# Service difficulty reports: N568NN A list on [N568NN](https://openairdocs.org/aircraft/N568NN.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VNAA2025112411102](https://openairdocs.org/sdr/VNAA2025112411102.md): Light · sparks · Nov 23, 2025 · N568NN · Cndair CL6002D24 · Flight Compartment Lighting > CA SIDE READING LIGHT SPARKED AND SMOKED. / REMOVED AND REPLACED CA SIDE MAP READING LIGHT IAW AMM 33-13-03-000/400-801. OPS TEST GOOD. - [SDR VNAA2025091111101](https://openairdocs.org/sdr/VNAA2025091111101.md): Fmu · faulted · Sep 7, 2025 · N568NN · Cndair CL6002D24 · Fuel Controlling System > L FADEC MSG IN FLIGHT. / REMOVED AND REPLACED R FADEC IAW AMM 73-21-01-000/400-801. REMOVED AND REPLACED LH ENGINE FMU IAW CRJ 900 AMM 73-21-03-000/400-801.OPS CHECK AND LEAK CHECK GOOD. PERFORMED HIGH POWER RUN IAW CRJ 900 AMM 71-00-00-866-806-A02-PSA. ALL P - [SDR VNAA2024071511101](https://openairdocs.org/sdr/VNAA2024071511101.md): Actuator · unserviceable · Jul 11, 2024 · N568NN · Cndair CL6002D24 · Trailing Edge Flap Actuator > FLAPS FAIL ON FINAL. FLAPS STUCK AT 45 / PERFORMED ELECTRICAL RIGGING OF RH FLAP IAW CRJ 900 AMM 27-52-00-820-802, RIGGING OUT OF TOLERANCES AND ADJUSTED. ON OPS CHECK OF FLAPS NOTED SQUEALING NOISE FROM FLAP PDU AND TORQUE TUBES ATTEMPTING TO GO FURTHER THAN - [SDR VNAA202404170002](https://openairdocs.org/sdr/VNAA202404170002.md): Skin · gouged · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Cargo/Baggage Doors > FWD CARGO DOOR HAS GOUGES AT THE DOOR SKIN EDGE COMMON TO THE LOWER FORWARD AND AFT CORNERS WITHIN SRM REPAIR LIMITS. - [SDR VNAA202404170001](https://openairdocs.org/sdr/VNAA202404170001.md): Fitting · gouged · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings > GOUGE DAMAGE TO LH WING TRAILING EDGE MACHINED FITTINGS AT WS199.40, WS202.67 AND WS231.23) CAUSED BY INCORRECT HARDWARE ORIENTATION. DAMAGE CLASSIFIED AND REPAIRED IAW MHIRJ REO 690-57-51-332 REV --. - [SDR VNAA202404160014](https://openairdocs.org/sdr/VNAA202404160014.md): Skin · gouged · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > NUMEROUS NICKS, GOUGES AND DENTS ON FUSELAGE SKIN BETWEEN FS1031.00 - FS1051.30 AND STR22R - STR25R. DAMAGE CAUSED BY LP PNEUMATIC DUCT PLUG TETHERED BY LANYARD COMING LOOSE IN FLIGHT AND IMPACTING AGAINST THE FUSELAGE REPEATEDLY. CLASSIFIED AND REPAIRED IAW - [SDR VNAA202404160012](https://openairdocs.org/sdr/VNAA202404160012.md): Shelf · cracked · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > SHELF THAT SECURES JB-6 HAS A CRACK IN THE FORWARD RH OUTBOARD CORNER APPROX. 1/4 INCH IN LENGTH - [SDR VNAA202404160008](https://openairdocs.org/sdr/VNAA202404160008.md): Skin Panel · burned · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > LIGHTNING STRIKE DAMAGE (SMALL HOLE IN SKIN PANEL) AT APPROXIMATELY FS 440.0 AND STGR 3R, CLASSIFIED IN MHIRJ REO 690-53-21-1744 - [SDR VNAA202404160007](https://openairdocs.org/sdr/VNAA202404160007.md): Skin · scratched · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SCRATCH IN FUSELAGE SKIN AT APPROXIMATELY FS 310.0 AND STGR 25L. DAMAGE WITHIN SRM ALLOWABLE LIMITS PER 53-21-01-101-002-A04 - [SDR VNAA202404160005](https://openairdocs.org/sdr/VNAA202404160005.md): Seat Track · corroded · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN RH I/B SEAT TRACK P/N SH690-33407-1 HAS CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0 - [SDR VNAA202404160004](https://openairdocs.org/sdr/VNAA202404160004.md): Seat Track · corroded · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN