# Service difficulty reports: N576NN A list on [N576NN](https://openairdocs.org/aircraft/N576NN.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VNAA2026100826402](https://openairdocs.org/sdr/VNAA2026100826402.md): Washer · disconnected · Oct 8, 2026 · N576NN · Cndair CL6002D24 · Emergency Exits > OVERHEAD BIN INTERFERES WITH L/H AFT OVERWING EMERGENCY EXIT DOOR OPENING / FOUND OVERHEAD BIN EYELET TO BE DISCONNECTED AT L/H AFT EMERGENCY DOOR. RECONNECTED EYELET IAW AMM 25-23-01-400-801-A50-PSA. OPS CHECKS GOOD AT THIS TIME. - [SDR VNAA2026021612503](https://openairdocs.org/sdr/VNAA2026021612503.md): Unknown · odor · Feb 13, 2026 · N576NN · Cndair CL6002D24 · Air Distribution System > BURNING SMELL COMING FROM AFTER CENTER BAGGAGE BAY. PERFORMED GVI OF CTR CARGO IAW AMM 25-50-00-220-801 AND T/S PER FIM 21-22-00-810-806. NO DEFECTS NOTED AT THIS TIME - [SDR VNAA2024091711101](https://openairdocs.org/sdr/VNAA2024091711101.md): Fuel Sys · no discrepancy · Sep 14, 2024 · N576NN · Cndair CL6002D24 · Aircraft Fuel System > SUSPECTED FUEL LEAK IN FLIGHT / PERFORMED ENGINE RUN FOR A DURATION OF 1 HR TO IDENTIFY ANY FUEL LEAKS IAW CRJ 900 AMM 71-00-00-866-806-PSA. STARTING FUEL LEVEL WAS 12330 LBS WITH A BURN RATE OF 1130 PPH AFTER 1 HR OF ENGINE RUN FUEL TOTAL WAS 11320 LBS BURNIN - [SDR VNA20240530001](https://openairdocs.org/sdr/VNA20240530001.md): Support · cracked · May 14, 2024 · N576NN · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM-53-11-43-201-001-A01 - [SDR VNAA20240524004](https://openairdocs.org/sdr/VNAA20240524004.md): Skin · cracked · May 14, 2024 · N576NN · Bombdr CL6002D15 · Trailing Edge Flaps > SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 42 AT RH WING WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LH INBOARD FLAP FLS 42 TO FLS 65.5 WAS EVALUAT - [SDR VNAA20240523010](https://openairdocs.org/sdr/VNAA20240523010.md): Rib · bent · May 14, 2024 · N576NN · Bombdr CL6002D15 · Ailerons > BENDED RIBLET LEADING EDGE ON RH AILERON BTW AILS 337.034 TO AILS 343.534. RIBLET ON LEADING EDGE OF RH AILERON BTW AILS 337.034 TO AILS 343.534 WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR VNAA20240523009](https://openairdocs.org/sdr/VNAA20240523009.md): Hinge Fitting · excess play · May 13, 2024 · N576NN · Bombdr CL6002D15 · Vertical Stabilizer > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B - [SDR VNAA20240523007](https://openairdocs.org/sdr/VNAA20240523007.md): Canister · cracked · May 13, 2024 · N576NN · Bombdr CL6002D15 · Wing Miscellaneous Structure > DISCREPANCY: CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -- - [SDR VNAA20240524007](https://openairdocs.org/sdr/VNAA20240524007.md): Bracket · corroded · May 10, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION ON MACHINED BRACKET (2 EAS) AT FS 629.00 AND FS 549.00 BTW STGR 27 TO STGR 26LH. DUE TO NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE, BRACKET MACHINED (2 EA'S) AT FS 629.00 AND FS 549.00 BTW STGR 27 TO STGR 26LH WERE REPLACED PER CRJ9 - [SDR