# Service difficulty reports: N593NN

A list on [N593NN](https://openairdocs.org/aircraft/N593NN.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 · 55 reports

- [SDR 1Q2R2026090250021](https://openairdocs.org/sdr/1Q2R2026090250021.md): Skin · damaged · Aug 11, 2026 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING DAMAGE AT FS226 STR22L
- [SDR 1Q2R2026090250020](https://openairdocs.org/sdr/1Q2R2026090250020.md): Skin · damaged · Apr 23, 2026 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING INSPECTIO, FOUND 3 SPOTS OF LIGHTNING DAMAGE ON SKIN @ STR26R BTWN FS31-FS333
- [SDR 1Q2R2026090250017](https://openairdocs.org/sdr/1Q2R2026090250017.md): Elevator · damaged · Apr 23, 2026 · N593NN · Cndair CL6002D24 · Elevator Structure
  > LEFT ELEVATOR TRAILING EDGE WELDED BY LIGHTNING IN A TOTAL OF (4) SPOTS.
- [SDR VNAA202502110019](https://openairdocs.org/sdr/VNAA202502110019.md): Web · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00. ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR VNAA202502110020](https://openairdocs.org/sdr/VNAA202502110020.md): Frame · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS421.00 BTW STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-06-101-006-A02
- [SDR VNAA202502110021](https://openairdocs.org/sdr/VNAA202502110021.md): Skin · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN SURFACE BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH AT THE MAIN AVIONICS BAY DOOR CUTOUT. REPAIRED PER REO 690-53-21-032 REV. - -
- [SDR VNAA202502110023](https://openairdocs.org/sdr/VNAA202502110023.md): Seat Track · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00. RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00 AT CABIN PAX ARE OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02,SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101
- [SDR VNAA202502110013](https://openairdocs.org/sdr/VNAA202502110013.md): Support · cracked · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > IN REF. TO JOB CARD: TRFKE001J05D DURING INSPECTION, FOUND CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 6
- [SDR VNAA202502110024](https://openairdocs.org/sdr/VNAA202502110024.md): Seat Track · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00. RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00 AT CABIN PAX ARE OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02,SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101
- [SDR VNAA202502110025](https://openairdocs.org/sdr/VNAA202502110025.md): Seat Track · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL (4 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX. SIDE SEAT RAIL (4 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFO
- [SDR VNAA202502110026](https://openairdocs.org/sdr/VNAA202502110026.md): Seat Track · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL (4 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX. RH SIDE SEAT RAIL (4 EAS) AT STGR 15 RH, BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX ARE OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-00
- [SDR VNAA202502110027](https://openairdocs.org/sdr/VNAA202502110027.md): Seat Track · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS (9EAS) LBL 9 AND RBL 9 BTW FS 477.00 TO FS 693.00 AT PASSENGER CABIN SEAT RAILS (9EAS) LBL 9 AND RBL 9 BTW FS 477.00 TO FS 693.00 AT PASSENGER CABIN ARE OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 THER
- [SDR VNAA202502110028](https://openairdocs.org/sdr/VNAA202502110028.md): Canister · cracked · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Wing Main, Frame Structure
  > IN REFERENCE TO JOB CARD TRFKE000WKWW WAS DETECTED CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -
- [SDR VNAA202502110029](https://openairdocs.org/sdr/VNAA202502110029.md): Canister · cracked · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. REPAIRED PER REO 670-57-42-577 REV - -
- [SDR VNAA202502110030](https://openairdocs.org/sdr/VNAA202502110030.md): Skin · dented · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF RH VENTRAL FIN FAIRING. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1498 REV - -
- [SDR VNAA202502110031](https://openairdocs.org/sdr/VNAA202502110031.md): Door Frame · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Structure
