# Service difficulty reports: N588NN

A list on [N588NN](https://openairdocs.org/aircraft/N588NN.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 VNAA2026042716701](https://openairdocs.org/sdr/VNAA2026042716701.md): Proximity Switch · faulted · Apr 24, 2026 · N588NN · Cndair CL6002D24 · Drag Control System
  > GND SPLR DEPLOY CAUTION N FLIGHT. REMOVE AND REPLACED INBOARD GROUND PROXIMITY SWITCH IAW AMM 27-63-07-000/400€“801. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
- [SDR VNAA2026031014004](https://openairdocs.org/sdr/VNAA2026031014004.md): Sensor · unserviceable · Mar 7, 2026 · N588NN · Cndair CL6002D24 · Landing Gear Brake System
  > HAD BRAKE OVHT WARNING MSG IN FLIGHT AT ABOUT 15000 FEET CW QRC/QRH DISAPPEARED FOR 3 MINUTES THEN CAME BACK ON INTERMITTENTLY. / REMOVED AND REPLACED #4 BRAKE THERMOCOUPLE SENSOR IAW 32-46-01-000/400-801-A01.PERFORMED SELF TEST IAW 32-46-01-740-801-A01. TEST
- [SDR VNAA2025110311101](https://openairdocs.org/sdr/VNAA2025110311101.md): Acm · unserviceable · Nov 1, 2025 · N588NN · Cndair CL6002D24 · Cabin Cooling System
  > AFT FLIGHT ATTENDANT REPORTED FUMES AND A ELECTRICAL SMELL IN THE CABIN. PASSENGERS WERE COMPLAINING ABOUT THEIR EYES BURNING. THE CAPTAIN MADE THE DECISION TO RETURN TO FIELD. THEY DECLARED AN EMERGENCY WITH ATC. FIRETRUCKS MET THE AIRCRAFT ON THE ARRIVAL BAC
- [SDR VNAA20241014014](https://openairdocs.org/sdr/VNAA20241014014.md): Hinge Fitting · damaged · Oct 5, 2024 · N588NN · Bombdr CL6002D15 · Ailerons
  > DURING INSTALLATION OF AIRCRAFT BUSHING AT HINGE # 3 OUTBD, BORE WAS FOUND BIGGER DIAMETER THAN THE STANDARD AT RH AILERON. REPAIR WAS PERFORMED ON REAR SPAR RH WING AILERON HINGE 3 OUTBD LUG PER REO 690-57-51-390 REV. - -
- [SDR VNAA2024101300](https://openairdocs.org/sdr/VNAA2024101300.md): Door Frame · corroded · Sep 21, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION AROUND SETLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR. CORROSION AROUND SETLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV. - -
- [SDR VNAA20241014011](https://openairdocs.org/sdr/VNAA20241014011.md): Angle · corroded · Sep 13, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR IN REF NRC 000160: CORROSION ON ANGLE KICKPLATE WAS FOUND. CORROSION ON ANGLE KICKPLATE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WAS REPLACE
- [SDR VNAA20241014010](https://openairdocs.org/sdr/VNAA20241014010.md): Web · cracked · Sep 13, 2024 · N588NN · Bombdr CL6002D15 · 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) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA20241014009](https://openairdocs.org/sdr/VNAA20241014009.md): Support Bracket · cracked · Sep 13, 2024 · N588NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA20241014008](https://openairdocs.org/sdr/VNAA20241014008.md): Support Bracket · cracked · Sep 13, 2024 · N588NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA20241014007](https://openairdocs.org/sdr/VNAA20241014007.md): Floorbeam · cracked · Sep 13, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > RACK ON FLOOR BEAM RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR BEAM RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-1851 REV. - -
- [SDR VNAA20241014021](https://openairdocs.org/sdr/VNAA20241014021.md): Seat Track · corroded · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON LBL 9 (2 EAS) AND RBL9 (2 EAS) BTW FS693.00 TO FS977.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49. CORROSION ON ANGLE MOUNTING BTW FS
- [SDR VNAA20241014020](https://openairdocs.org/sdr/VNAA20241014020.md): Seat Track · corroded · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON LBL 9 (2 EAS) AND RBL9 (2 EAS) BTW FS693.00 TO FS977. CORROSION ON SEAT RAIL ON LBL 9 (2 EAS) AND RBL9 (2 EAS) BTW FS693.00 TO FS977.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-
- [SDR VNAA20241014019](https://openairdocs.org/sdr/VNAA20241014019.md): Seat Track · corroded · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS693. CORROSION ON SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS693.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02
- [SDR VNAA20241014018](https://openairdocs.org/sdr/VNAA20241014018.md): Seat Track · cracked · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 (5EAS) RH AND (4EAS) LH BTW FS 379.00 TO FS 669.40. CORROSION ON SIDE SEAT RAIL STGR 15 (5EAS) RH AND (4EAS) LH BTW FS 379.00 TO FS 669.40 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31
- [SDR VNAA20241014017](https://openairdocs.org/sdr/VNAA20241014017.md): Seat Track · cracked · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 (7EAS) LH AND (7EAS) RH BTW FS 669.40 TO FS 977. SIDE SEAT RAIL STGR 15 (7EAS) LH AND (7EAS) RH BTW FS 669.40 TO FS 977.00 ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE R
- [SDR VNAA20241014016](https://openairdocs.org/sdr/VNAA20241014016.md): Bracket · excess play · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Rudder Structure
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL 2103 REV B.
