# Service difficulty reports: N589NN

A list on [N589NN](https://openairdocs.org/aircraft/N589NN.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 · 62 reports

- [SDR VNAA2026061619002](https://openairdocs.org/sdr/VNAA2026061619002.md): Diode · faulted · Jun 14, 2026 · N589NN · Cndair CL6002D24 · DC Power Distribution System
  > DC EMERGENCY BUSS CAUTION MSG IN FLIGHT. REMOVED AND REPLACED EMERGENCY BUSS DIODE (CR82) IAW AMM 24-61-01-000-400-801-A01. OPS CHECKED GOOD.
- [SDR VNAA2025072211101](https://openairdocs.org/sdr/VNAA2025072211101.md): Actuator · failed · Jul 18, 2025 · N589NN · Cndair CL6002D24 · Trailing Edge Flap Actuator
  > FLAPS FAIL ON TAKE OFF. COMPLETED INSTALL OF LH #3 FLAP ACTUATOR IAW CRJ 900 AMM 27-52-09-400-803 AND LH #4 FLAP ACTUATOR IAW AMM 27-52-09-400-804. OPS CHECK GOOD.
- [SDR VNAA2025070911101](https://openairdocs.org/sdr/VNAA2025070911101.md): Actuator · tripped · Jul 6, 2025 · N589NN · Cndair CL6002D24 · Trailing Edge Flap Actuator
  > RTF-FLAPS FAIL CAUTION MSG ON TAKE OFF. / FOUND B1 CODE 006551. CLEARED INHIBITS AND SELF TEST FOR SFECU PASSED IAW CRJ 900 AMM 45-45-00-970-821. FOUND LH OB INB FLAP ACTUATOR TRIPPED. RESET THE TRIPPED ACTUATOR IAW CRJ 900 AMM 27-52-09-610-802. PERFORMED OPS
- [SDR VNAA2025022811103](https://openairdocs.org/sdr/VNAA2025022811103.md): Flap System · malfunctioned · Feb 24, 2025 · N589NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > ON APPROACH TO GPT, PILOTS MOVED THE FLAP LEVER TO 8 AND GOT A STICK SHAKER FOLLOWED BY A STICK PUSHER. PILOTS WERE ABLE TO MANUALLY PULL THE NOSE UP FROM A DIVE DOWN SCENARIO. PILOTS DISCONNECTED THE STICK PUSHER SWITCHES AND BEGAN TO CLIMB PERFORMING A GO AR
- [SDR VNAA202410210034](https://openairdocs.org/sdr/VNAA202410210034.md): Drip Tray · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH TRAY DRIP ASSY. RH TRAY DRIP ASSY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01.
- [SDR VNAA202410210033](https://openairdocs.org/sdr/VNAA202410210033.md): Lug · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WAS FOUND. CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV-.
- [SDR VNAA202410210032](https://openairdocs.org/sdr/VNAA202410210032.md): Lug · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Ailerons
  > "DESCRIPTION: CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WAS FOUND. HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--"
- [SDR VNAA202410210031](https://openairdocs.org/sdr/VNAA202410210031.md): Skin · dented · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > " SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH.WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-580 REV."
- [SDR VNAA202410210030](https://openairdocs.org/sdr/VNAA202410210030.md): Skin · dented · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-579 REV."
- [SDR VNAA202410210029](https://openairdocs.org/sdr/VNAA202410210029.md): Floor Support · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CRACK ON FLOOR SUPPORT RBL12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE, FLOOR SUPPORT RBL 12 TBW FS221.73 TO FS229 FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-1855 REV."
- [SDR VNAA202410210028](https://openairdocs.org/sdr/VNAA202410210028.md): Seat Track · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS FROM STA 847 TO 977 AND LBL9. SEAT RAILS FROM STA 847 TO 977 AND LBL9 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONF (A12)"
- [SDR VNAA202410210027](https://openairdocs.org/sdr/VNAA202410210027.md): Seat Track · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS FROM STA 847 TO 977, RBL9. SEAT RAIL FROM STA 847 TO 977, RBL 9 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 SRM 53-00-49-201-002-A01 AND PER CRJ900 AMM 53-00-49 (CONFIG A12).
