# Service difficulty reports: N581NN

A list on [N581NN](https://openairdocs.org/aircraft/N581NN.md).

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

- [SDR VNAA2026021014105](https://openairdocs.org/sdr/VNAA2026021014105.md): Exhaust Fan · failed · Mar 9, 2026 · N581NN · Cndair CL6002D24 · Air Distribution Fan
  > BURNING SMELL MID CABIN. UPON INVESTIGATION, SUSPECT SMELL TO BE COMING FROM AFT LAV EXHAUST FAN. UPON REMOVAL AND REPLACEMENT, FOUND FAN MOTOR TO BE SEIZED IAW AMM 21-23-93-000/400-802-A01. LEAK AND OPS CHECKS GOOD. SMELL EXTINGUISHED
- [SDR VNAA2025111011101](https://openairdocs.org/sdr/VNAA2025111011101.md): Warning Message · illuminated · Nov 9, 2025 · N581NN · Cndair CL6002D24 · Service Doors
  > FWD SERVICE DOOR HANDLE CAUTION MSG IN FLIGHT / INTERROGATED MDC FOUND HISTORICAL B1 007792.CHECKED RIG ON PX38 FOUND AT.048. PERFORMED RIG OF PX38 IAW CRJ 900 AMM 52€“70€“06€“820€“802. PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801. OPS CHECK.
- [SDR VNAA2025021011103](https://openairdocs.org/sdr/VNAA2025021011103.md): Light · inoperative · Feb 7, 2025 · N581NN · Cndair CL6002D24 · Flight Compartment Lighting
  > SMOKE COMING FROM FO PANEL BELOW ASHTRAY. THE EVENT LASTED APPROXIMATELY 2-3 MINUTES WITH NO MEDICAL ATTENTION REQUIRED. / REMOVED AND REPLACED FO FLOODLIGHT DS78 IAW CRJ900 AMM 33-11-03-000/400-801-A01.
- [SDR VNAA202407050006](https://openairdocs.org/sdr/VNAA202407050006.md): Skin · dented · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > R/H VENTRAL FIN (FOOTPRINT/FUSELAGE SKIN) HAS MULTIPLE DENTS ACROSS ENTIRE LENGTH, AND MULTIPUL SCRATCHES AT FWD. SECTION BETWEEN 1ST AND 2ND SETS OF NUT PLATE HOLES.
- [SDR VNAA202407050005](https://openairdocs.org/sdr/VNAA202407050005.md): Skin · damaged · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REO 690-53-61-1367 250 FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED GOUGE DAMAGE TO FUSELAGE SKIN BETWEEN FS1015.00-FS1051.30 AND STR22R- STR27 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 250 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO.
- [SDR VNAA202407050004](https://openairdocs.org/sdr/VNAA202407050004.md): Floorbeam · corroded · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > UPON REMOVAL OF CORROSION CAP PLATE FOUND CORROSION ON FS 280 L/H CROSS BEAM BETWEEN BL 0 AND LBL
- [SDR VNAA202407050003](https://openairdocs.org/sdr/VNAA202407050003.md): Floor Support · corroded · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H COCKPIT ENTRY WAY FLOOR ANGLE AND POST IS CORRODED
- [SDR VNAA202407050002](https://openairdocs.org/sdr/VNAA202407050002.md): Floorbeam · cracked · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H COCKPIT FLOOR BEAM IS CRACKED AT FS 280.
- [SDR VNAA202407050001](https://openairdocs.org/sdr/VNAA202407050001.md): Door Frame · corroded · Jul 5, 2024 · N581NN · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H COCKPIT ENTRY WAY POST IS CORRODED
- [SDR VNAA202209011113](https://openairdocs.org/sdr/VNAA202209011113.md): Door · damaged · Sep 1, 2022 · N581NN · Cndair CL6002D24 · Passenger/Crew Doors
  > UPPER LEFT CORNER OF PAX DOOR IS SCUFFED AND SCRATCHED. COMPLIED WITH PERMANENT REPAIR OF UPPER LEFT CORNER OF PAX DOOR IAW EA 22-C9-52-0274 REV C. SECTION 3.
