N637NN

Service difficulty reports · 27

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 = 'N637NN' 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 VNAA2026051117801Pcu · faultedIB SPOILERONS / IB FLT SPLRS CAUTION IN FLIGHT. REMOVED & REPLACED LH IB MULTI-FUNCTION SPOILER PCU(MPE33) IAW AMM 27-62-01-000/400-801-A02, PERFORMED BLEEDING OF HYD SYSTEM #1&#2 IAW AMM 29-10-00-870-801-A01, LEAK TEST OF THE MULTI-FUNCTION SPOILER DONE IAWMay 4, 2026 · N637NN · Cndair CL6002D24 · Flight Control SystemSDR VNAA202508030010Fitting · corrodedCORROSION ON FITTING (1EA) OF ACCESS 104 AT GALLEY 1. FITTING (1EA) OF ACCESS 104 AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-32-02.Jun 3, 2025 · N637NN · Cndair CL6002D24 · Buffet/GalleysSDR VNAA202508030012Fitting · corrodedCORROSION ON FITTINGS OF ACCESS 407 (1 EA) AT GALLEY 4. FITTING OF ACCESS 407 (1 EA) AT GALLEY 4 WAS REPLACED PER CMM 25-32-99.Jun 2, 2025 · N637NN · Cndair CL6002D24 · Buffet/GalleysSDR VNAA202508030011Fitting · corrodedCORROSION ON FITTINGS OF ACCESS 306 (1EA) AND 307 (2EAS) AT GALLEY 3. FLOORS FITTINGS WITH P/N CDSP2019-7C-650 AND P/N CDSP2019-7C-700 OF ACCESS 306 (1EA) AND 307 (2EAS) AT GALLEY 3 WERE REPLACED PER CMM 25-33-13.Jun 2, 2025 · N637NN · Cndair CL6002D24 · Buffet/GalleysSDR VNAA202508030013Lug · corrodedCORROSION ON BORE OF LUGS L2, L5 AT LH AILERON WAS FOUND. BORE OF LUGS L2, L5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-107REV -B.May 30, 2025 · N637NN · Cndair CL6002D24 · AileronsSDR VNAA202508030009Hinge Fitting · corrodedCORROSION ON HINGE FITTING ASSEMBLY (2EAS) AT NLG DOOR. HINGE FITTINGS ASSEMBLY (2 EAS) AT NLG DOOR WERE REPLACED PER CRJ-900 CMM 32-22-06.May 30, 2025 · N637NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202508030008Hinge Fitting · corrodedCORROSION ON BORE OF LUGS R1, R2, R5, R6 AT RH AILERON. BORE OF LUGS R1, R2, R5, R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237REV -.May 30, 2025 · N637NN · Cndair CL6002D24 · AileronsSDR VNAA202508030007Hinge Fitting · corrodedCORROSION ON BORE LUGS (INB/OUTB) OF AILERON HINGE 2, 3 AND SCRACHTS ON BORE LUG (INB) OF HINGE 1 AT LH WING REAR SPAR. BORE LUGS (INB/OUTB) OF AILERON HINGE 2, 3 AND SCRACHTS ON BORE LUG (INB) OF HINGE 1 AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-4May 30, 2025 · N637NN · Cndair CL6002D24 · AileronsSDR VNAA202508030006Hinge Bracket · gougedSCRATCHS ON BORE LUGS AND GOUGES ON LUGS OF AILERON HINGE 3 (INB/OUTB LUGS) AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGE 3 (INB/OUTB LUGS) AT RH WING REAR SPAR WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER DWG : CC670-1May 30, 2025 · N637NN · Cndair CL6002D24 · AileronsSDR VNAA202508030005Hinge Fitting · gougedSCRATCH ON BORE LUG AND GOUGE ON LUG OF AILERON HINGE 2 (OUTB LUG) AT RH WING REAR SPAR. BORE LUG OF AILERON HINGE 2 (OUTB LUG) AT RH WING REAR SPAR WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER DWG : CC670-18052 REV. -D. LUMay 28, 2025 · N637NN · Cndair CL6002D24 · AileronsSDR VNAA202508030002Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS1069.75 TO FS1098.20 IN AREA COVERED BY RH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN BTW FS1069.75 TO FS1098.20 IN AREA COVERED BY RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 670-51-00-085 REV. -A AND RMay 28, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202508020009Intercostal · corrodedCORROSION ON INTERNAL STRUCTURE INTERCOSTALS BTW FS 349 - 364, S25L - 25R AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS BTW FS 349 -364, S26L - S26R AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM 53-21-23-101-003-A01 AND REPLACED PER