# Service difficulty reports: N586NN

A list on [N586NN](https://openairdocs.org/aircraft/N586NN.md).

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

- [SDR VNAA2025050911101](https://openairdocs.org/sdr/VNAA2025050911101.md): Control Unit · faulted · May 8, 2025 · N586NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MSG ON TAKE OFF. / REMOVED AND REPLACED SFECU 1 IAW AMM 27-51-05€“000/400-801-A01. PERFORMED OPS TEST OF THE FLAPS/SLATS SYS IAW AMM 27-50-00-710-801-A02 AND SELF-TEST OF THE SFECU IAW AMM 27-51-05-740-801-A01. OPS TEST AND SELF TEST GOOD AT
- [SDR VNAA202411240002](https://openairdocs.org/sdr/VNAA202411240002.md): Skin · damaged · Nov 16, 2024 · N586NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REO 690-53-21-1683-2750FH PERM REPAIR - TEMPORARY DISPOSITION FOR DAMAGED HOLES ON FUSELAGE STRUCTURE FOR LAVATORY WASTE DOOR HINGE AT FS379.00 BTWN STR21R - STR22R PERFORM A PERMANENT REPAIR IAW APPROVED PROCEDURES 2750FH. PERMANENT REPAIR ON DAMAGED HOLES O
- [SDR VNAA202411240031](https://openairdocs.org/sdr/VNAA202411240031.md): Seat Track · corroded · Oct 22, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON BULKHEAD SIDE POST AT LBL 9.00. CORROSION ON BULKHEAD SIDE POST AT LBL 9.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01
- [SDR VNAA202411240030](https://openairdocs.org/sdr/VNAA202411240030.md): Seat Track · corroded · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (2 EA). EVALUATED,SEAT RAILS OF LBL9 BTW FS693.00 TO FS977.00. (2 EA),THEREFORE IS OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM53-51-49-101-001-A02 AND SEAT R
- [SDR VNAA202411240028](https://openairdocs.org/sdr/VNAA202411240028.md): Floor Support · corroded · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (4EAS) LOCATED ON FS310.00 LBL 19, FS317.00 RBL 3, FS295.00 RBL 3 AND BTW FS280.00 TO FS295.00 RBL 16 AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (4EAS) LOCATED ON FS310.00 LBL 19, FS317.00 RBL 3, FS295.00 RBL 3 AND BTW FS280.00 TO
- [SDR VNAA202411240027](https://openairdocs.org/sdr/VNAA202411240027.md): Angle · corroded · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE BTW FS 1015 AND SGTR-20LH AT AFT CARGO COMPARTMENT. CORROSION ON ANGLE BTW FS 1015 AND SGTR-20LH AT AFT CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND C
- [SDR VNAA202411240026](https://openairdocs.org/sdr/VNAA202411240026.md): Hinge Fitting · excess play · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Rudder Structure
  > 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 VNAA202411240019](https://openairdocs.org/sdr/VNAA202411240019.md): Intercostal · corroded · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH/LH INTERCOSTALS (2 EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. RH/LH INTERCOSTALS (2 EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-
- [SDR VNAA202411240014](https://openairdocs.org/sdr/VNAA202411240014.md): Skin · corroded · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 R
- [SDR VNAA202411240001](https://openairdocs.org/sdr/VNAA202411240001.md): Floorbeam · cracked · Oct 21, 2024 · N586NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. REPAIRED PER REO 690-53-11-1876 RE
- [SDR VNAA202411240029](https://openairdocs.org/sdr/VNAA202411240029.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ/900 AMM 53-00-49
- [SDR VNAA202411240025](https://openairdocs.org/sdr/VNAA202411240025.md): Plate · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 53-20-333-JIC IT WAS DETECTED CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CA
