N569NN
Service difficulty reports · 42
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 = 'N569NN' 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 = 'N569NN' 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 VNAA2026030313402Acm · smokeSMOKE IN CABIN, MAINLY IN BACK OF CABIN. DENSE SMOKE IN THE TOP. REMOVED AND REPLACED RH PACK ACM IAW AMM 21-51-08-000/400-801-A01. INSTALLATION COMPLETED UP TO CLOSE OUT. PERFORMED OPS TEST AND LEAK TEST OF THE R PACK IAW AMM 21-51-00-710-801-A01 AND AMM 21-SDR VNAA2025082211102Smoke Detector · false activationUPON REACHING CRUISE ALTITUDE SMOKE ALARM WENT OFF AND CREW RAN QRH. PERFORMED OPERATIONAL TEST OF FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00-710-802-A01-PSA. OPS TEST GOOD.SDR VNAA2025060911101Start Valve · inoperativeLEFT ENG START VALVE OPENED IN FLT. EMERGENCY DECLARED. / REMOVE AND REPLACED RELAYS K23,K25,AND K31 OF JB11-PCB4 IAW CRJ 900 AMM 20-42-00-960-801-A03. REMOVED AND REINSTALLED JB1A IAW CRJ 900 AMM 24-06-09-000/400-801. PERFORMED OPERATIONAL CHECKS OF JB11 IAW SDR VNAA2024080511101Sensor · erraticBTMS RHIB INDICATION 20 AND SPARADIC IN FLIGHT / REMOVED AND REPLACED RHIB BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. OPS TEST GOOD.SDR VNAA2024071911101Windshield · arcedL WINDSHIELD ARCING IN FLIGHT / REMOVED AND REPLACED THE LH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA.OPERATIONAL TEST PERFORMED IAW CRJ 900 AMM 30-41-06-710-801 AND AMM 21-31-00-910-801.OPS.TEST GOOD AT THIS TIME.SDR VNAA2024053111101Blade · unserviceableLEFT ENGINE HIGH VIBES ON TAKEOFF. 2.0 MAX. COULDNT ADVANCE THRUST ABOVE IDLE WITHOUIT HIGH VIBES RETURN TO FIELD / REMOVED AND REPLACED FAN BLADE PINS FOR LH ENG IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. OPS CHECK GOODSDR VNAA202403070006Doubler · corrodedF.S. 280.00 L/H WEB DOUBLER IS CORRODED ON THE END AT COCKPIT ENTRANCE. REMOVED SPLICE PLATE AND CUT WEB IAW CRJ-900-SRM-53-11-10-201-004-A01 STEPS 1 AND 2, FABRICATED AND INSTALLED REPAIR PARTS FOR LH WEB REPAIR IAW CRJ-900-SRM-53-11-10-201-004-A01 CC6SDR VNAA202403070016Seat Track · corroded132686 DISCREPANCY: SEAT TRACK AT LBL 27 IS CORRODED BETWEEN FS 927 AND FS 985. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK BETWEEN FS 927 AND FS 985 AT LBL27 IAW CRJ 900 AMM 53-00-49-400-801-A12. 20275-288-0-0ASDR VNAA202403070015Angle · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED MID CAP ANGLE I.A.W. CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR VNAA202403070014Frame · corrodedFS 319.70 FRAME IS CORRODED BETWEEN STGR 25L AND STGR 27. REPAIRED FS 319.70 FRAME IAW CRJ-900 SRM 53-00-06-201-001-A03 SH670-31355-1SSDR VNAA202403070013Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR MOTOR ASSIST PULLEY LOCATION. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE AFT DRAG ANGLE P# 601R31772-5S IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.SDR VNAA202403070012Floor Skin · corrodedTHE FWD-MOST MOUNTING AREA ON THE FLOOR IS SEVERELY CORRODED/DAMAGE AND REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE FITTING P/N: CDSP2019-7C-760 AT GALLEY FWD-MOST MOUNTING AREA IAW CRJ900 SRM 51-41-02-001-001-A01. CDSP2019-7C-760SDR VNAA202403070011Seat Track · corrodedSEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.847+16 TO F.S.985 IS GOUGED AND CORRODED.. REMOVED SEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.847+16 TO F.S.985 IAW CRJ900 AMM53-00-49-000-801 (CONFIG A12) INSTALLED NEW SERVICEABLE SEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.84SDR VNAA202403070009Angle · corrodedHN00134783 DISCREPANCY: AFTER REMOVAL OF F.S 280 J ANGLE. LH FLOOR BEAM FOUND TO BE CORRODED CORRECTIVE ACTION: REMOVED AND INSTALLED NEW BEAM P/N CC670-34094-1 IAW CRJ-900-SRM-51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01 CC670-34SDR VNAA202403070010Rib · crackedFIXED L/E CLOSING RIB AT SS 446.86 IS CRACKED. REMOVED AND REPLACED FIXED L/E CLOSING RIB AT SS 446.86 IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND MHIRJ REO 690-57-41-409 REV-- DATED 2024-01-16. CC670-12529-4SDR VNAA202403070008Floorbeam · crackedF.S. 280.00 FLOORBEAM AT RBL 9.00 OUTBOARD SIDE IS CRACKED. REPLACED R/H F.S.280 FLOOR BEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 CC670-34094-2SDR VNAA202403070007Doubler · corrodedF.S. 280.00 L/H WEB DOUBLER IS CORRODED ON THE END AT COCKPIT ENTRANCE. REMOVED SPLICE PLATE AND CUT WEB IAW CRJ-900-SRM-53-11-10-201-004-A01 STEPS 1 AND 2, FABRICATED AND INSTALLED REPAIR PARTS FOR LH WEB REPAIR IAW CRJ-900-SRM-53-11-10-201-004-A01 CC6SDR VNAA202403070005Angle · corrodedF.S. 280.00, FORWARD "J" ANGLE IS HEAVILY CORRODED. UPON REMOVAL OF CHANNEL, FORWARD FACE OF F.S. 280.00 CROSSBEAM COVERED BY CHANNEL WILL NEED EVALUATED FOR CORROSION. REMOVED F.S 280 'J' ANGLE CC670-34095-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21SDR VNAA202403070004Angle · crackedHN00134375 DISCREPANCY: R/H COCKPIT SIDEPOST, LOWER AFT CLIP IS CRACKED IN RADIUS. INSTALLED NEW SERVICEABLE RH COCKPIT LOWER AFT FITTING PN/ GC212-0045-4S IAW CRJ900 SRM 51-42-21-001-001-A01 GC212-0045-4SDR VNAA202403070003Skin · corrodedPAX DOOR INNER SKIN FOUND CORRODED IN MULTIPLE AREAS. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER SKIN P/N:601R318024-15 IAW CRJ900 SRM 51-40-11-001-001-A01. REFERENCE JOB CARD HN00133323 FOR INSTALL.SDR VNAA202403070002Slat Track · crackedRIGHT SLAT TRACK 3-3 IS CHAFED. CHAFE IS APPROX 0.250 LONG, 0.250 WIDE AND 0.010 DEEP. REPAIRED SLAT TRACK 3-3 IAW MHIRJ REO 690-57-42-1020 REV-- DATED 1-2-24 CC670-12092-9SDR VNAA202403070001Seat Track · corrodedSEAT TRACK SEGMENT AT LBL9 BETWEEN F.S.847+16 TO F.S.985 IS CORRODED.. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL9 BETWEEN F.S.847+16 TO F.S.985 IAW CRJ 900 AMM 53-00-49-400-801-A12SDR VNAA202308311111Unknown · unknownDEPARTING OFF 18L, APPLIED FULL POWER AND THEY IMMEDIATELY SMELLED AND SAW SMOKE COMING OUT OF GASPER / RE-PERFORMED POST COMP WASH EVACUATION RUN AS REQUIRED FOR L ENGINE BLEED IAW CRJ-900 AMM 72ˆ’00ˆ’00ˆ’100ˆ’803ˆ’A01ˆ’PSA. NO FUMES OR SMOKE NOTED AFTESDR VNAA202307261111Sensor · faultedBRAKE OVHT WARNIMG MESSAGE IN FLIGHT. REMOVED AND REPLACED LOB BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801. SELF TEST OF THE THERMOCOUPLE SENSOR GOOD PER AMM 32-46-01-740-801. THIS CLEARS MEL.SDR VNAA202306221111Unknown · unknownLOUD HISSING NOISE AT FLT LV 230 FELT PRESS CHANGE DECLARED EMERGENCY. INSPECTS PAX SEAL FOUND SEAL IN LWR RH CORNER TO BE LOOSE AND OUT OF TRACK. REINSTALLED SEAL INTO TRACK CLEAN SEAL AND PREFOMED PRESS CK NO LEAKS NOTED. SYS LEAK CHECK GOOD AT THIS TIME IAWSDR VNAA202303091111None · noneSTRONG SMELL IN CABIN RECORDED BY BOTH FA'S AND SEVERAL PAX RIGHT AFTER PUSHBACK COCKPIT INDICATIONS NORMAL. C/W RIGHT HAND ENGINE WASH IAW CRJ 900 AMM 72-00-00-100-803-A01-PSA.SDR VNAA202109131111Gcu · malfunctionedWHILE ENROUTE TO ECP, CAPTAIN STATED THAT THE COCKPIT WENT DARK AND WHEN THE LIGHTS CAME BACK ON THEY HAD AN