Consolidated 108-2

Service difficulty reports · 16

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 = '1082'
  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 2011FA0000372Terminal · meltedTHE POSITIVE STUD MELTED OUT FROM THE ARMMETER AND THE ACFT LOST POWER TO THE BUSS BAR.May 24, 2011 · N346C · Univar 1082 · Electrical Power System WiringSDR 2010FA0001054Wheel · failedCAST SHOULDER THAT HOLDS THE WHEEL BRG RACE FROM MOVING INWARD ON THE AXLE, BROKE OUT, CAUSING THE RACE AND BRG TO TRAVEL INWARD. THE WHEEL WAS NO LONGER HELD CENTERED ON AXLE, AND WHEEL SUBSEQUENTLY HAD EXTREME CAMBER ANGLE. THE EXTREME ANGLE BROKE A PORTIOAug 28, 2010 · N9569K · Univar 1082 · Wheel/Ski/FloatSDR CA091113001Tube · corroded(CAN) TUBING RUSTED OUT AFT FITTING.Oct 25, 2009 · Univar 1082 · Fuselage Main, FrameSDR 2009FA0000850Gear · fracturedON A FLIGHT THE ENGINE STOPPED SUDDENLY WITH NO WARNING. THE AIRCRAFT LANDED. THE ENGINE ACCESSORY CASE HAD MAJOR DAMAGE. THE MAGNETOS WERE BROKEN AWAY FROM THE CASE AND THERE WERE SOME LARGE HOLES IN THE CASE. A TEARDOWN INSPECTION REVEALED THAT THE CRANKCAug 3, 2009 · N373C · Univar 1082 · Reciprocating Engine Power SectionSDR 20000717SH010Crankshaft · failedENGINE BEGAN RUNNING ROUGH AND THEN THE PROPELLER LOCKED IN THE VERTICAL POSITION. POST-INCIDENT INSPECTION OF THE ENGINE REVEALED THE CRANKSHAFT HAD FAILED. (X)Jun 10, 2000 · N9830K · Univar 1082 · Reciprocating Engine Power SectionSDR 99ZZZX23Seat · brokenSEAT BROKE AT BOTH HORIZONTAL LEGS. MATERIAL .50 INCH OUTSIDE DIAMETER, .035 INCH WALL 4130 STEEL TUBES. FRACTURES SHOW EVIDENCE OF CRYSTALLIZATION FROM BENDING STRESSES. EXAMINATION REVEALED COPILOT'S SEAT PREVIOUSLY REPAIRED SAME LOCATION. THIS FAILURE ODec 8, 1998 · N381C · Univar 1082 · Flight Compartment EquipmentSDR CA980430023Hub · worn(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CYLINDER SUPPORT WAS FOUND BENT AND THE CYLINDER WAS WORN.Apr 23, 1998 · Univar 1082 · Propeller Hub SectionSDR CA980406003Control Column · corroded(CAN) WHILE PAINT STRIPPING THE CONTROL COLUMN A PIN HOLE APPEARED. REMOVING THE ALUMINUM PLUG, A LINE OF CORROSION WAS FOUND HALF WAY AROUND THE INSIDE OF THE COLUMN AT THE HEIGHT OF THE PLUG. CORROSION WAS THROUGH AT THE PIN HOLE AND GRADUALLY LESS TO THE Mar 30, 1998 · Univar 1082 · Control Column SectionSDR 98ZZZX313Crankshaft · crackedINSPECTION FOUND CRANKSHAFT PROPELLER FLANGE CRACKED BETWEEN HOLES IN TWO PLACES.Dec 2, 1997 · N9504K · Univar 1082 · Reciprocating Engine Power SectionSDR CA970305006Weld · failed(CAN) THE WELD THAT HOLDS THE AXLE ATTACHMENT BUSHING TO THE LANDING GEAR LEG FAILED. REPLACED.Feb 4, 1997 · Univar 1082 · Main Landing Gear Strut/Axle/TruckSDR 96ZZZX3353Valve · stuckPILOT REPORTED FUEL SELECTOR VALVE STUCK BETWEEN DETENTS WHILE ATTEMPTING TO CHANGE FROM RT TO LT FUEL TANK. AFTER PUTTING BOTH HANDS ON VALVE HANDLE, THE PASSENGER AND PILOT WERE ABLE TO ROTATE THE VALVE TO THE LT TANK. DISASSEMBLED THE VALVE AND FOUND SCORJun 5, 1996 · N9609K · Univar 1082 · Fuel Selector/Shut-Off ValveSDR EY2R9600203Hub · corrodedPROP ASSY HUB IS CORRODEDJan 1, 1996 · Univar 1082 · Propeller Hub SectionSDR EY2R9600202Blade · corrodedBLADE ASSY SN C45338YS IS CORRODEDJan 1, 1996 · Univar 1082 · Propeller Blade SectionSDR EY2R9600201Blade · corrodedBLADE ASSY SN K31785YS IS CORRODEDJan 1, 1996 · Univar 1082 · Propeller Blade SectionSDR 95ZZZX4488Crankshaft · brokeCRANKSHAFT - REGROUND 18 HOURS EARLIER. AT OVERHAUL, BROKE AT REAR THROW WITH LOSS OF POWER. GRINDING MAY HAVE BEEN THE WORK OF AN AUTOSHOP WITH NO INTEREST IN FILLET RADIUS. ENGINE RAN SMOOTH UNTIL THEN. SECOND REPORTED BROKEN CRANKSHAFT OF SAME TYPE.Aug 1, 1995 · N9619K · Univar 1082 · Reciprocating Engine Power SectionSDR 95ZZZX4201Horn · notchedINSPECTION OF CONTROL HORN FOUND IT 'NOTCHED'. HARD RT RUDDER APPLICATION REPEATEDLY HIT VERTICAL ASSEMBLY CAUSING IMPACT DAMAGE. SOME ONE FAILED TO 'FIX' DAMAGE. NOTCH CAUSED INTERFERENCE OF CONTROL MOVEMENT. OWNER ADVISED TO GROUND AIRCRAFT UNTIL REPAIREJun 9, 1995 · N9653K · Univar 1082 · Rudder Control System
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