# Service difficulty reports: N595NN

A list on [N595NN](https://openairdocs.org/aircraft/N595NN.md).

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

- [SDR VNAA2025111211101](https://openairdocs.org/sdr/VNAA2025111211101.md): Smoke Detector · false activation · Nov 11, 2025 · N595NN · Cndair CL6002D24 · Smoke Detection
  > SMOKE FWD LAV WARNING DISP IN FLIGHT. COMPLETED QRC DIVERTED MEM / PERFORMED OPS CHECK OF FWD LAV SMOKE DETECTOR IAW AMM 26-16-00-710-804-A01-PSA. NO DEFECTS NOTED AT THIS TIME. NO BURN MARKS NOTED.
- [SDR VNAA2025041411103](https://openairdocs.org/sdr/VNAA2025041411103.md): Sink · clogged · Apr 13, 2025 · N595NN · Cndair CL6002D24 · Lavatories
  > AFT LAV SINK OVER FLOWED, CAUSED SMOKE AFT LAV TO DISPLAY ON ED1 VISIBLE SMOKE IN LAV, SINK FAUCET CAME OFF COMPLETELY. VISIBLE SMOKE WAS NOTED IN THE AFT LAV, AND NO MEDICAL ATTENTION WAS REQUIRED / OPENED UP ALL COMPARTMENTS FOR DETAILED INTERNAL GVI INSPECT
- [SDR VNAA202501210030](https://openairdocs.org/sdr/VNAA202501210030.md): Seat Track · cracked · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MANUFACTURING PART. IN REFERENCE NRC 00218: FABRICATE FITTING SEAT TRACK P/N: 9401251-1 (2 EAS) IN REFERENCE TO EA NO: A1-690-25-00357 MMARY OF NRC 00218: FITTING SEAT TRACK P/N: 9401251-1 (2 EAS) WERE FABRICATED PER EA NO: A1-690-25-00357.
- [SDR VNAA202501210025](https://openairdocs.org/sdr/VNAA202501210025.md): Seat Track · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS (4 EAS) AT RBL9/LBL9 FROM FS693 TO FS 969.00 CORROSION ON SEAT RAILS (4 EAS) AT RBL9/LBL9 FROM FS693 TO FS 969.00 AT PASSENGER CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-
- [SDR VNAA202501210024](https://openairdocs.org/sdr/VNAA202501210024.md): Seat Track · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15LH FROM FS744.15 TO FS 969.00 CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15LH FROM FS744.15 TO FS 969.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-49-10
- [SDR VNAA202501210023](https://openairdocs.org/sdr/VNAA202501210023.md): Seat Track · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15RH FROM FS744.15 TO FS 969.00. CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15RH FROM FS744.15 TO FS 969.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-49-101-
- [SDR VNAA202501210022](https://openairdocs.org/sdr/VNAA202501210022.md): Seat Track · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS LBL9 (3 EAS), LBL27 (2 EAS) AND RBL9 (5 EAS) BETWEEN FS447.40 TO FS693.00 AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 (3 EAS), LBL27 (2 EAS) AND RBL9 (5 EAS) BETWEEN FS447.40 TO FS693.00 AT PASSENGER CABIN WAS REMOVED PER CRJ900
- [SDR VNAA202501210021](https://openairdocs.org/sdr/VNAA202501210021.md): Seat Track · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS LBL9 (1 EA), LBL27 (1 EA) AND RBL9 (1 EA) BETWEEN FS 349.00 TO FS 477.40 AT PASSENGER CABIN, CORROSION ON SEAT RAIL LBL27 (1 EA) AND RBL9 (1 EA) BETWEEN FS 349.00 TO FS 477.40 AT PASSENGER CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-
- [SDR VNAA202501210019](https://openairdocs.org/sdr/VNAA202501210019.md): Stringer · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 20LH BTW FS310.00 AND FS333.00 CORROSION ON STGR 20LH BTW FS310.00 AND FS333.00 WAS ATTENDED PER REO 690-53-21-1863 REV.--.
