# Service difficulty reports: N580NN

A list on [N580NN](https://openairdocs.org/aircraft/N580NN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 58 reports

- [SDR VNAA2025102811101](https://openairdocs.org/sdr/VNAA2025102811101.md): Windshield · arced · Oct 26, 2025 · N580NN · Cndair CL6002D24 · Flight Compartment Windows
  > FO 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.
- [SDR VNAA2025102211104](https://openairdocs.org/sdr/VNAA2025102211104.md): Hinge · gouged · Oct 22, 2025 · N580NN · Cndair CL6002D24 · Ailerons
  > FITTING, 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.
- [SDR VNAA2025102211103](https://openairdocs.org/sdr/VNAA2025102211103.md): Hinge · gouged · Oct 22, 2025 · N580NN · Cndair CL6002D24 · Ailerons
  > FITTING, 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.
- [SDR VNAA2025102211102](https://openairdocs.org/sdr/VNAA2025102211102.md): Hinge · gouged · Oct 22, 2025 · N580NN · Cndair CL6002D24 · Ailerons
  > FITTING, 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.
- [SDR VNAA202408090003](https://openairdocs.org/sdr/VNAA202408090003.md): Skin · damaged · Aug 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN BTWN STRG 25L - 26R BTWN FS280.00 - FS333. REPAIRED PER REO 690-53-21-1804 REV. --
- [SDR VNAA202408080004](https://openairdocs.org/sdr/VNAA202408080004.md): Skin · dented · Aug 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENTS 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-A01
- [SDR VNAA202408090009](https://openairdocs.org/sdr/VNAA202408090009.md): Web · cracked · Aug 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
- [SDR VNAA202408090011](https://openairdocs.org/sdr/VNAA202408090011.md): Intercostal · corroded · Jul 31, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 SRM
- [SDR VNAA202408090021](https://openairdocs.org/sdr/VNAA202408090021.md): Angle · corroded · Jul 25, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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-900
- [SDR VNAA202408090026](https://openairdocs.org/sdr/VNAA202408090026.md): Hinge · worn · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Vertical Stabilizer
  > FREE 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.
- [SDR VNAA202408090025](https://openairdocs.org/sdr/VNAA202408090025.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR VNAA202408090024](https://openairdocs.org/sdr/VNAA202408090024.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 (C
- [SDR VNAA202408090023](https://openairdocs.org/sdr/VNAA202408090023.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 53-00
- [SDR VNAA202408090022](https://openairdocs.org/sdr/VNAA202408090022.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 REPLA
- [SDR VNAA202408090020](https://openairdocs.org/sdr/VNAA202408090020.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 CRJ9
- [SDR VNAA202408090019](https://openairdocs.org/sdr/VNAA202408090019.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 CRJ
- [SDR VNAA202408090018](https://openairdocs.org/sdr/VNAA202408090018.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 53-00-49
- [SDR VNAA202408090017](https://openairdocs.org/sdr/VNAA202408090017.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR VNAA202408090016](https://openairdocs.org/sdr/VNAA202408090016.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR VNAA202408090015](https://openairdocs.org/sdr/VNAA202408090015.md): Seat Track · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR VNAA202408090012](https://openairdocs.org/sdr/VNAA202408090012.md): Intercostal · corroded · Jul 4, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 SRM
- [SDR VNAA202408090013](https://openairdocs.org/sdr/VNAA202408090013.md): Floorbeam · corroded · Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION 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 PE
- [SDR VNAA202408090010](https://openairdocs.org/sdr/VNAA202408090010.md): Attach Angle · corroded · Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION 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 2
- [SDR VNAA202408090008](https://openairdocs.org/sdr/VNAA202408090008.md): Skin · damaged · Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING 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-A03
- [SDR VNAA202408090007](https://openairdocs.org/sdr/VNAA202408090007.md): Skin · damaged · Jul 3, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE LIGHTNING STRIKE DAMAGE - TYPE 3: DAMAGE AROUND FASTENER CSK WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202408090014](https://openairdocs.org/sdr/VNAA202408090014.md): Bracket · corroded · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL 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 OF
- [SDR VNAA202408090006](https://openairdocs.org/sdr/VNAA202408090006.md): Access Panel · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Wing, Plate/Skin
  > AILERON POWER CONTROL UNIT AND TENSION REGULATOR ACCESS DOOR (552JB) WAS REPAIRED PER REO 690-57-22-080 REV - -
- [SDR VNAA202408090005](https://openairdocs.org/sdr/VNAA202408090005.md): Skin · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Wing, Plate/Skin
  > IN 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 HO
