Viking DHC-6-400
Service difficulty reports · 23
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'DHC6400' 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 aircraft_model_key = 'DHC6400' 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 G7HA202307130001Distribution Vlv · burnedON TEN OCCASIONS SINCE 2020, PILOTS REPORTED THE UNCOMMANDED INFLATION OF ALL THEIR DEICE BOOTS AT ONCE DURING TAKE-OFF. ON EVERY OCCASION, THEY WERE ABLE TO RESET THE SYSTEM AND RESTORE THE PROPER OPERATION OF THE BOOTS. THE SYSTEM RESUMED PROPER SEQUENTIAL ISDR 8G9R705DSwitch · inoperativeAIRCRAFT NLG DID NOT RETRACT AFTER TAKEOFF. ABLE TO LAND WITHOUT INCIDENT. UPON INSPECTION, TECHNICIANS FOUND CENTERING SWITCH OUT OF ADJUSTMENT. TECHNICIANS CORRECTED SWITCH. AIRCRAFT MAY HAVE EXPERIENCED A LANDING GEAR OVERSPEED CONDITION SO AN INSPECTION WASDR 2021F00206Circuit Card · shortedON JULY 22, 2021 AT APPROXIMATELY 0920, INFLIGHT AND IN IMC WHILE PERFORMING THE RNAV RWY 5 APPROACH INTO PAAD THE CREW EXPERIENCED A TEMPORARY LOSS OF VERTICAL AND LATERAL COURSE GUIDANCE AND A CASCADING PRESENTATION OF CAS MESSAGES INCLUDING AMBER: AGM 2 FASDR CA190808010Screw · wrong part(CAN) DEFECT DESCRIPTION DWG: C6CF1225 REV U. IN ASSY 3, 6 AN526-632R4 SCREWS WERE FOUND NONCONFORMING, NOT IN SAFETY OF THE ANCHOR NUT ON THE C6CF1244-3 FWD COVER OF THE C6CF1225-S7 CONTROL COLUMN CONTAIN ACTION WAS CARRIED OUT IN YYJ ON MSN AIRCRAFT NUMBER SDR CA190807008Rod End · corroded(CAN) MSN 974 LEFT ENGINE FAILED TO RETURN TO LOWER POWER SETTING DURING TAXI THIS MORNING. WHEN L/H POWER LEVER RETURN TO IDLE POSITION THE NG STILL 68%, R/H IS NORMAL. AFTER REMOVE THE FCU CONTROL ROD , CORROSION IS FOUND ON ROD END BEARING. THEN WE HAVE RESDR CA190528017Washer · missing(CAN) QTY 2 COTTER PINS MS24665-132 AND QTY 2 WASHERS AN960PD316L WERE NOT INSTALLED AS SHOWN IN MANUFACTURING DRAWINGS. VIKING IS CONTINUING TO INVESTIGATE (TC# 20190528017)SDR 2019FA0000164Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000163Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000162Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000161Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000160Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR CA190522024Control Rod · damaged(CAN) ON THE 9TH OF MAY DURING PRE-FLIGHT CHECKS ON DQ-FLA (MSN: 968) THE CONTROL ROD ASSY (PN: C6FS5018 3) ON THE DOOR AIRSTAIR CABIN WAS FOUND DAMAGED. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CONTROL ROD ASSEMBLY FAILED DUE TO EXCESSIVE CORROSIONSDR CA190528016Sump · malfunctioned(CAN) SEVERAL SUMPS DISPLAYED VARIOUS DEGREES OF FUEL SEEPAGE DURING THE PAINT INSPECTION AT SPOKANE ON APRIL 15. THE SUMPS WERE CLEANED AND DRIED AT THAT TIME TO BE RE-EVALUATED AT YYJ. THE AIRCRAFT WAS LEFT WITH 660 LBS. OF FUEL IN THE FWD TANK AND 805 LBS.SDR CA190528018Rod End · damaged(CAN) VSC30-3A ROD ENDS MAY HAVE CONDITIONS. MISSING HARD CHROME PLATING OF ROD END BALL AS PER VSC30 REV A. DEFECTS FOUND ON BEARING RACE SUCH AS NICKS, JAGGED EDGES, BURR`S ETC. MISSING PART MARKING AS PER NOTE 8 OF SPECLINE DWG 75E03-303A REV C. PART SDR CA190418011Screen · corroded(CAN) MAU COOLING FAN SCREEN FOUND CORRODED AND WITH PIECES MISSING. VIKING IS CONTINUING TO INVESTIGATE. ATA 31 (TC# 20190418011)SDR CA190412002Rod End · failed(CAN) ROD END FAILED DUE TO CORROSION. HAS REQUESTED THE PARTS TO BE RETURNED FOR INVESTIGATION. (TC# 20190412002)SDR CA190327025Pressure Switch · intermittent(CAN) HYDRAULIC PRESSURE SWITCH P/N P12M-H185 S/N 102 WAS SNAGGED FOR INTERMITTENT OPERATION PRIOR TO A/C DEPARTURE.SDR CA190424021Hose · leaking(CAN) HOSE SPLIT AND LEAKING.SDR CA180616005Probe · false indication(CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616005)SDR CA180616004Pressure Switch · broken(CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616004)SDR CA180616003Pressure Switch · fluctuates(CAN) HYDRAULIC PRESSURE SWITCH PRE MOD 6/2313 DROPS TO 1220 PSI. OUTSIDE THE PERMISSIBLE LIMIT, SWITCH OPENS AT INCONSISTENT PRESSURES IN 1480, 1520,1500 PSI`S ATA 29-00. (TC# 20180616003)SDR CA180404016Control Cable · chafed(CAN) DURING THE EMMA 2 INSPECTION IT WAS DISCOVERED THAT THE LEFT HAND AILERON CABLE WAS CHAFING ON THE STEERING CABLE AT THE BASE OF THE YOKE. THE CHAFING OCCURRED AS THE YOKE WAS PULLED BACK PAST LEVEL FLIGHT. CABLES WERE INSPECTED AND FOUND TO BE UNDAMASDR CA180222018Pump · failed(CAN) FORWARD BOOT PUMP 1 FAILURE ON TAXI IN AT GLA. (TC NR 20180222018).
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