# Service difficulty reports: N583NN

A list on [N583NN](https://openairdocs.org/aircraft/N583NN.md).

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

- [SDR VNAA2026031014206](https://openairdocs.org/sdr/VNAA2026031014206.md): Actuator · faulted · Mar 9, 2026 · N583NN · Cndair CL6002D24 · Rudder Control System
  > CAUTION RUDDER LIMITER MSG IN FLIGHT. / REMOVED THE (LH) RTLA 1 FROM STEPS 4A (5) THROUGH COMPLETION AND REPLACED LH RTLA 1 IAW CRJ900 AMM 27-25-03-000/400-801-A04. ALL OPS CHECKED GOOD.
- [SDR VNAA2025042811102](https://openairdocs.org/sdr/VNAA2025042811102.md): Fuel Cap · unsecure · Apr 26, 2025 · N583NN · Cndair CL6002D24 · Fuel Storage
  > RIGHT HAND OVERWING FUELING CAP CAME OPEN IN FLIGHT / INSPECTED RH WING GRAVITY FUEL FILLER CAP IAW CRJ900 AMM 28-11-16-210-801 NO DAMAGE NOTED. INSPECTED RH WING SKIN AROUND FILLER CAP RECEPTICLE NO DAMAGE NOTED. SUMPED RH WING TANK IAW CRJ900 AMM 12-11-28-75
- [SDR VNAA2025021911102](https://openairdocs.org/sdr/VNAA2025021911102.md): Wire Harness · damaged · Feb 16, 2025 · N583NN · Cndair CL6002D24 · Ice/Rain Protection System Wiring
  > L WING A/I CAUTION MSG. DURING CLIMB OUT OF CLT. / REMOVED AND REPLACED LH OUTBOARD TELESCOPIC HARNESS IAW CRJ 900 AMM 30-11-10-000/400-802. OPS CHECK GOOD. NO FURTHER FAULTS FOUND AT THIS TIME.
- [SDR VNAA2025011311103](https://openairdocs.org/sdr/VNAA2025011311103.md): Spoiler Sys · abnormal · Jan 12, 2025 · N583NN · Cndair CL6002D24 · Drag Control System
  > OB SPOILERONS AND OB FLT SPOILERS CAUTION MSG IN FLIGHT. / C/W SYSTEM RESET 5.1.18 PER MIPM AND PERFORMED OPERATIONAL TEST OF THE MFS IAW 900 AMM 27ˆ’62ˆ’01ˆ’710ˆ’801
- [SDR VNAA202407020003](https://openairdocs.org/sdr/VNAA202407020003.md): Web · cracked · Jun 25, 2024 · N583NN · Cndair CL6002D24 · Fuselage Miscellaneous 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 (REO) 670-53-11-509 REV-E.
- [SDR VNAA202407030008](https://openairdocs.org/sdr/VNAA202407030008.md): Floor Support · corroded · Jun 24, 2024 · N583NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH SILL AND DRAIN DISBONDED ON SILL BTW FS 280.00 TO FS295. RH SILL WAS REPAIRED AND DRAIN WAS BONDED ON SILL BTW FS 280.00 TO FS295.00 PER CRJ/900 SRM 53-21-43-201-002-A01
- [SDR VNAA202407030006](https://openairdocs.org/sdr/VNAA202407030006.md): Floorbeam · cracked · Jun 24, 2024 · N583NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1770 REV -.
- [SDR VNAA202407030010](https://openairdocs.org/sdr/VNAA202407030010.md): Strut · corroded · Jun 18, 2024 · N583NN · Cndair CL6002D24 · Main Landing Gear Strut/Axle/Truck
  > AFTER REMOVAL OF MLG PISTON AXLE//CORROSION AT LH MLG CYLINDER THREADS. THE MLG OUTER CYLINDER GLAND NUT THREADS WERE REPAIRED PER REO670-32-11-221 REV.G.
- [SDR VNAA202407020013](https://openairdocs.org/sdr/VNAA202407020013.md): Floorbeam · corroded · Jun 12, 2024 · N583NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FS280 FLOOR PANEL SUPPORT ANGLE. CORROSION ON FS280 FLOOR PANEL SUPPORT ANGLE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED IS OUT LIMITS THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-0
- [SDR VNAA202407020012](https://openairdocs.org/sdr/VNAA202407020012.md): Bracket · corroded · Jun 12, 2024 · N583NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED BRACKETS (6 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. DUE TO NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE, BRACKET MACHINED (6 EAS) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT WERE REPLACED PER SRM 53-32-58-101-0
- [SDR VNAA202407030003](https://openairdocs.org/sdr/VNAA202407030003.md): Seat Track · corroded · Jun 10, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS AT RBL 9.00 FROM FS 349.00 TO FS473.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN. DUE TO EXCESIVE DAMAGE SEAT RAILS AT RBL 9.00 FROM FS 349.00 TO FS473.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM
