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 = 'T206H' 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 = 'T206H' 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 CA081002002Piston · separated(CAN) RT MLG FAILED TO RETRACT. FOUND HYDRAULIC CYLINDER PISTON HAD SEPARATED FROM CYLINDER RAM.SDR CA080904002Boot · separated(CAN) DEICE BOOT RETAINING STRAP SEPARATING FROM NR 3 BLADE, DISCOVERED DURING ANNUAL INSP. (AT ELECTRICAL LEAD AREA). NR 3 DEICE BOOT REPLACED. MCCAULEY SL2006-5 PERFORMED ON ALL 3 BOOTS.SDR CA090505009Pin · split(CAN) REAR CARGO/PAX DOOR SPLIT PIN, PN NAS561P4-6, FOUND TO HAVE BACKED OUT OF RT DOOR BOLT, PN 1211942-2, WHICH RELEASED PUSH ROD, PN 1511209-11, WHICH DISABLED THE DOOR OPENING AND CLOSING FUNCTION. IN THE EVENT OF AN ACFT INCIDENT/ACCIDENT, WITH THE ACFTSDR ACOR032508001Plug · looseFUEL SERVO REGULATOR HEX PLUG LOOSE ON NON AFFECTED SERVO RSA-10 S/N 70259806. DATA REFERENCED AD 2008-06-51 E, SB 08-73-01, AND PRECISION SB PRS-107. SERVO HAS NOT BEEN NEW, REBUILT, OVERHAULED, OR REPAIRED ON OR SINCE AUGUST 22, 2006SDR 2008FA0000252Mount · failedORIGINAL STARTER (TT 433.4) WAS REMOVED BECAUSE IT FAILED (SMELLED BURNED). A REPLACEMENT WAS ORDERED FROM MFG AND INSTALLED. CHANGED THE SPARK PLUGS AND CHECKED ENGINE TIMING, WHICH WAS FOUND GOOD. AFTER INSTALLATION OF STARTER STARTED THE AC (5) TIMES ANDSDR CA080218003Indicator · misinstalled(CAN) IT WAS FOUND DURING AN INSP OF THE FLOATS THAT THE MLG INDICATOR COVERS COULD BE INSTALLED ON THE WRONG FLOAT. IF INSTALLED INCORRECTLY THE GEAR INDICATION IS REVERSED.SDR 2008FA0000215Nut · looseWHILE PERFORMING SB PRS-107, FOUND PN 383493 HEX NUT ACCESS PLUG FINGER LOOSE. ALSO, FOUND RED DYE INSIDE FUEL SERVO AIR CHAMBER. THIS AC HAS HAD AN ISSUE WITH LEAN IDLE MIXTURE IN THE PAST. NOTE: HEX NUT WILL BE LOOSER IF ENGINE IS WARMED UP. SUSPECT UNDESDR 2008FA0000066Fitting · failedPRIOR TO COMPLIANCE WITH FAR 91.411, A STATIC SYSTEM CHECK WAS CONDUCTED. UNDER TEST SYSTEM SHOWED APPROXIMATELY 100 FPM DESCENT RATE. INSPECTION REVEALED THE 90 DEGREE PLASTIC FITTINGS (ONE ON EACH SIDE OF THE FORWARD FUSELAGE) FOR STATIC SYSTEM PLUMBING WERESDR 2007FA0001044Casting · crackedAIRCRAFT OPERATED ON MOSTLY UNIMPROVED AIRSTRIPS. PART IS SAME AS 206F AND G MODELS. PART IN QUESTION WAS INSTALLED AT TIME OF MFG OF AIRPLANE. CASTING IS CRACKED IN (3) DIFFERENT LOCATIONS. WE OPERATE NUMEROUS OF THESE AC AND HAVE A LONG HISTORY WITH 206 SDR 2007FA0000974Coil · openPILOT REPORTED