# Service difficulty reports: N584NN

A list on [N584NN](https://openairdocs.org/aircraft/N584NN.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 · 64 reports

- [SDR VNAA2026010811101](https://openairdocs.org/sdr/VNAA2026010811101.md): Mcu · faulted · Jan 6, 2026 · N584NN · Cndair CL6002D24 · Stabilizer Control System
  > STAB TRIM RUNAWAY ON APPROACH / INTERROGATED MDC FOUND B1 CODE 007955 UNDER DIRECTION FROM MOC AND TROUBLESHOOTING IAW FIM 27-42-07-810-809-A01. REMOVED AND REPLACED MCU IAW AMM 27-42-07-000/400-801-A01. OPS CHECKS GOOD. MCU REMOVED PN 7074-5 SN 1002
- [SDR VNAA2025031911101](https://openairdocs.org/sdr/VNAA2025031911101.md): Elec Connector · unserviceable · Mar 17, 2025 · N584NN · Cndair CL6002D24 · Landing Gear System Wiring
  > ANTI SKID INBD CAUTION MSG/ WITH IND GRND SPOILER FAULT STAUS MSG. / DISASSEMBLED CONNECTOR AT WHEEL SPEED TRANSDUCER AND FOUND TO BE UNSERVICEABLE. REMOVED AND REPLACED CONNECTOR IAW CRJ900 AMM 32-61-05-000/400-803. OPS CHECK GOOD AND BITE TEST GOOD.
- [SDR VNAA202407110030](https://openairdocs.org/sdr/VNAA202407110030.md): Intercostal · corroded · Jun 20, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECONDARY NRC: AFTER FRAME REMOVAL IN REF NRC 00130, CORROSION ON INTERCOSTAL STGR 27 BLW FS1031.00 AND FS1047.00. CORROSION ON INTERCOSTAL STGR 27 BLW FS1031.00 AND FS1047.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED, THEREFORE IT IS WHI
- [SDR VNAA202407110019](https://openairdocs.org/sdr/VNAA202407110019.md): Doubler · worn · Jun 20, 2024 · N584NN · Cndair CL6002D24 · Trailing Edge Flaps
  > IN REF TO JOBCARD 275000·218_R/H.JIC: WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WAS REPAIRED PER REO 670-57-52-352 REV --
- [SDR VNAA202407110027](https://openairdocs.org/sdr/VNAA202407110027.md): Unknown · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECONDARY NRC FROM NRC 00128': AFTER REMOVAL, CORROSION ON STRAY ASSY FS 280.00. LH SIDE. CORROSION ON STRAY ASSY FS 280.00. LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED UNDER NRC 00128.
- [SDR VNAA202407110026](https://openairdocs.org/sdr/VNAA202407110026.md): Frame · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 1047.00 BTW STGR 27 TO STGR 26 LH. CORROSION ON FRAME STA 1051.30 BTW STGR 27 TO STGR 26 LH WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PER CRJ900 SRM 53-61-06-101-003-A02 THEREFORE WAS REPLACED PER CRJ90
- [SDR VNAA202407110016](https://openairdocs.org/sdr/VNAA202407110016.md): Seat Track · corroded · Jun 5, 2024 · N584NN · 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. (3EA) ARE OUT OFF LIMITS PER CRJ-900 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 VNAA202407110015](https://openairdocs.org/sdr/VNAA202407110015.md): Seat Track · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL27 BTW FS485.00 TO FS581.00 (2EA). DUE TO ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROSS-SECTION, SEAT RAILS OF LBL27 BTW FS485.00 TO FS581.00 (2EA) ARE OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 THEREFORE WERE RE
- [SDR VNAA202407110014](https://openairdocs.org/sdr/VNAA202407110014.md): Seat Track · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA). SEAT RAIL OF LBL9 BTW FS379.00 TO FS693.00 (5EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49(CONFIG A12)
- [SDR VNAA202407110011](https://openairdocs.org/sdr/VNAA202407110011.md): Seat Track · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 CONF(A12)
- [SDR VNAA202407110010](https://openairdocs.org/sdr/VNAA202407110010.md): Seat Track · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BLW FS485.00 TO FS720.85.00 (4EA). LH SIDE SEAT RAIL BLW FS485.00 TO FS720.85.00 (4EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACE PER
- [SDR VNAA202407110008](https://openairdocs.org/sdr/VNAA202407110008.md): Seat Track · corroded · Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) ARE OUT OFF 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 (A12)
- [SDR VNAA202407110024](https://openairdocs.org/sdr/VNAA202407110024.md): Floorbeam · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > SECONDARY NRC FROM NRC 00084': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ-900 SRM 5
- [SDR VNAA202407110023](https://openairdocs.org/sdr/VNAA202407110023.md): Floorbeam · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-10-001-
- [SDR VNAA202407110022](https://openairdocs.org/sdr/VNAA202407110022.md): Bracket · cracked · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > DURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. PER REO 670-57-42-577. REV.--