- [SDR VNAA20241014015](https://openairdocs.org/sdr/VNAA20241014015.md): Bracket · worn · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Rudder Structure
  > WEAR ON RUDDER BRACKET OF LOWER PCU (ACCESS PANEL 325DR) AT VERTICAL STABILIZER. RUDDER BRACKET OF LOWER PCU (ACCESS PANEL 325DR) AT VERTICAL STABILIZER WAS REPAIRED PER REO #690-55-31-088 REV.--
- [SDR VNAA20241014006](https://openairdocs.org/sdr/VNAA20241014006.md): Door Frame · corroded · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SR
- [SDR VNAA20241014005](https://openairdocs.org/sdr/VNAA20241014005.md): Skin · mechanic error · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > IN REFERENCE TO RC TRFKE00BFLD5': 2150FH PERM REPAIR - SPEED TAPE APPLIED - TEMPORARY REPAIR FOR TOOLING DAMAGE TO WING FIXED LEADING EDGE SKIN PANEL AND UNDERLYING RIB AT SS111.92, RHS WITHIN 2150 FLIGHT HOURS, REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDA
- [SDR VNAA202402280011](https://openairdocs.org/sdr/VNAA202402280011.md): Intercostal · mechanic error · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WRONG HOLES DRILLED AT INTERCOSTAL (2EAS) BTW FS847+48 TO FS847+62 RH/LH AT CABIN PAX. INTERCOSTAL (2EAS) BTW FS847+48 TO FS847+62 RH/LH AT CABIN PAX WERE REPAIRED PER REO 690-53-51-440 REV. -- AND REO 690-53-51-438 REV. --
- [SDR VNAA202402280010](https://openairdocs.org/sdr/VNAA202402280010.md): Web · corroded · Sep 12, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR WEB BTW FS349 TO FS360 RH SIDE AT CABIN PAX. FLOOR WEB BTW FS349 TO FS360 RH SIDE AT CABIN PAX WAS REPAIRED PER REO 690-53-21-1837 REV. --
- [SDR VNAA202402280009](https://openairdocs.org/sdr/VNAA202402280009.md): Floor Support · corroded · Sep 11, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL27 BTW FS1000 TO FS1065 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL27 BTW FS1000 TO FS1005 AND BTW FS1036 TO FS1065 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTUREWAS EVALUA
- [SDR VNAA20241013008](https://openairdocs.org/sdr/VNAA20241013008.md): Floor Support · corroded · Sep 11, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL9 BTW FS1000 TO FS1080 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL9 BTW FS1000 TO FS1022 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE WAS EVALUATED WITHOUT ADDITIONAL DAM
- [SDR VNAA20241013007](https://openairdocs.org/sdr/VNAA20241013007.md): Post · corroded · Sep 11, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280. CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280 WAS REMOVED PER CRJ900 SRM 51-21- 06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ-900
- [SDR VNA2024F00018](https://openairdocs.org/sdr/VNA2024F00018.md): Post · corroded · Sep 11, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280. CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280 WAS REMOVED PER CRJ900 SRM 51-21- 06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ-
- [SDR VNAA20241013006](https://openairdocs.org/sdr/VNAA20241013006.md): Floorbeam · cracked · Sep 10, 2024 · N588NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > 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 WAS REPAIRED PER REO 690-53-11-1844
- [SDR VNAA20241013005](https://openairdocs.org/sdr/VNAA20241013005.md): Support Angle · corroded · Sep 10, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE FS 279 (LBL9/RBL9) AT COCKPIT CABIN. CORROSION ON FLOOR PANEL SUPPORT ANGLE FS 279 (LBL9/RBL9) AT COCKPIT CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01
- [SDR VNAA20241014003](https://openairdocs.org/sdr/VNAA20241014003.md): Skin · worn · Sep 9, 2024 · N588NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 686AB, 692AB AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 686AB, 692AB AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-489 REV.--