- [SDR VNAA202205031111](https://openairdocs.org/sdr/VNAA202205031111.md): None · none · Apr 30, 2022 · N581NN · Cndair CL6002D24 · Steering Unit
  > INTERROGATED MDC FOUND B1 CODE 007465. REMOVED AND REPLACED NWS MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. PERFORMED OPS TEST OF NWS MANIFOLD IAW CRJ 900 AMM 32-51-50-400-801.OPS CHECK GOOD.
- [SDR VNAA202204221111](https://openairdocs.org/sdr/VNAA202204221111.md): Unknown · odor · Apr 21, 2022 · N581NN · Cndair CL6002D24 · Air Distribution System
  > FA WHILE SEATED SMELLED A BURNING SMELL IN CABIN AFTER TAKE OFF ROLL BELOW 1000FT.CONTINUED TO CLT. SMELL DISSAPATED THROUGH FLIGHT. LANDED W/O INCIDENT. NO COMPLAINTS FROM PAX. BOTH FLIGHT ATTENDANTS SMELLING BURNING RUBBER AFTER TAKEOFF. SMELL DISSIPATED AND
- [SDR VNAA202105111111](https://openairdocs.org/sdr/VNAA202105111111.md): Heater · failed · May 8, 2021 · N581NN · Cndair CL6002D24 · Heating System
  > WHILE ENROUTE TO CLT, THE FLIGHT ATTENDANTS TURNED THE GALLEY SERVICE HEATER ON AND WITHIN A FEW SHORT MINUTES, SMOKE STARTED TO BILLOW OUT OF THE HEATER. IT WAS BAD ENOUGH THAT IT MADE ITS WAY INTO THE COCKPIT. THEY TURNED OFF THE HEATED AND THE SMOKE SLOWLY
- [SDR VNAA202010179993](https://openairdocs.org/sdr/VNAA202010179993.md): Angle · corroded · Oct 17, 2020 · N581NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 FWD "J" ANGLE IS CORRODED.
- [SDR VNAA2020101799903](https://openairdocs.org/sdr/VNAA2020101799903.md): Hinge · corroded · Oct 17, 2020 · N581NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR TOP STEP HINGE IS CORRODED.
- [SDR VNAA202010179992](https://openairdocs.org/sdr/VNAA202010179992.md): Seat Track · corroded · Oct 17, 2020 · N581NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK CORRODED RBL 9 FROM FS 501 TO FS 581. REMOVED AND REPLACED TRACK.
- [SDR VNAA202010179991](https://openairdocs.org/sdr/VNAA202010179991.md): Seat Track · corroded · Oct 17, 2020 · N581NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK IS CORRODED AT RBL 9 FS 349.0 TO FS 501.0. REMOVED RT FLOOR SEAT TRACK. INSTALLED RT FLOOR SEAT TRACK.
- [SDR VNAA2019122871101](https://openairdocs.org/sdr/VNAA2019122871101.md): Acm · failed · Dec 27, 2019 · N581NN · Cndair CL6002D24 · Cabin Cooling System
  > A SMOKE ODOR WAS NOTICED BY THE FAS DURING PUSH BACK AND TAXI OUT. THE PILOTS CONFIRMED SMELL AND DEPLANED IN THE ALLEY WAY THROUGH THE MAIN CABIN DOOR. EVAC ON RAMP DUE TO WHITE SMOKE AND STRONG ODOR IN CABIN. C/W OPERATIONAL TEST OF THE A/C SYSTEM IAW AMM 21
- [SDR VNAA2017111211101](https://openairdocs.org/sdr/VNAA2017111211101.md): Engine · odor · Nov 12, 2017 · N581NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTED AC ESSENTIAL BUSS CAUTION MESSAGE AND GENERATOR 1 FAULT IN FLIGHT. CREW RAN QRH AND ATTEMPTED TO START APU WHICH TOOK THREE ATTEMPTS. FLT DIVERTED, AND DECLARED EMERGENCY. LANDED SAFELY. LT & RT ENGINES HAD COMPRESSOR WASHES DURING OVE

## 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 = 'N581NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N581NN/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.