- [SDR VNAA202407030012](https://openairdocs.org/sdr/VNAA202407030012.md): Lug · corroded · Jun 1, 2024 · N583NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > AFTER BUSHING REMOVAL IN REF CARDTRFKE00BN3Q8:271500-RH-PSA, SCRATCHES ON LUG R5, LUG R6 ON AILERON RH. SCRATCHES ON LUG R5, LUG R6 ON AILERON RH WERE REPAIRED PER REO 670-57-61-237 REV - -
- [SDR VNAA202407030011](https://openairdocs.org/sdr/VNAA202407030011.md): Lug · corroded · Jun 1, 2024 · N583NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > AFTER BUSHING REMOVAL IN REF CARD TRFKE00BN30R:271500-LH-PSA, WEAR ON LUG L2, LUG L5 ON AILERON LH. CORROSION AND WEAR ON LUG L2, LUG L5 ON AILERON LH WERE REPAIRED PER REO 670-57-61-237 REV - - & REO 690-57-61-327 REV. - -
- [SDR VNAA202407030009](https://openairdocs.org/sdr/VNAA202407030009.md): Floorbeam · cracked · May 31, 2024 · N583NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON FLOORBEAM 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 BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR
- [SDR VNAA202407030007](https://openairdocs.org/sdr/VNAA202407030007.md): Hinge · excess play · May 31, 2024 · N583NN · Cndair CL6002D24 · 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 FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.
- [SDR VNAA202407030005](https://openairdocs.org/sdr/VNAA202407030005.md): Seat Track · corroded · May 30, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS AT LBL 27.00 FROM FS 349.00 TO FS 581.00 AT PASSENGER CABIN. FLOOR SEAT RAILS AT LBL 27.00 FROM FS 349.00 TO FS 581.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND SRM 53-21-49-101-001-A
- [SDR VNAA202407030002](https://openairdocs.org/sdr/VNAA202407030002.md): Seat Track · corroded · May 29, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFI
- [SDR VNAA202407030001](https://openairdocs.org/sdr/VNAA202407030001.md): Seat Track · corroded · May 29, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND WERE REPLACED PER
- [SDR VNAA202407020015](https://openairdocs.org/sdr/VNAA202407020015.md): Seat Track · corroded · May 29, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202407020011](https://openairdocs.org/sdr/VNAA202407020011.md): Drag Angle · cracked · May 29, 2024 · N583NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAT
- [SDR VNAA202407020010](https://openairdocs.org/sdr/VNAA202407020010.md): Drag Angle · cracked · May 29, 2024 · N583NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR VNAA202407020009](https://openairdocs.org/sdr/VNAA202407020009.md): Seat Track · corroded · May 28, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). LEFT SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WE
- [SDR VNAA202407020008](https://openairdocs.org/sdr/VNAA202407020008.md): Rib · cracked · May 28, 2024 · N583NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-355 REV.--
- [SDR VNAA202407020007](https://openairdocs.org/sdr/VNAA202407020007.md): Support · cracked · May 28, 2024 · N583NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-020 REV.--
- [SDR VNAA202407020006](https://openairdocs.org/sdr/VNAA202407020006.md): Seal · worn · May 28, 2024 · N583NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > STRIKER SEAL OF CENTER CARGO DOOR CUT OUT FWD FRAME WITHIN 3525.55 FH (BEFORE 19,015.45 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. STRIKER SEAL OF CENTER CARGO DOOR CUT OUT FWD FRAME WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A0
- [SDR VNAA202407020005](https://openairdocs.org/sdr/VNAA202407020005.md): Fireshield · worn · May 28, 2024 · N583NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > RIGHT FWD CORE COWL FIRE SHIELD ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. R/H FWD CORE COWL FIRE SHIELD WAS REPAIRED PER REO N° 690-54-23-382 REV.--
- [SDR VNAA202407020014](https://openairdocs.org/sdr/VNAA202407020014.md): Skin · corroded · May 26, 2024 · N583NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 25 LH. CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 26 LH WAS REPAIRED PER REO 690-53-21-1782 REV -- AND BAY BTW STGR 25LH TO STGR 26LH WAS CLEANED PER CRJ900 SRM
- [SDR VNAA202407020002](https://openairdocs.org/sdr/VNAA202407020002.md): Skin · worn · May 26, 2024 · N583NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-476 REV.
