N950AR, cancelled Oct 3, 2020
Service difficulty reports · 18
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 = 'N950AR' AND deregistration_id = 'N950AR-2020-10-03' 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 = 'N950AR' AND deregistration_id = 'N950AR-2020-10-03' 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 WRN2016F00000Skin · delaminatedHIGH VIBRATION ON CLIMB CONTINUED FOR REMAINDER OF FLIGHT. FOUND RT WING NR 2 SPOILER DELAMINATED.SDR WRNA201601080003Spoiler · delaminatedRETURNED TO DEPARTURE DUE TO HIGH STRUCTURE VIBRATION ON CLIMB PHASE PASSING 16,000 AND REMAINED FOR REST OF FLIGHT.SDR WRNA20140027Skin · dentedDURING POSTFLIGHT WALKAROUND, FOUND A DENT ON FUSELAGE FWD OF THE FWD CARGO DOOR. REPAIRED IAW STS EO 100-2014-114. ALL WORK DOCUMENTED ON NR 26850, 002651, 003002.SDR WRNA201409040023Pitot Line · contaminatedTHE CREW REPORTED THAT DURING TAKEOFF, THERE WAS AN AIRSPEED DIFFERENCE AFTER 80KTS. THE F/O AIRSPEED INDICATOR DROPPED TO 55 KTS WHILE THE CAPTAIN’S AIRSPEED INDICATOR READ 95 KTS. REJECTED TAKEOFF AT 95 KIAS AND TAXIED BACK TO THE RAMP WITHOUT ANY FURTHER SDR WRNA201407230015Engine · making metalON REACHING TOP OF CLIMB, A LEVEL 2 OIL PRESSURE LOW DISPLAYED. CREW FOLLOWED THE QRH PROCEDURES SIMULTANEOUSLY FOLLOWING THE QRH PROCEDURES "ENGINE SHUTDOWN IN FLIGHT" FOR ENG NR 2. THE CREW ACCOMPLISHED THE CHECKLIST THEN PROCEEDED TO DUMP APPROXIMATELY 50SDR WRNA201406260013Fitting · crackedDURING HEAVY CHECK, MAIN DECK CARGO HANDLING SYSTEM, CENTERLINE RESTRAINT ASSY SIDE FITTINGS WERE FOUND CRACKED. R & R 38 EACH CENTERLINE RESTRAINTS SIDE FITTINGS. REPAIR OF SIDE FITTINGS ACCOMPLISHED IAW EO SLC-121214.SDR WRNA201406260012Floor Panel · damagedDURING HEAVY CHECK, FLIGHT COMPARTMENT, MAIN DECK, AND LOWER CARGO COMPARTMENT FLOOR PANELS WERE FOUND DAMAGED. REPAIRED FLOOR PANELS IAW EO SLC-140313.SDR WRNA20140011Plate · corrodedDURING HEAVY CHECK, LT WING UPPER PLATE AT LWS 160 AND S15L WAS FOUND TO BE CORRODED. DAMAGE REPAIRED IAW EO SLC-140317.SDR WRNA201406260010Plate · corrodedDURING HEAVY CHECK, UPPER PLATING AROUND BS 1229 AROUND RBL 8 FOUND CORRODED. REPAIRED IAW EO SLC-140611.SDR WRNA201406260009Plate · corrodedDURING HEAVY MAINTENANCE, MAINTENANCE FOUND UPPER PLATING AROUND BS 1229 BETWEEN RBL 57 TO 78 CORRODED. REPAIRED IAW EO SLC-140609.SDR WRNA201200011Hydraulic Line · brokenHYD NR 3 FAIL DURING CRUISE, FL380 20 MIN FROM SVMI. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. MX FOUND PIPE ASSY BROKEN, TO HORIZONTAL STAB TRIM MOTOR NR 1. REMOVED AND REPLACED HYD LINE IAW 27-43-04. PERFORMED SYSTEM TEST AND FUNCTIONAL TEST OF HORISDR WRNA201200009Pump · malfunctionedNR 1 SYSTEM HYD FLUID LOSS. RETURNED TO AIRFIELD. LANDING NORMAL. REPLACED NR 1 ENGINE LEFT AND RIGHT EDHP'S IAW 29-11-20, HYD MANIFOLD IAW 29-12-30. RUN UP AND LEAK CHECKED SYSTEM FOUND SATISFACTORY IAW 71-00-00. AIRCRAFT RETURNED TO SERVICE.SDR WRNA201200008Hydraulic System · lowDURING CRUISE, LEVEL 2 ALERT 'HYD SYSTEM NR 1 LOW" ILLUMINATED. A/C RETURNED TO DEPARTURE SITE, WITH NORMAL LANDING. MX SERVICED HYD SYSTEM NR 1 IAW 12-13-00, OP'S CHECK GOOD. NO LEAKS NOTED. A/C RETURNED TO SERVICE.SDR WRNA201200005Oil Filter · dirtyDURING CLIMB CREW CALLED AND REPORTED NR 3 ENG HAD HIGH OIL TEMP. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. MX T/S OIL TEMP WRITE UP IAW MD11 FIM 79-00-03 PG 108,109. PERFORMED INSP UP TO STEP 4 AND STEP 9, 14. REMOVED AND REPLACED MAIN OIL FILTER IAWSDR WRNA201200002O-Ring · cutDURING CRUISE HYD 3 ELEV "OFF" LIGHT ON. HYD QTY CHECKED 4.2 GAL AND KEPT ON DROPPING TO BELOW 2.5 GALS. HYD 3 FAIL. DIVERTED TO VCP, LANDING NORMAL. MX FOUND O-RING CUT ON HYD FILTER MODULE. REMOVED AND REPLACED O-RING IAW 20-40-02. SERVICED NR 3 HYD IASDR WRNA20111270011Transmitter · failedAFTER TAKEOFF, DEFLECTED AILERON DISAGREE LIGHT CAME ON. FUEL DUMPED TO REACH APPROVED LANDING WT. AIRCRAFT RETURNED TO AIRFILED. LANDING NORMAL. MX FOUND FLAP HANDLE POSITION XMITTER AT FAULT. UNIT REMOVED AND REPLACED IAW 27-54-03. OP'S CHECK SATISFACTSDR WRNA201100009Cadc · unserviceableAFTER TAKEOFF CAPT'S PRIMARY FLT DISPLAY LOST ALL AIRSPEED AND ALTITUDE INDICATIONS. ELEVATOR LOAD FEEL AND FLAP LIMIT OVERRIDE ILLUMINATED, CAUSED BY THE LOSS OF CADC-1. THEN LOST CADC-2, AS WELL. PERFORMED APPROPRIATE CHECKLIST, REGAINED CADC-2. CREW CONTSDR WRNA201000006Actuator · failedDURING CLIMB/CRUISE LEVEL 2 ALERT "AIL DEFLECTOR DISAGREE" ILLUMINATED. QRH (QUICK REF HANDBOOK) PROCEDURES FOLLOWED, LIGHT REMAINED ON. AIRCRAFT DUMPED APPROX. 48,400 LBS IF FUEL FOR APPROVED LANDING WEIGHT. A/C RETURNED TO FIELD. LANDING NORMAL. MX FOUN
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