- [SDR VNAA202410210026](https://openairdocs.org/sdr/VNAA202410210026.md): Floor Support · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS FROM STA 1000 TO STA 1069 LBL9 & LBL27 OF FLOOR STRUCTURE (C2). FLOOR SUPPORTS LBL27 ANT LBL9 AT FS1000 TO FS1069 WERE EVALUATED OUT OF LIMITS AND WERE REPAIRED PER CRJ900 SRM 53-61-43-101-001-A02 AND CRJ900 SRM 53-00-41-201-001-A0
- [SDR VNAA202410210025](https://openairdocs.org/sdr/VNAA202410210025.md): Doubler · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT WERE EVALUATED OUT OR LIMITS PER CRJ
- [SDR VNAA202410210024](https://openairdocs.org/sdr/VNAA202410210024.md): Floor Support · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT SPLICE LOWER CHORD BTW STA 865-881 AND 9RBL AT FLOOR STRUCTURE OF PASSENGER CABIN (CPAX). FLOOR SUPPORT SPLICE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-43-101-001-A02; FABRICATED PER DWG NO. SH670-32161 REV. NC AND WAS REPLA
- [SDR VNAA202410210023](https://openairdocs.org/sdr/VNAA202410210023.md): Rib · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-381 REV.
- [SDR VNAA202410210022](https://openairdocs.org/sdr/VNAA202410210022.md): Canister · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Aircraft Fuel System
  > CRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 LH FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.
- [SDR VNAA202410210021](https://openairdocs.org/sdr/VNAA202410210021.md): Floorbeam · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON LH SIDE FLOOR BEAM AT FS 280.00. LH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-00
- [SDR VNAA202410210020](https://openairdocs.org/sdr/VNAA202410210020.md): Floorbeam · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON RH SIDE FLOOR BEAM AT FS 280.00. RH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-00
- [SDR VNAA2024102100019](https://openairdocs.org/sdr/VNAA2024102100019.md): Rib · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > "CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE RH WING WAS REPAIRED PER REO 690-57-51-380 REV."
- [SDR VNAA202410210018](https://openairdocs.org/sdr/VNAA202410210018.md): Hinge Fitting · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Rudder Structure
  > "AFTER RUDDER REMOVAL, 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 Y NO. 3 AT VERTICAL STABILIZER REAR SPAR WERE REPLACED PER RIL #2103 REV. B."
- [SDR VNAA202410210017](https://openairdocs.org/sdr/VNAA202410210017.md): Seat Track · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "DESCRIPTION: CORROSION ON SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847. SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847.00 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND
- [SDR VNAA202410210016](https://openairdocs.org/sdr/VNAA202410210016.md): Seat Track · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40. EVALUATED,SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40 DUE TO EXCESIVE DAMAGE, THEREFORE ARE OUT OF LIMITS PER CRJ-900 SR
- [SDR VNAA202410210015](https://openairdocs.org/sdr/VNAA202410210015.md): Seat Track · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977. EVALUATED, SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02, CRJ-900 SRM
- [SDR VNAA202410210014](https://openairdocs.org/sdr/VNAA202410210014.md): Angle · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CORROSION ON MOUNTING ANGLE OF GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. MOUNTING ANGLE WAS EVALAUTED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01"
- [SDR VNAA202410210013](https://openairdocs.org/sdr/VNAA202410210013.md): Plate · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON KICK PLATE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE. CORROSION WAS REMOVED ON KICK PLATE PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE IS WHITHIN OF LIMITS AND DUE TO EXCESSIVE DAMAGE MID CAP A
- [SDR VNAA202410210012](https://openairdocs.org/sdr/VNAA202410210012.md): Door Sill · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT. EVALUATED, DUE TO EXCESSIVE CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT,THEREFORE OUT OF LIMIT PER CRJ 900 SRM 53-61-23-201-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06