VNAA20240523001](https://openairdocs.org/sdr/VNAA20240523001.md): Seat Track · corroded · Apr 29, 2024 · N576NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > INITIAL INSPECTION: CORROSION ON SEAT RAILS LBL9 BTW FS 364.00 TO FS 485.00 (1EA) AND FS 581.00 TO FS 693.00 (2EA) AT PASSENGER CABIN. FS 64 TO FS 485 (1EA) AND FS 581.00 TO FS 693.00 (2EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 - [SDR VNAA20240523008](https://openairdocs.org/sdr/VNAA20240523008.md): Floor Support · corroded · Apr 25, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REMOVED PER CRJ900 SRM 5 - [SDR VNAA20240523002](https://openairdocs.org/sdr/VNAA20240523002.md): Floor Support · corroded · Apr 25, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTM - [SDR VNAA20240523006](https://openairdocs.org/sdr/VNAA20240523006.md): Canister · cracked · Apr 23, 2024 · N576NN · Bombdr CL6002D15 · Wing Miscellaneous Structure > CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -- - [SDR VNAA20240523005](https://openairdocs.org/sdr/VNAA20240523005.md): Seat Track · corroded · Apr 23, 2024 · N576NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SIDE SEAT RAILS STGR15 LH (2EAS) AND STGR15 RH (2EAS) BTW FS 668 TO FS 847. CORROSION ON SIDE SEAT RAILS STGR15 LH (2EAS) AND STGR15 RH (2EAS) BTW FS 668 TO FS 847 WAS EVALUATED OUT OF LIMITS PER CRJ/900 SRM 53-41-49-101-001-A02 AND WERE REPLACE - [SDR VNAA20240523004](https://openairdocs.org/sdr/VNAA20240523004.md): Floorbeam · cracked · Apr 23, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam > CRACKED CENTER COCKPIT FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1741 R - [SDR VNAA202405240010](https://openairdocs.org/sdr/VNAA202405240010.md): Floorbeam · cracked · Apr 22, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam > CRACK ON ANGLE TO ATTACH CROSSBEAM AND INTERCOSTAL RBL12 FS280 AT FLOOR INTERNAL STRUCTURE. ANGLE TO ATTACH CROSSBEAM AND INTERCOSTAL RBL12 FS280 AT FLOOR INTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR VNAA20240524009](https://openairdocs.org/sdr/VNAA20240524009.md): Stiffener · damaged · Apr 22, 2024 · N576NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure > BULLET FAIRING STIFFENER, LHS WITHIN 1100 FH, REPAIR OR REPLACE DISCREPANT PART PER APPROVED PROCEDURES. NEW BULLET FAIRING STIFFENER WITH P/N AV670-21650-005 IT WAS VERIFIED PER CRJ-900 IPC 55-32-86. - [SDR VNAA20240524001](https://openairdocs.org/sdr/VNAA20240524001.md): Rib · cracked · Apr 22, 2024 · N576NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead > CRACK ON INB MACHINED RIB LH AT TRAILING EDGE ON WS 148.00. CRACK ON INB MACHINED RIB LH AT TRAILING EDGE ON WS 148.00 WAS REPAIRED PER REO 690-57-51-352 REV--. - [SDR VNAA20240524008](https://openairdocs.org/sdr/VNAA20240524008.md): Bracket · damaged · Apr 19, 2024 · N576NN · Bombdr CL6002D15 · Leading Edge Devices > PERMANENT REPAIR - BLEED DETECTION LOOP BRACKET FASTENER HOLE ELONGATED IN LH #3 SLAT ACCOMPLISH PERMANENT REPAIR PER EA 21-C9-57-141 REV C. BLEED DETECTION LOOP BRACKET FASTENER