- [SDR VNAA202407110021](https://openairdocs.org/sdr/VNAA202407110021.md): Bracket · cracked · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > DURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577. REV.--
- [SDR VNAA202407110017](https://openairdocs.org/sdr/VNAA202407110017.md): Seat Track · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (3EA) SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (3EA) ARE OUT OFF 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 CONF(A12
- [SDR VNAA202407110009](https://openairdocs.org/sdr/VNAA202407110009.md): Seat Track · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 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) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900
- [SDR VNAA202407110007](https://openairdocs.org/sdr/VNAA202407110007.md): Angle · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE MID CAP AT LOWER PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON ANGLE MID CAP AT LOWER PASSENGER DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PER CRJ 900 SRM 53-21-23-101-001-A02, THEREFO
- [SDR VNAA202407100010](https://openairdocs.org/sdr/VNAA202407100010.md): Bracket · corroded · Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATES (02 EAS) AND BRACKETS, MACHINED (07 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. PAINT ON PLATES (02 EAS) AND BRACKET MACHINED (49 P) FS.517.00 STGR.23LH OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS REMOVED PER SRM 51-2
- [SDR VNAA202407110025](https://openairdocs.org/sdr/VNAA202407110025.md): Bulkhead Web · corroded · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > SECONDARY NRC FROM NRC 00084': AFTER REMOVAL, CORROSION ON RH LOWER WEB AT BULKHEAD FS 280.00 RBL 12 ABOVE FLOOR. CORROSION ON RH LOWER WEB AT BULKHEAD FS 280.00 RBL 12 ABOVE FLOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPAIRED
- [SDR VNAA202407110013](https://openairdocs.org/sdr/VNAA202407110013.md): Seat Track · corroded · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS720.85. (6EA). SEAT RAILS OF RBL9 BTW FS349.00 TO FS720.85. (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49(CONFIG A12)
- [SDR VNAA202407110006](https://openairdocs.org/sdr/VNAA202407110006.md): Rib · cracked · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > IN REFERENCE TO RC TRFKE001TV3L': AFTER INTERNAL ZONAL INSPECTION, CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-359 REV -.
- [SDR VNAA202407110005](https://openairdocs.org/sdr/VNAA202407110005.md): Floorbeam · cracked · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-1
- [SDR VNAA202407110004](https://openairdocs.org/sdr/VNAA202407110004.md): Post · corroded · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00. CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PE
- [SDR VNAA202407100002](https://openairdocs.org/sdr/VNAA202407100002.md): Skin · damaged · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > LIGHTNING STRIKE ON EXTERNAL SKIN OF FWD/CTR BAGGAGE-BAY DOOR (REAR LOWER CORNER). REPAIRED PER REO 690-52-35-420. REV. -- AND PER REO 690-52-35-421. REV. --
- [SDR VNAA202407090005](https://openairdocs.org/sdr/VNAA202407090005.md): Skin · damaged · Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN REF. TRFKE00BFL7B:REO 690-53-00-532.1500FH PERM REPAIR - TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BTW FS379.00-FS437.00 & STR25L-STR27 AND FS897.00- FS913.00 & STR2L-STR3L WITHIN 1500FH ACCOMPLISH APERMANENT REPAIR IAW APPROVED PROCEDU
- [SDR VNAA202407110003](https://openairdocs.org/sdr/VNAA202407110003.md): Floor Support · corroded · Jun 2, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00, DUE EXCESSIVE CORROSIÓN ON FLOOR SUPPORT ANGLE UPPER FACE AT FS 280 BTW RBL 9.00 AND LBL 9.00 ITS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. PER SRM 51-42-06-001
- [SDR VNAA202407110002](https://openairdocs.org/sdr/VNAA202407110002.md): Intercostal · corroded · Jun 1, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 AT MAIN AVIONICS COMPARTMENT. SUMMARY:EVALUATED, DUE TO EXCESIVE DAMAGE ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 PER CRJ-900
- [SDR VNAA202407110001](https://openairdocs.org/sdr/VNAA202407110001.md): Skin · corroded · Jun 1, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. DOOR CUT-OUTINNER SKIN AT E/E MAIN COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 REV--.