- [SDR VNAA202410210011](https://openairdocs.org/sdr/VNAA202410210011.md): Stringer · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "CORROSION ON STRINGER 21RH FS 319.70 TO FS 333. STGR21 RH BTW FS319 TO FS333 WAS EVALUATED PER CRJ900 SRM 53-21-03-101-002-A04 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01"
- [SDR VNAA202410210010](https://openairdocs.org/sdr/VNAA202410210010.md): Crossbeam · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Structure
  > "I"INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. WAS REPAIRED PER REO 690-
- [SDR VNAA202410210009](https://openairdocs.org/sdr/VNAA202410210009.md): Floorbeam · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53
- [SDR VNAA202410210008](https://openairdocs.org/sdr/VNAA202410210008.md): Frame · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Frame
  > "CORROSION ON FRAME FS364.00 NEAR STGR 27 BEHIND OF SENSOR PX41 AT MAIN AVIONICS COMPARTMENT. FRAME FS364 WAS RE INSPECTED PER CRJ900 NDTM PART 01 51-20-009-210-A01 AND ONLY NUTPLATE BRACKET WAS FOUND WITH CORROSION, WAS FABRICATED PER DWG SH670-32456 REV. NC
- [SDR VNAA202410210007](https://openairdocs.org/sdr/VNAA202410210007.md): Intercostal · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. EVALUATED, DUE TO NOT ALLOWED DAMAGE ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT,THEREFORE
- [SDR VNAA202410210006](https://openairdocs.org/sdr/VNAA202410210006.md): Frame · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Frame
  > "DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900
- [SDR VNAA202410210005](https://openairdocs.org/sdr/VNAA202410210005.md): Frame · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Frame
  > "DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900
- [SDR VNAA202410210004](https://openairdocs.org/sdr/VNAA202410210004.md): Angle · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6 C
- [SDR VNAA202410210003](https://openairdocs.org/sdr/VNAA202410210003.md): Fitting · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > " CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFOR
- [SDR VNAA202410210002](https://openairdocs.org/sdr/VNAA202410210002.md): Bracket · corroded · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CORROSION ON BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ-900 SRM 5
- [SDR VNAA202410210001](https://openairdocs.org/sdr/VNAA202410210001.md): Drag Angle · cracked · Oct 21, 2024 · N589NN · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > "INITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TR RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (T
- [SDR VNAA2024081311101](https://openairdocs.org/sdr/VNAA2024081311101.md): Sensor · unserviceable · Aug 10, 2024 · N589NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVHT WARNING MSG IN FLIGHT, LHOB BTMS EICAS INDICATION BOX SHOWED RED, AND INDICATED 20, IN CRUISE FLIGHT / REMOVED AND REPLACED ASCU IAW CRJ900 AMM 32-44-06-000/400-801-A01 AND REMOVED AND REPLACED LH OB BRAKE TEMP SENSOR IAW CRJ900 AMM 32-46-01-000/400
- [SDR VNAA2024050911101](https://openairdocs.org/sdr/VNAA2024050911101.md): Warning Message · false indication · May 7, 2024 · N589NN · Cndair CL6002D24 · Central Warning
  > ELEVATOR SPLIT CAUTION MSG IN FLT / TROUBLESHOOT AND PERFORMED OPERATIONAL TEST OF THE ELEVATOR CONTROL SYSTEM IAW CRJ 900 FIM 27-31-00-810-803-A02 AND AMM 27-31-00-710-801-A01. OPS CHECK GOOD AT THIS TIME. FAULT CLEARED AND FAULT DID NOT RE-APPEAR.
- [SDR VNAA2023102011101](https://openairdocs.org/sdr/VNAA2023102011101.md): Detector · unserviceable · Oct 19, 2023 · N589NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > DURING CRUISE, THE CREW NOTICED A FLAPS/STALL FAIL MESSAGE / REMOVED AND REPLACED RIB SKEW DETECTOR MT5 IAW CRJ900 AMM 27-52-45-000/400-802-A01. OPS CHECK GOOD. RIG CHECK GOOD.
- [SDR VNAA2023092911101](https://openairdocs.org/sdr/VNAA2023092911101.md): Pseu · unserviceable · Sep 29, 2023 · N589NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > NLG DID NOT DEPLOY WHEN LEVER SELECTED DOWN, HAD TO MANUALLY EXTEND PER QRH. REMOVED & REPLACED PSEU I.A.W. CRJ900 AMM 32-61-01-000/400-801. PERFORMED MULTIPLE OPS CHECKS OF LANDING GEAR EXTENSION/RETRACTION I.A.W. CRJ900 AMM 32-30-00-865-801. OPS CHECKS GOOD.
