# Service difficulty reports: Stinson 108-2 A list on [Stinson 108-2](https://openairdocs.org/model/stinson-108-2.md). Newest first. General aviation reporting is voluntary. - [SDR 2011FA0000372](https://openairdocs.org/sdr/2011FA0000372.md): Terminal · melted · May 24, 2011 · N346C · Univar 1082 · Electrical Power System Wiring > THE POSITIVE STUD MELTED OUT FROM THE ARMMETER AND THE ACFT LOST POWER TO THE BUSS BAR. - [SDR 2010FA0001054](https://openairdocs.org/sdr/2010FA0001054.md): Wheel · failed · Aug 28, 2010 · N9569K · Univar 1082 · Wheel/Ski/Float > CAST 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 PORTIO - [SDR CA091113001](https://openairdocs.org/sdr/CA091113001.md): Tube · corroded · Oct 25, 2009 · Univar 1082 · Fuselage Main, Frame > (CAN) TUBING RUSTED OUT AFT FITTING. - [SDR 2009FA0000850](https://openairdocs.org/sdr/2009FA0000850.md): Gear · fractured · Aug 3, 2009 · N373C · Univar 1082 · Reciprocating Engine Power Section > ON 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 CRANKC - [SDR 20000717SH010](https://openairdocs.org/sdr/20000717SH010.md): Crankshaft · failed · Jun 10, 2000 · N9830K · Univar 1082 · Reciprocating Engine Power Section > ENGINE BEGAN RUNNING ROUGH AND THEN THE PROPELLER LOCKED IN THE VERTICAL POSITION. POST-INCIDENT INSPECTION OF THE ENGINE REVEALED THE CRANKSHAFT HAD FAILED. (X) - [SDR 99ZZZX23](https://openairdocs.org/sdr/99ZZZX23.md): Seat · broken · Dec 8, 1998 · N381C · Univar 1082 · Flight Compartment Equipment > SEAT 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 O - [SDR CA980430023](https://openairdocs.org/sdr/CA980430023.md): Hub · worn · Apr 23, 1998 · Univar 1082 · Propeller Hub Section > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CYLINDER SUPPORT WAS FOUND BENT AND THE CYLINDER WAS WORN. - [SDR CA980406003](https://openairdocs.org/sdr/CA980406003.md): Control Column · corroded · Mar 30, 1998 · Univar 1082 · Control Column Section > (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 - [SDR 98ZZZX313](https://openairdocs.org/sdr/98ZZZX313.md): Crankshaft · cracked · Dec 2, 1997 · N9504K · Univar 1082 · Reciprocating Engine Power Section > INSPECTION FOUND CRANKSHAFT PROPELLER FLANGE CRACKED BETWEEN HOLES IN TWO PLACES. - [SDR CA970305006](https://openairdocs.org/sdr/CA970305006.md): Weld · failed · Feb 4, 1997 · Univar 1082 · Main Landing Gear Strut/Axle/Truck > (CAN) THE WELD THAT HOLDS THE AXLE ATTACHMENT BUSHING TO THE LANDING GEAR LEG FAILED. REPLACED. - [SDR 96ZZZX3353](https://openairdocs.org/sdr/96ZZZX3353.md): Valve · stuck · Jun 5, 1996 · N9609K · Univar 1082 · Fuel Selector/Shut-Off Valve > PILOT 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 SCOR - [SDR EY2R9600203](https://openairdocs.org/sdr/EY2R9600203.md): Hub · corroded · Jan 1, 1996 · Univar 1082 · Propeller Hub Section > PROP ASSY HUB IS CORRODED - [SDR EY2R9600202](https://openairdocs.org/sdr/EY2R9600202.md): Blade · corroded · Jan 1, 1996 · Univar 1082 · Propeller Blade Section > BLADE ASSY SN C45338YS IS CORRODED - [SDR EY2R9600201](https://openairdocs.org/sdr/EY2R9600201.md): Blade · corroded · Jan 1, 1996 · Univar 1082 · Propeller Blade Section > BLADE ASSY SN K31785YS IS CORRODED - [SDR 95ZZZX4488](https://openairdocs.org/sdr/95ZZZX4488.md): Crankshaft · broke · Aug 1, 1995 · N9619K · Univar 1082 · Reciprocating Engine Power Section > CRANKSHAFT - 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. - [SDR 95ZZZX4201](https://openairdocs.org/sdr/95ZZZX4201.md): Horn · notched · Jun 9, 1995 · N9653K · Univar 1082 · Rudder Control System > INSPECTION 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 REPAIRE ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/stinson-108-2/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.