AC ESS BUS FAIL MESSAGE. CREW FOLLOWED THE QRH WITH NO VALID RESULTS. DECIDED TO RETURN TO CLT. CAPTAIN DID DECLARE GOING BACK AND THEN CANCELED THE EMSDR VNAA2020073111101Warning Message · false activationOB FLT SPOILER OB SPOILERONS CAUTION MSGS IN FLIGHT. CW SELF TEST OF THE SSCU IAW AMM OPS CHECK GOOD.SDR VNAA2020032421101Warning System · false activationCREW HAD A STEERING INOP CAUTION MESSAGE EN ROUTE TO OAJ. THE CREW FOLLOWED THEIR QRH AND AIR RETURNED BACK TO CLT. THEY DECLARED AN EMERGENCY AS A PRECAUTION BUT ONCE THE CREW LANDED SAFELY AND WAS TAXIING ON THEIR OWN THE EMERGENCY CREWS WERE CALLED OFF. THESDR VNAA202003229994Web · crackedMULTIPLE CRACKS LOCATED ON PAX DOOR AFT WEB BENEATH STRUT.INSTALLED REPAIR PARTS IAW CRJ 900 SRM 52-11-04-201-004-A01.SDR VNAA202003229993Web · crackedCRACKS FOUND DOING REPAIR OF PAX DOOR AFT WEB, CRACKS LOCATED IN STEP REDIUS OF 2ND & 3RD STEP OF AFT WEB. FABRICATED REPAIR PARTS IAW CRJ900 SRM 52-11-04-201-004-A01. INSTALLED REPAIR PARTS IAW CRJ900 SRM 52-11-04-201-004-A01SDR VNAA202003229992Web · crackedMULTIPLE CRACKS LOCATED ON PAX DOOR AFT WEB BENEATH STRUT.CUTOUT DAMAGE IAW CRJ900 SRM 52-11-04-201-004-A01. REPAIR ZONE 4 TYPE 2SDR VNAA202003229991Frame · corrodedLOWER FRAME SECTOR AT F.S. 310.00 CORRODED BETWEEN STR 26L & 26R, FWD & ACT FACE. COMPLIED WITH STEPS 1-3 OF CRJ 900 SRM 53-00-06-201-006-A01 FOR 201 SPLICE REPAIR.SDR VNAA2020010211101Cabin Pressure · malfunctionedCREW HAD A CABIN ALTITUDE ISSUE AFTER TAKEOFF SO THEY DECLARED AN EMERGENCY AND RETURNED TO CLT WHERE THEY LANDED WITHOUT FURTHER INCIDENT. PERFORMED OPERATION TEST OF PRESS CONTROL SYSTEM IN MAN MODE, OPS CHECK GOOD.SDR VNAA2019072311101Wire Harness · chafedDURING APPROACH. THE CREW RECEIVED A MAIN LANDING GEAR OVERHEAT WARNING MESSAGE. THE CREW RAN THE QRH AND WAS UNABLE TO GET THE MESSAGE TO EXTINGUISH. TEMPERATURES WERE NORMAL DURING THE APPROACH. FOLLOWING THE QRH THE CREW DECLARED AN EMERGENCY AND THE TRUCKSSDR VNAA2019053111101Panel · cracked690-52-11-565 (CRACKS IN PAX DOOR ZONE 2) C/W PERM REPAIR IAW GREO 670-52-11-287 REV E. "CONTINUATION OF SDR REPORT VNAA2019053111101 (ADDITIONAL CRACK FOUND WHILE INSPECTION EXISTING CRACK IN PAX DOOR ZONE 2)"SDR VNAA2017072311101Unknown · odorAIRCRAFT PUSHED BACK FROM THE GATE AND AFTER THE CREW STARTED THE RIGHT ENGINE THEY REPORTED THAT A SMOKE ODOR WAS PRESENT IN THE COCKPIT AND CABIN AND THAT THE GROUND CREW COULD ALSO DETECT THE ODOR IN THE AFT CARGO BAY. THE WAS AIRCRAFT PUSHED BACK TO THE GASDR VNAA2016121500029Mcu · faultySTABILIZER AND MACH TRIM FAIL MESSAGE. REMOVED AND REPLACED MCU.SDR VNAA2016102900037Outflow Valve · inoperativeCABIN ALTITUDE CAUTION MESSAGE DURING CRUISE. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO THE NEAREST SUITABLE MAINTENANCE FACILITY. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE OUTSDR VNAA2016101200013Acm · failedRIGHT A/C PACK AUTO FAIL MESSAGE AND RIGHT TEMP 99C DURING TAXI, CREW ALSO REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT ACM DIFFICULT TO ROTATE. MAINTENANCE REMOVED AND REPLACED RIGHT ACM AND PERFORMEDSDR VNAA2016030800013Pressure Sensor · dirtyCREW REPORTED RECEIVING A LT MAIN EJECTOR CAUTION MESSAGE, ALONG WITH THE FUEL BOOST PUMPS CYCLING DURING CRUISE AT FL220. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED THE LT PRIMARY EJECTOR’S PRESSURE SENSOR CONNESDR VNAA2015062500037Tire · failedRT INBD TIRE BLEW WHILE LANDING. R & R BOTH RT MLG WHEEL, TIRE ASSEMBLIES,
Back to N569NN