- [SDR VNAA202407020001](https://openairdocs.org/sdr/VNAA202407020001.md): Skin · worn · May 26, 2024 · N583NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-475 REV.--
- [SDR VNAA202407020004](https://openairdocs.org/sdr/VNAA202407020004.md): Skin · nicked · May 24, 2024 · N583NN · Cndair CL6002D24 · Leading Edge Devices
  > PERM REPAIR BEFORE 19,159.54 FH - DISPOSITION FOR TRIMMED NICK DAMAGE ON SLAT TRAILING EDGE BETWEEN SS341.66 - TRACK2-3, LHS THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 800 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV-. SLAT TRAILING ED
- [SDR VNAA202407030004](https://openairdocs.org/sdr/VNAA202407030004.md): Seat Track · corroded · May 14, 2024 · N583NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS AT LBL 9.00 FROM FS 374.00 TO FS485.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN. FLOOR SEAT RAILS AT LBL 9.00 FROM FS 374.00 TO FS485.00 AND FS 581.00 TO 680.00 AT PASSENGER CABIN WERE REPLACED PER CRJ900 AMM 53-00-49.
- [SDR VNAA202307011111](https://openairdocs.org/sdr/VNAA202307011111.md): Pin · unserviceable · Jun 30, 2023 · N583NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > ""HIGH VIBE FAN IN FLIGHT LH ENGINE / REMOVED AND REPLACED ALL FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000-801, 72-21-02-400-801-A01-PSA. PREFORMED ENGINE VIBRATION CHECK IAW CRJ 900 AMM 71-00-00-720-806. N1 91.5 VIBE.3 / VIBRATION CHECK GOOD AT THIS TIME
- [SDR VNAA202202161111](https://openairdocs.org/sdr/VNAA202202161111.md): None · unserviceable · Feb 12, 2022 · N583NN · Cndair CL6002D24 · Powerplant System
  > LH ENG VIBE OUT OF LIMITS ON CLIMBOUT AT LEVEL OFF WE WERE UNABLE TO KEEP VIBE IN LIMITS, VIBE INCREASED WHEN POWER REDUCED, SHUT DOWN L ENGINE / REMOVED AND REPLACED LH ENGINE FAN BLADE RETAINING PINS IAW CRJ900 AMM 72-21-02-000/400-801. PERFORMED VIBE CHECK
- [SDR VNAA2020102311101](https://openairdocs.org/sdr/VNAA2020102311101.md): Battery Pack · discharged · Oct 22, 2020 · N583NN · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF WING INOPERABLE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, IAW CRJ 900 AMM 33-51-17-000/400-801. OPERATIONS CHECK.
- [SDR VNAA2020082011102](https://openairdocs.org/sdr/VNAA2020082011102.md): Window · cracked · Aug 19, 2020 · N583NN · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDOW CRACKED. WHILE IN CRUISE, THE FO SIDE WINDOW SHOWED SIGNS OF CRACKING. AN EMERGENCY WAS DECLARED AND THE FLIGHT DESCENDED TO A LOWER ALTITUDE. FLIGHT CONTINUED ON AND LANDED IN PHL SAFELY. TRUCKS WERE ROLLED AS A PRECAUTION BUT WERE CALLED OFF W
- [SDR VNAA2019102401101](https://openairdocs.org/sdr/VNAA2019102401101.md): Acm · failed · Oct 20, 2019 · N583NN · Cndair CL6002D24 · Cabin Cooling System
  > R PACK AUTO FAIL DUE TO HIGH OUTPUT TEMP. SMELL PRESENT IN CABIN. DEFERRED WITH CREW. MX GAINED ACCESS TO THE AIR CYCLE MACHINES TURBINES TO CONFIRM THAT THEY ARE SEIZED AND CAN'T TURN. MX REPLACED RH AIR CYCLE MACHINE. OPS CHECK GOOD.
- [SDR VNAA2019091311101](https://openairdocs.org/sdr/VNAA2019091311101.md): Bonding Jumper · broken · Sep 13, 2019 · N583NN · Cndair CL6002D24 · Drag Control System
  > DURING APPROACH TO LAND FLIGHT SPOILERS AND SPOILERONS MESSAGE CAME ON. THE CREW FOLLOWED THE QRH AND DECLARED AND EMERGENCY FOR LANDING. NO EMERGENCY EQUIPMENT RESPONDED. FLIGHT LANDED WITHOUT ISSUE AND TAXIED TO THE GATE. MX INSPECTED AIRCRAFT FOUND ELECTRIC
- [SDR VNAA2016042500024](https://openairdocs.org/sdr/VNAA2016042500024.md): Sensor · damaged · Apr 25, 2016 · N583NN · Cndair CL6002D24 · Leading Edge Slat Control System
  > BIRD STRIKE LT L/E OTBD FOLLOWED BY FLAPS HALFSPEED AND SLAT STATUS MESSAGES. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LT OTBD SLAT DISCONNECT SENSOR, AND DEFERED THE FLAP SUB SYS IAW MEL. MAINTENANCE CL

## 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 = 'N583NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N583NN/reports

---
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