- [SDR VNAA202501210018](https://openairdocs.org/sdr/VNAA202501210018.md): Floor Support · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP BTW FS 310.00 AND 333.00 LBL 43. MID CAP BTW FS 310.00 AND 333.00 LBL 43 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01
- [SDR VNAA202501210017](https://openairdocs.org/sdr/VNAA202501210017.md): Floor Support · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY FLOOR SUPPORTS (5EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FWD FUSELAGE FLOOR STRUCTURE. PER CRJ-900 SRM 51-42-21-001-001-A01 AND GALLEY FLOOR SUPPORT (1EAS) LOCATED BTW FS 280.00 - FS 295.00 WAS CLEANED PER CRJ900 SRM 51-26-00-001-
- [SDR VNAA202501210014](https://openairdocs.org/sdr/VNAA202501210014.md): Intercostal · corroded · Jan 18, 2025 · N595NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 AND STGR 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 AND STGR 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED W
- [SDR VNAA202501210016](https://openairdocs.org/sdr/VNAA202501210016.md): Access Panel · corroded · Jan 17, 2025 · N595NN · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING CORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING WAS REPAIRED PER REO 690-57-31-251 REV- -
- [SDR VNAA20250121007](https://openairdocs.org/sdr/VNAA20250121007.md): Track · cracked · Jan 17, 2025 · N595NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON STRUCTURE OF THE AFT DOOR TRACK AT AFT BAGGAGE BAY DOOR CRACK ON STRUCTURE OF THE AFT DOOR TRACK (DIAPHRAGM) AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01.
- [SDR VNAA2025012100 13](https://openairdocs.org/sdr/VNAA2025012100%2013.md): Intercostal · corroded · Jan 17, 2025 · N595NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 349.00 TO FS= 364.00 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 349.00 TO FS.364 STG 20RH AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-21-0
- [SDR VNAA202501210012](https://openairdocs.org/sdr/VNAA202501210012.md): Floorbeam · corroded · Jan 17, 2025 · N595NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CK 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 COMPARTMENT FLOOR STRUCTURE B
- [SDR VNAA202501210026](https://openairdocs.org/sdr/VNAA202501210026.md): Hinge Fitting · excess play · Jan 16, 2025 · N595NN · Cndair CL6002D24 · Vertical Stabilizer
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. CORRECTIVE ACTION: SUMMARY: HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.
- [SDR VNAA202501210028](https://openairdocs.org/sdr/VNAA202501210028.md): Canister · cracked · Jan 15, 2025 · N595NN · Cndair CL6002D24 · Fuel Storage
  > CRACK IN CANISTER NO.3, STA. WS148 OF INTERNAL LH MAIN FUEL TANK CRACK IN CANISTER NO.3, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.
- [SDR VNAA20250121009](https://openairdocs.org/sdr/VNAA20250121009.md): Plate · corroded · Jan 15, 2025 · N595NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202501210027](https://openairdocs.org/sdr/VNAA202501210027.md): Canister · cracked · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Fuel Storage
  > CRACK IN CANISTER NO.3, STA. WS148 OF INTERNAL RH MAIN FUEL TANK CANISTER WELDED NO. 3 IN STA WS 148.00 RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
- [SDR VNAA202501210015](https://openairdocs.org/sdr/VNAA202501210015.md): Intercostal · corroded · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM-51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR VNAA20250121008](https://openairdocs.org/sdr/VNAA20250121008.md): Skin · dented · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF THE TASK CARD 200-01-JIC. IT WAS DETECTED DENT ON SKIN RH BTW FS 169.00 TO FS 177.00 AT FWD FUSELAGE DENT ON SKIN RH BTW FS 169.00 TO FS 177.00 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-11-1925 REV - -
- [SDR VNAA20250121006](https://openairdocs.org/sdr/VNAA20250121006.md): Drag Angle · cracked · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACKS ON RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES). RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR VNAA20250121005](https://openairdocs.org/sdr/VNAA20250121005.md): Fairing · elongated · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > BULLET FAIRING FWD FRAME ELONGATED FASTENER HOLE BULLET FAIRING FWD FRAME ELONGATED FASTENER HOLE WAS REPAIRED PER REO 690-55-32-188 REV.--
- [SDR VNAA20250121004](https://openairdocs.org/sdr/VNAA20250121004.md): Arm · excess play · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > FWD BAGGAGE BAY DOOR FWD INNER ARM WITHIN 2099.65 FLIGHT HOURS AFTER SECTION I (3963.35FH FROM EA 23-C9-52- 0913 RELEASE) (BEFORE 19,894.41 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES.CORRECTIVE ACTION: SUMMARY: FWD BAGG
- [SDR VNAA20250121003](https://openairdocs.org/sdr/VNAA20250121003.md): Fan Cowl · dented · Jan 14, 2025 · N595NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > TRFKE00AP6E2:EA23-C9-54-0795-PERM REPAIR BEFORE 19,894.41 FH - DOOR ASSY, FAN COWL, LWR (LH)ORRECTIVE ACTION: SUMMARY: DOOR ASSY, FAN COWL, LWR (LH) WAS REPAIRED PER REO 670-54-14-1012. REV. B. AND REO 690-54-14-761 REV -- (P1).