- [SDR VNAA20241013003](https://openairdocs.org/sdr/VNAA20241013003.md): Bracket · corroded · Sep 9, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED (4 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT & CTR CARGO COMPARTMENT. MACHINED (4 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT & CTR CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 A
- [SDR VNAA20241013002](https://openairdocs.org/sdr/VNAA20241013002.md): Mount · cracked · Sep 9, 2024 · N588NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM). CRACK ON AF REFUEL DUCT MOUNTING SUPPORT BTW FS. 677.00 TO FS. 669.40 BTW SRGR 22 RH AND 21 RH WAS REPAIRED PER REO
- [SDR VNAA20241013001](https://openairdocs.org/sdr/VNAA20241013001.md): Support Bracket · gouged · Sep 8, 2024 · N588NN · Bombdr CL6002D15 · Nacelle/Pylon Miscellaneous Structure
  > RH ENGINE FADEC UPPER SUPPORT BRACKET OUTBOARD BOTTOM RIVET LOOSE. RH ENGINE FADEC UPPER SUPPORT BRACKET OUTBOARD BOTTOM WAS REPAIRED PER REO 690-71-61-200 REV. -A.
- [SDR VNAA20241014004](https://openairdocs.org/sdr/VNAA20241014004.md): Skin · worn · Sep 7, 2024 · N588NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRINGS (586AB, 592AB) AT LH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (586AB, 592AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-488 REV.--
- [SDR VNAA20241014002](https://openairdocs.org/sdr/VNAA20241014002.md): Housing · worn · Sep 7, 2024 · N588NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 690-52-31-107 REV. --
- [SDR VNAA20241014001](https://openairdocs.org/sdr/VNAA20241014001.md): Drag Angle · cracked · Sep 7, 2024 · N588NN · Bombdr CL6002D15 · Vertical Stabilizer
  > CRACK ON DOUBLER OF LH 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 DOBLER OF LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67
- [SDR VNAA20241014013](https://openairdocs.org/sdr/VNAA20241014013.md): Hinge Fitting · corroded · Sep 2, 2024 · N588NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON LUG R1, R2, R4, R5 AND R6 AT RH AILERON ASSY. LUG R1, R2, R5 AND R6 AT RH AILERON ASSY WERE REPAIRED PER PER REO 670-57-61-107 REV. B AND LUG R4 WAS CLEANEAD & THEREFORE IT DOES NOT PRESENT DAMAGE PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANIN
- [SDR VNAA20241014012](https://openairdocs.org/sdr/VNAA20241014012.md): Hinge Fitting · corroded · Sep 2, 2024 · N588NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > CORROSION ON HINGE 1 INB BORE, HINGE 2 INB/OUTB BORE AND HINGE 4 INB/OUT BORE AT REAR SPAR AT RH WING. HINGE 1 INB BORE, HINGE 2 INB/OUTB BORE AND HINGE 4 INB/OUT BORE AT REAR SPAR AT RH WING WERE REPAIRED PER REO 690-57-51-383 REV. -- AND ETI-190-24-010 RE
- [SDR VNAA2023053111211](https://openairdocs.org/sdr/VNAA2023053111211.md): Acm · smoke · May 27, 2023 · N588NN · Cndair CL6002D24 · Air Distribution System
  > CABIN FILLED WITH SMOKE AS WE PARKED AT THE GATE. STOPPED AFTER SHUTTING R PACK DOWN SMELLED LIKE SULFUR / TURNED ON PACK FOR T/S AND FOUND IT TO FLAG B1 CODE 211943. PACK TEMPERATURE ROSE TO 100 DEGREES C QUICKLY AND AN OVER TEMP CONDITION OCCURRED AUTOMATICA
- [SDR VNAA202305111111](https://openairdocs.org/sdr/VNAA202305111111.md): Brake Assy · unserviceable · May 10, 2023 · N588NN · Cndair CL6002D24 · Landing Gear Brake System
  > RH BRAKE EFFECTINESS ON LANDING DIMINISHED. PLANE PULLED LEFT WITH EVEN PRESSURE ON BRAKES TOO. INBD TEMP 0 1 OUTBD 0 8 SUSPECT INBD BRAKE RH SIDE NOT WORKING CORRECTLY. REMOVED AND REPLACED R/H IB BRAKE IAW CRJ900 AMM 32-43-26-000/400€“801-A02. BLEED BRAKES