  > N REF TO: DURING INSPECTION OF THE TASK CARD 53-20-220-JIC WAS DETECTED CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. EVALUATED, DUE TO EXCESSIVE DAMAGE, MID CAP BTW FS 310.00 AND 349.00 AT SURROUND STRUCTURE PASSENGER
- [SDR VNAA202502110032](https://openairdocs.org/sdr/VNAA202502110032.md): Floor Support · cracked · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPAR
- [SDR VNAA202502110033](https://openairdocs.org/sdr/VNAA202502110033.md): Door Frame · gouged · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER REMOTION OF PASSENGER DOOR////GOUGE ON SURROUND LOWER AFT SEAL AT SURROUND STRUCTURE PASSENGER DOOR. GOUGE ON SURROUND LOWER AFT SEAL AT SURROUND STRUCTURE PASSENGER DOOR WAS REPAIRED PER REO 690-53-21-1874 REV - -
- [SDR VNAA202502110034](https://openairdocs.org/sdr/VNAA202502110034.md): Floor Support · cracked · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECONDARY NRC: AFTER REMOTION OF FLOOR SUPPORT: CRACK ON ANGLE FLOOR SUPPORT RH/LH AT COCKPIT. ANGLE FLOOR SUPPORT RH/LH AT COCKPIT WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR VNAA202502110035](https://openairdocs.org/sdr/VNAA202502110035.md): Strap · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN REF TO: AFTER REMOVAL OF CHANNEL, CRACK AND CORROSION ON STRAP JOINT WAS FOUND. CORROSION ON STRAP JOINT BTW FAIRINGS 196DR AND 195DL WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE IS OUT OF LIMITS AND REPLACED PER CRJ-900 SRM 53-00-
- [SDR VNAA202502110036](https://openairdocs.org/sdr/VNAA202502110036.md): Fitting · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION WAS FOUND ON INB FITTING, OUTBD FITTING, CENTER FITTING (LUGS L1 TO L6) AT AILERON LH. L1, L3, L4 & L6 WERE CLEANING PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANING AND L2 & L5 WERE REPAIRED PER REO 670-57-61-237 REV -- PAR F
- [SDR VNAA202502110037](https://openairdocs.org/sdr/VNAA202502110037.md): Fitting · corroded · Feb 11, 2025 · N593NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION WAS FOUND ON INB FITTING, OUTBD FITTING, CENTER FITTING (LUGS R1 TO R6) AT AILERON RH. R1, R3, R4 & R6 WERE CLEANING PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANING AND R2 & R5 WERE REPAIRED PER REO 670-57-61-237 REV -- PAR F
- [SDR VNAA202502110012](https://openairdocs.org/sdr/VNAA202502110012.md): Plate · corroded · Feb 5, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICKPLATE AT PASSENGER DOOR. KICKPLATE AT PASSENGER DOOR WAS EVALUATED ARE OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA202502110016](https://openairdocs.org/sdr/VNAA202502110016.md): Drip Tray · corroded · Jan 14, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH DRIP TRAY FS280 AT FLOOR STRUCTURE. EVALUATED, EXESIVE DAMAGE IS OUT LIMITS ON RH DRIP TRAY FS280 AT FLOOR STRUCTURE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR VNAA202502110018](https://openairdocs.org/sdr/VNAA202502110018.md): Web · cracked · Jan 7, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE FS193.00. SUMMARY: ELECTRICAL BAY FLOOR WEB RIGHT SIDE FS193.00 WAS REPAIRED PER REO 690-53-11-1932 REV. --
- [SDR VNAA202502110017](https://openairdocs.org/sdr/VNAA202502110017.md): Hinge · cracked · Jan 7, 2025 · N593NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK ON FWD/MID/AFT HINGE(3E/A), MISSING DECAL AND DEGRADED BLACK/YELLOW PAINT AT STEP PLATE AFT CARGO. FWD/MID/AFT HINGE(3E/A) AT STEP PLATE AFT CARGO WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, DECAL WAS REPLACED ON ST•EP PLATE AT AFT BAGGAGE BAY P
- [SDR VNAA202502110015](https://openairdocs.org/sdr/VNAA202502110015.md): Intercostal · corroded · Jan 7, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STGR 27 TO STGR 26RH, FS 349.00 TO FS 364.00. DUE TO EXCESSIVE CORROSION ON INTERCOSTAL BTW STGR 27 TO STGR 26RH, FS 349.00 TO FS 364.00 WAS FOUND OFF OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 THEREFORE WAS REPLACED PER CR
- [SDR VNAA202502110011](https://openairdocs.org/sdr/VNAA202502110011.md): Counterbalance · nicked · Jan 7, 2025 · N593NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > NICKS AND GOUGES ON FWD/AFT COUNTERBALANCE ARMS AT FWD BAGGAGE BAY DOOR AND FWD COUNTERBALANCE ARM AT CENTER BAGGAGE BAY DOOR NICKS AND GOUGES ON FWD/AFT COUNTERBALANCE ARMS AT FWD BAGGAGE BAY DOOR AND FWD COUNTERBALANCE ARM AT CENTER BAGGAGE BAY DOOR WERE REP
