N559NN
Service difficulty reports · 75
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 = 'N559NN' 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 = 'N559NN' 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 VNAA2026062920404Fan · unserviceableAPU DOOR CAUTION MSG AFTER TAKE OFF. FA AND AFT FA REPORT A STRONG BURNING ODOR AT THE SAME TIME DURING TAKE OFF . RAN APU DOOR CAUTION QRH FAULT PERSISTED / REMOVED AND REPLACED RH RECIRCULATION FAN IAW AMM 21-22-10-000/400 801-A01. LEAK TEST PASS OP TEST GSDR VNAA2025022111103Door · openLOW PRESSURE AIR DOOR LEFT OPEN, COVER MISSING / REMOVED AND REPLACED LOW PRESSURE AIR DOOR IAW CRJ 900 AMM 52-45-53-400-801.SDR VNAA2024111911101Drain · overflowELECTRICAL FIRE SMELL OBSERVED IN GALLEY IN FLIGHT. CREW COMMUNICATION WAS ESTABLISHED, AND NO SMELL WAS OBSERVED IN THE FLIGHT DECK OR BY PASSENGERS IN THE CABIN. NOTE: NO FIRE OR SMOKE PRESENT. / TROUBLESHOT SMELL OBSERVED IN GALLEY IN FLIGHT. TAXIED AIRCRAFSDR VNAA2024092711102Warning Message · false activationAVIONICS BAY DOOR AMBER CAS MESSAGE IN FLIGHT / PERFORMED OPS CHECK OF MAIN AVIONICS DOOR IAW CRJ 900 AMM 52-42-00-710-801-A01. NO FOD FOUND AND DOOR IS CLOSED.SDR VNAA202311230004Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1614. REV.--SDR VNAA202311260012Hinge · corrodedAFTER REMOVAL OF BUSHINGS, BEARINGS, AND HARDWARE, CORROSION ON HINGE FITTING LUG BORES AT LH AILERON, HINGE NO. 2 BOTH LUG BORES, HINGE NO. 3 BOTH LUG BORES, HINGE NO. 4 BORE LUG (SINGLE BORE LUG) AND BOTH PCU OUTPUT LINKS LUG BORES. HINGE FITTING LUG BORES SDR VNAA202311230010Stringer · corrodedCORROSION AROUND FASTENERS ABOVE STGR 26RH AND BTW FS364.00 - FS349.00 AT AVIONIC COMPARTMENT DOOR SURROUND STRUCTURE. STRINGER 26R BTW FS364.00 - FS349.00 AT AVIONIC COMPARTMENT DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-A01 AND CRJ90SDR VNAA202311230007Web · crackedCRACK 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 CRJ900 SRM SRM 53-11-43-201-001-A01SDR VNAA20231120004Access Panel · wornWEAR ON LEADING EDGE ACCESS PANELS 622 AR AND 622BR ALSO NICK ON ACCESS PANEL 622BR. REPAIRED PER EA 23-C9-57-1502 REV IR. SECTION III - PERMANENT REPAIR AND EA 23-C9-57-1503 REV IR. SECTION III - PERMANENT REPAIRSDR VNAA202311250001Skin · corrodedCORROSION AROUND SETTLEMENT AREA WAS FOUND AT THE MAIN AVIONICS COMPARTMENT DOOR BETWEEN FS364 TO FS 394 AND STGR 25R - STGR 25L. CORROSION AROUND SETTLEMENT AREA WAS FOUND AT THE MAIN AVIONICS COMPARTMENT DOOR BETWEEN FS364 TO FS394 AND STGR25R/STGR25L WAS RSDR VNAA202311230003Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH. EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV. -F AND EA 23-C9-53-1442 REV.IRSDR VNAA20231121002Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. DUE TO EXCESIVE CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WERE REPLACED PER CRJ900 SRM 53-00-00-101-001-A01 ASDR VNAA202311230005Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 @ FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT SDR VNAA202311260006Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1006.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL 27 BTW FS 1006.