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 = 'DHC6' 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 = 'DHC6' 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 CA060109003Collar · incorrectTHE STEERING COLLAR WAS ASSEMBLED AT THE FACTORY INCORRECTLY. THERE ARE TWO DISCS WHICH ARE ATTACHED TO THE COLLAR. ONE DISC IS BARE METAL AND IS SUPPOSED TO BE AT THE SIDE THAT IS FACING THE STRUT TOUCHING THE FRICTION DISC (WHICH IS GLUED TO THE STRUT ITSELSDR CA041222018Actuator · mismanufactured(CAN) SLIDE ACTUATOR MANUFACTURED TO INCORRECT LIMITS. SLIDE ACTUATOR WILL NOT FIT ONTO BETA SWITCH BRACKET P/N C6E1060-3. GROOVE FOR SLIDE ON A C6E1017-29 IS .1300 +/- .0005. GROOVE ON SLIDE FROM J.A.S. PDM C6E1017-29 IS .1200 +/- .0005. TRACK ON BETA SWITCHSDR 2004FA0000896Control Rod · faultyDURING A VISUAL INSPECTION OF THE CONTROL ROD, IT WAS DISCOVERED THE ROD DID NOT HAVE A CRIMPED SLEEVE WHICH IT SHOULD.SDR 2004FA0000895Control Rod · faultyDURING A VISUAL INSPECTION OF THE CONTROL ROD, IT WAS DISCOVERED THE ROD DID NOT HAVE A CRIMPED SLEEVE WHICH IT SHOULD.SDR CA040209008Pressure Switch · out of tolerance(CAN) PRESSURE SWITCH HAS A CALIBRATION VARIANCE THAT FALLS OUTSIDE OF THE DRAWING SPECIFICATION. THE ACTUATION OF THE UNIT HAS A TIGHTER TOLERANCE FROM ACTUATION, THAN SPECIFIED. THE SWITCH IS DESIGNED TO DEACTUATE, ON DECREASING PRESSURE, AT A VALUE 150 TO SDR JRP2004F00000Fitting · crackedLATERAL CRACK BETWEEN RIVETS IN VERTICAL LEG OF FITTING AT WS 40 AND AT WS 47.5 FITTING IS PART OF FORWARD WING ATTACHMENT ASSEMBLY. NOTE: PART NAME IS FRONT SPAR CAP ADAPTOR FITTING.SDR 2003FA0001204Pad · deterioratedREPORTED (AFT FUEL LOW) LIGHT ILLUMINATING WITH 300-400 LBS REMAINING ON GAUGE. (SHOULD BE 110 LBS). TROUBLESHOOTING REVEALED FLAPPER PAD (SEAL) WAS DETERIORATED TO THE CONSISTENCY OF A (GUMMY BEAR). AS FUEL IS MOVED INTO THE NR 5 (ENG FEED) TANK, BY MOTIVESDR 08270324Connector · arcedPILOT REPORTED DURING CRUSE FLT SMOKE ENTERED COCKPIT FROM AC ELECTRICAL PANEL AREA. NO SYSTEM MALFUNCTION WAS NOTED. NO ELECTRICAL POWER WAS LOST. ONCE ON GROUND DC POWER COULD NOT BE TURNED OFF THROUGH NORMAL SWITCHING. BATTERY WAS DISCONNECTED TO REMOVE DCSDR CA030904005Block · failed(CAN) REBOUND BLOCKS FOUND TO HAVE WRONG THREAD. BLOCKS CAN BE REPAIRED. REPAIR FOUND TO BE MINOR. PAPER TRAIL FOLLOWED TO EXACT POINT DEFECT OCCURRED. ALL BLOCKS, BY S/N LOCATED. A FIELD REPAIR AND SB CURRENTLY BEING DEVELOPED. WILL BE ISSUED TO CUSTOMERS WITSDR CA030904004Block · failed(CAN) REBOUND