RH I/B SEAT TRACK P/N BA690-31111-1 AND HAS CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0 - [SDR VNAA202404160003](https://openairdocs.org/sdr/VNAA202404160003.md): Seat Track · corroded · Apr 6, 2024 · N568NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN RH I/B SEAT TRACKS P/N SH670-32159-1, BA690-31111-1 AND SH690-33407-1 HAVE CORROSION AROUND MULTIPLE ATTACH FASTENER LOCATIONS THAT ARE OUT OF SRM LIMITS. FS280.00-FS581 RBL 9.0 - [SDR VNAA202404170004](https://openairdocs.org/sdr/VNAA202404170004.md): Bearing · worn · Apr 5, 2024 · N568NN · Cndair CL6002D24 · Rudder Structure > RUDDER FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 1 & 2 PER CRJ 900 AMM TASK 27-21-00-720-803. MAXIMUM ALLOWABLE BACKLASH ON HYDRAULIC SYSTEM 1 IS 0.250". HIGHEST TESTED VALUE WAS 0.395". MAX ALLOWABLE BEARING BACKLASH VALUE IS 0.120", MEASURED VALUE WAS 0.132" - [SDR VNAA202404170003](https://openairdocs.org/sdr/VNAA202404170003.md): Bearing · worn · Apr 5, 2024 · N568NN · Cndair CL6002D24 · Rudder Structure > RUDDER FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 1 & 2 PER CRJ 900 AMM TASK 27-21-00-720-803. MAXIMUM ALLOWABLE BACKLASH ON HYDRAULIC SYSTEM 1 IS 0.250". HIGHEST TESTED VALUE WAS 0.395". MAX ALLOWABLE BEARING BACKLASH VALUE IS 0.120", MEASURED VALUE WAS 0.132" - [SDR VNAA202404160010](https://openairdocs.org/sdr/VNAA202404160010.md): Cowling · dented · Apr 5, 2024 · N568NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > RH NACELLE, I/B SIDE, FAN COWL PANEL (442AB), TOP EDGE OF PANEL DAMAGED (2 DENTS) APPROX. 12" FROM AFT END OF PANEL. DAMAGE CLASSIFIED IN PSA AIRLINES EA A1-690-54-00024 REV A. - [SDR VNAA202404160009](https://openairdocs.org/sdr/VNAA202404160009.md): Fairing · unserviceable · Apr 5, 2024 · N568NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > RH ENGINE, FWD FAN COWL HINGE LINE FAIRING DAMAGED/BENT BEYOND REPAIR LIMITS. (PANEL 442BB) - [SDR VNAA202404160011](https://openairdocs.org/sdr/VNAA202404160011.md): Bracket · cracked · Mar 19, 2024 · N568NN · Cndair CL6002D24 · Service Doors > SERVICE DOOR STABILIZATION BRACKET (P/N CC670-38380-3), CRACKED (UPPER STABILIZER BAR MOUNT AT ROD ATTACH POINT) - [SDR VNAA202404170006](https://openairdocs.org/sdr/VNAA202404170006.md): Bearing · worn · Mar 4, 2024 · N568NN · Cndair CL6002D24 · Elevator Structure > LH ELEVATOR FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 3 PER CRJ900 AMM CH. 27-31-00-720-804. MAXIMUM ALLOWABLE BACKLASH IS 0.070", MEASURED VALUE WAS.090". SPHERICAL BALL P3A3211, AND BUSHING B0309008-08-055 AT LH ELEVATOR, PCU #3 WORN BEYOND LIMITS. - [SDR VNAA202404170005](https://openairdocs.org/sdr/VNAA202404170005.md): Bushing · worn · Mar 4, 2024 · N568NN · Cndair CL6002D24 · Elevator Structure > LH ELEVATOR FAILS BACKLASH CHECK FOR HYDRAULIC SYSTEM 3 PER CRJ900 AMM CH. 27-31-00-720-804. MAXIMUM ALLOWABLE BACKLASH IS 0.070", MEASURED VALUE WAS.090". SPHERICAL BALL P3A3211, AND BUSHING B0309008-08-055 AT LH ELEVATOR, PCU #3 WORN BEYOND LIMITS. - [SDR VNAA202404160006](https://openairdocs.org/sdr/VNAA202404160006.md): Drain · corroded · Feb 28, 2024 · N568NN · Cndair CL6002D24 · Buffet/Galleys > RH FWD GALLEY SERVICE DOOR AFT DRAIN TUBE ASSEMBLY CORRODED THROUGH. - [SDR VNAA202404160013](https://openairdocs.org/sdr/VNAA202404160013.md): Channel · cracked · Feb 26, 2024 · N568NN · Cndair CL6002D24 · Aerodynamic Fairings > WING/FUSELAGE FAIRING, RH (PANEL 196DR) SUPPORT CHANNEL HAS A 1.33" CRACK, 7.4" FROM FWD END OF