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1465 REV. IRSDR VNAA202311260002Angle · crackedCRACK ON CLIP, STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE. CLIP, STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE WAS REPLACED PER EA 23-C9-53-1463 REV. IRSDR VNAA202311250008Intercostal · corrodedCORROSION ON INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS 319.70 AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS 319.70 AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-0SDR VNAA202311250002Intercostal · corrodedCORROSION ON INTERCOSTAL AT STGR 20R BTW FS333.00 TO FS 364.00. CORROSION ON INTERCOSTAL BTW FS 333.00 TO FS 364.00 STRG 20RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED AREA BTW FS349.00 TO FS364.00 IS WITHIN LIMITS AND AREA BTW FS333.0SDR VNAA202311230008Stringer · wornWEAR ON STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS FABRICATED AND REPLACE PER PER EA 23-C9-53-1448. REV. IR. SECTION III-PERMANSDR VNAA20231120001Skin · damagedNICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.5. NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.5 WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND REWORKED AREA ON FLS45.00 TO 65.5 WAS EVALUATED ISSDR VNAA202311250011Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS669.40 TO FS720.85. DUE TO EXCESSIVE CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS669.40 TO FS720.85. WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (CONFIG A12)SDR VNAA202311250010Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS 847.00 + 18.00 TO FS899.70. DUE TO EXCESSIVE CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS 847.00 + 18.00 TO FS899.70. WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00 (CONFIG A1SDR VNAA202311250004Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 669.40 TO FS 720.85. DUE TO NOT PERMISIBLE DAMAGE ON SIDE SEAT RAIL 15 RH, BTW FS 669.40 TO FS 720.85. AT PASSENGER CABIN WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (CONFIG. SDR VNAA202311250009Seat Track · corrodedCORROSION ON LH SEAT RAIL AT LBL 9, BTW FS 847.00 + 16.00 TO FS954.00 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON LH SEAT RAIL AT LBL 9, BTW FS 847.00 + 16.00 TO FS 954.00 WAS REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-9SDR VNAA202311230009Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL LBL 9 BTW FS379.00 TO FS485.00. DUE TO EXCESSIVE CORROSION ON FLOOR SEAT RAIL LBL 9 BTW FS379.00 TO FS485.00. WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53-00-49-000-801 (CONFIG. A12) AND AMM 53-00-49-400-8SDR VNAA202311230002Drag 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 DATUSDR VNAA202311230001Drag 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 VNAA202311260013Skin · dentedFUSELAGE DENT, AFT OF AFT CARGO DOOR WITHIN 800 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR/REPLACEMENT OF THE DAMAGE IN ACCORDANCE WITH APPROVED PROCEDURES.
FUSELAGE DENT AFT OF AFT CARGO DOOR WAS REPAIRED PER EA 21-C9-53-866 REV. D SECTION ISDR VNAA202311260011Aileron · corrodedCORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH HINGE NO 1, NO 2, NO 3 & NO 4 AND BOTH PCU OUTPUT LINK LUG BORES WAS FOUND. CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH HINGE NO 1, NO 2, NO 3 & NO 4 AND BOTH PCU OUTPUT LINK LUG BORES WERE RSDR VNAA202311260010Aileron · corrodedCORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH WING REAR SPAR HINGE NO 1, NO 2, NO 3 & NO 4 WAS FOUND. CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH WING REAR SPAR HINGE NO 1, NO 2, NO 3 & NO 4 WERE REPAIRED PER REO 690-57-51-306 REV. -ASDR VNAA202311260009Aileron · wornAFTER REMOVAL OF RH AILERON BUSHINGS, BEARINGS AND HARDWARE, WEAR AT SEVERAL LOCATIONS (OUTER FACES OF LUGS) OF RH AILERON CENTER HINGE FITTING. (OUTER FACES OF LUGS) OF RH AILERON CENTER HINGE FITTING. WERE REPAIRED PER REO. 690-57-61-305. REV. --SDR VNAA202311260008Floorbeam · corrodedAFTER FLOOR SUPPORT LBL 11 TO RBL 11 FS280 REMOVAL, CORROSION ON FLOOR STRUCTURE CROSSBEAM AT FS280.00. FLOOR STRUCTURE CROSSBEAM AT FS280.