Dornier DO-228-202
Service difficulty reports · 51
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 = 'DO228202' 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 = 'DO228202' 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 BIGA20200623002Control Box · malfunctionedTHE RIGHT FIRE CONTROL BOX FLASHED A FIRE WARNING WHILE IN FLIGHT. TROUBLESHOOTING REVEALED THE BOX WAS FAULTY AND IT WAS REPLACED WITH A SERVICEABLE UNIT. NO FURTHER INDICATIONS WERE OBSERVED.SDR BIGA20200609001Restrictor Valve · leakingTHE RESTRICTOR VALVE ASSEMBLY (ATTACHED TO THE SHUTTLE VALVE ON THE NOSE LANDING GEAR ACTUATOR) BLEW OUT IT'S BODY SEALING O-RING LEADING TO COMPLETE HYDRAULIC FLUID LOSS AFFECTING STEERING, BRAKING AND FLAP ACUATION. THIS HAPPENED ON TAXI FOR FLIGHT. THE LANDSDR XV6A2016122700004Pump · inoperativeAFTER STARTING ENGINES AND TURNING HYDRAULICS ON, THERE WAS NO PRESSURE. INSTALLED SERVICEABLE HYDRAULIC POWER PACK ASSY IAW DO228 AMM 29-10-19. FUNCTIONAL AND LEAK CHECKED GOOD. (SUSPECT HYDRAULIC PUMP FAILED INTERNALLY. HYDRAULIC PUMP MOTOR OPS CHECK GOOSDR XV6A2016102500003Control Handle · intermittentAFTER LANDING CHECKLIST WAS COMPLETED, PULLED THE LANDING GEAR HANDLE, DID NOT RESPOND (NO RED BLINKING LIGHT, NO NOISE FROM THE LANDING GEAR EXTENSION), NOTHING HAPPENED. CYCLED IT 3 TIMES WITH NO RESPONSE. THEN FLIPPED HYDRAULIC TO MANUAL, CYCLED GEAR HANDSDR XV6A2016052200002Unknown · odorELECTRICAL "HOT" ODOR NOTED WHILE IN PATTERN. PERFORMED POWER/ON OPS CHECKS OF EXTERNAL POWER, AVIONICS POWER, STATIC INVERTERS, INSTRUMENT PANEL AND COCKPIT LIGHTS, AND PASSENGER INFORMATION LIGHTS. APPLIED HYD POWER, CHECKED COCKPIT HEATERS, EXTENDED AND RESDR XV6A2016050300001Hose · chafedAFTER GEAR EXTENSION NWS, NOSE WHEEL STEERING, BYPASS ANNUNCIATOR ILLUMINATED AND HYDRAULIC PRESSURE INDICATED 0 BAR. AFTER INSPECTION FOUND NWS HYD LINE CHAFED, CAUSING LOSS OF HYDRAULIC PRESSURE. R & R SAID LINE IAW DO-228, AMM 32-20-01. TIMES AND CYCLES OSDR BIGA20160219001Fire Warning · false activationAFTER CONFIRMING A BLEED AIR SEAL COUPLING LEAK ON SDR BIGA20160114-001, THE ACFT FIRE DETECTION SYS WAS GND TESTED NORMAL. A TEST FLIGHT WAS REQUESTED, DURING THE FLIGHT THE LT FIRE DETECTION FLICKERED. AGAIN THE SYS WAS TESTED ON THE GND & COULD NOT BE DUPSDR BIGA20160114001Seal · wornPILOT WAS PERFORMING A NIGHT CURRENCY FLIGHT, AS HE BEGAN HIS FINAL APPROACH THE LT ENG FIRE WARNING CAME ON. THE PILOT PULLED BACK POWER & THE FIRE LIGHT