- [SDR VNAA202411240024](https://openairdocs.org/sdr/VNAA202411240024.md): Door Sill · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON DOOR SILL BTW FS519.64 TO FS562.36 AT SURROUND STRUCTURE FWD CARGO DOOR. DOOR SILL BTW FS519.64 TO FS562.36 AT SURROUND STRUCTURE FWD CARGO DOOR WAS REPAIRED PER REO 690-53-31-885 REV--
- [SDR VNAA202411240023](https://openairdocs.org/sdr/VNAA202411240023.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAILS OF LBL27 BTW FS 477.40 TO FS 693.00 (1 EA). SEAT RAIL OF LBL27 BTW FS 477.40 TO FS 693.00 (1 EA) IS OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202411240022](https://openairdocs.org/sdr/VNAA202411240022.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS 477.40 TO FS 693.00 (4 EAS). SEAT RAILS OF LBL9 BTW FS 477.40 TO FS 693.00 (4 EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02. PER CONFIGURATION, NEW SEAT RAILS O
- [SDR VNAA202411240021](https://openairdocs.org/sdr/VNAA202411240021.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS 477.40 TO FS 693.00 (4 EAS). SEAT RAILS OF RBL9 BTW FS 477.40 TO FS 693.00 (4 EAS) ARE OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CON
- [SDR VNAA202411240020](https://openairdocs.org/sdr/VNAA202411240020.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · 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 CRJ900 SRM 53-31-49-101-001-A02 AND
- [SDR VNAA202411240018](https://openairdocs.org/sdr/VNAA202411240018.md): Floorbeam · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE WAS FOUND OUT OF LIMITS PER CRJ 900 SRM 53-21-43-101-001-A03 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND
- [SDR VNAA202411240017](https://openairdocs.org/sdr/VNAA202411240017.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 (7EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 AT PASSENGER COMPARTMENT. SIDE SEAT RAIL STGR 15 (7EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 AT PASSENGER COMPARTMENT ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101
- [SDR VNAA202411240016](https://openairdocs.org/sdr/VNAA202411240016.md): Seat Track · corroded · Oct 20, 2024 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 (4EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL STGR 15 (4EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40 ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFORE WE
- [SDR VNAA202411240015](https://openairdocs.org/sdr/VNAA202411240015.md): Bracket · corroded · Oct 19, 2024 · N586NN · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-
- [SDR VNAA202411240013](https://openairdocs.org/sdr/VNAA202411240013.md): Nozzle · dented · Oct 19, 2024 · N586NN · Cndair CL6002D24 · Engine Collector/Tailpipe/Nozzle
  > DENTS ON NOZZLE ASSY EXHAUST AT LH ENGINE DENTS ON NOZZLE ASSY EXHAUST AT LH ENGINE WERE REPAIRED PER REO 690-54-15-003 REV. - -.
- [SDR VNAA202411240007](https://openairdocs.org/sdr/VNAA202411240007.md): Cap · corroded · Oct 19, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SILL, MID CAP AND KICK PLATE AT PASSENGER DOOR. CORROSION ON MID CAP AND KICK PLATE AT PASSENGER DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. KICK PLATE WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-001- A02. MID CAP WAS EVALU
- [SDR VNAA202411240012](https://openairdocs.org/sdr/VNAA202411240012.md): Inlet · dented · Oct 18, 2024 · N586NN · Cndair CL6002D24 · Engine Air Intake System
  > DENTS (5 EAS) ON LOWER LH ENGINE NOSE INLET COWL BTW 5/7 O´CLOCK POSITION. DENTS (5 EAS) ON LOWER LH ENGINE NOSE INLET COWL BTW 5/7 O´CLOCK POSITION WERE REPAIRED PER REO 690-54-11-528 REV. - - AND PER REO 670-51-00-085 REV. -A.
