N588NN
Service difficulty reports · 55
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA2026042716701Proximity Switch · faultedGND 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 VNAA2026031014004Sensor · unserviceableHAD 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. TESTSDR VNAA2025110311101Acm · unserviceableAFT 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 BACSDR VNAA20241014014Hinge Fitting · damagedDURING 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 VNAA2024101300Door Frame · corrodedCORROSION 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 VNAA20241014011Angle · corrodedAFTER 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 REPLACESDR VNAA20241014010Web · crackedCRACK 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-A01SDR VNAA20241014009Support Bracket · crackedCRACK 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 VNAA20241014008Support Bracket · crackedCRACK 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 VNAA20241014007Floorbeam · crackedRACK 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 VNAA20241014021Seat Track · corrodedCORROSION 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 FSSDR VNAA20241014020Seat Track · corrodedCORROSION 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 VNAA20241014019Seat Track · corrodedCORROSION 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-A02SDR VNAA20241014018Seat Track · crackedCORROSION 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 53-31SDR VNAA20241014017Seat Track · crackedCORROSION 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 RSDR VNAA20241014016Bracket · excess playFREE 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 VNAA20241014015Bracket · wornWEAR 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 VNAA20241014006Door Frame · corrodedCORROSION 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 SRSDR VNAA20241014005Skin · mechanic errorIN 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 ACCORDASDR VNAA202402280011Intercostal · mechanic errorWRONG 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 VNAA202402280010Web · corrodedCORROSION 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 VNAA202402280009Floor Support · corrodedCORROSION 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 EVALUASDR VNAA20241013008Floor Support · corrodedCORROSION 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 DAMSDR VNAA20241013007Post · corrodedCORROSION 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-900SDR VNA2024F00018Post · corrodedCORROSION 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 VNAA20241013006Floorbeam · crackedCRACKED 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 690-53-11-1844SDR VNAA20241013005Support Angle · corrodedCORROSION 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-A01SDR VNAA20241014003Skin · wornWEAR 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 VNAA20241013003Bracket · corrodedCORROSION 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 ASDR VNAA20241013002Mount · crackedAFTER 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 VNAA20241013001Support Bracket · gougedRH 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 VNAA20241014004Skin · wornWEAR 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 VNAA20241014002Housing · wornWEAR 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 VNAA20241014001Drag Angle · crackedCRACK 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 67SDR VNAA20241014013Hinge Fitting · corrodedCORROSION 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 CLEANINSDR VNAA20241014012Hinge Fitting · corrodedCORROSION 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 RESDR VNAA2023053111211Acm · smokeCABIN 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 AUTOMATICASDR VNAA202305111111Brake Assy · unserviceableRH 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 VNAA2022100999991Skin · damagedDURING 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 COSDR VNAA202208041112Pseu · unserviceableGEAR 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 32-61SDR VNAA202206011112Door · not openedMAIN CABIN DOOR WONT OPEN. PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW CRJ 900 52-11-00-710-801 OPS CHECK GOOD."SDR VNAA202105229997Seat Track · corrodedRH SEAT RAIL CENTER FS 581 CORRODEDSDR VNAA202105229996Seat Track · corrodedRH SEAT RAIL CENTER FS 349-549 CORRODEDSDR VNAA202105229995Seat Track · corrodedLH SEAT RAIL OB FS364-485 CORRODEDSDR VNAA202105229994Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLESDR VNAA202105229993Bracket · crackedSERVICE DOOR, UPPER CONNECTING BRACKET CRACKED AT ROD ATTACHMENT POINTSDR VNAA202105229992Diaphragm · crackedCRACK 0.700" IN AFT FAIRING DIAPHRAGM SH690-39316-1, AT FS 849SDR VNAA2019112751101Door · unknownPASSENGER DOOR WILL NOT LATCH. MAINTENANCE REPOSITIONED THE AIRCRAFT ON THE RAMP AND THE DOOR OPERATIONS CHECKED GOOD.SDR VNAA2018112911101Pump · leakingTHE 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 VNAA2018070511101Pseu · malfunctionedLANDING 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.
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