N580NN

Service difficulty reports · 58

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 = 'N580NN' 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 VNAA2025102811101Windshield · arcedFO WINDSHIELD ARCED / REMOVED AND REPLACED THE COPILOT SIDE WINDSHIELD IAW AMM 56-11-01-000/400-801-A01-PSA. OPS CK AND LEAK CK GOOD IAW AMM 30-41-06-710-801-A01 AND AMM 21-31-00-910-801-A02-PSA RESPECTIVELY.Oct 26, 2025 · N580NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2025102211104Hinge · gougedFITTING, AILERON, HINGE NO. 3 GOUGE DAMAGE. / VERIFIED PERM REPAIR OF THE RH AILERON HINGE FITTING NO. 3 IAW EA 57-2025-0822-A. DETAILS ON FILE FORM 337 COMPLETED. NO FURTHER DEFECTS NOTED AT THIS TIME.Oct 22, 2025 · N580NN · Cndair CL6002D24 · AileronsSDR VNAA2025102211103Hinge · gougedFITTING, AILERON, HINGE NO. 2 GOUGE DAMAGE. / VERIFIED PERM REPAIR OF THE RH AILERON HINGE FITTING NO. 2 IAW EA 57-2025-0824-A. DETAILS ON FILE FORM 337 COMPLETED. NO FURTHER DEFECTS NOTED AT THIS TIME.Oct 22, 2025 · N580NN · Cndair CL6002D24 · AileronsSDR VNAA2025102211102Hinge · gougedFITTING, INBOARD, AILERON, HINGE NO. 4 GOUGE DAMAGE. / VERIFIED PERM REPAIR OF THE RH AILERON HINGE FITTING NO. 4 IAW EA 57-2025-0825-A. DETAILS ON FILE FORM 337 COMPLETED. NO FURTHER DEFECTS NOTED AT THIS TIME.Oct 22, 2025 · N580NN · Cndair CL6002D24 · AileronsSDR VNAA202408090003Skin · damagedFUSELAGE LOWER SKIN BTWN STRG 25L - 26R BTWN FS280.00 - FS333. REPAIRED PER REO 690-53-21-1804 REV. --Aug 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408080004Skin · dentedDENTS TO FUSELAGE SKIN BETWEEN FS193.00 - FS202.75. FUSELAGE SKIN BETWEEN FS193.00 - FS202.75 WAS REPLACED PER REO 690-53-11-1812 REV.-- AND CRJ-900 SRM 51-42-06-001-001-A01Aug 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408090009Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.Aug 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202408090011Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. DUE TO DAMAGES WERE NOT ALLOWABLE ON INTERCOSTALS PER CRJ900 SRM 53-21-23-101-003-A02, WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRMJul 31, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202408090021Angle · corrodedCORROSION ON ANGLE MOUNTING BTW FS 310.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE MOUNTING BTW FS 310.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND CRJ-900Jul 25, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202408090026Hinge · wornFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103. REV.B.Jul 4, 2024 · N580NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202408090025Seat Track · corrodedCORROSION ON SEAT RAILS BTW FS=693 TO FS=847, RBL9/LBL9. SEAT RAILS BTW FS=693 TO FS=847, RBL9/LBL9 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090024Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS=669.40 TO FS=977.00, STGR 15 LH AND 15RH. SIDE SEAT RAILS BTW FS=669.40 TO FS=977.00, STGR 15 LH AND 15RH WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02, AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CJul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090023Seat Track · corrodedCORROSION ON SEAT RAIL (SEVERAL LOCATIONS) LBL27 BTW FS927.00 TO FS 977.00 AT PASSENGER CABIN. SEAT RAIL LBL27 BTW FS927.00 TO FS 977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090022Seat Track · corrodedCORROSION