N611NN
Service difficulty reports · 26
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 = 'N611NN' 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 = 'N611NN' 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 VNAA2025102411102Sensor · not reportedRH IB BRAKE TEMP SENSOR INDICATED A STEADY 14 AFTER SELECTING GEAR DOWN. / REMOVED AND REPLACED RH INBOARD BRAKE TEMPERATURE SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01 & 32-46-01-000/400-801-A01-PSA. OPS TEST CHECKED GOOD. THIS CLEARS MEL.SDR VNAA2025052711102Thermocouple · failedBRAKE OVHT WARNING INFLIGHT. FULL STOP. RIGHT MAIN OUTBOARD GEAR / REMOVED AND REPLACED RH OUTBOARD THERMOCOUPLE SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. OPS CHECK GOOD.SDR VNAA2025011311102Valve · abnormalA/SKID FAULT STATUS MSG IN FLIGHT. / INTERROGATED MDC FOUND B1-006066 TROUBLE SHOT IAW CRJ900 FIM 32-44-06-810-811 BY CHANGING THE BRAKE METERING VALVE IAW CRJ900 AMM 32-43-36-000/400-801, OPS CHECK AND LEAK CHECK GOOD. PERFORMED OPS CHECK OF SPIN-DOWN FUNCTISDR VNAA2024100311101Unknown · odorUSUAL ORDOR COMING FROM PACKS, SIMILAR TO BURNING OIL OR ELECTRICAL. BOTH PACKS ON, RECIRC FAN ON, APU POWERED ON, ENGINES OFF. / TROUBLESHOT PER CRJ-900 FIM 21-21-00-810-806-A01. FURTHER TROUBLESHOOTING REQUIRED.SDR VNAA2024091111101Unknown · odorSMELL OF BURNING CRAYONS AND EXPIRED MILK OBSERVED BY CREW DURING RIGHT START FOLLOWED BY OBSERVED HAZE / PERFORMED AIRCRAFT ENGINE RUN FOR ABNORMAL SMELL, OPERATED LH AND RH A/C PACKS FROM FULL HOT TO FULL COLD TO MID TEMP FOR ANY ABNORMAL SMELLS, IAW CRJ 90SDR VNAA2024073011101Filter · odorBAD SMELL OF DIRTY SOCKS NOTED DURING DESCENT WHILE RH PACK SELECTED ON AND LH PACK SELECTED OFF / REMOVED AND REPLACED R/H RECIRCULATION FAN FILTER IAW CRJ900 AMM 21-22-12-400-801-A01 AND FIM 21-21-00-810-806 AND 21-22-00-810-806. OPS CHECK GOOD AND LEAK CHECSDR VNAA2024080111103Manifold · odorFOWL SMELL FROM FLIGHT DECK AIR VENTS IMMEDIATELY AFTER TAKEOFF ROTATION. SMELL WAS ON FLIGHT DECK ONLY AND SIMILAR TO SOUR MILK. SMELL CLEARED DURING CLIMB. NO SAFETY OF FLIGHT CONCERNS PRESENT. / REMOVED AND REPLACED MANIFOLD MIX IAW CRJ 900 AMM 21-22-06-00SDR VNAA2024080111102Sensor · faultedBRAKE OVHT WARNING IN FLIGHT, RIGHT OB BRAKE / REMOVED AND REPLACED RIGHT OB BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. SELF TEST OF THE TERMOCOUPLE SENSOR PASSED. NO ADDITIONAL DEFECTS NOTED AT THIS TIME.SDR VNAA2023103011101Acm · odorSTRONG ODOR IN FLIGHT DECK. SMELLS LIKE MAYBE BURNING ELECTRICAL OR SLIGHT FUEL SMELL. REMOVED AND REPLACED THE LH AIR CYCLE MACHINE (ACM) IAW CRJ900 AMM 21-51-08-000/400-801-A01 OPS CHECK AND LEACK CHECK GOOD AT THIS TIME.SDR VNAA202310260007Hinge Fitting · corrodedCORROSION ON HINGE FITTING (1EA) AT ACCESS DOOR NBR 196ER. HINGE FITTING (1EA) AT ACCESS DOOR NBR 196ER WAS REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01)SDR VNAA202310260006Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS677.00 TO FS847.00 (1EA) AND FS847.00+16.00 TO FS897.70 (1EA). SUMMARY: DUE NOT ALLOWABE DAMAGE ON LH SIDE SEAT RAIL BTW FS677.00 TO FS720.85 (1EA), FS 785.15 TO FS847.00 (1EA) AND FS847.00 + 16.00 TO FS897.70 (1EA) WERE RESDR VNAA202310260005Skin · damagedTEMPORARY DISPOSITION FOR DAMAGE TO FUSELAGE SKIN PANEL BETWEEN FS 202.75 - FS 220 & STR 14L - 15L THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 800 FLIGHT HOURS FROM. FUSELAGE SKIN BTW FS202.75 TO FS220 STGR14L TO STGR15L AND PITOT MOUNTING PLATE WERESDR VNAA202310260004Door · dentedSEVERAL DENTS ON LOWER FAN COWL DOOR BTW 7/4 O´CLOCK POSITION AT LH ENGINE. DENTS ON LOWER FAN COWL DOOR BTW 7/4 O´CLOCK POSITION AT LH ENGINE WERE REPAIRED PER REO 670-54-14-1012 REV. BSDR VNAA202310260009Drag Angle · crackedDAMAGE DESCRIPTION: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). