Short Bros SD3-60
Service difficulty reports · 313
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 = 'SD360' 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 = 'SD360' 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 AU000526Wire · broken(AUS) LT PROPELLER INDICATION SYSTEM WIRE BROKEN.SDR 20000517SH002Smoke Detector · false indicationDURING FLIGHT, THE ''SMOKE FWD'' LIGHT CAME ON. THE CHECKLIST WAS FOLLOWED AND THE ENTIRE CONTENTS OF THE COCKPIT EXTINGUISHER WAS EMPTIED INTO FWD COMPARTMENT. THE LIGHT EVENTUALLY WENT OUT. INSPECTION AFTER LANDING REVEALED NO EVIDENCE OF FIRE/ SMOLDERINGSDR AU000376Bearing · failed(AUS) ENGINE NR 1 BEARING FAILED.SDR AU000255Engine · malfunctioned(AUS) RT ENGINE OIL PRESSURE DROPPED. WHEN THE ENGINE POWER WAS REDUCED UNUSUAL NOISES WERE HEARD FROM THE ENGINE.SDR 20000501SH044Smoke Detector · false indicationAT ROTATION, THE SMOKE AFT CWP LIGHT ILLUMINATED. THE PILOT REQUESTED ''PRIORITY HANDLING FOR AN IMMEDIATE RETURN, KS23. THE AIRCRAFT LANDED IN CRW WITHOUT INCIDENT. THE CRW MECHANIC WAS DISPATCHED TO THE AIRCRAFT. THE MECHANIC CHECKED THE SMOKE DETECTORS, SDR AU000268Tire · deflated(AUS) LT MAIN LANDING GEAR TYRE FLAT.SDR AU000150Pressure Switch · failed(AUS) AUTO-FEATHER SYSTEM RT PRESSURE SWITCH FAILED.SDR AU000033Wire · damaged(AUS) LEFT ENGINE FIRE DETECTION WIRE FAULTY.SDR CA000118029Fuel Control · failed(CAN) TACH VALVE GUIDE PIN BACKED OUT WHICH DAMAGED THE BALLHEAD RETAINER AND THE BEARING SEIZED. THE FCU COUPLING WAS ALSO DAMAGED AS A RESULT. PIN HAS PRELOAD AND IS BRAISED IN DURRING ASSY. THIS IS THE FIRST INSTANCE NOTED AND WOODWARD IS INVESTIGATING.SDR CA000110035Bearing · failed(CAN) PRE SB 60034-73-1 BEARING FOUND TO BE FAILING DURING ROUTINE BENCH CHECK. POST SB BEARING AVAILABLE WHICH HAS LARGER RETAINER TYPE BALL BEARINGS.SDR 99ZZZX4553Gland Nut · failedGLAND NUT FAILED CAUSING THE SHOCK STRUT TO SEPARATE AND NOT SUPPORT THE AIRCRAFT ON LANDING.SDR AU991081Bearing · failed(AUS) ENGINE FAILURE. SUSPECT BEARING FAILURE.SDR CA990907009Bolts · sheared(CAN) ONE BOLT FOUND SHEARED AND BETA ROD PN B-3475A-3 WAS PULLED OUT. ON REMOVAL OF THE PROP, ANOTHER BOLT SHEARED.SDR AU990540Engine · failed(AUS) LT ENGINE FAILURE. SUSPECT BEARING FAILURE.SDR 99ZZZX1146Smoke Detector · malfunctionedEN ROUTE TO SDF, APPROXIMATELY 10 MINUTES FROM LANDING, THE FORWARD SMOKE CWP LIGHT CAME ON. THE CAPTAIN INSTRUCTED THE F/O TO DISCHARGE THE FORWARD HAND HELD FIRE EXTINGUISHER BOTTLE INTO THE FORWARD COMPARTMENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THERESDR 99ZZZX1145Smoke Detector · malfunctionedEN ROUTE TO SDF, APPROXIMATELY 10 MINUTES FROM LANDING, THE FORWARD SMOKE CWP LIGHT CAME ON. THE CAPTAIN INSTRUCTED THE F/O TO DISCHARGE THE FORWARD HAND HELD FIRE EXTINGUISHER BOTTLE INTO THE FORWARD COMPARTMENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THERESDR AU990099Oil Cooler · faulty(AUS) RT ENGINE OIL COOLER FAULTY.SDR AU990007Detector · jammed(AUS) DURING THE TAKEOFF ROLL, STICK SHAKER ACTIVATION OCCURRED. INVESTIGATION FOUND THE LEFT STALL VANE HAD STUCK IN THE UP POSITION.SDR