- [SDR VNAA20250121001](https://openairdocs.org/sdr/VNAA20250121001.md): Floorbeam · corroded · Jan 14, 2025 · N595NN · 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 690-53-11-1914 REV --
- [SDR VNAA202501210029](https://openairdocs.org/sdr/VNAA202501210029.md): Floorbeam · corroded · Dec 26, 2024 · N595NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION AT MOUNTING ANGLE AND 3 LOWER SILL ANGLES (WEB FLOOR PROTECTOR ANGLES) OF SERVICE DOOR SURROUND STRUCTURE. CORROSION ON 3 LOWER SILL ANGLES (WEB FLOOR PROTECTOR ANGLES) OF SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED WITHIN LIMITS PER
- [SDR VNAA20250121002](https://openairdocs.org/sdr/VNAA20250121002.md): Seat Track · damaged · Dec 26, 2024 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > TEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS WAS PERFORMED PER REO 670-53-11-210 REV-D
- [SDR VNAA202501210020](https://openairdocs.org/sdr/VNAA202501210020.md): Seat Track · corroded · Dec 18, 2024 · N595NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL (2 EAS) OF STRG 15RH/STRG 15LH BETWEEN FS669.40 TO FS720.85 CORROSION AT SIDE SEAT RAIL (2EAS) OF STRG 15RH/STRG 15LH BETWEEN FS669.40 TO FS720.85 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER C
- [SDR VNAA202501210011](https://openairdocs.org/sdr/VNAA202501210011.md): Skin · worn · Dec 16, 2024 · N595NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WAS REPAIRED PER REO 690-53-21-032 REV. ••
- [SDR VNAA2024090211101](https://openairdocs.org/sdr/VNAA2024090211101.md): Acm · odor · Aug 29, 2024 · N595NN · Cndair CL6002D24 · Cabin Cooling System
  > STRONG SMELL IN CABIN WITH HAZY AIR. R PACK TEMP CLIMBED TO 73C. / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801. OPERATIONAL CHECK GOOD NO FAULTS, LEAK CHECK GOOD.
- [SDR VNAA2024011711101](https://openairdocs.org/sdr/VNAA2024011711101.md): Cover · missing · Jan 15, 2024 · N595NN · Cndair CL6002D24 · Service Doors
  > UPON FURTHER INSPECTION NOTED COVER MISSING FOR LOW PRESSURE GROUND AIR CONNECTION AND LANYARD END FRAYED. REF. CRJ900 AMM 21-20-02-400-801-A01 / INSTALLED NEW LOW PRESSURE GROUND AIR CONNECTION COVER IAW CRJ 900 AMM 21-20-02-400-801-A01. REMOVED AND REPLACED
- [SDR VNAA202306061111](https://openairdocs.org/sdr/VNAA202306061111.md): Acm · smoke · Jun 3, 2023 · N595NN · Cndair CL6002D24 · Cabin Cooling System
  > SMOKE IN THE CABIN / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801. REMOVED AND REPLACED MT20 IAW CRJ-900 AMM 21-51-10-000/400-801. RH PACK FAULT CLEARED. ALL OPS CHECKS AND LEAK CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR VNAA202208021111](https://openairdocs.org/sdr/VNAA202208021111.md): Spoiler · warning message · Jul 31, 2022 · N595NN · Cndair CL6002D24 · Drag Control System
