N635NN
Service difficulty reports · 29
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 = 'N635NN' 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 = 'N635NN' 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 VNAA2026100526201Target · missingGEAR DISAGREE ON CLIMB OUT C/A FOUND NLG PROX SENSOR TARGET MISSING. INSTALLED RH NLG CTR PROX SENSOR TARGET.SDR VNAA202603140006Skin · scratchedRIGHT FUSELAGE SKIN SCRATCHED. WITHIN 661 FLIGHT HOURS FROM REVISION REQUEST, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: SUBMIT AN RFTS WITH UPDATED DAMAGE REPORT.SDR VNAA202603130005Support · crackedCRACK ON MOTOR SUPPORT OF PASSENGER DOOR. MOTOR SUPPORT OF PASSENGER DOOR WAS REPAIRED PER CRJ/900 SRM 52-11-04-201-009-A01SDR VNAA202603140013Fitting · corrodedCORROSION ON FITTING (1 EA) BELOW THE SERVICE TABLE AT FWD LAV. FITTINGBELOW THE SERVICE TABLE AT FWD LAV WAS REPLACED PER CMM 25-40-40SDR VNAA202603140012Fitting · corrodedCORROSION FLOOR FITTING BEHIND ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING BEHIND ACCESS 108 (1 EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96SDR VNAA202603140011Support Fitting · corrodedCRACK ON CENTER FLOOR BEAM RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. CORROSION ON FITTING SUPPORT (FLOOR STRUCTURE) BTW FS 280.0 TO FS 300.0 CORDENATES RBL 23 AND LBL 23 ALSO LBL 31 AT PASSENGER CABIN. CORROSION ON FITTING SUPPORTSDR VNAA202603140010Floor Support · crackedCRACK ON CENTER FLOOR SUPPORT RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON CENTER FLOOR SUPPORT RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COSDR VNAA202603140009Overhead Bin · debonded450FH PERM REPAIR - CARGO PIT TAPE APPLIED - OVERHEAD BIN 12/13 ACWITH DISBONDED CENTER SUPPORT WITHIN 450 FLIGHT HOURS AFTERSECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT LOCATIONIN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING CSDR VNA2026F00005Overhead Bin · debonded450FH PERM REPAIR - CARGO PIT TAPE APPLIED - OVERHEAD BIN 12/13 ACWITH DISBONDED CENTER SUPPORT WITHIN 450 FLIGHT HOURS AFTERSECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT LOCATIONIN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING CSDR VNAA202603140008Floorbeam · corrodedCORROSION WAS FOUND ON CROSSBEAM FS 280 RH SIDE. RH CROSSBEAM FS280 AT COCKPIT CABIN WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01SDR VNAA202603140007Floorbeam · corrodedCORROSION WAS FOUND ON FLOORBEAM BS 280 LT. CORROSION WAS FOUND ON CROSSBEAM FS 280 LH WAS EVALUATED DUE EXCESSIVE CORROSION PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPLACED IAW SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR VNAA202603140005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL FROM FS 379 TO FS 669 AND STGR 15LH AND STGR 15 RH . CORROSION ON SIDE SEAT RAIL FROM FS 379 TO FS 669 AND STGR 15LH (3EAS) AND STGR 15 RH (4EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01. REPLACED PER CRJ-90SDR VNAA202603140004Seat Track · corrodedCORROSION ON SIDE SEAT TRACK FROM FS699 TO FS977 STGR 15LT AND STGR 15RT. THE SEAT TRACK EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49 CONFIG.A12.SDR VNAA202603140003Seat Track · corrodedCORROSION ON LH SEAT TRACK (3 EAS) BTW FS 364.0 TO FS 693.0, LBL 27 AT PASSENGER CABIN. THE