ON SEAT RAILS (SEVERAL LOCATIONS) LBL 9 AND RBL 9 BTW FS 874.00 TO FS 977.00 AT PASSENGER CABIN. SEAT RAILS LBL 9 AND RBL 9 BTW FS 874.00 TO FS 977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLAJul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090020Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.00 TO FS 677.00 RBL 9.00 AT CABIN PAX. SEAT RAIL BTW FS 477.00 TO FS 677.00 RBL 9.00 AT CABIN PAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ9Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090019Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.00 TO FS 677.00 LBL 9.00 AT CABIN PAX. SEAT RAIL BTW FS 477.00 TO FS 677.00 LBL 9.00 AT CABIN PAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJJul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090018Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 LH/RH BTW FS 379 TO FS 720.85. SIDE SEAT RAIL STGR 15 LH/RH BTW FS 379 TO FS 720.85 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090017Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL AT LBL27.00 FROM FS 349.00 TO FS 581.00 CPAX. FLOOR SEAT RAIL AT LBL27.00 FROM FS 349.00 TO FS 581.00 CPAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49(CONFIG.A12)Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090016Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL AT LBL 9.00 FROM FS 349.00 TO FS 477.00 CPAX. FLOOR SEAT RAIL AT LBL 9.00 FROM FS 349.00 TO FS 477.00 CPAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090015Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 477.00 CPAX. FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 477.00 CPAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202408090012Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRMJul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202408090013Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PEJul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202408090010Attach Angle · corrodedCORROSION ON ANGLE ATTACHED TO STRINGER 26LH (2EA) IN STA. FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT.(E/E) WA REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND ANGLE ATTACHED TO STRINGER 2Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR VNAA202408090008Skin · damagedLIGHTNING DAMAGE TO 3 RIVETS BETWEEN FS 501 - FS 517 AND BETWEEN SGTR 24RH - STGR 25 RH (RFTS-111818 REV.1) WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408090007Skin · damagedFUSELAGE LIGHTNING STRIKE DAMAGE - TYPE 3: DAMAGE AROUND FASTENER CSK WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408090014Bracket · corrodedINITIAL INSPECTION: CORROSION ON BRACKET MACHINED (8 EAS) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/22LH AND FS501.00 TO FS661.00+32.00. BRACKETS MACHINED (8EAS) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO WERE EVALUATED OUT OFJul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202408090006Access Panel · damagedAILERON POWER CONTROL UNIT AND TENSION REGULATOR ACCESS DOOR (552JB) WAS REPAIRED PER REO 690-57-22-080 REV - -Jul 2, 2024 · N580NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202408090005Skin · damagedIN REF TO TRFKE00BX31E: PERM REPAIR BEFORE 19,649.07 FH - TEMPORARY DISPOSITION FOR BLENDED LIGHTNING STRIKE DAMAGE TO LOWER FWD AND CENTER WING PLANKS BETWEEN WS29.76-WS48.95 & STGR22-31, LHS THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1130 