  > CA OF 5646 ON TAIL 595 DECLARED EMERGENCY AT 2230Z FOR FLT SPLRS CAUTION MESSAGE IN FLIGHT, LANDED SAFELY WITH NO INJURIES, NO O2 MASKS, AND NO CALL FOR BRACE. TRUCKS ROLLED AND CA HAD THEM STANDBY TO BE SAFE UNTIL HE LANDED AND THEY WERE CLEARED OUT. IB FLT S
- [SDR VNAA202110181111](https://openairdocs.org/sdr/VNAA202110181111.md): Acm · smoke · Oct 14, 2021 · N595NN · Cndair CL6002D24 · Cabin Cooling System
  > AT 1000FT ABOUT 3-4NM OUT OF KGSP THE CREW HAD REALIZED THERE WAS SMOKE IN THE CABIN/COCKPIT. PILOTS WERE THEN NOTIFIED OF A LH PACJK FAILURE. CREW LANDED SAFELY ON THE GROUND AT 1758. DISPATCH WAS NOT NOTIFIED OF THE OCCURANCE UNTIL 1805Z, THEY BLOCKED IN AT
- [SDR VNAA202107201111](https://openairdocs.org/sdr/VNAA202107201111.md): Selector Valve · malfunctioned · Jul 16, 2021 · N595NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE RED MESSAGE WITH GEAR SELECT DOWN GOING INTO BHM. THE GEAR EMERGENCY HANDLE WAS USED, BUT NO EMERGNCY WAS DECLARED. AIRCRAFT LANDED SAFELY IN BHM. THEY HAD TO BE TOWED INTO THE GATE. R+R MLG SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801-A01
- [SDR VNAA202104121111](https://openairdocs.org/sdr/VNAA202104121111.md): Skin · scratched · Apr 7, 2021 · N595NN · Cndair CL6002D24 · Passenger/Crew Doors
  > DURING SCHEDULED MAINTENANCE AT CVG THE MAIN CABIN (PAX) OUTER DOOR SKIN WAS REPORTED TO BE SCRATCHED / GOUGED ON THE UPPER FORWARD CORNER OF THE DOOR. DAMAGE WAS REPORTED AT SIX (6) LOCATIONS. SEE FIGURE 1 SHEET 1-3 FOR SIZE AND LOCATION OF DAMAGE. / PER ENGI
- [SDR VNAA202102041111](https://openairdocs.org/sdr/VNAA202102041111.md): Shutoff Valve · unserviceable · Feb 1, 2021 · N595NN · Cndair CL6002D24 · Air Intake Anti/De-Ice System
  > AFTER BEING CLEARED FOR TAKEOFF IN TYS, CREW REPORTED A REJECTED TAKE OFF WHILE ON RWY 23L, AT 2KTS. CREW REPORTED A LT ENG BLEED (C) MSG. AIRCRAFT RETURN TO GATE. R & R LT COWL ANTI-ICE SOV IAW CRJ900 AMM 30-22-01-000/400-801-A01. OPS CHECK GOOD.
- [SDR VNAA2020111211211](https://openairdocs.org/sdr/VNAA2020111211211.md): Warning Message · illuminated · Nov 10, 2020 · N595NN · Cndair CL6002D24 · Drag Control System
  > MAINTENANCE EMERGENCY FOR INBOARD SPOILERONS CAUTION MESSAGE IN FLIGHT. CREW DID NOT HAVE PASSENGERS BRACE OR THE FIRE TRUCKS ROLL. WAS ABLE TO LAND SAFELY AND TAXI TO GATE UNDER OWN POWER.
- [SDR VNAA2020022751101](https://openairdocs.org/sdr/VNAA2020022751101.md): Windshield · arced · Feb 25, 2020 · N595NN · Cndair CL6002D24 · Flight Compartment Windows
  > IN FLIGHT THE CAPTAINS SIDE WINDSHIELD HEAT TERMINAL BLOCK BEGAN TO SMOKE AND STRONG ELECTRICAL BURNING. REMOVED AND REPLACED WINDSHIELD (LH) IAW CRJ 900 AMM. LEAK AND OPS CHECK GOOD.