RT MAGNETO FAILED WHEN CHECKED DURING RUN UP. FOUND COIL HAD OPEN CIRCUIT WHEN CHECK IAW TABLE SEVEN IN UNISON'S 4300/6300 SERIES MM P/N L-1363C.SDR 2007FA0001034Door · misriggedMM (52-30-00 PG 201), (THE AFT DOOR IS HINGED AT FUSELAGE STA 112 AND IS A STRUCTURAL, LOAD CARRYING MEMBER WHEN CLOSED AND LOCKED). REMOVED AFT CARGO DOOR ROYALITE AND TRIM TO GAIN ACCESS TO LWR AFT CABIN LOWER HOOK ADJUSTMENT ROD. THIS WAS DUE TO A CLUB MSDR 2007FA0001048Casting · crackedAIRCRAFT OPERATED ON MOSTLY UNIMPROVED AIRSTRIPS. PART IS SAME AS 206F AND G MODELS. PART IN QUESTION WAS INSTALLED AT TIME OF MFG OF AIRPLANE. CASTING CRACKED AND FAILED UPON LANDING. AFT BOLT ALSO WAS CRACKED AND SHEARED. LANDING WAS A NORMAL APPROACH ASDR CA070823007Pump · leaking(CAN) FUEL DYE RESIDUE NOTED ON ELECTRIC FUEL BOOST PUMP HOUSING, FOUND TO BE FROM AN AUX PORT PLUG. PLUG RESEALED, FURTHER CHECK FOR SEEPING SATISFACTORY. (TC NR 20070823007)SDR CA070823003Lock · broken(CAN) RT SEAT LOCKING PIN SHEATH FOUND BROKEN AT THE SEAT LEG ATTACH POINT. THE LOCKING PIN WOULD RETRACT BUT NOT ENGAGE ON THAT SIDE. THE SEAT LOCK MECHANISM COMPRISES OF A SPRING LOADED HANDLE , WITH TWO CABLES ATTACHED AND TWO SHEATHS SECURED TO THE SEAT LESDR 2007FA0000854Exhaust Stack · looseDURING AN INSPECTION, FOUND THE EXHAUST STACK AT NR 2 CYLINDER, PULLED DOWN .0625 INCH APPROX. FURTHER INVESTIGATION FOUND THE NR1, NR3, NR5 AND NR 6 ENGINE CYLINDERS EXHAUST STACKS PULLED DOWN, BUT NOT AS MUCH. AFTER RECOMMENDATIONS FROM ENGINE MFG ALSO, THSDR 2007FA0000164Engine · making metalUNDER NORMAL CONDITIONS AND UNDER OIL SAMPLE PROGRAM, ENGINE HAS HAD (6) HIGH BAD SAMPLES, HIGH IRON, COPPER AND ALUMINUM. AC IS A PUBLIC USE AIRCRAFT WITH CUSTOMS AND BORDER PROTECTION, BUT AM REPLACING ENGINE WITH NEW/ OVERHAUL. CONTACTED MFG ABOUT PROBLEMSDR CA061124006Boot · failed(CAN) DURING PHASE NR 2 INSPECTION IT WAS NOTED ON PRE-INSPECTION RUNUP THAT THE PROP DE-ICE WAS INOPERATIVE. INVESTIGATION REVEALED THAT 2 OF THE 3 DE-ICE BOOT LEADS WERE DEFECTIVE. NEW PARTS ORDERED.SDR 2006FA0000967Window · damagedTHE FACTORY ORIGINAL REAR WINDOW OF THIS AC BEGAN TO DEVELOP A CONCAVE AREA IN THE CENTER OF THE WINDOW. THIS AREA WOULD BECOME MORE PRONOUNCED IN DIRECT SUNLIGHT. THIS AC IS 6 YEARS OLD AD HAS ACCUMULATED 674.52 HOURS. THE AC WAS HANGER KEPT MOST OF THE TISDR 2006FA0000593Line · leakingDURING NORMAL OPERATION RT BRAKE STARTED LEAKING. REMOVED WHEEL FAIRING AND FOUND A SCREW FROM THE FAIRING CHAFING INTO