- [SDR VNAA202407100004](https://openairdocs.org/sdr/VNAA202407100004.md): Skin · dented · May 31, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN. DENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN WAS REPAIRED PER REO 670-51-00-085 REV-A AND PER REO 690-53-21-1784 REV--
- [SDR VNAA202407100009](https://openairdocs.org/sdr/VNAA202407100009.md): Door Sill · corroded · May 30, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON LOWER SILL OF AFT BAGGAGE-BAY DOOR CUT OUT. LOWER SILL OF AFT BAGGAGE-BAY DOOR CUT OU WAS EVALUATED, THE BLEN DEPTH EXCEEDED 0.016,THEREFORE IS OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND REPLACED PER CRJ900 SRM 51
- [SDR VNAA202407100008](https://openairdocs.org/sdr/VNAA202407100008.md): Web · cracked · May 30, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER REO 690-53-11-1775 REV.--
- [SDR VNAA202407090002](https://openairdocs.org/sdr/VNAA202407090002.md): Drag Angle · cracked · May 30, 2024 · N584NN · 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) REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01
- [SDR VNAA202407090001](https://openairdocs.org/sdr/VNAA202407090001.md): Drag Angle · cracked · May 30, 2024 · N584NN · 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) REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR VNAA202407100007](https://openairdocs.org/sdr/VNAA202407100007.md): Skin · nicked · May 29, 2024 · N584NN · Cndair CL6002D24 · Trailing Edge Flaps
  > INITIAL ISPECTION:SEVERAL NICKS ON INBD FLAP FLS 15.00 TO FLS 75.60 AT LH WINGSEVERAL NICKS ON INBO FLAP FLS 15.00 TO FLS 75.60 AT LH WING WERE BLENOEO OUT PER CRJ900 SRM 51-12-00-001-001-A01 ANO WERE EVALUATEO BTW FLS15 TO FLS45 OUT OF LIMITS ANO BTW FLS45 TO
- [SDR VNAA202407100006](https://openairdocs.org/sdr/VNAA202407100006.md): Panel · worn · May 29, 2024 · N584NN · Cndair CL6002D24 · Wing, Plate/Skin
  > INITIAL INSPECTION: WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING. WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING WERE REPAIRED PER REO 690-57-41-432 REV- -AND REO 690-57-41-431 REV- -
- [SDR VNAA202407100005](https://openairdocs.org/sdr/VNAA202407100005.md): Skin · nicked · May 29, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE. SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE WERE REPAIRED PER REO 690-53-61-1410 REV -
- [SDR VNAA202407100003](https://openairdocs.org/sdr/VNAA202407100003.md): Skin · worn · May 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > IN REFERENCE TO RC TRFKE000YNZV': WEAR ON INNER SKIN IN FWD/CTR BAGGAGE BAY DOOR. WEAR ON INNER SKIN IN FWD/CTR BAGGAGE BAY DOOR REPAIRED PER REO 690-52-35-428 REV--AND REO 690-52-35-427REV -
- [SDR VNAA202407100001](https://openairdocs.org/sdr/VNAA202407100001.md): Arm · worn · May 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > IN REFERENCE TO RC TRFKE001RPE1': WEAR ON FWD/AFT COUNTERBALANCE ARMS AT FWD/CTR BAGGAGE BAY DOOR. WEAR ON FWD/AFT COUNTERBALANCE ARMS AT FWD BAGGAGE BAY DOOR AND WEAR ON AFT COUNTERBALANCE ARMS AT CTR BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-52-35-418 REV.