FLIGHT HOJul 2, 2024 · N580NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202408090004Skin · damagedIN REF TO TRFKE00BXVFS: PERM REPAIR BEFORE 19,849.07 FH - TEMPORARY DISPOSITION FOR BLENDED LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BTW FS349.00 - FS409.00 & BTW STR25L - STR27 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1130 FLIGHT HOURS FROM TIME OJul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408090002Skin · damagedIN REF TO TRFKE00BXNV6: 1600FH PERM REPAIR - TEMPORARY DISPOSITION FOR LIGHTNING STRIKE DAMAGE BLEND-OUT TO SIDE WINDOW FRAME SECTOR AT FS280.00 BTW STR9R - STR10R WITHIN 1600FH, PERFORM A PERM REPAIR IAW APPROVED PROCEDURES. SIDE WINDOW FRAME SECTOR AT FS28Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408090001Skin · damagedIN REF TO TRFKE00BX2L1: 1200FH PERM REPAIR - TEMPORARY DISPOSITION FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS533.0 - FS549.0 AND STR24R - STR25R VISUALLY INSPECT REWORKED AREA FOR ANY DAMAGE PROPAGATION AT INTERVALS NOT TO EXCEED 400 FLIGHT HOURS.Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408080005Skin · damagedLIGHTNING STRIKE TO FUSELAGE SKIN BETWEEN FS169.00 - FS173.00 & BL0.0 - LBL7.5. LIGHTNING STRIKE TO FUSELAGE SKIN BETWEEN FS169.00 - FS173.00 & BL0.0 - LBL7.5 WAS REPAIRED PER REO 690-53-11-1803. REV --Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202408080002Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01Jun 30, 2024 · N580NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202408080001Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM . CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WERE Jun 30, 2024 · N580NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202408090028Aileron · corrodedCORROSION AND WEAR ON LUG BORE OF R1, R2, R5 AND R6 OF CENTER HINGE FITTINGS OF RIGHT AILERON. LUG BORE OF R1, R2, R5 AND R6 OF CENTER HINGE FITTINGS OF RIGHT AILERON WERE REPAIRED PER REO 670-57-61-237 REV. - -May 14, 2024 · N580NN · Cndair CL6002D24 · AileronsSDR VNAA202408090027Hinge Fitting · corrodedCORROSION AND WEAR WERE FOUND ON LUG BORE OF L2, L4 AND L5 OF CENTER HINGE FITTINGS OF LEFT AILERON. LUG BORE OF L2, L4 AND L5 OF CENTER HINGE FITTINGS OF LEFT AILERON WERE REPAIRED PER REO 670-57-61-237 REV --May 14, 2024 · N580NN · Cndair CL6002D24 · AileronsSDR VNAA2024051011101Acm · failedR PACK AUTO FAIL CAUTION MSG AFTER LANDING ACCOMPANIED WITH CLEAR FOG AND BURNT METAL SMELL. R PACK TEMP SHOWS 99 WILL NOT COOL AUTO/MAN / REMOVED AND REPLACED RIGHT SIDE AIR CYCLE MACHINE IAW CRJ-900 AMM 21-51-08-000/400-801 A01. OPERATIONAL NORMAL, NO DEFECMay 6, 2024 · N580NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA2024032011101Acm · unserviceableSMOKE IN THE CABIN JUST BEFORE TAKE OFF FOLLOWED BY R PACK AUTO FAIL CAUTION MSG / REMOVED AND REPLACED RH AIR CYCLE MACHINE IAW CRJ 900 AMM 21-51-08-000/400-801-A01. OPS AND LEAK CHECKS GOOD.Mar 17, 2024 · N580NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA2024011911101Warning Message · illuminatedL W/SHLD HEAT CAUTION QRH RESET 6-8 RESET SWITCH CAUTION CLEARED BUT STRONG ELECTRIC BURN SMELL / INSP LEFT WINDSHIELD FOR ELEC SMELL AND DAMAGE IAW CRJ 900 FIM 21-21-00-810-806-A01 NO DEFECTS NOTED ALSO SWAPPED TO SPARE SENSOR ON LH WINDSHIELD IAW CRJ 900 AMMJan 17, 2024 · N580NN · Cndair CL6002D24 · Windshield/Door Rain/Ice