THE LOWER BRAKE LINE CAUSING THE LINE TO LEAK AND ALMOST FAIL, THEREFORE IT IS RECOMMENDED THAT PROPER ROUTING IS ASSURED DURING INSPECTIONSDR CA060203007Guard · looseWHILE INSTALLING ALTERNATOR/WIRING UPGRADE, IT WAS NOTICED THAT THE STRAP COVER WAS LOOSE ON THE CABLE GUARD ON THE LEFT SIDE AILERON CONTROL QUADRANT. SUBSEQUENT INSPECTION REVEALED THE RIGHT SIDE WAS ALSO LOOSE. TOP AND BOTTOM SCREWS ON THE LEFT AND RIGHT SDR 2006FA0000040Altimeter · erraticAT TAKEOFF POWER (2500 RPM) AND CRUISE OVER 2390 RPM, THE STANDBY ALTIMETER MAY OSCILLATE 20 FT TO 100 FT (3500 FT CRUISE ALTITUDE).AT CRUISE, THE AUTOPILOT UNCOUPLED ITSELF THREE TIMES.DESCENT AND APPROACH (BELOW 2390 RPM) OSC. WAS 20 TO 40 FEET. BELOW 2300 RSDR CA050608004Rod End · bent(CAN) ROD END ON FLAP SYNCHRONIZING ROD FOUND BENT FROM CONTACT WITH FLAP BELLCRANK DUE TO RIGGING OF FLAP SYSTEM FROM MANUFACTURE. NEW ROD INSTALLED AND SYSTEM RIGGED SO IT WOULD NOT CONTACT THE BELLCRANK.SDR 2005FA0000452Pump · leakingBOOST PUMP WAS LEAKING AT SEAM BETWEEN ELECTRIC MOTOR AND VANE PUMP. FUEL HAD A CHANCE TO LEAK INTO ELECTRIC MOTOR BRUSHES. BELIEVE THIS TO A MAJOR FIRE HAZZARD. BOTH PUMP AND AIRCRAFT WERE NEW. THIS COULD HAVE BEEN PREVENTED BY BETTER QUALITY CONTROL AT SDR 2005FA0000473Caliper · leakingNOTICED LT BRAKE LEAKING FLUID ON IB SIDE OF CALIPER. CLEANED, INSPECTED, COULDN`T FIND LEAK. REMOVED CALIPER BENCH TESTED WITH HYD POWER SUPPLY, FOUND CALIPER TO BE LEAKING THROUGH PIN HOLES IN HOUSING IN 3 PLACES. (EA23200505995)SDR 2006FA0000154Pump · failedTHIS FUEL PUMP IS LOCATED UNDERT HE PILOTS SIDE FLOORBOARDS AND IS AN ELECTRICLY DRIVE AUX FUEL PUMP. THE AC ORIGINAL FUEL PUMP A10055B FAILED AFTER 53 HOURS IN SERVICE ON MARCH OF 2005. IT FAILED IN A WAY TO ALLOW FUEL TO ENTER THE ELECTRIC SIDE OF THE MOTOSDR 2004FA0000893Oil Filter · separatedREMOVED THIS FILTER AND CUT OPEN TO INSPECT CONTENTS AS PAR OF A ROUTINE OIL CHANGE. FOUND THE FILTER MEDIA HAD SEPARATED WHERE THE ENDS ARE CRIMPED TOGETHER. FOUND THE GASKET BETWEEN THE INNER FILTER AND THE END PLATE IMPROPERLY INSTALLED. THIS GASKET WASSDR 2005FA0000240Pedal · misalignedRT SIDE BRAKE PEDALS: DURING A FLT CHECK, THE INSTRUCTOR FOUND HE RARELY HAD BRAKES DUE TO TOE PEDALS GOING OVER TOO FAR, HIS FOOT COULD NOT GO OVER ANYMORE TO STOP THE AIRCRAFT. DURING OK OUT, SEEMS THE LINKAGE ON PEDALS IS MISALIGNED ALLOWING THE PDEALS TOSDR 2004FA0000434Flap Track · misinstalledMECHANIC HEARD (POPPING) NOISE WHEN FLAPS WERE EXTENDED