- [SDR VNAA202502110014](https://openairdocs.org/sdr/VNAA202502110014.md): Bracket · corroded · Jan 6, 2025 · N593NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON PLATES (2 EAS) AND BRACKETS MACHINED (4 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. EVALUATED, PLATES (2 EAS) AND BRACKETS MACHINED (4 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT ARE OUT OF LIMITS
- [SDR VNAA202502110010](https://openairdocs.org/sdr/VNAA202502110010.md): Skin · worn · Jan 4, 2025 · N593NN · Cndair CL6002D24 · Wing, Plate/Skin
  > DURING INSPECTION OF LOWER WING SKIN: WEAR ON SETTLEMENT AREA OF ACCESS PANELS: 697AB, 695AB, 692AB, 686AB, 683AB. WEAR ON SETTLEMENT AREA OF ACCESS PANELS: 697AB, 695AB, 692AB, 686AB, 683AB. WERE REPAIRED PER REO 690-57-21-507 REV. ••·
- [SDR VNAA202502110008](https://openairdocs.org/sdr/VNAA202502110008.md): Drag Angle · cracked · Jan 4, 2025 · N593NN · 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 VNAA202502110007](https://openairdocs.org/sdr/VNAA202502110007.md): Housing · worn · Jan 4, 2025 · N593NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > INITIAL INSPECTION: WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 690-52-31-114. REV - -
- [SDR VNAA202502110006](https://openairdocs.org/sdr/VNAA202502110006.md): Floorbeam · cracked · Jan 4, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690--53-11-1922 REV
- [SDR VNAA202502110005](https://openairdocs.org/sdr/VNAA202502110005.md): Floorbeam · cracked · Jan 4, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: 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 69
- [SDR VNAA202502110004](https://openairdocs.org/sdr/VNAA202502110004.md): Skin · damaged · Jan 3, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AROUND FASTENER COUNTERSINK. AREA ON FS 663 +16 STGR- 17L (1EA) WAS REINSPECTED PER CRJ-900 SRM 51-11-00-001-001-A01 AND CRJ 900 NDT MANUAL 51-20-009-210 STEP 4. AND NO DAMAGE WAS FOUND, AND AREAS ON FS 452.5 BTW STGR20L
- [SDR VNAA202502110003](https://openairdocs.org/sdr/VNAA202502110003.md): Skin · damaged · Jan 3, 2025 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT FASTENER LOCATION. LIGHTNING STRIKES ON AREAS FS364.00 BTW STGR 21L AND STGR 22L (1EA), FS376 ON STGR 21L (1EA), FS390 ON STGR 20L (1EA), FS408 ON STGR 20L (1EA), FS437.00 BTW STGR 19L AND STGR 20L (1EA), FS46900 BTW S
- [SDR VNAA202502110002](https://openairdocs.org/sdr/VNAA202502110002.md): Nut Plate · damaged · Jan 3, 2025 · N593NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > ELONGATED HOLE AND DAMAGED NUTPLATE (P/N MS21059L3, FOR INSTALLATION OF NAS8603-4 BOLT, REF) AT 1-OFF LOCATION TO RH SLAT #2 AFT SKIN BETWEEN SLAT STA 315.75 AND TRACK 2-3. REPAIRED PER REO 690-57-42-1149 REV - -
- [SDR VNAA202502110001](https://openairdocs.org/sdr/VNAA202502110001.md): Rib · damaged · Jan 3, 2025 · N593NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > IN REFERENCE TO RC TRFKE009ALDS': 690-57-41-353-PERM REPAIR - ELONGATED HOLE ON LH INBOARD FIXED L/E MACHINED RIB AT SLAT STA. 57.16 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 5800 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV "- -" PRO
- [SDR VNAA202502110009](https://openairdocs.org/sdr/VNAA202502110009.md): Drag Angle · cracked · Nov 30, 2024 · N593NN · 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 VNAA202306121111](https://openairdocs.org/sdr/VNAA202306121111.md): Selector Valve · unserviceable · Jun 10, 2023 · N593NN · Cndair CL6002D24 · Landing Gear System
  > GEAR DISAGREE MASTER WARNING WITH GEAR HANDLE UP / REMOVED AND REPLACED PSEU IAW CRJ 900 AMM 32-61-01-000/400-801-A01.NO FIX, RETURNED TO ORIGINAL CONFIG. REMOVED AND REPLACED LG CONTROL HANDLE IAW CRJ 900 AMM 32-31-01-000/400-801. NO FIX, RETURNED TO ORIGINAL
- [SDR VNAA202305311111](https://openairdocs.org/sdr/VNAA202305311111.md): Selector Valve · faulted · May 28, 2023 · N593NN · Cndair CL6002D24 · Landing Gear System
  > SHORTLY AFTER T/O GEAR DISAGREE WARNING SOUNDS LIKE NOSE GEAR DID NOT RETRACT / SWAPPED LANDING GEAR SELECTOR VALVE IAW CRJ900 AMM 32-32-10-000/400-801. OPERATIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION IAW CRJ900 AMM 32-30-00-710-801 GOOD.
