# Service difficulty reports: N590NN

A list on [N590NN](https://openairdocs.org/aircraft/N590NN.md).

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

- [SDR VNAA2025022111101](https://openairdocs.org/sdr/VNAA2025022111101.md): Windshield · cracked · Feb 18, 2025 · N590NN · Cndair CL6002D24 · Flight Compartment Windows
  > CA SIDE WINDSHEILD CRACKED IN FLIGHT. / REMOVED AND REPLACED THE CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD.
- [SDR VNAA20250102028](https://openairdocs.org/sdr/VNAA20250102028.md): Hinge Fitting · corroded · Dec 11, 2024 · N590NN · Bombdr CL6002D15 · Wing Main, Frame Structure
  > CORROSION ON CENTER FITTINGS BORE LUG L1,L2,AND L5 AT LH CENTER FITTINGS BORE LUG L1,L2,AND L5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV. -- AND REO 690-57-61-356 REV. --
- [SDR VNAA20250102026](https://openairdocs.org/sdr/VNAA20250102026.md): Door Sill · corroded · Dec 4, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > IN REFERENCE TO JOB TRFKE001P2A5:53-30-307-JIC/002: AFTER REMOVAL DOOR SILL, CORROSION ON AFT CHORD INNER AT SURROUND STRUCTURE AFT CARGO DOOR WAS FOUND. EVALUATED, DUE TO DAMAGE IS NOT ALLOWED, AFT INNER CHORD PER CRJ-900 SRM 53-61-23-101-001-A01 AND AFT CHO
- [SDR VNAA20250102029](https://openairdocs.org/sdr/VNAA20250102029.md): Bushing · damaged · Dec 2, 2024 · N590NN · Bombdr CL6002D15 · Wing Main, Frame Structure
  > HOUSING OF RH AILERON LUG #6 WAS MEASURED AND WAS FOUND OUT LIMITS BY STANDARD (NOMINAL MEASUREMENT). BUSHING OF RH AILERON LUG #6 WAS FABRICATED PER REO 670-57-61-107 REV- B
- [SDR VNAA20250102027](https://openairdocs.org/sdr/VNAA20250102027.md): Hinge Fitting · corroded · Dec 2, 2024 · N590NN · Bombdr CL6002D15 · Wing Main, Frame Structure
  > CORROSION ON CENTER FITTINGS BORE LUG R1, R2, R5 AND R4 WAS FOUND AT RH AILERON. CENTER FITTINGS BORE LUG R1,R2,R5 AND R4 WAS FOUND AT RH AILERON WAS REPAIRED PER REO 670-57-61-107 REV - B
- [SDR VNAA20250102015](https://openairdocs.org/sdr/VNAA20250102015.md): Web · corroded · Dec 2, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA20250102011](https://openairdocs.org/sdr/VNAA20250102011.md): Floorbeam · cracked · Dec 2, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1893
- [SDR VNAA20250102024](https://openairdocs.org/sdr/VNAA20250102024.md): Seat Track · corroded · Nov 30, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL (2 EAS) BTW FS 477.40 TOFS 693.00 ON RBL 9. SEAT RAIL (2 EAS) BTW FS 477.40 TOFS 693.00 ON RBL 9 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG. A12).
- [SDR VNAA202501032023](https://openairdocs.org/sdr/VNAA202501032023.md): Canister · cracked · Nov 30, 2024 · N590NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > IN REFERENCE TO JOB CARD 500-08E2-JIC: DURING INSPECTION ON AREA WAS DETECTED CRACK IN CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--
- [SDR VNAA20250102022](https://openairdocs.org/sdr/VNAA20250102022.md): Floor Support · corroded · Nov 30, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS LH (3EAS) BTW FS280.00 TO FS310.00 AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS LH (3EAS) BTW FS280.00 TO FS310.00 AT FUSELAGE FLOOR STRUCTURE WERE FOUND OUT LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ 900 SRM 53-21-43-101-001-A03 THEREF
- [SDR VNAA20250102031](https://openairdocs.org/sdr/VNAA20250102031.md): Seat Track · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN. RH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND WERE R
- [SDR VNAA20250102030](https://openairdocs.org/sdr/VNAA20250102030.md): Seat Track · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN. LH SIDE SEAT RAIL BTW FS379.00 - FS669.40 (4 EAS) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 A
- [SDR VNAA20250102010](https://openairdocs.org/sdr/VNAA20250102010.md): Plate · corroded · Nov 29, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF. DRAIN PLATE OF FLOOR PANEL 232BRF WAS REPLACED PER CRJ/900 AMM 53-00-47.