CHANNEL. PN:BA690-39311-1. - [SDR VNAA202404160002](https://openairdocs.org/sdr/VNAA202404160002.md): Mount Fitting · corroded · Feb 16, 2024 · N568NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > G1 GALLEY HAS 2 CORRODED FLOOR FITTING MOUNTS. FWD OUTBD AND AFT INBD LOCATIONS. - [SDR VNAA202404160001](https://openairdocs.org/sdr/VNAA202404160001.md): Mount Fitting · unserviceable · Feb 16, 2024 · N568NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > FWD LAVATORY FWD OUTBOARD FLOOR MOUNT EXFOLIATING CORROSION THROUGH MOUNT. - [SDR VNAA2023113011102](https://openairdocs.org/sdr/VNAA2023113011102.md): Unknown · unknown · Nov 27, 2023 · N568NN · Cndair CL6002D24 · Air Distribution System > DIRTY SOCK SMELL COMING THRU VENTILATION SYSTEM / PERFORMED POST WASH BLEED DRY OUT PROCEDURE ON L & R BLEEDS IAW CRJ-900 AMM 72-00-00-100-803-A01-PSA STEPS H(6) THROUGH SHUTDOWN. NO ABNORMAL ODORS NOTED AFTER EXTENDED VERIFICATION STEP. - [SDR VNAA202204211111](https://openairdocs.org/sdr/VNAA202204211111.md): Pressure Valve · departed · Apr 17, 2022 · N568NN · Cndair CL6002D24 · Fuselage Main, Structure > THE LOW PRESSURE DOOR WAS LEFT OPEN DEPARTING CLT AND THE LOW PRESSURE VALVE DOOR CAME OFF SOMEWHERE BETWEEN CLT AIRPORT AND JAN AIRPORT. CLT OPS HAS BEEN NOTIFIED OF THE MISSING VALVE COVER AND AIRCRAFT DAMAGE AS WELL. A DENT NEXT TO THE LOW PRESSURE VALVE DO - [SDR VNAA2020090311101](https://openairdocs.org/sdr/VNAA2020090311101.md): Fan · failed · Aug 30, 2020 · N568NN · Cndair CL6002D24 · Air Distribution Fan > RECIRC FAN FAULT STATUS MESSAGE FOLLOWED BY BURNING RUBBER SMELL. TROUBLE SHOT RECIRC FAN FAULT STATUS MESSAGE "RECIRC FAN 2, FAILED WIRING/LOW FAN SPEED" IAW CRJ 900 FIM 21-22-10-810-802-A02. REMOVED AND REPLACED RT RECIRC FAN IAW CRJ 900 AMM 21-22-10-000/4 - [SDR VNAA202006089998](https://openairdocs.org/sdr/VNAA202006089998.md): Intercostal · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > INTERCOSTALS CORRDED. - [SDR VNAA202006089997](https://openairdocs.org/sdr/VNAA202006089997.md): Seat Track · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > FLOOR SEAT TRACK CORRODED AT RBL 9.00 BETWEEN FS 485 AND FS 533.00. - [SDR VNAA202006089996](https://openairdocs.org/sdr/VNAA202006089996.md): Floorbeam · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam > FS 280 CROSSBEAM FWD FLOOR SUPPORT ANGLE BETWEEN LBL 12 AND RBL 12 IS CORRODED. - [SDR VNAA202006089995](https://openairdocs.org/sdr/VNAA202006089995.md): Seat Track · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > FLOOR SEAT TRACK CORRODED AT LBL 27.00 AND BETWEEN FS 364 TO FS 485.00. - [SDR VNAA202006089994](https://openairdocs.org/sdr/VNAA202006089994.md): Seat Track · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > FLOOR SEAT TRACK AT LBL 9.00 AND BETWEEN FS 374.00 TO FS 483 CORRODED IN SEVERAL LOCATIONS. SEAT TRACK REPLACED. - [SDR VNAA202006089993](https://openairdocs.org/sdr/VNAA202006089993.md): Seat Track · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > FLOOR SEAT TRACK CORRODED AT RBL 9.00 AND BETWEEN FS 364 TO FS 483.00. REPLACED SEAT TRACK. - [SDR VNAA202006089992](https://openairdocs.org/sdr/VNAA202006089992.md): Floor Support · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > INTERCOSTALS BELOW FLOOR AT PAX DOOR FROM FS 310.00 TO FS 349.00 ARE CORRODED. REPLACED INTERCOSTALS. - [SDR VNAA202006089991](https://openairdocs.org/sdr/VNAA202006089991.md): Intercostal · corroded · Jun 8, 2020 · N568NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > L/H AND R/H INTERCOSTALS