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 DATA2012000004Uplock Switch · faultyON GEAR EXTENSION PRIOR TO LANDING, NO NLG INDICATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT.SDR DATA2012000002Brake Assy · fireON TAXI PRIOR TO TAKE OFF, AIRCRAFT BRAKES OVERHEATED DUE TO EXCESSIVE USE BY FLIGHT CREW, LEADING TO A FIRE AT THE RIGHT MAIN LANDING GEAR.SDR CA120312022Control Cable · frayed(CAN) DURING A SCHEDULED VISUAL INSPECTION OF THE FLAP CONTROL CABLES, A BADLY FRAYED CABLE WAS DISCOVERED, WHERE THE CABLE PASSES OVER A PULLEY THAT IS SOMEWHAT HARD TO SEE. THE CABLE WAS REPLACED, NO FURTHER ISSUES.SDR EXDA201112190001Bulb · burned outAS FLIGHT CREW PERFORMED PRE-LANDING CHECKS, NOTICED THE NLG DOWN AND LOCKED INDICATOR LIGHT DID NOT ILLUMINATE. CAPTAIN INFORMED THE ATC, FOLLOWED THE LANDING GEAR MALFUNCTION CHECKLIST AND LANDED WITHOUT INCIDENT. REPLACED DEFECTIVE BULB AND GROUND FUNCTIOSDR DATA2011000004Engine · bird ingestionFLIGHT 1465 ASW TO SDF IN LEVEL CRUISE APPROX 9000FT, FLIGHT CREW NOTICED SEVERE LOSS OF POWER FROM THE LEFT ENGINE. OBSERVED APPROX 45 PERCENT NG, LOW FUEL FLOW AND ITT, LOW & FLUCTUATING RPM. UNSUCCESSFUL RESTART ATTEMPT, PERFORMED SHUTDOWN & DECLARED EMERSDR TXHA2012F00014Pump · malfunctionedAFTER DEPARTURE, GEAR UP SELECTION, HYD LEFT AND HYDRAULIC RIGHT LIGHT ILLUMINATED ON CWP, HYD RIGHT CAME BACK ON-LINE. RETURNED TO DEPARTURE, SERVICED HYD SYS.SDR AVSA2011103100002Engine · unknownUNKNOWN, REMOVED FROM SERVICE.SDR CA111017006Circuit Breaker · unserviceable(CAN) ACFT RETURNED TO BASE AFTER THE ODOR OF SMOKE WAS DISCOVERED IN THE COCKPIT. UPON INSPECTION, IT WAS DISCOVERED THAT THE PILOTS RMI INTERNAL LIGHTING HAD FAILED, WHEN THE LIGHTING FAILED THE 1 AMP CIRCUIT BREAKER DID NOT POP, ALLOWING THE UNIT TO HEAT USDR DATR001632Bolt · failedRT SIDE ENGINE EXPERIENCED A LOW OIL PRESSURE LIGHT 1.5 HOURS INTO MISSION AND SUBSEQUENT PRESSURE LOSS. ENGINE WAS SHUTDOWN IN FLIGHT AND ACFT DIVERTED. THE ENGINE WAS RECEIVED AT THIS FACILITY FOR INVESTIGATION. THE PROPELLER SHAFT WAS HARD TO TURN AND A SDR TXHA2011090900001Wheel · crackedON REPOSITIONING THE ACFT, THE LT MAIN TIRE BLEW AND RIM WAS DAMAGED.SDR TXHA20110824001Hydraulic System · leakingAFTER DEPARTURE HYD LT LIGHT ILLUMINATED, WHEN GEAR WAS RETRACTED. RETURNED TO DEPARTURE BASE. ACFT HYD SYS WAS SERVICED AND ACFT DEPARTED WITHOUT FURTHER INCIDENT.SDR TXHA20110818001Shaft · shearedON TAKEOFF ROLL THE LT ENGINE FLAMED OUT, PILOT ABORTED TAKEOFF NO FURTHER