N630NN

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 = 'N630NN' 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 VNAA202510300004Hinge · wornIN REFERENCE TO CARD TRFKE00EQH21': 52-11-01-201-002-A01-PERM REPAIR - PASSENGER DOOR HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IAW SRM TASK 52-11-01-201-002-A01. HINGE AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 52-11-01-201-002-A01Oct 18, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202510310011Retainer · corrodedAFT MAIN AVIONICS COMPARTMENT DOOR SEAL REMOVAL IN REFERENCE NRC00053 CORROSION ON SEAL RETAINER AT SURROUND WAS FOUND. WERE EVALUATED,DUE TO EXCESSIVE DAMAGE ON SEAL RETAINER(4EA) AT MAIN AVIONICS COMPARTMENT DOOR PER SRM 53-00-00-101-001-A01 AND REPLACED Oct 7, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202510310009Floor Support · corrodedCORROSION FLOOR FITTING ON ACCESS 305 (2EA´S) ON GALLEY 3 CORECTIVE ACTION: SUMMARY OF NRC00208: FLOOR FITTING (2 EAS) AND MANUFACTURED DOUBLER (1 EA) ON ACCESS 305 AT GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-30 AND FABRICATED PER REO 690-25-31-04Oct 2, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202510310008Floor Support · corrodedINTERIOR SHEET METAL: CORROSION FLOOR FITTING IN FRONT OF ACCESS 107 (1EA) ON GALLEY 1 FLOOR FITTING PN: CDSP2019-7C-620 ON ACCESS 107(1 EA) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-44Oct 2, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202510310010Floor Support · crackedAFTER ANGLE REMOVAL IN REFERENCE NRC00115 BTW FS 265 TO FS280 CRACK WAS FOUND ON ANGLE. FLOOR ANGLE BS 265 TO FS280 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202510310007Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15RH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS783.15 TO FS846.00. SEAT RAIL (02 SEGMENTS) STGR 15RH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS783.15 TO FS846.00 WERE Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202510310006Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15LH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS 783.15 TO FS846.00. SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15LH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS 783.15 TO FSep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202510310004Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9 BTW FS 482 TO 581, FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN. SECTIONS SEAT RAIL RBL 9 BTW FS 482 TO 581, FS 581 TO 661+32 AND 661+32 TO 677 WERE REPLACED PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 AMM 53-00-49 CONFIG A12Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202510310002Support · crackedDURING INSPECTION OF THE TASK CARD 53-20-260_R/H-JIC IT WAS DETECTED CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW CORECTIVE ACTION: AFT REFUEL DUCT MOUNT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW WAS REPAIRED PER REO 690-28-Sep 27, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202510310005Seat Track · corrodedCORROSION ON SEAT RAIL LBL 9 BTW FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN. SEAT RAILS LBL 9 BTW FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN PAX WERE EVALUATED OUT OFF LIMITS AND SEAT RAILS WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 AMMSep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202510310003Door Sill · corrodedCORROSIÓN ON SILL DOOR BTW STA 319.70-344 AT PASSENGER CABIN (CPAX). CORECTIVE ACTION: SILL DOOR BTW STA 319.70-344 AT PASSENGER CABIN (CPAX) WAS EVALUATED,THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-00Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202510310001Rib · crackedDURING INSPECTION OF THE TASK CARD 57-20-201_L/H-JIC. IT WAS DETECTED CRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.Sep 26, 2025 · N630NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202510300010Stringer · corrodedCORROSION ON SPLICE AND STGR 26RH BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT. CORECTIVE ACTION: CORROSION ON SPLICE AND STGR 26RH BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT WERE REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, WERE EVALUATED,THEREFORE ISep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202510300009Stringer · corrodedCORROSION ON STGR 25 LH BTW FS 295 TO FS 310 AT MAIN AVIONICS COMPARTMENT. STGR 25 LH BTW FS 295 TO FS 310 AT MAIN AVIONICS COMPARTMENT WAS EVALUTED PER CRJ-900 SRM 53-21-03-101-006-A04 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202510300008Floorbeam · crackedDURING INSPECTION OF THE TASK CARD 53-10-219B IT WAS DETECTED CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280 AT FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280 AT FLOOR STRUCTURSep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202510300006Skin · corrodedCORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR. CORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV -Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202510300007Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Sep 25, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202510300005Drag 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 BL0.0). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA202510300003Hinge · crackedIN REFERENCE TO CARD TRFKE00EQGK4': 53-21-23-201-007-A01-PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ900 SRM TASK 53-21-23-201-007-A01.// ENGINEERING COMMENTS: GENERATE NEW RFTS REQSep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202510300002Fitting · damagedREPAIR DAMAGED JACKING PAD HELICOIL INSERT LEFT, JACK FITTING LT WING WAS REPLACED PER SRM 51-42-21-001-001-A01.Sep 23, 2025 · N630NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA202510300001Hinge · corrodedCORROSION ON HINGES AND HINGE FITTINGS AT AFT LAVATORY SERVICE DOOR 196ER (ATTACHMENT HARDWARE INCLUDED). EVALUATED, DUE TO ECXSSESIVE DAMAGE ON HINGES (2 EAS) AND HINGE FITTINGS (2 EAS) AT AFT LAVATORY SERVICE DOOR 196ER PER CRJ 900 SRM 53-00-00-101-001-A0Sep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA2025072811101Seal · detachedMAIN CABIN DOOR SEAL CAME LOOSE IN FLIGHT / INSTALLED PORTIONS OF PASSENGER DOOR SEAL THAT WERE LOOSE IAW CRJ 900 AMM 52-11-07-400-801-A02-PSA, PRESSURE CHECK GOOD NO LEAKS DETECTED. NO FURTHER DEFECTS NOTED AT THIS TIME.Jul 26, 2025 · N630NN · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA2025031411103Pin · faultedEXCESSIVE N1 VIBRATION ON RH ENG. RAN QRH PROCEDURE. DID NOT CORRECT ISSUE AT NORMAL POWER SETTINGS. HAD TO REDUCE RH THRUST TO 72-73% TO KEEP VIB BELOW 1.7. / REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ900 AMM 72-21-02-400-801-A01-PSA. PERFORMED VIBMar 12, 2025 · N630NN · Cndair CL6002D24 · Turbine Engine Air Inlet SectionSDR VNAA2024122311101Window · unserviceableCA WINDOW STARTED ARCING AROUND 16K FT FOLLOWED BY WINDOW HEAT CAUTION MSG. THERE WAS NO SMOKE OR ODOR, ONLY ARCING AND LASTED NO MORE THAN 10 MINUTES AND NO MEDICAL ATTENTION WAS REQUIRED. / REMOVED AND REPLACED CA SIDE WINDOW IAW AMM 56-12-01-400-801-A01-PSADec 19, 2024 · N630NN · Cndair · Flight Compartment WindowsSDR VNAA2024082711101Steering Sys · malfunctionedSTEERING INOP CAUTION MSG IN FLIGHT. / PERFORMED FUNCTIONAL CHECK OF NOSE WHEEL STEERING IAW CRJ900 AMM 32ˆ’51ˆ’00ˆ’720ˆ’801. OPS CHECK GOOD, NO DEFECTS FOUND AT THIS TIME. ALSO VISUALLY INSP. SURROUNDING NLG COMPONENTS. NO VISUAL DEFECTS NOTED.Aug 24, 2024 · N630NN · Cndair CL6002D24 · Landing Gear Steering System
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