Superior 0-320-D1A

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 engine_model_key = 'O320D1A'
  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.

SDR CA150603006Starter · misoverhauled(CAN) STUDENT HEARD GRINDING NOISES WHEN ATTEMPTING TO START ACFT. MAINTENANCE FOUND THE BENDIX SHAFT FWD BUSHING MISSING ON STATER, WHICH ALLOWED BENDIX ASSEMBLY TO MOVE AROUND WHEN STARTING.Jun 3, 2015 · Grob G115C · Engine StarterSDR CA150304004Bushing · broken(CAN) UPON LANDING AND TAXI, THE PILOT REPORTED A NOISE AND DIFFICULTY TAXIING. SHUTDOWN THE ACFT AND DISCOVERED THE NOSE WHEEL ASSY TILTED AND THE CENTER BOLT MISSING. THE CENTER BOLT ASSY WAS FOUND BEHIND THE ACFT. AFTER A INSPECTION IT WAS DISCOVERED THMar 4, 2015 · Grob G115C · Nose/Tail Landing GearSDR CA141007002Starter Gen · engaged(CAN) PILOT REPORT LOSS OF POWER AFTER REDUCING POWER FOR DECENT AFTER REDUCING TO 1500 RPM FOR DESCENT THE PILOT NOTICED THE ENGINE AT 1100 RPM. HE ADDED POWER WITH NO AFFECT. PILOT IS UNSURE IF THE ENGINE WAS STILL RUNNING AT THE TIME OF TOUCHDOWN IN FIELD AOct 6, 2014 · Grob G115C · Starter-GeneratorSDR CA140130011Tube · failed(CAN) DURING FLIGHT THE PILOT NOTICE A LOSS OF FUEL INDICATION IN THE LT TANK. THE ACFT RETURNED WITH OUT INCIDENT. DURING THE INSPECTION OF THE SNAG IT WAS FOUND LT IMMERSION TUBE, FUEL TRANSMITTER, HAD COME APART. THE BOTTOM NUT THAT HOLD THE TUBE COVER Jan 29, 2014 · Grob G115C · Aircraft Fuel Distribution SystemSDR CA131121002Starter · inoperative(CAN) THE ENGINE FAILED TO START THE AIRCRAFT DURING AN ATTEMPTED START. BENDIX DID ENGAGE THE RING GEAR BUT WOULD NOT TURN THE ENGINE. THE STARTER WAS REPLACED WITH A O/H UNIT AND ENGINE STARTED NORMAL. THE STARTER WAS PURCHASED AS AN O/H UNIT. THE MALFUNCNov 20, 2013 · Grob G115C · Engine StarterSDR CA130715016Alternator · failed(CAN) AIRCRAFT EXPERIENCED LOSS OF TACHOMETER IN FLIGHT AND GENERATOR LIGHT ILLUMINATED. ACFT LANDED WITHOUT INCIDENT. INSPECTION OF THE GENERATOR SYS SHOWED THE GENERATOR BELT HAD DISASSEMBLED AND THE GENERATOR CASE WAS BROKEN. THERE WAS NO OTHER DAMAGE. Jul 12, 2013 · Grob G115C · AC Generator-AlternatorSDR CA111110006Muffler · broken(CAN) LEFT MUFFLER OUTLET PIPE FOUND MISSING. INSPECTION OF REMAINING MUFFLER DISCOVERED EXTENSIVE INTERNAL CORROSION AND PARTIAL COLLAPSE OF INNER CONE.Nov 4, 2011 · Grob G115C · Engine Noise SuppressorSDR 2009FA0000792Arm · crackedTHE STEERING ARM ON LT SIDE OF THE TAILWHEEL ASSY WAS FOUND CRACKED ACROSS THE RADIUS OF BEND NEAR THE HUB OF THE STEERING ASSY. THIS WAS FOUND ON A PREFLIGHT INSP. OF NOTE IS THE FACT THE ARM WAS BENT DOWN TO "LEVEL" WHEREAS THE STANDARD ANGLE IS UP BY 5-10Aug 12, 2009 · N801AT · Arctic S1B2 · Landing Gear Steering SystemSDR CA081120001Buckle · unserviceable(CAN) BUCKLE WOULD NOT RELEASE.Nov 19, 2008 · Grob G115C · Emergency EquipmentSDR 2005FA0001051Mount · chafedLOWER RT DIAGONAL ENGINE MOUNT TUBE FOUND CHAFED DO TO EXHAUST PIPE COMING INTO CONTACT WITH THE TUBE, THIS HAPPENED DO TO THE CLOSE PROXIMITY OF THE EXHAUST SYSTEM TO THE MOUNT. CORRECTED BY REPOSITIONING EXHAUST SUPPORT CLAMPS. WHILE REPAIRING THE CHAFED TJul 19, 2005 · N6YE · Amtr VANSRV6A · Engine Mount SectionSDR AUS20031044Bellcrank · corroded(AUS) FLAP BELLCRANK CORRODED. FOUND DURING INSPECTION IAW AD/PA23/50.Sep 30, 2003 · Piper PA23160 · Trailing Edge Flap