- [SDR VNAA2020021501101](https://openairdocs.org/sdr/VNAA2020021501101.md): Motor · failed · Feb 10, 2020 · N595NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), Main
  > CREW LOST HYDRAULIC SYSTEM 3 DURING APPROACH INTO ATL. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX REPLENISHED HYDRAULIC SYSTEM 3 TO CORRECT LEVEL. REMOVED AND REPLACED #3B HYDRAULIC PUMP DUE TO HYDRAULIC FLUID STARVATION IAW CRJ 900 AM
- [SDR VNAA202001031102](https://openairdocs.org/sdr/VNAA202001031102.md): Warning Message · false activation · Jan 1, 2020 · N595NN · Cndair CL6002D24 · Drag Control System
  > OB SPLRNS AND OB FLT SPLRS AMBER MESSAGE. PERFORMED SYSTEM RESET, PROBLEM DID NOT REOCCUR
- [SDR VNAA20191212101](https://openairdocs.org/sdr/VNAA20191212101.md): Warning Message · false activation · Dec 11, 2019 · N595NN · Cndair CL6002D24 · Drag Control System
  > AT FL100 FLIGHT 5345 RECEIVED INBOARD FLIGHT SPOILERONS AND SPOILER CAUTION MESSAGE. CAPT FOLLOWED QRH WHILE FO FLEW THE AC. PAX WERE NOTIFIED OF THE EMERGENCY LANDING BY THE FLIGHT ATTENDANTS. THE AC LANDED SAFELY AND TAXI TO THE GATE UNDER OWN POWER. EMERGEN
- [SDR VNAA201908121101](https://openairdocs.org/sdr/VNAA201908121101.md): Windshield · cracked · Aug 10, 2019 · N595NN · Cndair CL6002D24 · Flight Compartment Windows
  > CLIMBING TO 17000, CAPTAIN SIDE WINDSHIELD CRACKED. CREW DECLARED EMERGENCY BACK TO DEPARTURE, WHERE CABIN WAS PREPPED FOR EMERGENCY LANDING. EMERGENCY EQUIPMENT RESPONDED AND AIRCRAFT WAS ABLE TO TAXI BACK TO GATE. MAINTENANCE REMOVED AND REPLACED LEFT WINDO
- [SDR VNAA2019100121001](https://openairdocs.org/sdr/VNAA2019100121001.md): Battery Pack · inoperative · Feb 10, 2019 · N595NN · Cndair CL6002D24 · Emergency Lighting
  > MULTIPLE FWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED 3 EMERGENCY LIGHT BATTERIES. P/N 2013-1A S/N 6114, 87108, 121690. OPS CHECKED GOOD.
- [SDR VNAA2019011511101](https://openairdocs.org/sdr/VNAA2019011511101.md): Shutoff Valve · malfunctioned · Jan 15, 2019 · N595NN · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > RECIVED A LT AND RT WING ANITICE CAUTION MSG ON DESCENT INTO MSN. CREW DECLARED AND LANDED WITHOUT INCIDENT. OUTSTATION MAINTENANCE REMOVED AND REPLACED THE LH WING A/I MODULATING SOV. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR VNAA2018092711101](https://openairdocs.org/sdr/VNAA2018092711101.md): Acm · failed · Sep 27, 2018 · N595NN · Cndair CL6002D24 · Cabin Cooling System
  > SUPPLEMENTAL INFORMATION: MX REMOVED AND REPLACED RH ACM. OPS AND LEAK CHECK GOOD. THIS CLEARS MEL
- [SDR VNAA2017100811101](https://openairdocs.org/sdr/VNAA2017100811101.md): A/C Pack · failed · Oct 8, 2017 · N595NN · Cndair CL6002D24 · Cabin Cooling System
  > DURING TAXI, RECEIVED A RT PACK AUTO FAIL MESSAGE AND THE FLIGHT ATTENDANT SMELLED SMOKE.
- [SDR VNAA2016121200021](https://openairdocs.org/sdr/VNAA2016121200021.md): Sign · broken · Dec 12, 2016 · N595NN · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT AT PASSENDOR DOOR BROKEN. SECURED HARDWARE ON ENTRANCE COMPARTMENT EMERGENCY EXIT SIGN.

## 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 = 'N595NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N595NN/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.