OR RETRACTED. FOUND THE UPPER FLAP TRACK HARDWARE WAS HITTING THE FLAP WELL CUT OUTS. THE BOLTS WERE INSTALLED FACING OB AT THE FACTORY. REVERSED HARDWARE AND PROBLEM WENT AWAY.SDR FTU2004F00002Chain · misinstalledFIRST TIME AC WAS IN OUR SHOP DURING AN ANNUAL INSP, THE RUDDER TRIM CHAIN IN THE CENTER PEDESTAL WAS FOUND NOT INSTALLED CORRECTLY. WERE THE CHAIN IS SUPPOSE TO RIDE OVER THE IDLER TENSIONING SPROCKET, IT WAS FOUND OFF THE SPROCKET AND JUST RESTING ON THE SPSDR 2003FA0000763B-Nut · crackedWHILE PERFORMING SB 03-53-02, FOUND 5 EA (B NUTS) CRACKED, DUE TO OVERTORQUE ON BRAKE LINES. SEG ATTACHED IPC PAGES AND LOCATION OF DAMAGED (B NUTS) NUMERED 1 THRU 5. AC TT 0025.1. LEFT AND RIGHT BRAKES.SDR S1F2003F00000Turbocharger · damagedON TAKEOFF TOWER REPORTED SMOKE FROM ENGINE TAILPIPE. MECHANIC FOUND TURBOCHARGER BEARING VERY LOOSE AND INTAKE BLADES ON TURBO BROKEN. INSTALLED NEW TURBOCHARGER.SDR CA030703014Seal · leaking(CAN) FOLLOWING A FLIGHT TEST THAT WAS CARRIED OUT AFTER ENGINE INSTALLATION. THE PILOT NOTICED AN EXCESSIVE OIL LEAK. THE ENGINE HAD RETURNED FROM OVERHAUL. FURTHER INVESTIGATION REVEALED THAT OIL SEAL WAS NOT INSTALLED. AN EMPTY SPACE WAS CREATED BECAUSE THASDR 2003FA0000455Mount Bracket · crackedENGINE JUST CAME BACK FROM LYCOMING FOR SB553 AND WAS BOLTED ON AIRFRAME. FOUND THE RT REAR LIFTING RING CRACKED 85 PERCENT THROUGH. CRACK HAD GRAY PAINT IN IT. THIS COULD HAVE BROKEN WITH THE ENGINE UP IN THE AIR AND FULL ON SOMEONE OR THE AIRCRAFT.SDR 2003FA0000606Sprocket · wornRUDDER TRIM SYST DID NOT SEEM TO BE RESPONDING TO INDICATED TRIM INPUT. INSP OF RUDDER TRIM SYS, IT WAS DISCOVERED THAT TRIM WHEEL SPROCKETS, PN 07612101 WERE NOT SHIMMED CORRECTLY TO ALLOW FOR PROPER ENGAGEMENT OF GEAR TEETH. TWO SPROCKETS ENGAGE AT 90 DEGRSDR 2002FA0001342Skin · crackedRIGHT FLAP SKIN CRACKED AROUND LEADING EDGE INBOARD.SDR 2002FA0001280Skin · crackedRT SIDE FLAP CRACKED SKIN AROUND RIVETS ON LEADING EDGE BOTTOM SECTION.SDR 2002FA0001261Skin · crackedFLAP HAS SEVERAL CRACKS ON SKIN AROUND RIVETS ON INBOARD LEADING EDGE.SDR 2002FA0001260Skin · crackedRIGHT SIDE FLAP CRACKED SKIN AROUND RIVETS IN INBOARD LEADING EDGE BOTTOM SKIN.SDR 2002FA0000327Line · damagedOXYGEN LINE WAS PERFORATED BY AN UPHOLSTERY TRIM SCRE. DURING THE PROCESS OF A ROUTINE ANNUAL INSPECTION, THE LEFT SIDE TRIM PANES WAS REMOVED AND THE HOLE WAS DISCOVERED. THE LINE SHOULD HAVE BEEN RUN LOWER AND TIED TO A GLUED ON SKIN ATTACH POINT, BUT WAS SDR 2003FA0000322Slip