- [SDR VNAA20250102009](https://openairdocs.org/sdr/VNAA20250102009.md): Angle · corroded · Nov 29, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE MOUNTING AND ANGLES (4EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLES (4EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATE
- [SDR VNAA20250102008](https://openairdocs.org/sdr/VNAA20250102008.md): Cap · corroded · Nov 29, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON KICKPLATE BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01,EVALUATED ON KICKPLATE,
- [SDR VNAA20250102007](https://openairdocs.org/sdr/VNAA20250102007.md): Hinge · excess play · Nov 29, 2024 · N590NN · Cndair CL6002D24 · Vertical Stabilizer
  > AFTER RUDDER REMOVAL, 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 VNAA20250102006](https://openairdocs.org/sdr/VNAA20250102006.md): Door Sill · corroded · Nov 29, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-
- [SDR VNAA20250102021](https://openairdocs.org/sdr/VNAA20250102021.md): Floorbeam · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM 9 LBL BTW FS 1000.00 TO FS 1047.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-001-A01 AND NO DAMAGE WAS FOUND ON FLOOR BEAM 9 LBL BTW FS 1000 TO FS 1022 AND BTW FS 1045 TO FS 1051 AND WAS R
- [SDR VNAA20250102020](https://openairdocs.org/sdr/VNAA20250102020.md): Floorbeam · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM 27 LBL BTW FS 1000.00 TO FS 1047.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. PAINT WAS REMOVED ON FLOORBEAM 27 LBL BTW FS 1000.00 TO FS 1005 AND BTW FS 1038 TO FS 1051 PER CRJ900 SRM 51-26-01-001-001-A01 AND NO DAMAGE WAS FOUND AND W
- [SDR VNAA20250102019](https://openairdocs.org/sdr/VNAA20250102019.md): Seat Track · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=349.00 TO FS=477.40 LBL 9 (1EA) / RBL 9 (1 EA). FLOOR SEAT RAILS BTW FS=349.00 TO FS=477.40 LBL 9 (1EA) / RBL 9 (1 EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-0
- [SDR VNAA20250102018](https://openairdocs.org/sdr/VNAA20250102018.md): Seat Track · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON RH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (7EA). RH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (7EA) 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 CRJ900 AM
- [SDR VNAA20250102017](https://openairdocs.org/sdr/VNAA20250102017.md): Seat Track · corroded · Nov 29, 2024 · N590NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (6EA). LH SIDE SEAT RAIL BTW FS669.40 TO FS977.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONFIG.A1
- [SDR VNA2025F00000](https://openairdocs.org/sdr/VNA2025F00000.md): Hinge · corroded · Nov 28, 2024 · N590NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK AND CORROSION ON FWD/MID/AFT HINGES, DEGRADED PAINT AND MISSING DECAL ON STEP PLATE AT AFT BAGGAGE BAY. DUE TO EXCESSIVE DAMAGE, FWD/MID/AFT HINGES ON STEP PLATE AT AFT BAGGAGE BAY WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01, REPLA
- [SDR VNAA20250102005](https://openairdocs.org/sdr/VNAA20250102005.md): Stringer · corroded · Nov 28, 2024 · N590NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IN STA. FS= 333 TO FS=349 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-42-21-001-001-A01.