LH SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR VNAA202603140002Seat Track · corrodedCORROSION ON LT SEAT TRACKS BTW FS 364.0 TO FS 683.0 LBL 9 AT PASSENGER CABIN. LT SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR VNAA202603140001Seat Track · corrodedCORROSION ON RT SEAT TRACKS BTW FS 349.0 TO FS 683.0, RBL 9 AT PASSENGER CABIN. THE SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-31-49-101-001-A02 AND WERE REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR VNAA202603130010Support Bracket · crackedCRACK ON LWR ANGLE OF WING RIB SS 15.50 (ROOT AREA) AT RH WING. BRACKET SUPPORT WAS FABRICATED PER DWG CC670-12148 REV -A AND REPLACED PER CRJ 900 SRM 51-42-06 001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202603130009Bulkhead Web · corrodedCORROSION ON LWR WEB OF BULKHEAD FS 280.0 LBL 12 (BEHIND CAP ANGLE) AT COCKPIT. CORROSION ON LWR WEB OF BULKHEAD FS 280.0 LBL 12 (BEHIND CAP ANGLE) AT COCKPIT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPAIRED CRJ-900 SRM 53SDR VNAA202603130008Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBLSDR VNAA202603130007Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBSDR VNAA202603130006Web · crackedCRACK IN THE WEB UNDER THE ADG PUMP FROM STA FS193 (FWD EQUIPMENT COMPARTMENT) CRACK IN THE WEB UNDER THE ADG PUMP FROM STA FS193 (FWD EQUIPMENT COMPARTMENT) WAS REPAIRED PER REO 690-53-11-2148REV. - -SDR VNAA202603130004Hinge Arm · corrodedCORRODED HINGE ARM (1 EA) AND HINGE FITTING (1 EA) ON SERVICE DOOR 195EL. HINGE ARM (1 EA) ON SERVICE DOOR 195EL WAS REPAIRED PER EA NO:5245-2026-0241 REV-- SECTION III PERMANENT REPAIR AND HINGE FITTING (1 EA) ON SERVICE DOOR 195EL WAS EVALUATED EXCESSIVE DSDR VNAA202603130003Hinge Fitting · corrodedCORRODED HINGE FITTINGS (2 EAS) AND HINGE ARMS (2 EAS) AT SERVICE DOOR 196ER. HINGE FITTINGS (2EAS) AND HINGE ARMS (2 EAS) AT SERVICE DOOR 196ER WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND REMOVED AND INSTALLED PER CRJ900 AMM 52-45-01SDR VNAA202603130002Drag 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 VNAA2026031310001Drag 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 VNAA2025060511101Fan · failedSTRONG SMOKE SMELL AFTER STARTING RIGHT ENGINE.(CLEARED UP AFTER A FEW MINUTES) / REMOVED AND REPLACED RH RECIRCULATION FAN IAW CRJ AMM 21-22-10-000/400-801. REMOVED AND REPLACED RH RECIRCULATION FILTER IAW CRJ AMM 21-22-12-000/400-801-A01.SDR VNAA2025041811102Manifold · failedSTEERING INOP CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED THE STEERING MANIFOLD IAW CRJ900 AMM 32-51-50-000/400-801. OPS AND LEAK CHK GOOD. STEERING INOP MSG CLEARED AND DID NOT REAPPEAR.SDR VNAA2025041811101Selector Valve · failedSTEERING INOP CAUTION ON TAKEOFF AFTER GEAR RETRACT. / REMOVED AND REPLACED MLG SELECTOR VALVE IAW CRJ 900 AMM 32ˆ’32ˆ’10ˆ’000/400ˆ’801 GEAR EXTENSION AND RETRACTION AND LEAK CHECK GOOD. STEERING INOP DID NOT SHOW.SDR VNAA2024072511101Windshield · smokeAFTER PERFORMING SAFETY AND POWER ON CHECKLIST, SMOKE WAS FOUND IN THE FLIGHT DECK / R/H WINDSHIELD ASSY IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. PERFORMED OPERATIONAL TEST OF THE WINDSHIELD SIDE WINDOW CONTROLLER IAW CRJ900 AMM 30-41-06-710-801-A01 AND D
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