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01SDR VNAA202311250003Post · corrodedCORROSION ON FLOOR POST BL 11.16 RH LOWER SIDE AT BULKHEAD FS 280.00. FLOOR POST BL 11.16 RH LOWER SIDE AT BULKHEAD FS 280.00 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 CRJ900 SRM 51-42SDR VNAA20231120002Skin · wornWEAR ON SETTLEMENT AREA OF ACCESS PANEL 686AB. WEAR ON SETTLEMENT AREA OF ACCESS PANEL 686AB WAS REPAIRED PER EA 23-C9-57-1447 REV IR SECTION III PERMANENT REPAIR.SDR VNAA202311260007Bracket · corrodedCORROSION ON BRACKETS, MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. DUE TO BRACKETS MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT NOT ALLOWABLE DAMAGE PER CRJ900 SRM 53-32-58-101-001-A01 WERE REPLACED PER CRJ900 SRM 51-42-2SDR VNAA202311260004Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM RBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1504 REV. IRSDR VNAA202311260001Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH. DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STSDR VNAA202311250020Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STASDR VNAA202311250019Hinge · excess playAFTER 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. RUDDER HINGE FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER CRJ-9SDR VNAA202311260005Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1006.00 TO FS 1057.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL 9 BTW FS 1006.00 TO FS 1057.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1479 REV. IRSDR VNAA202311260003Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1491 REV. IR SECTION III - PSDR VNAA202311250018Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 BTW FS 581 TO FS 669.40 (2EA´S). SEAT RAIL LBL9 BTW FS 581 TO FS 669.40 WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202311250017Seat Track · corrodedCORROSION ON SEAT RAIL RBL9 BTW FS585 TO FS 669.40 (3EA´S). SEAT RAIL RBL9 BTW FS585 TO FS 669.40 (3EA´S) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202311250016Hinge · wornWEAR ON SEVERAL LUG OF PASSENGER DOOR HINGE (PASSENGER DOOR SIDE) WERE BLENDED OUT AND REWORKED AREA WAS MEASURED AND FOUND WITH THE FOLLOWING DIMENTION: MINIMUM REMAINING LUG WALL THICKNESS IS 0.104IN, THEREFORE REWORKED AREAS ARE WITHIN LIMITS PER CRJ-900 SRSDR VNAA202311250015Hinge · wornWEAR ON SEVERAL LUG LANDS OF PASSENGER DOOR HINGE (FUSELAGE SIDE). LUG LANDS OF PASSENGER DOOR HINGE (FUSELAGE SIDE) WAS REPAIRED PER REO 690-53-21-1668 REV.--SDR VNAA202311250014Angle · corrodedCORROSION ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND RESDR VNAA202311250013Angle · corrodedCORROSION ON LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS=310.00 TO FS= 349.00 WAS REPLACED PER SRM 51-42-06-001-001-A01SDR VNAA202311250012Striker · corrodedCORROSION AT SEAL STRIKER BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE SEAL STRIKER BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR VNAA202311250007Skin · corrodedCORROSION ON FUSELAGE SKIN FS= 319.00 TO FS= 333.00 BTWN STGR 25RH TO STGR 24RH AT MAIN AVIONICS COMPARTMENT. FUSELAGE SKIN FS= 319.00 TO FS= 333.00 BTWN STGR 25RH TO STGR 24RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA 23-C9-53-1547 REV. IR SECTION IIISDR VNAA202311250006Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 847.00 + 19.00 TO FS900.00. RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 847.00 + 19.00 TO FS900.00 WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202311250005Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS785.15 TO FS847.00 + 8.00. CORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS785.15 TO FS847.00 + 8.00 WAS REPLACED PER CRJ900 AMM 53-00-49
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