BLOCKS FOUND TO HAVE WRONG THREAD. BLOCKS CAN BE REPAIRED. REPAIR FOUND TO BE MINOR. PAPER TRAIL FOLLOWED TO EXACT POINT DEFECT OCCURRED. ALL BLOCKS, BY S/N LOCATED. A FIELD REPAIR AND SB CURRENTLY BEING DEVELOPED. WILL BE ISSUED TO CUSTOMERS WITSDR OEZ2003F00000Hinge Bracket · brokenDURING SCHEDULED INSPECTION MAINTENANCE PERSONNEL FOUND RIGHT ELEVATOR OUTBOARD HINGE PLATE LOOSE WITH RIVETS (WORKING) AT ATTACHMENT TO OUTBOARD STABILIZER RIB. UPON DISASSEMBLY FOR REPAIR. HINGE PLATE BRACKET WAS FOUND CRACKED AND BROKEN AWAY FROM FORWARD SDR 2003FA0000162Exhaust Pipe · crackedEXHAUST DUCT, CRACK IN BASEMETAL. VIBRATIONSDR 2003FA0000166Structure · crackedMAIN LANDING GEAR, CRACKED AT TAC OF WELD. UNKNOWN. NO OTER APPARENT DAMAGE.SDR CA021016025Case · cracked(CAN) DURING INSPECTION, CRACK FOUND ALONG WELDED SEAM.SDR CA020913012Longeron · cracked(CAN) NR 2 ENGINE NACELLE LONGERON CRACKED ON INBOARD SIDE.SDR AUS20020879Wheel · damaged(AUS) LH MAIN WHEEL OUTER HUB DAMAGED. TYRE DEFLATED.SDR AUS20020877Structure · damaged(AUS) FORWARD BULKHEAD, NLG ATTACHMENT FITTINGS AND SURROUNDING LOWER FUSELAGE STRUCTURE DAMAGED WHEN THE NOSEWHEEL CONTACTED A ROCKDURING LANDING.SDR AUS20020878Antenna · damaged(AUS) VHF ANTENNA DAMAGED BY IMPACT FROM AN UNKNOWN OBJECT. FUSELAGESKIN AFT OF THE ANTENNA MOUNT SUFFERED A 50.8MM (2IN) TEAR. THE ANTENNA IS MOUNTED ON THE LOWER FUSELAGE AT STN 376. FODSDR CA020507016Hinge · mismanufactured(CAN) HINGE HALF - MISMANUFACTURED. PLEASE NOTE RMA RECEIVED TWO C6WFM1218-27 CLEATS FROM DIFFERENT SUPPLIERS, 1 MAY 4/01 FOR RMA INVENTROY AND 1 APRIL 23/02 FOR A WORK ORDER. BOTH CLEATS ARE MISMANUFACTURED. THE CLEAT FROM C6WFM1218-27 APRIL 23/02 IS LOT 000SDR CA020304003Fork · mismanufactured(CAN) PART NOT MANUFACTURED AS PER DEHAVILLAND/BOMBARDIER SPEC. FOUR FORKS FROM INVENTORY FOUND NOT FILLET RADIUS TO O.031 INCH. SEVEN OF EIGHT ON AIRCRAFT SEATS NOT FILLET RADIUS TO O.031 INCH. THIS MAY PUT UNDUE STRESS ON HEAD OF BOLT LEADING TO SEAT BELT RESDR 2001F00244Indicator · failedAPPROXIMATELY 5 MINUTES FROM LANDING NR 1 OIL PRESSURE WAS NOTED AT 15 PSI WITH NO CAUTION LIGHT. HOWEVER, THE ENGINE WAS SECURED AND SINGLE ENGINE LANDING PERFORMED. (M)SDR AUS20010471Landing Gear · fod(AUS) NOSE LANDING GEAR FAILED WHEN THE NOSE WHEEL CONTACTED A ROCK ONLANDING. TYRE DEFLATED AND NOSE WHEEL SHATTERED. NLG FORK FAILEDAT THE OLEO AND THE REMAINDER OF THE NLG BENT BACK CAUSING DAMAGE TO THE BULKHEAD, ATTACHMENT FITTINGS AND SURROUNDINGLOWER FSDR AUS20010453Connector · melted(AUS) BATTERY SHUNT GROUND CONNECTION MELTED.SDR CA010323005Adapter · failed(CAN) LOWER LT MOUNTING / MATING SURFACE INCORRECTLY MACHINED. SURFACE WAS MACHINED CYLINDRICALLY INSTEAD OF SPHERICAL CONVEX. IF INSTALLED THE MATING SURFACES WOULD NOT MATCH CAUSING STRESS AND POSSIBLE FAILURE OF THE MOUNT. CONCERNED THAT MORE WERE PRODUCED SDR CA010130011Engine · failed(CAN) RT ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. AFTER REACHING CRUISING ALTERNATE RT ENGINE LOW OIL PRESSURE CAPTION APPEARED. LOW OIL PRESSURE GAUGE INDICATION OBSERVED. PRECAUTIONARY ENGINE SHUT DOWN. DIVERTED BACK TO AIRFIELD.SDR CA001027017Arm · failed(CAN) THE SIX ATTACH HOLES ARE COUNTERSUNK TOO DEEP FOR THE INTENDED FASTENERS (PLT110-6) IF INSTALLED THIS ITEM COULD COME LOOSE RESULTING IN LOSS OF LT ELEVATOR CONTROL. CONCERNED ABOUT MOR IN SAME BATCH IN SERVICE. PLEASE SEE ATTACHED PHOTO COPY.SDR CA000926008Sleeve · missing(CAN) BOMBARDIER NOT IN COMPLIANCE WITH AIRWORTHINESS DIRECTIVE CF-80-03R. SLEEVE MISSING FROM SWAGED AREA OF ROD ENDS. ROD PURCHASED NEW AS A SPARE PART. (X)SDR CA000824019Rib · wrong part(CAN) PART IS STAMPED WITH P/N C6W1035-S14 BUT IT IS NOT THIS PART.SDR CA000824018Spar · wrong part(CAN) PART IS STAMPED WITH P/N C6WM1147-27 BUT IS NOT THIS PART.SDR AU000507Pipe · fod(AUS) FORWARD FUEL TANK TRANSFER PIPE BLOCKED BY BLANKING PLUG. FOD. (X)SDR CA000824017Rib · wrong part(CAN) PART IS STAMPED WITH P/N C6W1035-S14 BUT IS NOT THIS PART. PART IS CERTIFIED BY STAN GROTEK OF BOMBARDIER ON 24-0078 FORM. WRONG PART FOR THIS PART NUMBER APPLICATION.SDR CA000306009Armature · misoverhauled(CAN) PUMP WAS SENT FOR OVERHAUL. INTERNAL INSPECTION REVEALED THAT THE ARMATURE HAD BEEN MODIFIED BY REDUCING THE ARMATURE SHAFT SIZE AND SUBSTITUTING THE ORIGINAL BEARING WITH A COMMERCIAL BEARING THAT HAD THE SAME OUTSIDE DIAMETER, BUT A SMALLER INSIDE DIASDR CA000128044Block · mismanufactured(CAN) ONE OF OUR NEWLY MNUFACTURED COMPRESSION BLOCKS SAGGED WHEN INSTALLED DURING REGULAR MAINTENENACE. BLOCK REMOVED AND NEW ONES INSTALLED WITHOUT PROBLEM. BLOCKS SENT FOR TESTING & CHEMICAL ANALYSIS. HAVE ISOLATED BLOCKS TO WHAT BATCH AND POUR.SDR CA981109006Line · mismanufactured(CAN) WELDED TUBE ASSY IS FIVE INCHES TOO LONG.SDR CA971020009Bearing · not lubed(CAN) NEW BEARINGS WERE RECEIVED FROM STORES TO REPLACE WORN ELEVATOR TRIM AND FLAP INERCONNECT SCREW JACK BEARINGS. A NUMBER OF THE NEW BEARINGS WERE NOT LUBRICATED INTERNALLY. THEY APPEARED TO BE DRY. THESE WERE RETURNED