- [SDR VNAA202307121113](https://openairdocs.org/sdr/VNAA202307121113.md): Manifold · unserviceable · Jul 11, 2023 · N589NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP AFTER TAKE OFF AND GEAR UP / REMOVED AND REPLACED THE STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. OPS CHECK AND LEAK CHECK GOOD.
- [SDR VNAA202306191111](https://openairdocs.org/sdr/VNAA202306191111.md): Unknown · unknown · Jun 16, 2023 · N589NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > NOSE WHEEL STEERING INOP CAUTION MESSAGE 10 SECONDS AFTER TAKE OFF. NO MESSAGE SHOWN UPON MEET AND GREET PERFORMED. RESET OF NWS IAW CRJ 900 AMM 32-50-00-810-802. NO DEFECTS NOTED
- [SDR VNAA202302021111](https://openairdocs.org/sdr/VNAA202302021111.md): Not Entered · not entered · Feb 1, 2023 · N589NN · Cndair CL6002D24 · Rudder, Plate/Skin
  > RH RUDDER SKIN STA136.90 - STA148.86 DENTED. PERFORMED PERMANENT REPAIR IAW EA 23-C9-55-0029-IR_APPROVED.
- [SDR VNAA202212061111](https://openairdocs.org/sdr/VNAA202212061111.md): Drain Mast · missing · Dec 3, 2022 · N589NN · Cndair CL6002D24 · APU Engine Fuel and Control
  > AFT FUEL DRAIN MISSING. REMOVED REMAINING PIECE OF THE DRAIN MAST AND SEAL IAW AMM 28-20-03-000-801-A01. NO FURTHER DEFECTS NOTED. A/C OK FOR FERRY FLIGHT. FERRY FLT 9977. REMOVED AND REPLACED AFT FUEL DRAIN MAST IAW AMM 28-20-03-000/400-801-A01.
- [SDR VNAA202207281111](https://openairdocs.org/sdr/VNAA202207281111.md): Sensor · fault message · Jul 25, 2022 · N589NN · Cndair CL6002D24 · Landing Gear Brake System
  > MX DIVERSION DUE TO BRAKE OVERHEAT WARNING MESSAGE. CREW FOLLOWED QRH AND DECIDED TO DIVERT TO THE NEAREST SUITABLE AIRPORT. TRUCKS WERE ROLLED IN ATL TO CHECK FOR BRAKE FIRES. CREW DID NOT PERFORM AN OVERWEIGHT LANDING. CREW WAS ABLE TO TAXI TO THE GATE AND M
- [SDR VNAA2022071211211](https://openairdocs.org/sdr/VNAA2022071211211.md): Stiffener · dented · Jul 10, 2022 · N589NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > DURING OVERNIGHT MX AT GSP, FOUND 3/4"" CRACK AND 1 1/2"" DENT ON FORWARD BAGGAGE BAY DOOR FORWARD LOWER STABILIZER / PERFORMED PERM REPAIR OF THE FWD BAGGAGE DOOR LOWER FWD STIFFENER IAW REO 690-52-35-298, EA 22-C9-52-0853, CRJ 900 SRM 51-42-06, AND CRJ 900 S
- [SDR VNAA202206301111](https://openairdocs.org/sdr/VNAA202206301111.md): Acm · unserviceable · Jun 29, 2022 · N589NN · Cndair CL6002D24 · Air Distribution System
  > ON DEPARTURE AFT FA IMMEDIATELY SMELLED SMOKE AND CALLED FWD FA. IT WAS DETERMINED THAT THE SMOKE ODOR WAS STRONGER IN THE REAR OF THE AIRCRAFT (ROW 11 BACK TO AFT FA STATION). SLIGHT SMOKY ODOR IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DECIDED TO RETURN
- [SDR VNAA202106309995](https://openairdocs.org/sdr/VNAA202106309995.md): Seat Track · corroded · Jun 22, 2021 · N589NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL9 CORRODED BEYOND LIMITS

Next page: https://openairdocs.org/aircraft/N589NN/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 = 'N589NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N589NN/reports

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