INCIDENT, RETURNED TO BLOCK. INVESTIGATION BY MX FOUND THE LT FUEL PUMP SHAFT SHEARED.SDR 2011F00149Probe · failedLT ENGINE ITT SPIKED TO 1150 THEY REDUCED POWER TO FLIGHT IDLE AND ITT REMAINED AT 830 DEG CENT. SHUTDOWN ENGINE AND CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. INVESTIGATION, SPLIT ENG AND DID A HOT SECTION INSPECTION AND FOUND NO DEFECTS. TESTED THE SDR 2011F00148Probe · failedLT ENGINE ITT SPIKED TO 1150, THEY REDUCED POWER TO FLIGHT IDLE AND ITT REMAINED AT 830 DEG CENT. SHUTDOWN ENGINE AND CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. INVESTIGATION, SPLIT ENG AND DID A HOT SECTION INSPECTION AND FOUND NO DEFECTS. TESTED THESDR DATA20110000002Control Cable · brokenDURING FLIGHT CONTROL CHECK PRIOR TO TAKEOFF, FLAPS WERE OPERATED FULL DOWN. LEFT FLAP DID NOT RETRACT WHEN COMMANDED TO FULL UP POSITION. MAINTENANCE OBSERVED LEFT FLAP CABLE BROKEN IN TRAILING EDGE OF WING NEAR FLAP SELECTOR VALVE.SDR 2011FA0000020Wire · shortedDURING FLIGHT CREW TRAINING FLIGHTS, LIGHT SMOKE AND ELECTRICAL ODOR CAME FROM BEHIND THE GLARESHIELD AT THE FWD RT WINDSHIELD. CREW CYCLED OFF WINDSHIELD HEAT AND SMOKE DISSIPATED. ACFT THEN LANDED WITHOUT INCIDENT. MX INSP OF WINDSHIELD REVEALED WINDOW INTESDR DATA2010000001Smoke Detector · false activationDURING APPROACH ERRONEOUS SMOKE INDICATION FROM SMOKE DETECTOR IN NOSE COMPARTMENT OF AIRCRAFT. SMOKE DETECTOR IS A SINGLE DETECTOR SINGLE OPERATING SYSTEM.SDR TXHA 7152010Engine · making metalUPON BLOCKING, PROP WAS FOUND FROZEN AND UNABLE TO TURN. INSPECTED FWD SCREEN AND OIL FILTER, FOUND METAL SHAVINGS IN POWER SECTION SCAVENGE SCREEN AND OIL FILTER. ENGINE WAS REMOVED AND SENT TO MFG FOR FURHTER INVESTIGATION.SDR TXH2010F00002Fire Loop · looseLT ENG HAD FIRE WARNING LIGHT ILLUMINATED, NO FIRE, FERRY PERMIT WAS ISSUED IAS GMM CHAP 5.18. NO PART WERE CHANGED. AFT FIRE LOOP FOUND LOOSE, CONNECTION RESECURED. OPS CK OK.SDR TXH2010F00003Bolt · failedENG SN PCE 106099 WAS REMOVED FOR METAL CONTAMINATION. IN FLIGHT, OIL PRESSURE FLUCTUATED 70-80 PSI, OIL TEMPERATURE IN CAUTION RANGE. POST FLIGHT INSP FOUND PROP BINDING WITH NOISE COMING FROM POWER SECTION GEAR BOX. REMOVED SCAVENGE PUMP OIL SCREEN AND FOSDR 2009FA0000669Smoke Detector · faultedSMOKE LIGHT CAME ON FOR AFT BAGGAGE COMPARTMENT DURING TAXI OUT, RETURNED TO BLOCK, INSPECTED AND FOUND NO FIRE OR SMOKE FALSE LIGHT INDICATION. MEL AFT SMOKE DETECTOR.SDR DATA200900002Engine · power lossUPON POWER UP FOR TAKEOFF, LT ENGINE BUFFET AND POWER LOSS. SHUTDOWN