- [SDR VNAA202411240011](https://openairdocs.org/sdr/VNAA202411240011.md): Web · cracked · Oct 18, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
- [SDR VNAA202411240010](https://openairdocs.org/sdr/VNAA202411240010.md): Web · cracked · Oct 17, 2024 · N586NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ/900 SRM 53-11-43-201-001-A01
- [SDR VNAA202411240009](https://openairdocs.org/sdr/VNAA202411240009.md): Hinge · corroded · Oct 17, 2024 · N586NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON UPPER HINGE AT ACCESS PANEL 832ET. CORROSION ON UPPER HINGE AT ACCESS PANEL 832ET WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-00-01-101-001-A01 AND REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR VNAA202411240008](https://openairdocs.org/sdr/VNAA202411240008.md): Panel · corroded · Oct 17, 2024 · N586NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON ACCESS PANEL 832FT AND 832DT. CORROSION ON ACCESS 832DT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 52-11-04-101- 001-A01. ACCESS PANEL 832FT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-11-04-101
- [SDR VNAA202411240006](https://openairdocs.org/sdr/VNAA202411240006.md): Skin · worn · Oct 16, 2024 · N586NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-495 REV.--
- [SDR VNAA202411240005](https://openairdocs.org/sdr/VNAA202411240005.md): Skin · worn · Oct 16, 2024 · N586NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-494 REV.--
- [SDR VNAA202411240004](https://openairdocs.org/sdr/VNAA202411240004.md): Drag Angle · cracked · Oct 16, 2024 · N586NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE
- [SDR VNAA202411240003](https://openairdocs.org/sdr/VNAA202411240003.md): Drag Angle · cracked · Oct 16, 2024 · N586NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TO
- [SDR VNAA2024100711102](https://openairdocs.org/sdr/VNAA2024100711102.md): Warning System · false indication · Oct 4, 2024 · N586NN · Cndair CL6002D24 · Overheat Detection
  > DUCTMON FAULT STATUS MSG, A/I ICE DUCT CAUTION MSG, A/I DUCT WARNING MSG, RH WING A/I CAUTION MSG, LH WING A/I CAUTION MSG IN CRUISE FLIGHT EMERGECY DECLARE TO EXIT ICING / PERFORMED BITE TEST OF THE AILC IAW CRJ 900 AMM 30-12-12-740-801-A01. NO FAULTS FOUND
- [SDR VNAA202202151111](https://openairdocs.org/sdr/VNAA202202151111.md): Windshield · smoke · Feb 11, 2022 · N586NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > FO WINDSHIELD LOWER HEAT BLOCK BEGAN PRODUCING SMOKE IN FLIGHT. NO FIRE. SMOKE SUBSIDED AFTER ABOUT 10 SECONDS AFTER TURNING OFF WINDHIELD HEAT / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-PSA. OPS CHECK AND LEAK CHECK REQUIRED. PE
- [SDR VNAA202108031112](https://openairdocs.org/sdr/VNAA202108031112.md): Acm · unserviceable · Aug 1, 2021 · N586NN · Cndair CL6002D24 · Cabin Cooling System
  > WHILE ON APPROACH INTO SDF. CREW START NOTICING SMOKE IN THE COCKPIT WHICH STARTED TO GET HEAVY, STARTED BURNING THEIR EYES AND THROAT. THEY THEN GOT A CHIME FROM THE THE CABIN TELLING THEM THAT THEY WERE GETTING THE SMOKE IN THE CABIN. THEY DECLARED AN EMERGE
- [SDR VNAA202107289991](https://openairdocs.org/sdr/VNAA202107289991.md): Rib · cracked · Jul 30, 2021 · N586NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > LH LEADING EDGE MACHINED RIB AT SS 57.16 0.50" CRACK ON UPPER FLANGE
- [SDR VNAA202106309996](https://openairdocs.org/sdr/VNAA202106309996.md): Seat Track · corroded · Jun 22, 2021 · N586NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT RBL 9 CORRODED BEYOND LIMITS
- [SDR VNAA2020092011101](https://openairdocs.org/sdr/VNAA2020092011101.md): Proximity Sensor · out of adjust · Sep 19, 2020 · N586NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > GEAR DISAGREE MESSAGE IN FLIGHT WHEN GEAR UP SELECTED. CREW DECLARED EMERGENCY AND DIVERTED TO CAK. INTERROGATED MDC AND FOUND MULTIPLE FAULTS FLAGGING NLG PROXIMITY SENSOR PX22. FOUND PX22 TO BE READING "DEGRADED FAR" IN MDC WITH GEAR UP WHEN IT WAS SUPPOS
- [SDR VNAA2020081411101](https://openairdocs.org/sdr/VNAA2020081411101.md): Acm · failed · Aug 11, 2020 · N586NN · Cndair CL6002D24 · Cabin Cooling System
  > STRONG ELEC SMELL IN CABIN. PERFORMED OPS TEST OF AIR COND. SYST. LH PACK CHECK BAD AND OPS CHECK PASS LIGHTS GOOD. REMOVED AND REPLACED LH ACM IAW CRJ900 AMM. ALSO REMOVED AND REPLACED LH WATER EXTRACTOR DUCT. LH PACK OPS CHECKS GOOD AT THIS TIME NO ELECTRICA
- [SDR VNAA2020072311101](https://openairdocs.org/sdr/VNAA2020072311101.md): Controller · faulted · Jul 19, 2020 · N586NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > CREW NOTICED SMALL CRACK IN WINDSHIELD THAT KEPT GROWING AS THEY APPROACHED STL AREA. DECIDED TO DECLARE EMERGENCY AND DIVERT TO EVV. FLIGHT LANDED SAFELY AND WITH NO FURTHER ISSUES. MX REMOVED AND REPLACED CAPTIANS WINDSHIELD AND WINDSHIELD TEMP CONTROLLER.