AT STGR 27 BETWEEN FS 349 AND FS 364 ARE CORRODED. REPLACED INTERCOSTALS. - [SDR VNAA2019101411101](https://openairdocs.org/sdr/VNAA2019101411101.md): Acm · failed · Oct 11, 2019 · N568NN · Cndair CL6002D24 · Cabin Cooling System > SMOKE IN CABIN. C/W GVI OF AFT EQUIPMENT BAY IAW CRJ 900 AMM 53-60-01-PSA. NO VISUAL DEFECTS NOTED. T/S PER CRJ 900 FIM 21-22-00-810-806 AND FOUND ISSUE TO BE WITH THE RH PACK. MAINTENANCE REMOVED AND REPLACED R/H AIR CYCLE MACHINE OPS CHECK GOOD AT THIS TIME - [SDR VNAA2019071011103](https://openairdocs.org/sdr/VNAA2019071011103.md): Proximity Sensor · out of adjust · Jul 10, 2019 · N568NN · Cndair CL6002D24 · Landing Gear Position and Warning > IN PREPARATION TO LAND THE CREW RECEIVED A ANTI SKID CAUTION MESSAGE WITH A WOW MESSAGE. THE CREW RAN THE QRH AND WAS NOT ABLE TO RESET THE SYSTEM. THEY DECLARED AN EMERGENCY AND GROUND EMERGENCY EQUIPMENT RESPONDED. THE AIRCRAFT LANDED WITHOUT ISSUE AND WAS - [SDR VNAA2018090711101](https://openairdocs.org/sdr/VNAA2018090711101.md): Warning System · false activation · Sep 7, 2018 · N568NN · Cndair CL6002D24 · Door Warning System > AIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT AND HAD SERVICE DOOR CAUTION LIGHT, THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE / MASKS DID NOT DROP, BUT EQUIPMENT DID ROLL. THE AIRCRAFT TAXIED INTO THE GATE UNDER ITS OWN POWER. MX INSPECTED A/C AND - [SDR VNAA2018031111101](https://openairdocs.org/sdr/VNAA2018031111101.md): Unknown · odor · Mar 11, 2018 · N568NN · Cndair CL6002D24 · Air Distribution System > AFTER PUSHING OFF THE GATE FAS REPORTED AN ODOR IN THE CABIN, LIKE A BURNING MATCH. RETURNED TO THE GATE. MAINTENANCE INSPECTED. FOUND NO EVIDENCE OF SOURCE OF BURNING ODOR. RAN ENGINES, NO ODOR NOTED. - [SDR VNAA2017030100002](https://openairdocs.org/sdr/VNAA2017030100002.md): Lens · missing · Mar 1, 2017 · N568NN · Cndair CL6002D24 · Emergency Lighting > SERVICE DOOR EXIT SIGN LENS IS MISSING. INSTALLED A REPLACEMENT LENS. - [SDR VNAA2016081200011](https://openairdocs.org/sdr/VNAA2016081200011.md): Cover · missing · Aug 12, 2016 · N568NN · Cndair CL6002D24 · Emergency Lighting > GALLEY FLOOR EMERGENCY LIGHT COVER MISSING. MAINTENANCE INSTALLED LENS COVER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016070500009](https://openairdocs.org/sdr/VNAA2016070500009.md): Circuit Breaker · popped · Jul 5, 2016 · N568NN · Cndair CL6002D24 · Emergency Lighting > EMERGENCY LIGHTS ON WITH SWITCH IN ARM POSITION. CREW RESET CIRCUIT BREAKER CBP-2 U3 AND THE ACFT CONTINUED SERVICE. - [SDR VNAA2015102300021](https://openairdocs.org/sdr/VNAA2015102300021.md): Fan · odor · Oct 23, 2015 · N568NN · Cndair CL6002D24 · Air Distribution Fan > SHORTLY AFTER TAKEOFF, CREW REPORTED SMOKE ODOR WHICH PROGRESSIVELY GOT WORSE DURING CLIMBOUT TO 1,000 FT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. TROUBLESHOT, AND FOUND ODOR COMING FROM FORWARD GALLEY EXHAUST FAN. - [SDR VNAA2015071400014](https://openairdocs.org/sdr/VNAA2015071400014.md): Probe · failed · Jul 14, 2015 · N568NN · Cndair CL6002D24 · Landing Gear Position and Warning > CREW REPORTED BRAKE OVERHEAT MESSAGE IN CRUISE AND ON APPROACH. INNER LT BRAKE TEMPERATURE MONITORING SYS, BTMS, INDICATOR WENT TO 20 BOTH TIMES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 2 MLG BRAKE TEMPERATURE PROBE AND PERFORMED CHECK ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N568NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N568NN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.