- [SDR VNAA202408090004](https://openairdocs.org/sdr/VNAA202408090004.md): Skin · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN 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 O
- [SDR VNAA202408090002](https://openairdocs.org/sdr/VNAA202408090002.md): Skin · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN 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 FS28
- [SDR VNAA202408090001](https://openairdocs.org/sdr/VNAA202408090001.md): Skin · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN 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.
- [SDR VNAA202408080005](https://openairdocs.org/sdr/VNAA202408080005.md): Skin · damaged · Jul 2, 2024 · N580NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING 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 --
- [SDR VNAA202408080002](https://openairdocs.org/sdr/VNAA202408080002.md): Drag Angle · cracked · Jun 30, 2024 · N580NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK 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-A01
- [SDR VNAA202408080001](https://openairdocs.org/sdr/VNAA202408080001.md): Drag Angle · cracked · Jun 30, 2024 · N580NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK 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
- [SDR VNAA202408090028](https://openairdocs.org/sdr/VNAA202408090028.md): Aileron · corroded · May 14, 2024 · N580NN · Cndair CL6002D24 · Ailerons
  > CORROSION 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. - -
- [SDR VNAA202408090027](https://openairdocs.org/sdr/VNAA202408090027.md): Hinge Fitting · corroded · May 14, 2024 · N580NN · Cndair CL6002D24 · Ailerons
  > CORROSION 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 --
- [SDR VNAA2024051011101](https://openairdocs.org/sdr/VNAA2024051011101.md): Acm · failed · May 6, 2024 · N580NN · Cndair CL6002D24 · Cabin Cooling System
  > R 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 DEFEC
- [SDR VNAA2024032011101](https://openairdocs.org/sdr/VNAA2024032011101.md): Acm · unserviceable · Mar 17, 2024 · N580NN · Cndair CL6002D24 · Cabin Cooling System
  > SMOKE 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.
- [SDR VNAA2024011911101](https://openairdocs.org/sdr/VNAA2024011911101.md): Warning Message · illuminated · Jan 17, 2024 · N580NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > L 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 AMM
- [SDR VNAA202408080003](https://openairdocs.org/sdr/VNAA202408080003.md): Support · corroded · Jul 1, 2023 · N580NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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-A01
- [SDR VNAA202212161112](https://openairdocs.org/sdr/VNAA202212161112.md): Drain Mast · missing · Dec 14, 2022 · N580NN · Cndair CL6002D24 · Aircraft Fuel Distribution System
  > FWD DRAIN MAST MISSING. REMOVED AND REPLACED FWD FUEL DRAIN MAST IAW CRJ900 AMM 28ˆ’20ˆ’03ˆ’000/400ˆ’802.
- [SDR VNAA2022071213111](https://openairdocs.org/sdr/VNAA2022071213111.md): Acm · smoke · Jul 11, 2022 · N580NN · Cndair CL6002D24 · Cabin Cooling System
  > FA 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 G
- [SDR VNAA202108201114](https://openairdocs.org/sdr/VNAA202108201114.md): Fadec · faulted · Aug 17, 2021 · N580NN · Cndair CL6002D24 · Fuel Controlling System
  > CREW 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 LAN
- [SDR VNAA202108091112](https://openairdocs.org/sdr/VNAA202108091112.md): Exhaust Fan · odor · Aug 6, 2021 · N580NN · Cndair CL6002D24 · Air Distribution Fan
  > PASSENGERS 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 SMELL
- [SDR VNAA202104201111](https://openairdocs.org/sdr/VNAA202104201111.md): Bushing · missing · Apr 16, 2021 · N580NN · Cndair CL6002D24 · Landing Gear Doors
  > NOSE 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 32-22-01-0
- [SDR VNAA202012089991](https://openairdocs.org/sdr/VNAA202012089991.md): Angle · corroded · Dec 8, 2020 · N580NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 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.
- [SDR VNAA2019120541102](https://openairdocs.org/sdr/VNAA2019120541102.md): Warning Message · illuminated · Dec 4, 2019 · N580NN · Cndair CL6002D24 · Landing Gear Steering System
  > NOSE 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 SUCCESSFUL
- [SDR VNAA2019080201](https://openairdocs.org/sdr/VNAA2019080201.md): Tire · failed · Aug 1, 2019 · N580NN · Cndair CL6002D24 · Tire
  > LH MLG TIRE LOST TREAD ON TAKEOFF. REMOVED & REPLACED #2 MLG TIRE & WHEEL ASSY
- [SDR VNAA2019021111102](https://openairdocs.org/sdr/VNAA2019021111102.md): Warning Message · false activation · Feb 11, 2019 · N580NN · Cndair CL6002D24 · Door Warning System
  > CREW 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 AT
- [SDR VNAA2017102501](https://openairdocs.org/sdr/VNAA2017102501.md): Fan · failed · Oct 25, 2017 · N580NN · Cndair CL6002D24 · Air Distribution Fan
  > CREW REPORTED A BURNING ODOR ALONG WITH A RECIRCULATION FAN FAULT MESSAGE DURING TAXI OUT.

Next page: https://openairdocs.org/aircraft/N580NN/reports.md?page=2

## 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 = 'N580NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N580NN/reports

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