N634NN

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 = 'N634NN' 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.

SDR VNAA20251216024Hinge Fitting · corrodedCORROSION FOUND ON INTERNAL FACE OF LUGS L1, L2, L3, L4, L5, L6 AND INBOARD LUG AT LH AILERON. FITTING #1 (1EA) AND L3, L4 OF CENTER HINGE FITTING (2EAS) WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01. LUGS BORES L 1 , L 2, L5 AND L6 AT AILERON LH WERE REPDec 16, 2025 · N634NN · Cndair CL6002D24 · AileronsSDR VNAA20251216023Hinge Fitting · corrodedCORROSION FOUND ON INTERNAL FACE OF BORE R1, R2, R3, R4, R5, R6, INBOARD AND OUTBOARD(UPPER AND LOWER (9EAS TOTAL). INBOARD AND OUTBOARD(UPPER AND LOWER) WERE CLEANED PER PER CRJ 900 SRM 51-26-00-001-001-A01. R2 & R5 WERE REPAIRED PER REO 670-57-61-237 REV -Dec 16, 2025 · N634NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR VNAA20251216022Canister · crackedCRACK ON CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -Dec 16, 2025 · N634NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA20251216021Rivet · corrodedCORROSION ON SEVERAL SHOP FORMED HEAD OF RIVETS INSTALLED ON OUTER CHORD AT INTERIOR SIDE OF FS1098.20 BTW STGR 24LH-24RH. RIVETS ON OUTER CHORD AT INTERIOR SIDE OF FS1098.20 BTW STGR 24LH-24RH WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20251216020Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AR TO FAIRING ACCESS PANEL 193AB. EVALUATED PER EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20251216019Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BLO.00). DRAG ANGLE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA20251216018Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BL 0). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % READec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA20251216016Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT LH WING. CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV-.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA20251216017Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING. CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV-.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA20251216015Seat Track · corrodedWEAR AND CORROSION ON SEAT RAIL LBL27 (4EAS) FROM FS379.00 TO FS693.00AT CABIN PAX. SEAT RAIL (1EA) LBL27 FS 379.00 TO FS 485.00 WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED,FOUND WITHIN LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01, SDec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251216014Seat Track · corrodedWEAR AND CORROSION ON SEAT RAIL LBL9 (7EAS) FROM FS379.00 TO FS977.00AT CABIN PAX. WEAR AND CORROSION ON SEAT RAIL LBL9 (7EAS) FROM FS379.00 TO FS977.00AT CABIN PAX WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-0Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251216013Seat Track · corrodedWEAR AND CORROSION ON SEAT RAIL RBL9 (8EAS) FROM FS379.00 TO FS977.00AT CABIN PAX. EVALUATED, DUE TO EXCESSIVE DAMAGE ON SEAT RAIL RBL9 (8EAS) FROM FS379.00 TO FS977.00AT CABIN PAX PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251216012Seat Track · corrodedWEAR AND CORROSION ON SIDE SEAT RAIL LH (9EAS) FROM FS379.00 TO FS977.00AT LH SIDE. WEAR AND CORROSION ON SIDE SEAT RAIL LT (9EAS) FROM BS 379 TO 977 AT LH SIDE.WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-ADec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251216011Seat Track · corrodedWEAR AND CORROSION ON SIDE SEAT RAIL RH (10 EAS) FROM FS379.00 TO FS977.00AT RH SIDE. WEAR AND CORROSION ON SIDE SEAT RAIL RH (10 EAS) FROM BS 379 TO 977 AT RH SIDE WAS EVALUATED WITH EXCESSIVE DAMAGE IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251216009Fitting · corrodedCORROSION ON GALLEY FLOOR FITTINGS FS286 RBL17 AND 37, FS295.00 RBL4, FS319.70 RBL5, FS288 LBL20 AND FS329 LBL20 AT CABIN PAX. EVALUATED EXCESSIVE DAMAGE ARE OUT LIMITS IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-21-001-001-A01.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR VNAA20251216010Doubler · corrodedCORROSION ON DOUBLER SILL ON SERVICE GALLEY SURROUND STRUCTURE FS319.00 BTW STGR17 TO STGR18 RH SIDE. CORROSION ON DOBLER SILL ON SERVICE GALLEY SURROUND STRUCTURE FS319.00 BTW STGR17 TO STGR18 RH SIDE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, WAS EVALDec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA20251216008Plate · corrodedCORROSION ON KICKPLATE ON INTERNAL SURROUND STRUCTURE BTW FS 310 TO FS349. EVALUATED, DUE TO EXCESSIVE DAMAGE PER CRJ/900 SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-42-06-001-001-A01Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202512186007Cap · corrodedCORROSION ON MIDCAP ON INTERNAL SURROUND STRUCTURE BTW FS349 TO FS310 ON THE PASSENGER DOOR. EVALUATED, DUE TO EXCESSI•VE DAMAGE ON MIDCAP ON INSTERNAL SURROUND STRUCTURE BTW BS 349 - BS 310 ON THE PASSENGER DOOR IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202512186006Fitting · corrodedCORROSION FLOOR FITTING ACCESS 109 (1EA) , BEHIND ACCESS 108 (1EA) , IN FRONT ACCESS 107 (1EA) AND FWD CORNER OF AISLE SIDE (1EA) ON GALLEY 1. FLOOR FITTING ACCESS 109 (1EA PN:CDSP2019-7C620 ) , BEHIND ACCESS 108 (1EA PN:CDSP2019-7C620), IN FRONT ACCESS 107 Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202512186005Fitting · corrodedCORROSION FLOOR FITTING UNDER THE WASTE AND AISLE SIDE ON FWD LAVATORY. THE FLOOR FITTINGS WERE REPLACED IAW CMM 25-40-40.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202512186004Floor Support · crackedCRACKED FLOOR SUPPORT, RBL 12, BTW BS 221.73 - 229. THE FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2087, REV -.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202512186003Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB, RT SIDE. BELOW ADG SUPPORT DOUBLER, BS 193. THE FLOOR WEB WAS REPAIRED IAW REO 670-53-11-509, REV E, & REO 690-53-11-2093, REV -.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202512186002Floorbeam · crackedCRACKED CENTER COCKPIT FLOORBEAM, LBL 12, BS 280. THE FLOORBEAM WAS REPAIRED IAW REO 690-53-11-2085, REV-.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA20251216001Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW BS 280 - 295 AND S23 - 24L. THE SKIN WAS REPAIRED IAW REO 690-53-21-2060, REV -.Dec 16, 2025 · N634NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2024080511102Warning Message · false activationIB FLT SPLRS CAUTION MSG AND IB SPOILERONS CAUTION MSG IN FLIGHT / RESET PER MIPM SUCCESSFUL. MESSAGES DID NOT REAPPEAR.Aug 2, 2024 · N634NN · Cndair CL6002D24 · Drag Control System
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