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 6SDR VNAA202310260003Skin · wornWEAR ON LEADING EDGE PANEL 522AL AT LH WING. WEAR ON LEADING EDGE PANEL 522AL AT LH WING WAS REPAIRED PER EA 23-C9-57-1343 RIV. IR SECTION III - PERMANENT REPAIRSDR VNAA202310260002Skin · wornWEAR ON FIXED LEADING EDGE (622AR,622BR) AT RH WING. WEAR ON FIXED LEADING EDGE (622AR,622BR) AT RH WING WAS REPAIRED PER EA 23-C9-57-1356 REV. IR SECTION III - PERMANENT REPAIRSDR VNAA202310260001Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. EVALUATED, AREA ON LOWER SKIN OF RH INBOARD FLAP FLS 45.00 TO FLS 65.50, THEREFORE IT IS WITHIN OF LIMITS AND DUE NO ALLOWABLE DAMAGE AT AREA ON LOWER SKIN OF RH INBOARD FLAP FLS 1SDR VNAA202310260008Drag Angle · crackedDAMAGE DESCRIPTION: 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 67SDR VNAA202303170001Skin · unknownPERM REPAIR - TEMP REPAIR TO FUSELAGE SKIN BETWEENFS193-FS202.75 & STR14R-STR16R) PERFORM A PERMANENT REPAIR WITHIN 8000FLIGHT HOURS FROM THE TIME OF INCORPORATION OF REO 690-53-11-1385.SDR VNAA202302051111Valve · unserviceableRAM AIR SOV NOT WORKING / REMOVED AND REPLACED RAM AIR VALVE IAW CRJ-900 AMM 21-52-04-000/400-801. OPS TEST AND LEAK TEST GOOD. RH PACK SHOWS OFF ON ECS SYSTEM WHEN ON / CYCLED CS INSP PACK DISCHARGE SENSOR WIRE AND PACK TEMP SENSOR WIRE NO DEFECTS NOTED PERFOSDR VNAA202205091112Fan · unserviceableDURING LANDING A RECIRC FAN FAULT MESSAGE OCCURRED, AFTERWARDS THE CREW NOTICED A SMOKE SMELL AND ONE OF THE FLIGHT ATTENDANTS AND SOME OF THE PAX SAW SMOKE IN THE CABIN. THE A/C LANDED SAFELY WITH NO OTHER ISSUES. RECIRC FAN FAULT STATUS MESSAGE IN FLIGHT AT SDR VNAA202110051115Handle · stuckPAX DOOR WONT OPEN, HANDLE STUCK / PERFORMED MULTIPLE CYCLES OF OPENING AND CLOSING THE DOOR WITHOUT ENCOUNTERING A STUCK CONDITION. FOUND INNER DOOR HANDLE WAS ABLE TO MOVE FREELY WHILE DOOR WAS OPEN. FOUND OPEN LOCK WAS NOT ENGAGING ON LATCH CAM ASSEMBLY. DESDR VNAA202110051113Yoke · failedMAIN CABIN DOOR GOT STUCK UPON OPENING / PERFORMED OPS TEST OF PAX DOOR IAW CRJ900 AMM 52-11-00-710-801-A02. OPS TEST GOOD. SUPPLEMENTAL INFORMATION: PULLEY YOKE OF PAX DOOR SUPPORT-WHEEL SYSTEM FAILED. / REMOVED AND REPLACED PULLEY YOKE, CABLE PAX DOOR SUPPORSDR VNAA202108251111Proximity Sensor · faultedAIRCRAFT WAS OPERATING AS A FERRY FLIGHT FROM CID/CLT DUE TO PREVIOUS PRESSURIZATION PROBLEMS. AFTER DEPARTING, THE CREW RECEIVED A DOOR LATCH CAUTION MESSAGE, THE SAME OCCURRENCE THAT LED TO IT INITIALLY FERRYING. CREW RAN THE QRH, WHICH ALLOWED THEM TO CONTISDR VNAA2020032011103Unknown · odorSTRONG SMELL OF BURNING DUST ON TAKEOFF AND LANDING COMING FROM PACKS. STARTED BOTH ENGINES. PERFORMED OPERATIONAL TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM, OPS CHECK GOOD AT THIS TIME. NO SMELL OF BURNING DUST.SDR VNAA2020030201101Position Sensor · failedFLIGHT CREW HAD A REPEAT MAINTENANCE ISSUES OF STAB TRIM AND PITCH FEEL AFTER DEPARTURE FROM CLT ENROUTE TO CLE. WE DIVERTED THE AIRCRAFT TO CVG FOR MAINTENANCE, THEN CREW AND PAX WILL CONTINUE IN OTHER AIRCRAFT. INTERROGATED MDC, FOUND B1-007971. ALL ELECTRI
Back to N611NN