPORT 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 FLSDR VNAA20250102002Stringer Splice · corrodedCORROSION ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT. (E/E) FOR EXCESSIVE DAMAGE ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-SDR VNAA20250102003Intercostal · corrodedCORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. CORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTSDR VNAA20250102001Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) WAS SDR VNAA20250102016Nozzle · dentedSEVERAL DENTS ON EXHAUST NOZZLE FROM 1 HR TO 7 HRS POSITION AT LH ENGNE. DENTS ON EXHAUST NOZZLE FROM 1 HR TO 7 HRS POSITION AT LH ENGNE WERE REPAIRED PER EA NO: A1-690-78-00018 REV --SDR VNAA20250102014Bracket · corrodedCORROSION ON MACHINED BRACKET (4 EAS) AND PLATE (2 EA) BTW FS477.400 AND FS669.40 OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. CORRECTIVE ACTION: EVALUATED, MACHINED BRACKET (4 EAS) AND PLATE (2 EA) BTW FS477.400 AND FS669.40 OF INTERNAL STRUCTURE AT SDR VNAA20250102013Plate · corrodedCORROSION ON STEP PLATE AT SERVICE DOOR. EVALUATED, DUE TO EXCESSIVE DAMAGE STEP PLATE DOOR COVER PER CRJ-900 SRM 53-00-01-101-001-A01 AND STEP PLATE AT SERVICE DOOR WAS VERIFIED ITEM30C P/N SH670-31407-7 AND REPLACED PER CRJ-900 AIPC 53-21-23-15SDR VNAA20250102012Door Frame · corrodedCORROSION ON INTERNAL SURROUND STRUCTURE SETTLEMENT AREA OF THE MAIN AVIONICS COMPARTMENT DOOR (CUT-OUT). REPAIRED PER REO 690-53-21-032 REV -.SDR VNAA2024010311101Acm · failedSMOKE FILLED CABIN ON SHORT FINAL. AFTER LANDING, SMOKE WENT AWAY AND R PACK AUTOFAIL MESSAGE APPEARED. / REMOVED AND REPLACED THE RH AIR CYCLE MACHINE IAW CRJ 900 AMM 21-51-08-000/400-801. PERFORMED OPERATIONAL TEST OF OF AIR CONDITIONING DISTRIBUTION SYSTEM SDR VNAA2023112711101Check Valve · unserviceableFLIGHT 5156 HAD MULTIPLE RH ENGINE FLAME OUTS WHILE ENROUTE. THE CREW WAS ABLE TO RELIGHT AND STABILIZE THE RH ENGINE/ REMOVED AND REPLACED THE RH ENGINE 6TH STAGE CHECK VALVE IAW CRJ900 AMM 36-11-03-000/400-801. PERFORMED BORESCOPE INSPECTION OF RH ENGINE COMSDR VNAA2023111311101Pin · unserviceableREMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97 / REMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97.SDR VNAA202112221111Windshield · false indicationSMOKE SEEN OUTSIDE OF LEFT SIDE CA WINDSHIELD FOR APPROX 5 SECONDS / PERFORMED OPS CHECK OF WINDOW HEAT IAW CRJ 900 AMM 30-41-06-710-801, OPS CHECK OF PITOT PROBE HEAT IAW CRJ 900 AMM 30-31-00-710-801, OPS CHECK GOOD NO DEFECTS NOTED. RAN #1 ENGINE, NO DEFECTSSDR VNAA202110221111Door · out of alignmentPAX DOOR JAMMED CLOSED IN THE UNLOCKED POSITION. REMOVED AND RE-INSTALLED BOTH FWD AND AFT SPIGOT ASSY AND SHIMMED AS REQUIRED IAW CRJ 900 AMM 53-21-23-400-803-A03. FUNCTIONAL TEST GOOD IAW CRJ 900 AMM 52-11-00-720-802-A01.SDR VNAA2021102112111Roller · lack of lubeTROUBLE CLOSING THE MAIN CABIN DOOR / APPLIED GREASE TO LATCH PINS AND ROLLERS OF MAIN CABIN DOOR IAW CRJ 900 AMM 12-20-52-640-809(A01), DOOR CLOSES NORMALLY.SDR VNAA202107219992Seat Track · corrodedRH SEAT TRACK RBL 9 FROM 485-581 HAS PITTING CORROSIONSDR VNAA202107219991Seat Track · corrodedRH SEAT TRACK RBL 9 FROM 364-469 HAS PITTING CORROSIONSDR VNAA2020092411104Acm · failedLIGHT SMOKE IN CABIN WITH RT PACK AUTO FAIL. REMOVED AND REPLACED RT ACM, IAW CRJ900 AMM 21-51-08-000/400-801. OPS AND LEAK CHECK GOOD AT THIS TIME.SDR VNAA2020021911102Battery Pack · failedLOWER SIDEWALL EMER EXIT LTS ROW 15F AND 15A DO NOT ILLUMINATE. MX REMOVED AND REPLACED BATTERY PACK #3 IAW AMM. OPS CHECKS GOOD.SDR VNAA2018121311101Warning System · false activationDURING LANDING, THE CREW REPORTED A SPOILER/SPOILERONS 'C' MSG. THEY DECLARED AND LANDED WITHOUT ISSUE. RESET SYSTEM WITH THE CREW, MESSAGE'S CLEARED AND DID NOT REOCCUR.SDR VNAA2016111600024Contactor · inoperativeEMERGENCY LIGHTS COME ON THEN GO OFF. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED CONTACTOR K117 AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA2016111500021Transducer · malfunctionedRIGHT ANTI ICE DUCT WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT LEAK DETECTION TRANSDUCER AND PERFORMED CHECKS IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS REL
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