- [SDR VNAA2019091511102](https://openairdocs.org/sdr/VNAA2019091511102.md): Warning System · false activation · Sep 15, 2019 · N586NN · Cndair CL6002D24 · Drag Control System
  > ON ARRIVAL AT FL160, WHEN FLAPS WERE SELECTED, RECEIVED SPOILERONS AND FLIGHT SPOILERS CAUTION MSG. CREW PUT FLAPS BACK TO 0 AND RAN QRH. DECLARED EMERGENCY AS A PRECAUTION. CABIN DID NOT BRACE. TRUCKS DID ROLL. / FLIGHT LANDED WITH OUT INCIDENT AND WAS ABL
- [SDR VNAA2019031311101](https://openairdocs.org/sdr/VNAA2019031311101.md): Selector Valve · failed · Mar 13, 2019 · N586NN · Cndair CL6002D24 · Landing Gear Selector
  > LANDING GEAR FAILED TO EXTEND SO THE CREW EXTENDED MANUALLY. THEY DECLARED AND EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. TRUCKS WERE ROLLED BUT THE CABIN WAS NOT BRACED. SUPLEMENTAL INFORMATION MX R&R MLG SELECTOR VALVE. OPS CHECK GOOD
- [SDR VNAA20181212111](https://openairdocs.org/sdr/VNAA20181212111.md): Warning System · false activation · Dec 12, 2018 · N586NN · Cndair CL6002D24 · Landing Gear Steering System
  > THE CREW REPORTED A NOSE WHEEL STEERING INOP 'C' MSG IN FLIGHT AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT ISSUE AND THE SYSTEM WAS RESET, OPS CHECK GOOD.
- [SDR VNAA2017092711101](https://openairdocs.org/sdr/VNAA2017092711101.md): Warning System · activated · Sep 27, 2017 · N586NN · Cndair CL6002D24 · Drag Control System
  > FLIGHT 5564 (AVP-CLT) DECLARED EMERGENCY ON DESCENT INTO CLT FOR RUNWAY 36C. CREW HAD AN INBOARD SPOILER MESSAGE AND OUTBOARD SPOILERON MESSAGE ON APPROACH. CREW FOLLOWED QRH AND CONTINUED INTO CLT AFTER DECLARING EMERGENCY AS PRECAUTION. CREW DID NOT REQUI
- [SDR VNAA2017080211101](https://openairdocs.org/sdr/VNAA2017080211101.md): Manifold · defective · Aug 2, 2017 · N586NN · Cndair CL6002D24 · Landing Gear Steering System
  > ON CLIMBOUT THE CREW RECEIVED A NOSE WHEEL STEERING CAUTION MESSAGE. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND DECLARED EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE STEERING MANIFOLD AND THE ROD END FO
- [SDR VNAA2017073011102](https://openairdocs.org/sdr/VNAA2017073011102.md): Warning Message · false activation · Jul 30, 2017 · N586NN · Cndair CL6002D24 · Landing Gear Steering System
  > AFTER TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING CAUTION MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTINUED TO THEIR DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED MULTIPLE GEAR SWINGS AND OPERATIONAL CHECKED GOOD.
- [SDR VNAA2017073011101](https://openairdocs.org/sdr/VNAA2017073011101.md): Steering Sys · malfunctioned · Jul 30, 2017 · N586NN · Cndair CL6002D24 · Landing Gear Steering System
  > AIRCRAFT EXPERIENCED A NOSE WHEEL STEERING INOPERATIVE MESSAGE. THE CREW CONTINUED TO DESTINATION AND THE TOWER DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. ONCE STOPPED, MAINTENANCE CONTROL WAS ABLE TO RESET THE NOSE WHEEL STEERING WITH THE CR

## 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 = 'N586NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N586NN/reports

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