TO DE HAVILLAND FOR INSPECTION. THESESDR CA961028002Body · mis manufactued(CAN) THIRD BATCH (5 EACH) OF FLAP SELECTOR VALVE BODIES REJECTED BECAUSE THE THREADS IN THE PORTS (A) ARE EXCESSIVELY LONG CAUSING 'O' RINGS TO REST ON THE LAST THREAD RATHER THAN THE SMOOTH WALL OF THE BORE. THIS RESULTS IN EXTERNAL LEAKAGE OF HYDRAULIC FLUISDR CA961002009Fork End · mis manufactured(CAN) NEW FLAP ROD WOULD NOT BE INSTALLED BECAUSE THE FORK END OF THE ROD WAS TOO NARROW TO ACCEPT THE BEARING OF THE ATTACHING ROD. NO DAMAGE FOUND ON ROD. SUBMITTER CONCERNED THAT SOME MAY TRY TO FORCE ROD INTO PLACE.SDR CA961002007Fork End · mis manufactured(CAN) THE NEW FLAP ROD COULD NOT BE INSTALLED AS THE FORK END WAS TOO NARROW TO ACCEPT THE BEARING OF THE ATTACHING ROD BETWEEN THE FORKS. NO EVIDENCE OF DAMAGE. ROD PURCHASED NEW FROM BRAD.SDR CA960311008Quadrant · warped(CAN)NEW QUADRANT BEING INSTALLED TO SATISFY CF-73-06R2. AT INSTALLATION IT WAS FOUND DISTORTED AT THE LOWER FORWARD END. NO INTERFERENCE NOTED, BUT QUADRANT WAS NOT USED. MARKS ON QUADRANT. MELT 950556 AND 12215/0.SDR 96ZZZX188Control Rod · crackedTHIS AIRCRAFT WAS MODIFIED TO INCORPORATE THE LATEST TYPE OF FLIGHT CONTROL RODS (6061 MATERIAL) AND INCREASE THE INSPECTION INTERVALS FOR THE FLIGHT CONTROL RODS (SB 61502). UPON THE FIRST INSPECTION, THIS CONTROL ROD WAS FOUND CRACKED IN THE MAGNAFORMED SLESDR CA960212018Control Cable · broken(CAN)LOOSE NOSE WHEEL TILLER NOTED ON PREFLIGHT. ON TAKEOFF ROLL PILOT REQUIRED A LOT OF LEFT RUDDER. GROUND OBSERVER TOLD CREW THAT NOSE WHEEL NOT CENTERED. AIRCRAFT LANDED IMMEDIATELY WITH SOME DIFFICULT Y, AS AIRCRAFT VEERED RIGHT. INSPECTION FOUND 4 STRANDSDR CA951127003Circuit Breaker · improper wired(CAN)AVIONICS BREAKER FOUND FED WITH INDIVIDUAL #18 GAUGE WIRE RATHER THAN THE NORMAL BUSS BAR ARRANGEMENT. IN ADDITION, SEVERAL OF THE CIRCUIT BREAKERS WERE IMPROPERLY LABELLED AND CONNECTED TO MORE THAN ONE SYSTEM. FOR EXAMPLE, THE BREAKER LABELLED "RNAV", SDR CA951127005Inner Cone · damaged(CAN) DURING A ROUTINE HOT SECTION INSPECTION (HSI), THE #3 BEARING COVER WAS FOUND TO BE WEARING AND IF NOT REPAIRED IT WOULD CAUSE SEPARATION FROM ITS LOCATION AND RUB ON THE TURBINE WHEEL.SDR CA951127004Inner Cone · shifted position(CAN) DURING AN INSPECTION THE #3 BEARING COVER WAS FOUND TO HAVE SHIFTED POSITION, THIS CONDITION IF NOT RECTIFIED WOULD ALLOW THE PART TO ROTATE AND CAUSE WEAR LEADING TO SEPARATION AND RUBBING ON THE TURBINE WHEEL.
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