N632NN
Service difficulty reports · 25
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 = 'N632NN' 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 = 'N632NN' 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 VNAA2026050817601Selector Valve · failedGEAR DISAGREE AND MANUAL GEAR EXTENSION. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10-000/400-801 A01 AND BLEED HYDRAULIC SYSTEM. #3 IAW AMM 29-10-00-870-802-A01 ,PERFORMED OPERATIONAL TEST OF THE LANDING-GEAR EXTENSION/RETRACTION SYSTEM SDR VNAA202602020001Seat Track · corrodedAFTER REMOVAL OF FITTING OF FWD LAVATORY A DETAILED VISUAL INSPECTION WAS PERFORMED IAW NDTM 52-2100 AND CORROSION WAS FOUND ON SEAT TRACK RBL 9 FS349-477. DUE TO EXCESSIVE DAMAGE, SEAT TRACK ON RBL 9 FS 349.00 TO FS 477.00, WAS REPLACED PER SRM 53-21-49-101SDR VNAA2026020201Floor 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 WL 79.50 WAS FOUND. CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMSDR VNAA20260201013Web · crackedCRACK ON WEB OF INBD AUXILIARY SPAR FWD FACE (MLG SHOCK STRUT BAY AREA) WS 24.50 APPROX AT LT WING. CRACKED WEB OF INBD AUXILIARY SPAR FWD FACE (MLG SHOCK STRUT BAY AREA) WS 24.50 APPROX AT LT WING WERE REPAIRED PER REO 690-57-21-550 REV-.SDR VNAA20260201019Seat Track · corrodedWEAR AND CORROSION ON SIDE SEAT TRACKS ON LBL 9 FS 370 TO FS 485 (1EA). SIDE SEAT TRACKS ON LBL 9 FS 370 TO FS 485 (1EA) WAS REPLACED PER AMM 53-00-49 (CONFIG.A12) AND SRM 51-41-02-001-001-A01.SDR VNAA20260201018Seat Track · corrodedWEAR AND CORROSION ON RBL 9 SEAT TRACKS BTW FS 477 TO FS 693 (5EAS). DUE TO EXCESSIVE DAMAGE ON RBL 9 SEAT TRACKS BTW FS 477 TO FS 693 (5EAS) WERE REPLACED PER SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND AMM 53-00-49 (COSDR VNAA20260201017Seat Track · corrodedWEAR AND CORROSION ON LBL 9 SEAT TRACKS BTW FS 581 TO FS 693 (3EAS). DUE TO EXCESSIVE DAMAGE ON LBL 9 SEAT TRACKS BTW FS 581 TO FS 693 (3EAS), WAS REPLACED PER SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND AMM 53-00-49 (CONFIG A12).SDR VNAA20260201016Seat Track · corrodedWEAR AND CORROSION ON LBL 27 SEAT RAILS BTW FS 364 TO FS 693 (2EAS). WEAR AND CORROSION ON LBL 27 SEAT RAILS BTW FS 364 TO FS 477 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49-400-801-A12, BSSDR VNAA20260201015Seat Track · corrodedCORROSION ON WARDROBE AND FWD LAVATORY FITTINGS ON SEAT TRACKS LBL 27 BTW FS 364-409 (2EAS) AND RBL 9 BTW FS 349-364 (1EA). WARDROBE AND FWD LAVATORY FITTINGS ON SEAT TRACKS LBL 27 BTW FS 364-409 (2EAS) AND RBL 9 BTW FS 349-364 (1EA) WERE REPLACED PER SRM 51SDR VNAA20260201014Fitting · corrodedCORROSION ON FITTINGS NUT ON FLOOR STRUCTURE BTW FS 379-394 RBL 17 (1EA), AND BTW FS 259-310 RBL 4 (1EA) AND BTW FS 280-295 RBL 9 TO RBL 37 (2EAS). FITTINGS NUT ON FLOOR STRUCTURE BTW FS 379-394 RBL 17 (1EA), AND BTW FS 259-310 RBL 4 (1EA) AND BTW FS 280-29SDR VNAA20260201010Angle · crackedCRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT RT WING. CRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT RH WING WAS REPAIRED PER REO 690-57-51-503 REV.