LT ENGINE. SUSPECT POWER SECTION FAILURE.SDR 2009FA0000013Control Cable · brokenTHE ACFT RT PROP CABLE BROKE. ACFT RETURNED TO HONOLULU STATION FOR INSPECTION AND REPAIR.SDR CA081029005Oil System · leaking(CAN) DURING CRUISE, THE PILOTS OBSERVED ENG TEMPERATURE RISING THRU 800°C AND PEAKING OVER 1000°C. FLAMES WERE NOTICED FROM THE EXHAUST. THE ENG WAS SHUTDOWN AND FIRE BOTTLES DISCHARGED. A SINGLE ENG LANDING FOLLOWED. POST FLIGHT INSPECTION REVEALED OIL LEAKSDR N973081107Indication Sys · malfunctionedWHILE EN ROUTE TO MCI THE FLIGHT CREW ELECTED TO SHUT DOWN THE RIGHT ENGINE AS A PRECAUTIONARY MEASURE DUE TO ERRATIC PROPELLER SPEED INDICATION AND DIVERTED TO COU. EXDA MAINTENANCE WAS DISPATCHED TO COU AND INSPECTED THE PROPELLER RIGGING IAW SHORTS MAINTENSDR DATA200700007Engine · failedN151CA DEPARTED MKE AT 00:00 ON A REPOSITION FLIGHT TO DNV. UPON REACHING CRUISE (5000FT) ALTITUDE, CRUISE POWER WAS SET BY THE FIRST OFFICER AS THE CAPTAIN WAS THE PILOT FLYING. SHORTLY AFTER CRUISE POWER WAS SET THE RIGHT ENGINE FAILED. BOTH TORQUE AND ITSDR DATA200700006Engine · surgesTHE CREW WAS DEPARTING CHARLESTON, SC, THE PILOT SMOOTHLY ADVANCED THE THROTTLES TO ALLOW THE PROPS TO SPIN UP TO MAX RPM, BEFORE SETTING TAKEOFF POWER. THE LEFT ENGINE STARTED SURGING AND BACKFIRING WHILE THE PILOT ADVANCED THE THROTTLES. THE COPILOT CALLESDR DATA200700005Engine · power lossWHILE IN CRUISE, LEFT ENGINE LOST POWER WITH INCREASE OF ITT TO 1200 FOLLOWED BY LOUD NOISE. FOLLOWED PROCEDURES AND SHUT DOWN ENGINE. DIVERTED TO MWA. ENGINE REPLACEMENT IN WORK.SDR CA070803007Engine · damaged(CAN) ON SHORT FINAL, THE ENGINE LOST POWER AND SMOKE WAS SEEN EXITING THE ENGINE EXHAUST. POST-FLIGHT INSPECTION REVEALED INTERNAL ENGINE DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE COMPLETED. (TC NR 20070803007)SDR CA070803011Bolt · sheared(CAN) ON CLIMB, ENGINE OIL PRESSURE WAS SEEN TO FALL TO ZERO AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A SHEARED 1ST STAGE REDUCTION GEAR CARRIER BOLT. (TC NR 20070803011)SDR DATA200700003Axle · separatedAFTER NORMAL LANDING, THE RIGHT MAIN WHEEL SEPARATED FROM THE AIRCRAFT ON TAXI. AFTER MAINTENANCE INSPECTION IT WAS DETERMINED THE AXLE SEPARATED FROM THE MAIN GEAR BEAM ASSEMBLY. ANOTHER SERVICEABLE LANDING GEAR BEAM WILL BE INSTALLED ALONG WITH OTHER REQUISDR DAT2006F00009Attach Bolt · brokenDURING THE SCHEDULED MAINTENANCE, THE PROP TORQUE WAS COMPLIED WITH ON THE RT SIDE, AT 30311.5 TAT AND 37942 TAC. THE INSPECTION FOUND (1) BROKEN