TY7A9901Retract Mech · malfunctionedTAKEOFF, GEAR FAIL TO RETRACT, EMERGENCY HANDLE APPEARED TO BE SLIGHTLY OUT OF POS 3 GREEN LIGHTS CONFIMRED DOWN/LOCKED, LANDED FOR VERIFICATION. RESET LANDING GEAR EXTENSION HANDLE PER MM 32-30-00. VISUALLY VERIFIED POSITION OF 3-WAY VALVE AT R/T STUB WING SDR 99ZZZM152Valve · out of positionTAKEOFF GEAR FAIL TO RETRACT EMERGENCY HANDLE APPEARED TO BE SLIGHTLY OUT OF POSITION 3 GREEN LIGHTS CONFIRMED GEAR DOWN AND LOCKED, LANDED FOR VERIFICATION CORRECTIVE ACTION. RESET LANDING GEAR EXTENSION HANDLE PER MM 32-30-00, VISUALLY VERIFIED POSITION OF SDR AU990008Switch · intermittent(AUS) SHORTLY AFTER TAKEOFF, STALL WARNING AND STICK SHAKER ACTIVATED. PROBLEM BECAME INTERMITTENT WHEN CREW CYCLED APPROPRIATE CBS. COULDN'T BE REPRODUCED ON GROUND - TEST SWITCH SUSPECTED AND REPLACED.SDR TY7A9802Turbine · failedLEFT ENGINE WAS REPLACED DUE TO TURBINE FAILURE AND PROPELLER REMOVED AND SERVICED.SDR PIVA12627Drag Brace · failedNO DOWNLOCK LEFT LANDING GEARS INDICATION BEFORE LANDING CREW DECLARE EMERGENCY. LEFT GEAR COLLAPSED UPON LANDING. NO DAMAGE TO THE AIRCRAFT. (M)SDR AU981464Patch · separated(AUS) NOSE WHEEL TIRE BALANCE PATCH SEPARATED FROM THE INSIDE OF THE TIRE.SDR PIVA12211Smoke Detectors · malfunctionedAFT CARGO SMOKE DETECTOR WARNING CAME ON DURING CLIMB-OUT. OCCURED TWICE, ONCE OUT OF SAIPAN AND ONCE OUT OF GUAM. THE AIRCRAFT RETURNED TO FIELD BOTH TIMES. THERE WAS NO FIRE FIGHTER TIME. THE AIRCRAFT WAS FERRIED TO SIAPAN FROM GUAM AFTER THE SECOND OCCUSDR 98ZZZX4119Wheel Assy · crackedAFTER TOUCHDOWN, AIRCRAFT PULLED TO RIGHT AND VIBRATION NOTICED INDICATING RT MAIN TIRE FLAT. BROUGHT AIRCRAFT TO STOP ON RUNWAY AND SHUT DOWN. ON POST-FLIGHT EXAM, NOTICED RT MAIN WHEEL RIM CRACKED AND TIRE FLAT. THE RUNWAY WAS CLOSED, AND MECHANIC SENT IMSDR 98ZZZX4036Wheel · crackedCAPTAIN AND FIRST OFFICER DID A VISUAL APPROACH TO RUNWAY 31 IN BFD. AFTER TOUCHDOWN, AIRCRAFT PULLED TO RIGHT AND VIBRATION NOTICED INDICATING RT MAIN TIRE FLAT. BROUGHT AIRCRAFT TO STOP ON RUNWAY AND SHUT DOWN. ON POST-FLIGHT EXAM, NOTICED RT MAIN WHEEL RSDR AU981037Wheel · damaged(AUS) RIGHT MAIN LANDING GEAR WHEEL OUTER RIM GROUND AWAY WHEN TIRE FAILED FOLLOWING BRAKE LOCK-UP.SDR AU981038Wheel · failed(AUS) RIGHT MAIN WHEEL OUTER RIM SECTION MISSING.SDR AU981022Hpu · failed(AUS) NR 2 HSI HEADING PROCESSOR UNIT FAILED.SDR 98ZZZM623Line · leakingBIL - PILOT REPORTED A LOSS OF BRAKING ACTION AND A LOSS OF HYDRAULC FLUID DURING TAXI. LEAKING PRESSURE HYDRAULIC FLUID LINE TO THE NOSE STEERING ACTUATOR. REMOVED AND REPLACED HOSE ASSY. REPLENISHED HYDRAULIC CONTENTS. LEAK AND FUNCTIONAL CHECKED. AIRCRSDR AU981023Tire · faulty(AUS) NOSE WHEEL TIRE BALANCE PATCH SEPARATED FROM THE INSIDE WALL OF THE TIRE.SDR 98ZZZX2960Hose · leakingAFTER DEPARTURE FROM ADF, THE LT AND RT HYDRAULIC CWP LIGHTS CAME ON. THE HYDRAULIC SYSTEM PRESSURE AND CONTENTS SHOWED 15 PERCENT. THE CREW PUT THE LANDING GEAR DOWN AND FOLLOWED EMERGENCY PROCEDURES. THE CREW DID NOT DECLARE AN EMERGENCY WITH THE TOWER ANSDR AU980765Brake Cable · separated(AUS) EMERGENCY BRAKE