- [SDR VNAA202303091112](https://openairdocs.org/sdr/VNAA202303091112.md): Windshield · arced · Mar 6, 2023 · N593NN · Cndair CL6002D24 · Passenger Compartment Windows
  > CA WINDSHIELD CRACKED LH WINDSHIELD HEAT ARCING JUST PRIOR TO WINDOW CRACKING / REMOVED AND REPLACED CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-PSA.
- [SDR VNAA202210061111](https://openairdocs.org/sdr/VNAA202210061111.md): None · unserviceable · Oct 3, 2022 · N593NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE ON APPROACH WHEN GEAR HANDLE SELECTED DOWN. REMOVED AND REPLACED MAIN LANDING GEAR LEVER IAW AMM 32-31-01-000/400-801. REMOVED AND REPLACED MAIN LANDING GEARS SELECTOR VALVE IAW AMM 32-32-10-000/400-801 OPS TEST AND LEAK TEST GOOD
- [SDR VNAA202109099992](https://openairdocs.org/sdr/VNAA202109099992.md): Seat Track · corroded · Sep 9, 2021 · N593NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 379 TO FS 485 AT LBL9. INSTALLED REPLACEMENT SEAT RAIL AT LBL9 & FS379 TO 485 IAW CRJ900 AMM 53-00-49-400-801 CONFIG A12.
- [SDR VNAA202109099991](https://openairdocs.org/sdr/VNAA202109099991.md): Seat Track · corroded · Sep 9, 2021 · N593NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 349 TO FS 485 AT RBL9. INSTALLED REPLACEMENT SEAT RAILS AT RBL9 AT FS349 TO 485 IAW CRJ900 AMM 53-00-49-400-801 CONFIG A12.
- [SDR VNAA2020101811102](https://openairdocs.org/sdr/VNAA2020101811102.md): Sensor · failed · Oct 15, 2020 · N593NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > MX AIR RETURN TO BHM, DUE TO BRAKE OVERHEAT WARNING MESSAGE. ON CLIMB OUT OF BHM THE BTMS WAS READING 20 ON THE RT OUTBOARD BRAKE. CREW FOLLOWED THE QRH AND LOWERED THE GEAR BACK DOWN AFTER TAKEOFF. TEMP WAS NOT GOING DOWN AND PER QRH HAD TO RETURN TO NEARE
- [SDR VNAA2020062511104](https://openairdocs.org/sdr/VNAA2020062511104.md): Battery Pack · discharged · Jun 25, 2020 · N593NN · Cndair CL6002D24 · Emergency Lighting
  > LOWER EMERGENCY LIGHTS AT OVER WING EXITS INOP. MX REMOVED AND REPLACED NR 3 EPSU. OPS CHECK GOOD.
- [SDR VNAA2020031411102](https://openairdocs.org/sdr/VNAA2020031411102.md): Wire Harness · defective · Mar 12, 2020 · N593NN · Cndair CL6002D24 · Landing Gear System Wiring
  > THE CREW GOT A BRAKE OVHT CAUTION MESSAGE AFTER TAKEOFF, FOLLOWED THEIR QRH AND THE MESSAGE WENT AWAY. IT HAPPENED AGAIN ENROUTE AND THE CREW DECLARED AN EMERGENCY, WENT TO A LOWER ALTITUDE AND DROPPED THE GEAR. THEY ARE CONTINUING TO AVP. DEFERRED RH OB BRAKE
- [SDR VNAA201910021103](https://openairdocs.org/sdr/VNAA201910021103.md): Battery Pack · inoperative · Oct 1, 2019 · N593NN · Cndair CL6002D24 · Emergency Lighting
  > FA STATION EMERGENCY LIGHT SWITCH LEFT ON. REPLACED 4 EPSU BATTERIES IAW CRJ900 AMM. OPS CHECK GOOD. P/N 2013-1A S/N 169527, 503263, 126020, 500031.
- [SDR VNAA2019071711101](https://openairdocs.org/sdr/VNAA2019071711101.md): Pan · contaminated · Jul 17, 2019 · N593NN · Cndair CL6002D24 · Potable Water System
  > CREW REPORTED STRONG ODOR IN FLT DECK/VOMMIT/DEAD ANIMAL. MX LOOKED AT THE AIRCRAFT AND DETERMINED IT WASNÏ¿½T A MX ISSUE. AIR CREW REFUSES THE AIRCRAFT. CONTACTED PEST CONTROL. THEY ARE SENDING OUT A TECH TO INSPECT FOR DEAD ANIMALS. UPON INSPECTION FOUND ODO

Next page: https://openairdocs.org/aircraft/N593NN/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 = 'N593NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N593NN/reports

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