HOLE ELONGATED IN LH #3 SLAT WAS REPAIRED PER REO 690-57-42-1059 REV. -- AND - [SDR VNAA20240524006](https://openairdocs.org/sdr/VNAA20240524006.md): Skin · worn · Apr 19, 2024 · N576NN · Bombdr CL6002D15 · Wing, Plate/Skin > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-463 REV -- - [SDR VNAA20240524003](https://openairdocs.org/sdr/VNAA20240524003.md): Skin · nicked · Apr 19, 2024 · N576NN · Bombdr CL6002D15 · Trailing Edge Flaps > SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 45 AT LH WING WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LH INBOARD FLAP FLS 45 TO FLS 65.5 WAS EVALUATED W - [SDR VNAA20240524002](https://openairdocs.org/sdr/VNAA20240524002.md): Skin · nicked · Apr 19, 2024 · N576NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin > SEVERAL NICKS ON FUSELAGE SKIN BTW FS 1027.00 TO FS 1047.00 AND STGR 22RH TO STGR 27. NICKS ON FUSELAGE SKIN BTW FS 1027.00 TO FS 1047.00 AND STGR 22RH TO STGR 27 WAS REPAIRED PER REO REO 690-53-61-1390 REV - - - [SDR VNAA20240524005](https://openairdocs.org/sdr/VNAA20240524005.md): Skin · worn · Apr 14, 2024 · N576NN · Bombdr CL6002D15 · Wing, Plate/Skin > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-461 REV.-- - [SDR VNAA202302271113](https://openairdocs.org/sdr/VNAA202302271113.md): None · none · Feb 24, 2023 · N576NN · Cndair CL6002D24 · Engine (Turbine/Turboprop) > POSSIBLE ENGINE 1 FLAMEOUT ON TAKE OFF. ENGINE FLAMEOUT/ REJECT REPORTED BY AIRCRAFT BEHIND-NO EICAS FLAMEOUT REPORTED CREW NOTED SLIGHT JERK AND THEN AIRCRAFT RECOVERED, INDICATIONS LOOKED NORMAL / RTO WAS 70 KTS OR LESS / REMOVED AND REPLACED LH ENGINE IAW C - [SDR VNAA202211171111](https://openairdocs.org/sdr/VNAA202211171111.md): Windshield · cracked · Nov 14, 2022 · N576NN · Cndair CL6002D24 · Flight Compartment Windows > ON DECENT THROUGH 13,000 FT CA WINDSHIELD CRACKED / REMOVED AND REPLACED CAPTAIN WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK OF TEMP CONTROLLER AND LEAK CHECK OF WINDSHIELD REQUIRED. OPERATIONAL CHECK OF LH WINDSHIELD TEMP CONTROLLER IS - [SDR VNAA202211161111](https://openairdocs.org/sdr/VNAA202211161111.md): Pseu · faulted · Nov 13, 2022 · N576NN · Cndair CL6002D24 · Cargo/Baggage Doors > AFT CARGO DOOR CAUTION MSG, PASSENGER DOOR WARNING MESSAGE, AND PROX SYS FAULT 1 STATUS MSG IN FLIGHT. C/W QRC AND QRH PROCEDURE. MESSAGES REMAINED FOR DURATION OF FLIGHT / REMOVED AND REPLACED PSEU IAW CRJ 900 AMM 32-61-01-000/400-801-A01. PERFORMED POWER-UP - [SDR VNAA202103241112](https://openairdocs.org/sdr/VNAA202103241112.md): Cam · unserviceable · Mar 22, 2021 · N576NN · Cndair CL6002D24 · Landing Gear Position and Warning > ON DEPATURE OUT OF CLT, CREW RECIEVED A GEAR DISAGREE, WEIGHT ON WHEEL AND NOSE WHEEL INOP MESSAGE. THEY FOLLOWED THERE QRH AND RETURNED TO CLT. THEY DID CALL FOR AN EMERGENCY AND HAD THE EMERGENCY VEHICLES STANDING BY. THEY LANDED WITHOUT INCIDENT AND THEY WE - [SDR VNAA202101261112](https://openairdocs.org/sdr/VNAA202101261112.md): Acm · failed · Jan 25, 2021 · N576NN · Cndair