Control SystemSDR AUS20031045Torque Tube · worn(AUS) FLAP TORQUE TUBE WORN BEYOND LIMITS. FOUND DURING INSPECTION IAWAD/PA23/89.Sep 30, 2003 · Piper PA23160 · Trailing Edge Flap Control SystemSDR CA030817001Spring · broken(CAN) WHILE TOWING THE AIRCRAFT TO ITS PARKING SPOT, A BANG WAS HEARD. THE AILERONS DEFLECTED FULL SCALE LT. THE AILERON AND RUDDER WERE NO LONGER INTERCONNECTED. ONE OF THE SPRINGS WAS FOUND TO HAVE BROKEN OFF AT THE ATTACHMENT POINT. WHILE REPLACING THE SPAug 8, 2003 · Grob G115C · Aileron Control SystemSDR CA030728003Wire Harness · failed(CAN) A WIRE BUNDLE BEHIND THE RT INSTRUMENT PANEL HAD CHAFED ON A SCREW SECURING A FACTORY INSTALLED BLANKING PLATE. THE NUT APPEARS TO HAVE BECOME LODGED IN THE CASING SECURING THE WIRE BUNDLE ALLOWING THE SCREW TO CHAFE THROUGH THE INSULATION ON TWO WIRES.Jul 28, 2003 · Grob G115C · Instrument System WiringSDR 2002FA0000853Muffler · separatedRT MUFFLER/EXHAUST LITERALLY FELL APART IN FLIGHT. BEYOND REPAIR. THE INLET FLANGE/PIPE ASSEMBLY COMPLETELY BROKE LOOSE FROM THE MUFFLER BODY. THE EXHAUST HANGAR, A RUBBER STRAP, WAS THE ONLY PART SECURING THE MUFFLER BODY TO THE AIRFRAME. THIS PART WAS PREVIOJul 23, 2002 · N115FN · Grob G115C · Engine Noise SuppressorSDR BIER200103057Carburetor · looseFOUND FUEL BOWL ATTACH SCREWS LOOSE WITH SUBSEQUENT FUEL LEAK AT BOWL GASKET, REQUIRED CARBURETOR REPLACEMENT DUE TO SCREW HOLE ELONGATION. SUBMITTER NOTES: LYCOMING SB 366, DATED SEPT 14, 1973 REFERENCES THIS FOR MARVEL-SCHEBLER CARBURETORS, WITH NO MENTION OJul 3, 2001 · N331AC · Grob G115C · Fuel Control/Reciprocating EnginesSDR CA981109026Bracket · broken(CAN) LEFT MAIN GEAR FOUND WITH EXCESSIVE PLAY DURING INSPECTION. LEFT MAIN GEAR UPPER BRACKET FOUND BROKEN AT THE FORWARD BOLT HOLE. CRACKS WERE FOUND IN THE WELDS AND THE BOLTS CLAMPING THE MAIN LANDING GEAR LEG WERE BENT.Oct 15, 1998 · Grob G115C · Main Landing Gear Attach SectionSDR CA980827013Plate · jammed(CAN) LATCH JAMMED ON CANOPY PLATE. CANOPY COULD NOT BE MOVED AFT AS IT WAS HOOKING ON THE PLATE. LATCH/LOCK IN THE OPEN POSITION. THIS WOULD STOP CANOPY EMERGENCY DEPLOYMENT.Aug 21, 1998 · Grob G115C · Flight Compartment WindowsSDR AU970284Hub · faulty(AUS) PROPELLER HUB BOLT HOLES (4OFF) TOO LARGE DUE TO INCORRECT DIAMETER BOLTS BEING USED - SEE MDR 97/0283Mar 24, 1997 · Propeller Hub SectionSDR AU970283Bolt · wrong part(AUS) PROPELLER HUB BOLTS (4OFF) INCORRECT PARTS. BOLTS MEASURE .375 -CORRECT MEASUREMENT .371. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Mar 6, 1997 · Propeller Hub SectionSDR AU960597Valve Guide · worn(AUS) ENGINE CYLINDER EXHAUST VALVE GUIDES (3OFF) EXCESSIVELY WORN - VALVE GUIDES WERE WITHIN SERVICE LIMITS BUT WOULD NOT LAST TO THENEXT TOP END OVERHAULMay 7, 1996 · Reciprocating Engine Cylinder SectionSDR 96ZZZX5137Magneto · coil failedON MAY 4, 1995, DUE TO HARD START PROBLEM, THE LEFT MAG COIL WAS FOUND DEFECTIVE. ON OCTOBER 28, 1995, THE RIGHT MAG FAILED IN-FLIGHT DUE TO A DEFECTIVE COIL.Oct 28, 1995 · N679CM · Amtr RV6 · Magneto/DistributorSDR 96ZZZX5138Magneto · coil failedON MAY 4, 1995, DUE TO HARD START PROBLEM, THE LEFT MAG COIL WAS FOUND DEFECTIVE. ON OCTOBER 28, 1995, THE RIGHT MAG FAILED IN-FLIGHT DUE TO A DEFECTIVE COIL.Oct 28, 1995 · N679CM · Amtr RV6 · Magneto/Distributor
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