- [SDR VNAA20250102004](https://openairdocs.org/sdr/VNAA20250102004.md): Stringer · corroded · Nov 28, 2024 · N590NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26RH IN STA. FS= 333 TO FS=349 AT MAIN AVIONICS COMPARTMENT. STRINGER R/H 26RH IN STA. FS= 333 TO FS=349 WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CRJ-
- [SDR VNAA20250102025](https://openairdocs.org/sdr/VNAA20250102025.md): Floor Support · cracked · Nov 28, 2024 · N590NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT 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 FL
- [SDR VNAA20250102002](https://openairdocs.org/sdr/VNAA20250102002.md): Stringer Splice · corroded · Nov 28, 2024 · N590NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT. (E/E) FOR EXCESSIVE DAMAGE ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-
- [SDR VNAA20250102003](https://openairdocs.org/sdr/VNAA20250102003.md): Intercostal · corroded · Nov 27, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. CORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INT
- [SDR VNAA20250102001](https://openairdocs.org/sdr/VNAA20250102001.md): Doubler · corroded · Nov 27, 2024 · N590NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) WAS
- [SDR VNAA20250102016](https://openairdocs.org/sdr/VNAA20250102016.md): Nozzle · dented · Nov 27, 2024 · N590NN · Cndair CL6002D24 · Engine Collector/Tailpipe/Nozzle
  > SEVERAL DENTS ON EXHAUST NOZZLE FROM 1 HR TO 7 HRS POSITION AT LH ENGNE. DENTS ON EXHAUST NOZZLE FROM 1 HR TO 7 HRS POSITION AT LH ENGNE WERE REPAIRED PER EA NO: A1-690-78-00018 REV --
- [SDR VNAA20250102014](https://openairdocs.org/sdr/VNAA20250102014.md): Bracket · corroded · Nov 26, 2024 · N590NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED BRACKET (4 EAS) AND PLATE (2 EA) BTW FS477.400 AND FS669.40 OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. CORRECTIVE ACTION: EVALUATED, MACHINED BRACKET (4 EAS) AND PLATE (2 EA) BTW FS477.400 AND FS669.40 OF INTERNAL STRUCTURE AT
- [SDR VNAA20250102013](https://openairdocs.org/sdr/VNAA20250102013.md): Plate · corroded · Nov 26, 2024 · N590NN · Cndair CL6002D24 · Service Doors
  > CORROSION ON STEP PLATE AT SERVICE DOOR. EVALUATED, DUE TO EXCESSIVE DAMAGE STEP PLATE DOOR COVER PER CRJ-900 SRM 53-00-01-101-001-A01 AND STEP PLATE AT SERVICE DOOR WAS VERIFIED ITEM30C P/N SH670-31407-7 AND REPLACED PER CRJ-900 AIPC 53-21-23-15
- [SDR VNAA20250102012](https://openairdocs.org/sdr/VNAA20250102012.md): Door Frame · corroded · Nov 26, 2024 · N590NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON INTERNAL SURROUND STRUCTURE SETTLEMENT AREA OF THE MAIN AVIONICS COMPARTMENT DOOR (CUT-OUT). REPAIRED PER REO 690-53-21-032 REV -.
- [SDR VNAA2024010311101](https://openairdocs.org/sdr/VNAA2024010311101.md): Acm · failed · Dec 30, 2023 · N590NN · Cndair CL6002D24 · Cabin Cooling System
  > SMOKE FILLED CABIN ON SHORT FINAL. AFTER LANDING, SMOKE WENT AWAY AND R PACK AUTOFAIL MESSAGE APPEARED. / REMOVED AND REPLACED THE RH AIR CYCLE MACHINE IAW CRJ 900 AMM 21-51-08-000/400-801. PERFORMED OPERATIONAL TEST OF OF AIR CONDITIONING DISTRIBUTION SYSTEM
- [SDR VNAA2023112711101](https://openairdocs.org/sdr/VNAA2023112711101.md): Check Valve · unserviceable · Nov 24, 2023 · N590NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > FLIGHT 5156 HAD MULTIPLE RH ENGINE FLAME OUTS WHILE ENROUTE. THE CREW WAS ABLE TO RELIGHT AND STABILIZE THE RH ENGINE/ REMOVED AND REPLACED THE RH ENGINE 6TH STAGE CHECK VALVE IAW CRJ900 AMM 36-11-03-000/400-801. PERFORMED BORESCOPE INSPECTION OF RH ENGINE COM
- [SDR VNAA2023111311101](https://openairdocs.org/sdr/VNAA2023111311101.md): Pin · unserviceable · Nov 9, 2023 · N590NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > REMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97 / REMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97.