- -SDR VNAA20260201009Angle · crackedCRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT LT WING. CRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT LH WING WAS REPAIRED PER REO 690-57-51-504 REV. - -SDR VNAA20260201008Seat Track · corrodedWEAR AND CORROSION ON SIDE SEAT TRACKS ON STGR 15RH FS 578 TO FS 977 (8EAS). DUE TO EXCESSIVE DAMAGE ON SIDE SEAT RAILS ON STGR 15RH FS 578 TO FS 977 (8EAS) WERE REPLACED PER AMM 53-00-49 (CONFIG A12) AND PER SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A0SDR VNAA20260201007Seat Track · corrodedWEAR AND CORROSION ON SIDE SEAT TRACKS ON STGR 15LH FS 661+16 TO FS 977 (8EAS). WEAR AND CORROSION ON SIDE SEAT TRACKS ON STGR 15LH FS 661+16 TO FS 977 (8EAS) WERE EVALUATED EXCESSIVE DAMAGE PER SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02, AND SRM 53-SDR VNAA20260201011Drip Tray · corrodedCORROSION ON DRIP TRAY RH/LH OF FS280.00 AT CABIN FLOOR STRUCTURE. CORROSION ON DRIP TRAY LH OF FS280.00 AT CABIN FLOOR STRUCTURE WAS EVALUATED DUE TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-42-13-001-001-A01 AND CORROSDR VNAA20260201012Sleeve · corrodedCORROSION ON INBD SLEEVE OF OTBD AXLE AT RT MLG. INBD SLEEVE OF OTBD AXLE AT RT MLG WAS REPLACED IAW CMM 32-11-06SDR VNAA20260201003Skin · damagedRIGHT INBD FLAP DAMAGE WITHIN 1080 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PERM REPAIR - TAPE APPLIED - TEMPORARY DISPOSITION FOR RH INBD FLAP DAMAGE WITHIN 1080 FLSDR VNAA20260201002Hinge · damaged585FH PERM REPAIR - SPEED TAPE APPLIED - FWD LAV SERVICE DOOR 142BR HINGE HOLES WITHIN 585 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. FUSELAGE STRUCTURE FOR FWD LAV SESDR VNAA20260201006Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUMS. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5%SDR VNAA20260201005Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPARSDR VNAA20260201004Hinge · corrodedCORROSION ON HINGE OF AFT LAVATORY SERVICE DOOR AT EXTERNAL FUSELAGE. HINGE OF AFT LAVATORY SERVICE DOOR AT EXTERNAL FUSELAGE WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01 AND CRJ/900 AMM 52-45-01.SDR VNAA20260201001Plate · corrodedDURING INSPECTION OF THE TASK CARD 53-20-220-JIC WAS DETECTED CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE EVALSDR VNAA2025021311101Pseu · unserviceableDIRECTLY AFTER TAKE OFF TRIED TO PULL UP GEAR GAVE WARNING WITH GEAR DISAGREE UPPER NOSE GEAR DID NOT RETRACT DECLAIRED EMERGENCY. / REMOVED AND REPLACED PSEU IAW CRJ 900 AMM 32-61-01-000/400-801, OPS CHECKS GOOD. WHILE TRYING TO PERFORM GEAR RETRACTION/EXTENSSDR VNAA2024121811101Unknown · odorBOTH FAS SMELLED A BURNING PLASTIC SMELL IN THE CABIN. NO SMOKE NOTED. THE ODOR STARTED TO DISSIPATE ON THEIR RTF, THE CREW THOUGHT THAT MIGHT BE RELATED TO THE REC FAN BEING TURNED OFF. THE SMELL CAME FROM THE CABIN AND LASTED LESS THAN 15 MINUTES. NO MEDICALSDR VNAA2024112611101Control Unit · faultedCARGO BOTTLE LO CAUTION ILLUMINATED MULTIPLE TIMES IN FLIGHT. / TROUBLESHOT IAW CRJ 900 FIM 26ˆ’25ˆ’01ˆ’810ˆ’801. PERFORMED VISUAL CHECK OF THE HRD AND LRD CARGO FIRE EXTINGUISHER CONTAINER PRESSURE GAUGES IAW CRJ 900 AMM 26-25-01-210-801. BOTTLES FOUND TO
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