Joint · wornTHERE IS AN EXHAUST ELBOW THAT COMES OFF THE WASTEGATE AND RETURNS TO THE TAILPIPE. THIS PIPE HAD WORN NEARLY THROUGH AT THE SLIP JOINT BETWEEN IT AND THE TAIL PIPE. THE TAIL PIPE WAS WORN TO A SHARP EDGE WHERE THE ELBOW ENTERS THE SLIP JOINT. THIS CONDITIOSDR CA010626026O-Ring · leaking(CAN) DURING APPROACH AND LANDING A FUEL ODOR WAS APPARENT. INVESTIGATION OF THE REPORTED SNAG REVEALED THAT THE FUEL SELECTOR WAS LEAKING AND SOME FUEL HAD ACCUMULATED IN THE FUSELAGE, UNDER THE CABIN F LOOR.SDR 20010423CW012Hose · burnedDURING THIS AIRCRAFTS FIRST INSPECTION, THE TURBO BREATHER HOSE WAS FOUND ROUTED NEXT TO THE EXHAUST SYSTEM AND BURNED, CAUSING AN OIL LEAK. FAILURE OF THIS HOSE WILL CAUSE OIL SYSTEM LEAKAGE AND SUBSEQUENT ENGINE FAILURE. NO POSITIVE RESPONSE FROM ENGINE OR SDR 20010302CW001Landing Gear · collapsedMAIN GEARS COLLAPSED ON FLOAT POND ENTRY / EXIT RAMP. INSPECTION FOUND RT AND LT MAIN GEAR ACTUATING CONTROL SHAFTS BROKEN. REPLACED RT AND LT ACTUATING CONTROL SHAFTS ON MAIN GEAR ASSEMBLY. GEAR RETRACTION TESTS COMPLETED SATISFACTORY.SDR 20010416CW011Spark Plug · inoperativeUPON ANNUAL INSPECTION, FOUND 2 SPARK PLUGS NOT WORKING. CERAMIC ON TERMINAL END WAS LOOSE INSIDE THE PLUG. REMOVED AND REPLACED.SDR S2L2002F00000Magneto · failedTHE MAGNETO APPEARS TO HAVE INTERNAL FAILURE. PART SHOWS GUIDENCE OF ARCHING AND EXCESSIVE HEAT. PICTURES ARE AVAILABLE ON REQUEST.SDR 20010129CW001Servo · inoperativeTHE PILOT INITIALLY COMPLAINED THAT THE AUTOPILOT WOULD NOT MAINTAIN CONSTANT VERTICAL SPEED. THIS ESCALLATED INTO A FULL NOSE DOWN TRIM RUNAWAY. THE PILOT RECOGNIZED THE PROBLEM AND RECOVERED FROM DIVE. THE PITCH SERVO WAS CHANGED AND THE PROBLEM DID NOT RSDR 20001013SH028Bolt · missingFOUND FORWARD SECURING BOLT MISSING FROM INTAKE PLENUM. SUBMITTER STATED THERE WAS NO SIGN OF EVER BEING INSTALLED. (X)SDR 20001013SH027Oxygen Bottle · misinstalledOXYGEN BOTTLE APPEARS TO BE INSTALLED ON WRONG SIDE OF AIRCRAFT. REF: CESSNA SERVICE MANUAL INSIDE OF AIRCRAFT TAILCONE. (X)SDR 20001013SH020Firewall · crackedDURING FIRST ANNUAL INSPECTION, FOUND CRACK IN DIAGONAL SUPPORT ACROSS LOWER RIGHT FIREWALL. CRACK APPEARS TO BE CAUSED BY A MANUFACTURING DEFECT. (X)SDR 20001013SH026Lanyard · missingLANYARD AND ALL ATTACHING HARDWARE FOUND MISSING AND NO SIGN OF EVER BEING INSTALLED DURING FIRST ANNUAL INSPECTION. SUBMITTER STATED THIS DEFECT COULD CAUSE AN IN-FLIGHT FIRE. (X)
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