PROP ATTACHMENT BOLT. THE PROPELLER WAS REMOVED IAW MM. THE PROPELLER WAS INSPECTED AND FOUND TO BE WITHIN THE SDR CA060926005Blade · corroded(CAN) UPON VISUAL INSPECTION , CORROSION WAS FOUND ON THE BLADE SHANK. AFTER REWORK TO MINIMUM DIMENSION DAMAGE STILL REMAINS. BLADE WIDTH AND THICKNESS IS WELL ABOVE MINIMUM DIMENSION. ALL 5 BLADES ARE U/S. (TC NR 20060926005)SDR DAT2006F00008Tire · failedTHE LANDING WAS NORMAL AND UNDER CONTROL. SLOWING TO ABOUT 60-70 KNOTS THE LT MAIN TIRE BLEW. WHEN THE TIRE BLEW AIRCRAFT WAS MAINTAINED ON CENTERLINE AND STEERING AIRCRAFT OFF THE ACTIVE RUNWAY. UPON FURTHER EVALUATION THE LT TIRE SHOWED SIGNS THAT WAS NOTSDR 2006FA0000676Spring · brokenFEATHERING SPRING WAS FOUND TO BE BROKEN WHILE STILL INSTALLED IN SPRING KIT. THE SPRING BROKE IN 3 DIFFERENT PIECES. KIT WAS DISASSEMBLED AND INSPECTED FOR FURTHER DAMAGE. NOTE: PROPELLER WAS REMOVED FROM SERVICE 08-DEC-00. (K)SDR DAT2006F00002Control Cable · brokenDURING THE TAKEOFF ROLL, A LT TURN TENDENCY WAS NOTICED AND THE TORQUE GAUGES WERE CHECKED. THE LT PROP GAUGE WAS INDICATING 12 RPM. DUE TO THE UNEXPECTED BEHAVIOR OF THE PROP THE FLIGHT CREW DECIDED TO RETURN TO DEPARTURE. AC LANDED WITHOUT INCIDENT. MECHSDR DAT2005F00014Gas Generator · surgesABORTED THE TAKEOFF DUE TO THE LT RTOP INDICATOR DID NOT ILLUMINATE ON THE TAKEOFF. AC WAS RETURNED TO MAINTENANCE HANGAR. CHIEF INSPECTOR TESTED THE RTOP SYSTEM ON THE GROUND. OPS CHECK GOOD IAW MM. AC WAS RETURNED TO SERVICE. (K)SDR DAT2005F00013Compressor · surgesAS POWER WAS BROUGHT TO TAKEOFF SETTINGS, THE RT TORQUE INSTANTLY INCREASED FROM 1400 LBS. THE RISE IN TORQUE OF THE LT ENGINE WAS FOLLOWED BY 2 COMPRESSOR STALLS, AT WHICH POINT THE TAKEOFF WAS ABORTED. AFTER A RUNUP WAS PERFORMED BY MAINTENANCE, IT WAS FOUSDR DAT2005F00010Engine · shutdownDEPARTING, CAPTAIN NOTICED THE LT ENGINE TORQUE DROPPING AND THE ITT RISE TO APPROX 850 DEGREES. THE CAPTAIN PUSHED THE LT POWER LEVEL UP SLIGHTLY TO VERIFY THAT IT HAD NOT WORKED ITSELF BACK. FLIGHT CREW COMPLETED THE VITAL ACTION ITEMS. FLIGHT CREW DECLARSDR DAT2005F00007Tire · failedAC HAD NORMAL STARTUP, TAXI OUT AND WAS CLEARED FOR TAKEOFF. FO WAS FLYING, CAPTAIN SET THE POWER, MADE THE CALLOUTS AND HAD JUST FINISHED SAYING (AIRSPEED ALIVE) WHEN FLIGHT CREW HEARD AN EXPLOSION, FELT THE LT WING DIP JUST AFTER A SLIGHT LT YAW. FLIGHT CRSDR DAT2005F00008Blade · crackedDURING THE SCHEDULED COMPLIANCE OF AD ON THE LT PROPELLER IT WAS FOUND 1 OF 6 PROPELLER BLADES WERE CRACKED. MECHANIC REMOVED AND REPLACED THE PROPELLER IAW MM. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)SDR TXH2005F00000Skin · crackedDEFECT WAS NOTED DURING INSPECTION OF HORIZONTAL AND VERTICAL STABILIZERS. SKIN AND RIB, TOP SIDE OF RUDDER BALANCE WEIGHT ATTACHMENT AND STRUCTURAL AREA CRACKED AND CORRODED. (WP13200509006) (K)SDR DAT2005F00006Line · contaminatedDURING FINAL APPROACH AND FINAL CHECKS, THE PROPS FWD THE RT ENGINE STARTED TO SURGE. POWER BROUGHT BACK ON RT ENGINE TO SLOW UP SURGE AND IT STOPPED SURGING MOMENTARILY AND THE GENERATOR AND OIL RT LIGHT ON THE CWP. THE NG`S WERE BELOW 50 PERCENT AND EMERGESDR DAT2005F00005Tire · failedDURING DEPARTURE ON TAKEOFF ROLL, ACCELERATION WAS NORMAL THROUGH 85 KNOTS, FLIGHT CREW HEARD A NOISE OUTSIDE OF THE AIRCRAFT. AC STARTED TO PULL TO LT AND THERE WAS CORRECTION MADE TO STRAIGHTEN THE AIRCRAFT. FLIGHT CREW NOTICED DURING THE CORRECTION THE ACSDR DAT2005F00003Line · leakingNORMAL DESCENT APPROACH AND FINAL CHECK LIST COMPLETE ALL SYSTEMS NORMAL THROUGH THE TOUCHDOWN. AFTER TOUCHDOWN BOTH THE HYD WCP WARNING LIGHTS ILLUMINATED. CHECK BRAKES AND NO RESPONSE. SELECTED EMERGENCY BRAKE AND USED FULL REVERSE TO STOP ON RUNWAY. THESDR CA050414011Circuit Breaker · failedREMOTE C/B FOR INLET HEAT STAYED IN CLOSED POSITION AND WOULD NOT OPEN. ALLOWING THE RT ENGINE INTAKE HEAT TO OPERATE WHEN AIRCRAFT POWER WAS TURNED ON AND CAUSED AN OVERHEAT SITUATION AT THE INTAKE ITSELF. PARTS WERE REPLACED WITH NEW AND AIRCRAFT WAS RELEASDR CA050104005Line · ruptured(CAN) UPON SELECTING GEAR DOWN DURING APPROACH THE STATED PRESSURE LINE RUPTURED CAUSING HYDRAULIC SYSTEM TO LOSE ALL FLUID. LANDING WAS ABORTED AND AN EMERGENCY WAS DECLARED. GEAR WAS EXTENDED USING EMERGENCY GEAR EXTENSION. AIRCRAFT LANDED SAFELY AND WAS TAXSDR CA041108008Bracket · cracked(CAN) BOTH ELEVATOR TRIM TAB MASS BALANCE BRACKETS WERE FOUND CRACKED DURING 9600 HOUR STRUCTURAL INSPECTION. THESE BRACKETS WERE RECENTLY REPLACED TO COMPLY WITH MAN DATORY S/B SD360-55-20. (REFERENCE AD 009-06-2003)SDR AUS20040378Connector · corroded(AUS) LT ENGINE FIRE WIRE CONNECTOR CORRODED. CONNECTOR IS LOCATED AT THE REAR FIREWALL POSITION.SDR 2004F00313Hose · crackedUPON BRAKE APP PRIOR TO MLG RETRACTION, FO HEARD A THUD. RETRACTED MLG NOTICED RT HYD IND ON CWP PRIOR TO ACCELERATION ALT. OBSERVED FALLING IND & HYD QTY GAUGE & 0 PRESSURE ON MAIN SYS PRESS GAUGE. CONTINUED TO CLIMB TO 2000 MSL. NORMAL EXTENSION FAILED. C
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