RemovalSDR VNAA202408080003Support · corrodedCORROSION ON LOWER SILL BTW FS1000 AND FS1047 STGR 17 AT SURROUND STRUCTURE OF THE AFT BAGGAGE-BAY DOOR CUT OUT WAS REMOVED AND LOWER SILL WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-61-23-201-001-A01Jul 1, 2023 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202212161112Drain Mast · missingFWD DRAIN MAST MISSING. REMOVED AND REPLACED FWD FUEL DRAIN MAST IAW CRJ900 AMM 28ˆ’20ˆ’03ˆ’000/400ˆ’802.Dec 14, 2022 · N580NN · Cndair CL6002D24 · Aircraft Fuel Distribution SystemSDR VNAA2022071213111Acm · smokeFA REPOTTED WHITE SMOKE IN CABIN AS SOON PLANE CLEARED THE RWY. CA TURNED OFF THE RH HAND PACK OFF AND SMOKE STARTED TO DISSIPATE. CREW CALLED ATC TO SEE IF THEY SEE ANY SMOKE ON THE OUTSIDE OF THE PLANE AFTER ATC CONFIRMED NO SMOKE CREW CONTINUED TO TAXI TO GJul 11, 2022 · N580NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202108201114Fadec · faultedCREW RECEIVED A LEFT FADEC AMBER CAUTION MESSAGE AFTER DEPARTURE FROM BGR, QRH INSTRUCTED THEM TO LAND AT NEAREST SUITABLE AIRPORT. AFTER CONSULTING DISPATCH CREW DECIDED TO DIVERT TO PWM. CREW DECLARED EMERGENCY, POWERED LEFT ENGING DOWN TO IDLE. AIRCRAFT LANAug 17, 2021 · N580NN · Cndair CL6002D24 · Fuel Controlling SystemSDR VNAA202108091112Exhaust Fan · odorPASSENGERS HAD TO DEPLANE AFTER BOARDING BUT BEFORE PUSHBACK DUE TO SMOKE IN THE AFT CABIN. MAINTENANCE REPORTED THAT THERE WAS ALSO A BURNING SMELL. ENGINES WERE OFF, APU BLEEDS ONLY. NO INJURIES. FLIGHT IS BEING SWAPPED TO A DIFFERENT AIRCRAFT. BURNING SMELLAug 6, 2021 · N580NN · Cndair CL6002D24 · Air Distribution FanSDR VNAA202104201111Bushing · missingNOSE DOOR OPEN RED MSG AFTER TAKEOFF. RAN QRH CHECKLIST PROX SYS FAULT STATUS MSG ALSO CAME ON / INSPECTED NOSE LANDING GEAR DOORS. FOUND MULTIPLE BUSHINGS MISSING ON THE MOUNTING POINTS FOR BOTH FORWARD NLG DOORS. INSTALLED BUSHINGS IAW CRJ 900 AMM 32-22-01-0Apr 16, 2021 · N580NN · Cndair CL6002D24 · Landing Gear DoorsSDR VNAA202012089991Angle · corrodedFS 280 FWD J ANGLE HAS AREAS OF CORROSION. REMOVE, DRILLED AND INSTALLED NEW J ANGLE, IAW CRJ900 SRM 51-42-21, SRM 51-40-11 AND SRM 51-22-06.Dec 8, 2020 · N580NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA2019120541102Warning Message · illuminatedNOSE WHEEL STEERING INOP MESSAGE ON TAKE OFF, CAPT WAS CONCERNED WITH GUSTING WINDS IN CVG SO RTF IN CLT, THIS IS A REPEAT ITEM WITH THIS AC SO WE SWAPPED TO ANOTHER AC AND WILL CONTINUE THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY AND WAS ABLE DO A SUCCESSFULDec 4, 2019 · N580NN · Cndair CL6002D24 · Landing Gear Steering SystemSDR VNAA2019080201Tire · failedLH MLG TIRE LOST TREAD ON TAKEOFF. REMOVED & REPLACED #2 MLG TIRE & WHEEL ASSYAug 1, 2019 · N580NN · Cndair CL6002D24 · TireSDR VNAA2019021111102Warning Message · false activationCREW RECEIVED FWD CARGO DOOR CAUTION MESSAGE. AFTER CHECKING QRH CREW DIVERTED TO TRI AS THE NEAREST SUITABLE AIRPORT. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT ISSUE. C/W OPERATIONAL TEST OF FWD BAGGAGE BAY DOOR AND PRESSURE CHECK, OPS CHECK GOOD ATFeb 11, 2019 · N580NN · Cndair CL6002D24 · Door Warning SystemSDR VNAA2017102501Fan · failedCREW REPORTED A BURNING ODOR ALONG WITH A RECIRCULATION FAN FAULT MESSAGE DURING TAXI OUT.Oct 25, 2017 · N580NN · Cndair CL6002D24 · Air Distribution Fan
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