ACCUMULATOR CABLE SEPARATED FROM THE ACTUATING HANDLE CAUSING THE EMERGENCY BRAKE SYSTEM TO REMAIN ACTIVATED. PART TOTAL CYCLES: 7,293.SDR AU980799Actuator · failed(AUS) HYDRAULIC FLAP ACTUATOR FAILED.SDR 99ZZZX551Valve · brokenON DESCENT, RIGHT ENGINE BEGAN TO SURGE WITH POWER LEVER MOVEMENTS. SHUT DOWN ENGINE FOR PRECAUTIONARY MEASURES AND LANDED ON ONE ENGINE. REMOVED AND REPLACED BLEED VALVE. OPS CHECK OK.SDR PIVA11648Pipe · rupturedHYDRAULIC PRESSURE FAILED IN-FLIGHT. HYDRAULIC FLUID LOSS DUE TO .50 INCH RUPTURE OF PIPE. P/N SD3-73-1019XA REQUIRING SHUT DOWN OF HYDRAULIC PUMPS AND RETURN TO FIELD. (X)SDR AU980579Actuator · failed(AUS) LT PROPELLER SYNCHRONIZATION SYSTEM FAILED. PROPELLER CONTROL ACTUATOR FULLY WOUND ONE WAY PREVENTING THE GOVERNOR ARM FROM REACHING THE MAXIMUM RPM STOP.SDR AU980580Support · damaged(AUS) AIRCRAFT TAIL SUPPORT STRUT (POGO STICK) NOT REMOVED AND STOWED BEFORE THE AIRCRAFT DEPARTED.SDR PIVA11079Engine · failedSHUT DOWN OF ONE ENGINE IN-FLIGHT PER FOLLOWING PILOT REPORT IN PIVA AFML PAGE 102793, NR 1 ENGINE FAILED IN-FLIGHT. NOTED COMPRESSOR STALL FOLLOWED BY 3 LARGE EXPLOSIONS AND FIRE ON RIGHT SIDE OF ENGINE. ENGINE SECURED AND EMERGENCY DECLARED. THE SPECIFIC SDR AU980390Bearing · misinstalled(AUS) DURING AD/SD3-60/48 (STUB WING SHEAR DECK AND RIB CORROSION INSPECTION), BOTH MAIN UNDERCARRIAGE SHOCK STRUT GLAND NUTS PN 200920604 WERE FOUND SHEARED. FURTHER INVESTIGATION REVEALED THAT THE BEARING PN 200920638 HAD PREVIOUSLY BEEN FITTED UPSIDE DOWN.SDR AU980254Fire Wire · faulty(AUS) LT ENGINE FIRE WIRE FAULTY.SDR AU980211Battery · overheated(AUS) LT BATTERY OVERHEATED. BATTERY WAS STILL TOO HOT TO HANDLE THREE HOURS LATER.SDR 98ZZZX1168Timer · failedTHE TAIL DE-ICE BOOTS WERE INOPERABLE DURING THE FLIGHT. THE DE-ICE TIMER WAS REPLACED. OPS CHECK GOOD.SDR 98ZZZX868Packing · brokenPRECAUTIONARY SHUT DOWN OF NR 2 ENGINE IN-FLIGHT. LOW TORQUE AND LOW OIL PRESSURE. FOUND OIL LEAK ON FRONT SCAVENGE OIL TRANSFER TUBE AREA. REPLACED AS 3209-117 PACKING.SDR AU980007Generator · failed(AUS) RH ENGINE STARTER/GENERATOR FAILEDSDR SABA980001Rod Assy · out of adjustON FLT FROM CLT TO OAJ, AIRCRAFT RETURNED TO CLT DUE TO FORWARD BAGGAGE COMPARTMENT DOOR LIGHT ILLUMINATED. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. PASSENGERS DEPLANED. MAINTENANCE ADJUSTED THE PUSH-PULL ROD ON THE FORWARD BAGGAGE COSDR AU980050Seal · failed(AUS) LH ENGINE GAS GENERATOR TACHO GENERATOR SHAFT SEAL FAILED.SDR CA971110001Guide Lug Pin · worn(CAN) PILOT REPORTED NR 1 PROPELLER WOULD NOT COME OUT OF FEATHER. INVESTIGATION FOUND THE SNAP RING (P/N 79-1210056) OF THE LOW PITCH STOP ROD ADRIFT. FURTHER INVESTIGATION REVEALED THE GUIDE LUG PIN HAD CAME OFF ITS SEAT AND FORCED THE SNAP RING OFF. THE PRSDR SABA970037Retract Mech · malfunctionedAFTER TAKEOFF FLAP WOULD ONLY RETRACT 3 TO 4 DEGREES. CREW TRIED CYCLING FLAPS WITH NO SUCCESS. PUT FLAPS TO 15 DEGREES AND RTF IN PGV. UPON LANDING FLAPS RETRACTED BUT CAPTAIN SAID THE LEFT FLAP WAS JERKY. CREW OPERATED FLAPS ON THE GROUND. OPS CHECKED G
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