CL6002D24 · Cabin Cooling System > WHILE TAXIING TO 36R THE FA REPORT TO THE CAPTAIN ABOUT SMOKE IN THE CABIN. THE CAPTAIN AND FO STARTED SMELLING BURNT RUBBER IN THE COCKPIT. PILOT TURNED OFF THE PACK AND DECIDED TO RETURN TO GATE. THE SMOKE CLEARED BY THE TIME THEY GOT BACK TO THE GATE. I - [SDR VNAA202006239993](https://openairdocs.org/sdr/VNAA202006239993.md): Seat Track · corroded · Jun 23, 2020 · N576NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > RH SIDE SEAT RAIL BEGINNING AT APPROX FS 744.5 CORRODED IN SEVERAL LOCATIONS. - [SDR VNAA202006239992](https://openairdocs.org/sdr/VNAA202006239992.md): Seat Track · corroded · Jun 23, 2020 · N576NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > LH SIDE SEAT RAIL BEGINNING AT APPROX FS 744.5 CORRODED IN SEVERAL LOCATIONS. REPLACED SEAT RAIL. - [SDR VNAA202006239991](https://openairdocs.org/sdr/VNAA202006239991.md): Seat Track · corroded · Jun 23, 2020 · N576NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 421 TO FS 437. REPLACED SEAT TRACK. - [SDR VNAA2020062111101](https://openairdocs.org/sdr/VNAA2020062111101.md): Contact · not seated · Jun 20, 2020 · N576NN · Cndair CL6002D24 · Light System Wiring > EMERGENCY LIGHTS FROM OVERWING EXITS AFT WILL ONLY ILLUMINATE WHEN POWER IS TURNED OFF. AFTER FURTHER TROUBLESHOOTING, FOUND PIN N AT OVERHEAD BIN CONNECTOR P5418 PUSHED BACK AND NOT LOCKED IN. (ARM DISABLE LINE FOR BATTERY PACKS #3 & #4). FULLY SEATED CONTACT - [SDR VNAA2019011611101](https://openairdocs.org/sdr/VNAA2019011611101.md): Ecu · failed · Jan 16, 2019 · N576NN · Cndair CL6002D24 · Steering Unit > THE CREW RECEIVED A "STEERING INOP" MESSAGE AFTTER TAKEOFF FROM DCA. THEY DISCUSSED THE ISSUE WITH THEIR DISPATCHER AND DECIDED TO CONTINUE TO PNS AND LANDED WITHOUT FURTHER INCIDENT. TRUCKS WERE ROLLED BUT THE CABIN WAS NOT BRACED. MX REPLACED THE NWS ECU. - [SDR VNAA2017071000002](https://openairdocs.org/sdr/VNAA2017071000002.md): Unknown · odor · Feb 10, 2017 · N576NN · Cndair CL6002D24 · Air Distribution System > RUBBER SMELL AND SMOKE AROUND ROW 8. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. - [SDR VNAA2016062300026](https://openairdocs.org/sdr/VNAA2016062300026.md): Sensor · faulty · Jun 23, 2016 · N576NN · Cndair CL6002D24 · Cabin Cooling System > RIGHT TEMP CAUTION MESSAGE IN FLIGHT. THE CREW DIVERTED TO NEAREST SUITABLE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, DEFERRED THE RT PACK AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE. REMOVED AND REPLACED RIGHT HAND PA - [SDR VNAA2016020300006](https://openairdocs.org/sdr/VNAA2016020300006.md): Sign · detached · Feb 3, 2016 · N576NN · Cndair CL6002D24 · Emergency Lighting > CREW REPORTED, EXIT SIGN FROM MAIN CABIN DOOR IS MISSING. MAINTENANCE INSPECTED, AND RESECURED EXIT SIGN. MAINTENANCE PERFORMED CHECKS IAW AMM AND THE ACFT WAS RELEASED FOR SERVICE. ## 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 = 'N576NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N576NN/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.