- [SDR VNAA2022100999991](https://openairdocs.org/sdr/VNAA2022100999991.md): Skin · damaged · Oct 8, 2022 · N588NN · Cndair CL6002D24 · Standard Practices/Structures
  > DURING OVER NIGHT MAINTENANCE AT GREENVILLE- SPARTANBURG INTERNATIONAL AIRPORT (GSP) MAINTENANCE FOUND LIGHTNING DAMAGE ON LH FUSELAGE SKIN BETWEEN FS 319.70 - FS 517 STR 3 AND STR 21- STR 23L MFG PART NUMBERS SH670-31633-955, SH670-31351-11, SH690-33202-17 CO
- [SDR VNAA202208041112](https://openairdocs.org/sdr/VNAA202208041112.md): Pseu · unserviceable · Aug 2, 2022 · N588NN · Cndair CL6002D24 · Landing Gear System
  > GEAR DISAGREE MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THEY DID LAND OVERWEIGHT AND ALSO DECLARED AN EMERGENCY. THEY DID NOT HAVE THE CABIN BRACE. REMOVED AND REPLACED PSEU IAW CRJ 900 AMM 32-61
- [SDR VNAA202206011112](https://openairdocs.org/sdr/VNAA202206011112.md): Door · not opened · May 29, 2022 · N588NN · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN DOOR WONT OPEN. PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW CRJ 900 52-11-00-710-801 OPS CHECK GOOD."
- [SDR VNAA202105229997](https://openairdocs.org/sdr/VNAA202105229997.md): Seat Track · corroded · May 20, 2021 · N588NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT RAIL CENTER FS 581 CORRODED
- [SDR VNAA202105229996](https://openairdocs.org/sdr/VNAA202105229996.md): Seat Track · corroded · May 20, 2021 · N588NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT RAIL CENTER FS 349-549 CORRODED
- [SDR VNAA202105229995](https://openairdocs.org/sdr/VNAA202105229995.md): Seat Track · corroded · May 20, 2021 · N588NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LH SEAT RAIL OB FS364-485 CORRODED
- [SDR VNAA202105229994](https://openairdocs.org/sdr/VNAA202105229994.md): Drag Angle · cracked · May 20, 2021 · N588NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE
- [SDR VNAA202105229993](https://openairdocs.org/sdr/VNAA202105229993.md): Bracket · cracked · May 20, 2021 · N588NN · Cndair CL6002D24 · Service Doors
  > SERVICE DOOR, UPPER CONNECTING BRACKET CRACKED AT ROD ATTACHMENT POINT
- [SDR VNAA202105229992](https://openairdocs.org/sdr/VNAA202105229992.md): Diaphragm · cracked · May 20, 2021 · N588NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 0.700" IN AFT FAIRING DIAPHRAGM SH690-39316-1, AT FS 849
- [SDR VNAA2019112751101](https://openairdocs.org/sdr/VNAA2019112751101.md): Door · unknown · Nov 25, 2019 · N588NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT LATCH. MAINTENANCE REPOSITIONED THE AIRCRAFT ON THE RAMP AND THE DOOR OPERATIONS CHECKED GOOD.
- [SDR VNAA2018112911101](https://openairdocs.org/sdr/VNAA2018112911101.md): Pump · leaking · Nov 29, 2018 · N588NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), Main
  > THE AIRCRAFT DIVERTED DUE TO HYDRAULIC SYSTEM #1 LOW PRESSURE WITH ZERO QUANTITY IN FLIGHT. MAINTENANCE WAS DISPATCHED AND REPLACED THE NR 1 ENGINE DRIVEN PUMP AND ALL HYDRAULIC SYSTEM FILTERS ON THE NR 1 SYSTEM AND SERVICED THE HYDRAULIC SYSTEM.
- [SDR VNAA2018070511101](https://openairdocs.org/sdr/VNAA2018070511101.md): Pseu · malfunctioned · Jul 5, 2018 · N588NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > LANDING GEAR RETRACTION SYSTEM ON FINAL APPROACH AT APPROX. 170 KTS AND 1600 AGL GEAR EXTENSION ATTEMPT RESULTED IN RED GEAR DISAGREE MSG. AS PER QRH,CYCLED GEAR 3 TIMES WITH NO SUCCESS, RESORTED TO MANUAL EXTENSION RESULTING IN 3 DOWN AND LOCKED INDICATIONS.

Next page: https://openairdocs.org/aircraft/N588NN/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 = 'N588NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N588NN/reports

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