- [SDR VNAA202407090009](https://openairdocs.org/sdr/VNAA202407090009.md): Skin · damaged · May 29, 2024 · N584NN · Cndair CL6002D24 · Elevator, Plate/Skin
  > IN REF. TRFKE00C9EWX:EA A1-690-55-00012. 526.07FH PERM REPAIR- RH ELEVATOR UPPER SKIN TRAILING EDGE LIGHTNING STRIKE DAMAGE 1. WITHIN 526.07 FH'S. (BEFORE 19,075.19 FH) FROM SECTION I REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES
- [SDR VNAA202407090008](https://openairdocs.org/sdr/VNAA202407090008.md): Skin · damaged · May 29, 2024 · N584NN · Cndair CL6002D24 · Wing, Plate/Skin
  > IN REF. TRFKE00C9ELU:REO 690-57-21-456. 560FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED LIGTHNING STRIKE DAMAGE TO LH WING LOWER PLANK BETWEEN WS264.00-WS274.00 AND STR22-STR23 WITHIN 560FH, PERFORM A PERM REPAIR IAW APPROVED PROCEDURES. NOTE: ROTO/SHOT
- [SDR VNAA202407090007](https://openairdocs.org/sdr/VNAA202407090007.md): Fireshield · chafed · May 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Bulkhead/Firewall
  > IN REF. TRFKE00BY829:670-54-23-1164. 1500FH PERM REPAIR - SPEED TAPE APPLIED - CHAFE DAMAGE TO FWD CORE COWL FIRESHIELD PERMANENT REPAIR CORE COWL DUE TO DENT/CHAFE DAMAGE, SEE W.O. OR L.B. AND 670-54-23-1164 FOR DETAILS. CHAFE DAMAGE TO FWD CORE COWL FIRESH
- [SDR VNAA202407090006](https://openairdocs.org/sdr/VNAA202407090006.md): Fireshield · chafed · May 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Bulkhead/Firewall
  > IN REF. TRFKE00BMX8D:EA A1-690-54-00008.1265FH PERM REPAIR - RH CORE COWL FIRE SHIELD CHAFE DAMAGE WITHIN 1265 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. RH CORE COWL
- [SDR VNAA202407090004](https://openairdocs.org/sdr/VNAA202407090004.md): Arm · worn · May 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > IN REF. TRFKE009EULT:EA 22-C9-52-1205. PERM REPAIR - CENTER BAGGAGE BAY DOOR WITHIN 3,927.79 FHS FROM IR (BEFORE 19,075.19 FH), REPAIR, OR REPLACE THE DISCREPAN! ÍTEM IN ACCORDANCE WITH APPROVED PROCEDURES, WEAR ON FWD COUNTERBALANCE ARMS AT CENTER BAGGAGE BAY
- [SDR VNAA202407090003](https://openairdocs.org/sdr/VNAA202407090003.md): Fireshield · worn · May 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > IN REF. TRFKE0095XD2:EA22-C9-54-0939. PERM REPAIR - LH ENGINE FWD CORE COWL FIRE SHIELD WITHIN 4270.48 FLIGHT HOURS FROM IR (BEFORE 19,075.18 FH'S) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. REPAIRED PER REO.NO.690-54-23-3
- [SDR VNAA202407110029](https://openairdocs.org/sdr/VNAA202407110029.md): Fitting · corroded · May 14, 2024 · N584NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER FITTING BORE LUGS L1, L2, L5 AND L6 AT LH AILERON. CORROSION ON CENTER FITTING BORE LUGS L1, L2, L5 AND L6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV --
- [SDR VNAA202407110028](https://openairdocs.org/sdr/VNAA202407110028.md): Fitting · corroded · May 14, 2024 · N584NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER FITTINGS AT RH AILERON LUG HOUSING R1,R2,R3,R4,R5 AND R6. CORROSION ON CENTER FITTINGS AT RH AILERON LUG HOUSING R1,R2,R3,R4,R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV --
- [SDR VNAA202407110020](https://openairdocs.org/sdr/VNAA202407110020.md): Floorbeam · cracked · May 14, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER REMOVAL, CRACK ON FWD FLOOR SUPPORT ANGLE AT 280 FLOOR STRUCTURE. FLOOR SUPPORT ANGLE AT FS280 FLOOR STRUCTURE CRJ900 SRM 53-11-43-001-001-A01 ITEM 137
- [SDR VNAA202407110018](https://openairdocs.org/sdr/VNAA202407110018.md): Hinge Fitting · worn · May 14, 2024 · N584NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous 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.

Next page: https://openairdocs.org/aircraft/N584NN/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 = 'N584NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N584NN/reports

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