- [SDR VNAA202112221111](https://openairdocs.org/sdr/VNAA202112221111.md): Windshield · false indication · Dec 21, 2021 · N590NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > SMOKE SEEN OUTSIDE OF LEFT SIDE CA WINDSHIELD FOR APPROX 5 SECONDS / PERFORMED OPS CHECK OF WINDOW HEAT IAW CRJ 900 AMM 30-41-06-710-801, OPS CHECK OF PITOT PROBE HEAT IAW CRJ 900 AMM 30-31-00-710-801, OPS CHECK GOOD NO DEFECTS NOTED. RAN #1 ENGINE, NO DEFECTS
- [SDR VNAA202110221111](https://openairdocs.org/sdr/VNAA202110221111.md): Door · out of alignment · Oct 19, 2021 · N590NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR JAMMED CLOSED IN THE UNLOCKED POSITION. REMOVED AND RE-INSTALLED BOTH FWD AND AFT SPIGOT ASSY AND SHIMMED AS REQUIRED IAW CRJ 900 AMM 53-21-23-400-803-A03. FUNCTIONAL TEST GOOD IAW CRJ 900 AMM 52-11-00-720-802-A01.
- [SDR VNAA2021102112111](https://openairdocs.org/sdr/VNAA2021102112111.md): Roller · lack of lube · Oct 18, 2021 · N590NN · Cndair CL6002D24 · Passenger/Crew Doors
  > TROUBLE CLOSING THE MAIN CABIN DOOR / APPLIED GREASE TO LATCH PINS AND ROLLERS OF MAIN CABIN DOOR IAW CRJ 900 AMM 12-20-52-640-809(A01), DOOR CLOSES NORMALLY.
- [SDR VNAA202107219992](https://openairdocs.org/sdr/VNAA202107219992.md): Seat Track · corroded · Jul 21, 2021 · N590NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT TRACK RBL 9 FROM 485-581 HAS PITTING CORROSION
- [SDR VNAA202107219991](https://openairdocs.org/sdr/VNAA202107219991.md): Seat Track · corroded · Jul 18, 2021 · N590NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT TRACK RBL 9 FROM 364-469 HAS PITTING CORROSION
- [SDR VNAA2020092411104](https://openairdocs.org/sdr/VNAA2020092411104.md): Acm · failed · Sep 22, 2020 · N590NN · Cndair CL6002D24 · Cabin Cooling System
  > LIGHT SMOKE IN CABIN WITH RT PACK AUTO FAIL. REMOVED AND REPLACED RT ACM, IAW CRJ900 AMM 21-51-08-000/400-801. OPS AND LEAK CHECK GOOD AT THIS TIME.
- [SDR VNAA2020021911102](https://openairdocs.org/sdr/VNAA2020021911102.md): Battery Pack · failed · Feb 19, 2020 · N590NN · Cndair CL6002D24 · Emergency Lighting
  > LOWER SIDEWALL EMER EXIT LTS ROW 15F AND 15A DO NOT ILLUMINATE. MX REMOVED AND REPLACED BATTERY PACK #3 IAW AMM. OPS CHECKS GOOD.
- [SDR VNAA2018121311101](https://openairdocs.org/sdr/VNAA2018121311101.md): Warning System · false activation · Dec 13, 2018 · N590NN · Cndair CL6002D24 · Drag Control System
  > DURING LANDING, THE CREW REPORTED A SPOILER/SPOILERONS 'C' MSG. THEY DECLARED AND LANDED WITHOUT ISSUE. RESET SYSTEM WITH THE CREW, MESSAGE'S CLEARED AND DID NOT REOCCUR.
- [SDR VNAA2016111600024](https://openairdocs.org/sdr/VNAA2016111600024.md): Contactor · inoperative · Nov 16, 2016 · N590NN · Cndair CL6002D24 · Light System Wiring
  > EMERGENCY LIGHTS COME ON THEN GO OFF. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED CONTACTOR K117 AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016111500021](https://openairdocs.org/sdr/VNAA2016111500021.md): Transducer · malfunctioned · Nov 15, 2016 · N590NN · Cndair CL6002D24 · Airfoil Anti/De-ice System
  > RIGHT ANTI ICE DUCT WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT LEAK DETECTION TRANSDUCER AND PERFORMED CHECKS IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS REL

## 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 = 'N590NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N590NN/reports

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