SRM 51May 28, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508020007Skin · corrodedCORROSION ON FUSELAGE SKIN JOINT INTERNAL STRUCTURE FS280.00 BTW STGR26LH / STGR24RH AT MAIN AVIONICS COMPARTMENT. CORROSION REMOVED PER SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER SRM 53-00-00-101-001-A01May 28, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202508020011Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -May 26, 2025 · N637NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202508030004Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --May 25, 2025 · N637NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202508030003Floor Support · crackedCRACK ON FLOOR SUPPORT BL 12 RH BTWN FS 217 TO FS 230. FLOOR SUPPORT BL 12 RH BTWN FS 217 TO FS 230 WAS REPAIRED PER REO 690-53-11-2012 REV. --May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508030001Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --May 25, 2025 · N637NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202508020013Stringer · corrodedCORROSION ON INTERNAL STRUCTURE OVER S26R BTW FS349 - 364 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL STRUCTURE OVER STGR26RH BTW FS349.00 / FS364.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 AND WAS May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202508020012Bracket · corrodedCORROSION ON MACHINED BRACKETS (8E/A'S) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON MACHINED BRACKETS (2E/A'S) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PMay 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508020010Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508020008Frame · corrodedCORROSION ON FRAME INTERNAL STRUCTURE ON FS 319.00 BTW S25L - S26R AT MAIN AVIONICS COMPARTMENT. CORROSION EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-06-201-005-A01 AND WAS REPAIRED PER SRM 53-00-06-201-006-A01.May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202508020006Stringer · corrodedCORROSION ON STGR 27 BTW FS 1162.00 TO FS 1181.00 AT AFT EQUIPMENT COMPARTMENT. REPAIRED PER EA 53-2025-0749 REV -.May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202508020001Hinge · corrodedCORROSION ON HINGE OF AFT POTABLE WATER SERVICE DOOR AND AFT LAVATORY SERVICE DOOR. HINGES OF AFT LAVATORY SERVICE DOOR (2EAS) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND PAINT ON HINGES OF AFT POTABLE WATER SERVICE DOOR (2EAS) WAS REMOVED PER CRJ90May 25, 2025 · N637NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202508020005Frame · corrodedCORROSION ON FRAME 1162.00 BTW STGR 25L TO 25R AT AFT EQUIPMENT COMPARTMENT. FRAME 1162.00 BTW STGR 25L TO 25R AT AFT EQUIPMENT COMPARTMENT WAS REPAIRED PER REO 690-53-70-090 REV -.May 24, 2025 · N637NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202508020004Support Plate · corrodedCORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 40 AND LBL40. REMOVED PER SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-42-06-001-001-A01.May 24, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508020003Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. CORROSION WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-May 24, 2025 · N637NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202508020002Frame · corrodedCORROSION ON FWD/AFT HANDLE FRAME EXTERNAL SIDE AT FWD AND CENTER BAGGAGE DOOR. FWD/AFT HANDLE FRAME EXTERNAL SIDE AT FWD AND CENTER BAGGAGE DOOR WERE REPAIRED PER REO 690-52-35-529 REV -, REO 690-52-35-530 REV -, REO 690-52-35-531 REV -, AND REO 690-52-35-5May 23, 2025 · N637NN · Cndair CL6002D24 · Cargo/Baggage Doors
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