WENT OUT BELOW 40% TORQUE. PUSHING THE POWER UP CAUSED THE LIGHT TO COME BACK ON. THE PILOT LANDED WITSDR CA151110009Wire · burned(CAN) ON START THE RT ENGINE WOULD NOT LITE OFF. ROTATION UNKNOWN. FLIGHT CREW NOTIFIED MAINTENANCE. FLIGHT WAS EVENTUALLY CANCELLED. UPON INVESTIGATION, MAINTENANCE NOTICED THE RCR AND WIRES WELDED AND BURNED.SDR BIGA20150406001Control Rod · wornDURING INSPECTION, THE AILERON CONTROL ROD WAS FOUND TO BE WORN APPROX 15% OF THE THICKNESS. THE ROD WAS WORN FROM THE AILERON GUST LOCK SYS & SEEMS ONLY WEAR ON THE PILOTS OTBD SIDE DUE TO A SLIGHT MISALIGNMENT OF THE GUST LOCK.SDR XV6A2015021600001Bearing · bindingAFTER LANDING, DURING FLAP RETRACTION, CONTROL WHEEL MOVES RIGHT. DURING INSPECTION, FOUND BOTH INBD AILERON BEARINGS TIGHT. R & R LT AND RT AILERON BEARING ARMS IAW EO-DO228-57-20-2015-01.SDR XV6A2014080500005Motor · failedGEAR HANDLE DOWN & NO INDICATION OF ANY HYD PRESS OR GEAR MOVEMENT. RAN QRH & PERFORMED EMER GEAR EXTENSION CHECKLIST. R & R HYD POWER PACK, OPERATIONS CHECKED GOOD. DISCOVERED HYD ELEC MOTOR FAILED ON HYD POWER PACK, ELEC MOTOR SENT FOR OVERHAUL FOR FINDINSDR XV6A2014072600003Actuator · failedNO INDICATION OF RT LG DOWN & LOCKED. R & R MLG ACTUATOR, OPS CHECKED GOOD.SDR XV6A2014071500002Engine · warning lightDURING CRUISE FLIGHT AT 9500 FT, MASTER WARNING HORN & LIGHT SOUNDED. LT OIL PRESSURE ANNUNCIATOR ILLUMINATED & TORQUE DROPPED. RAN QRH ENG FAILURE CHECKLIST, DECLARED AN EMERGENCY & DIVERTED. REMOVED LT PROPELLER & ENGINE AS AN ASSEMBLY. INSTALLED SERVICESDR BIGA20140711001Wire · brokenTHE LEFT GENERATOR SYSTEM KICKED OFF LINE. AFTER TROUBLESHOOTING THE SYSTEM THE 20 GAUGE "D" WIRE WAS FOUND TO BE BROKEN INSIDE THE SHEATH IN THE ENGINE COMPARTMENT AND WAS ONLY DETECTABLE BY OHM CHECKING THE HARNESS. DURING THE OHM READING CHECKS OF THE GENSDR XV6A2013112500009Shutoff Valve · stuckLEFT ENGINE FIRE BOTTLE FIRED DUE TO FIRE INDICATION DURING VENT. 1C EMERGENCY EXIT REMOVED FOR POSSIBLE GROUND EVAC. ENGINE VENT WAS DUE TO ABORTED START, LEFT ENGINE HUNG AT 32-33 PERCENT, NO TEMP LIMIT REACHED - 60 SECONDS. DURING TROUBLESHOOTING OF NR 3SDR XV6A2013040600003Uplock · malfunctionedAFTER SELECTING GEAR UP, GEAR INTRANSIT LIGHT ILLUMINATED AND PUMP PRESSURE ZERO. REMOVED AND REPLACED RIGHT MLG UPLOCK IAW DO228 AMM 32-30-10. OPS CHECK GOOD.SDR XV6A2013033000002Fabric · missingUPPER LEFT FABRIC OF ELEVATOR MISSING WAS DETECTED ON POST FLIGHT WALK AROUND. REMOVED AND REPLACED LEFT ELEVATOR IAW DO228 AMM 55-20-00 OPS CHECK GOOD. NOTE: APPROXIMATE TIME SINCE RECOVERING FOR LEFT ELEVATOR 952.3 FLIGHT HOURS.SDR CA120716018Skin · separated(CAN) DEPARTED WHILE LEVELING OFF INTO CRUISE, A BANG WAS HEARD AND FOLLOWED BY A VIBRATION FELT IN THE CONTROLS AND CONTROLLABILITY PROBLEMS. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY BACK. AFTER LANDING IT WAS DISCOVERED THAT APPROXIMATELY 95 PERCENT SDR XV6A2012052500005Uplock Switch · inoperativeUPON LEAVING BAR 10, PLACED GEAR HANDLE IN UP POSITION, GEAR UNSAFE LIGHT CONTINUED TO FLASH. RAN QRH AND PLACED GEAR IN THE DOWN POSITION, THEN RECYCLED TO THE UP POSITION, GEAR UNSAFE CONTINUED TO FLASH. RETURNED GEAR TO THE DOWN POSITION. AIRCRAFT DIVERTSDR XV6A2012051600004Relay · intermittentON FINAL APPROACH AT 1Z1, GEAR DOWN SELECTED AND NO HYDRAULIC PRESSURE INDICATED AND GEAR DID NOT EXTEND. TRIED SEVERAL TIMES TO SWITCH MANUAL "ON" AND IT DID NOT WORK. RETURNED TO VGT AND TRIED SEVERAL TIMES AGAIN TO GET HYDRAULICS TO WORK TO NO AVAIL. FINSDR XV6A2012051500003Gauge · faultyDURING CRUISE, NR 1 OIL TEMP WENT INTO RED LINE. CONTACTED MOC AND PERFORMED PRECAUTIONARY ENGINE SHUT-DOWN (LEFT ENGINE). TROUBLESHOT SYSTEM, VERIFIED OIL TEMP INDICATION INACCURATE. REPLACED OIL TEMP BULB, NO HELP, ORIGINAL TEMP BULB REINSTALLED. ALL WIRSDR CA120516004Adapter · failed(CAN) ON THE 12 OF MAY 0424ZULU, ACFT WAS INBD FOR LANDING WHEN THE CREW REPORTED THEY HAD AN OIL FLUCTUATION FOLLOWED SHORTLY BY A TORQUE FLUCTUATION ON THE RT ENGINE. THE RT ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND REQUESTED ARFF VEHICLES ON STANDSDR BIGA201205151202Linkage · out of adjustTHE AIRCRAFT WAS TEST FLOWN FOR NTS SHUTDOWN WHICH REQUIRES THE SHUTDOWN OF THE NR 2 ENGINE IN FLIGHT. THE SPEED LEVER WAS PULLED OVER THE GATE AND INTO THE STOP AND FEATHER POSITION, THE MANUAL FUEL SHUTOFF CUT THE FUEL TO THE ENGINE, BUT THE FEATHER VALVE DSDR XV6A2011102500015Thermocouple · faultyDURING FLIGHT, NR 1 ENGINE INDICATED HIGH OIL TEMP, IN YELLOW. CREW ACCOMPLISHED QRH AND MADE AN UNSCHEDULED LANDING INTO 1G4. REPLACED LT OIL TEMP INDICATOR WITH REPAIRED INDICATOR, PROBLEM STILL EXISTS. REPLACED LT OIL TEMP BULB WITH NEW BULB. OPS CHECK SDR CA110707005Skin · delaminatedELEVATOR FABRIC DELAMINATED AND SEPARATED FROM STRUCTURE OF CONTROL SURFACE CAUSING AIRFRAME BUFFET AND UNCOMMANDED ELEVATOR OSCILLATIONS.SDR XV6A2010101300012Tire · failedFOUND LT AND RT NOSE WHEEL AND TIRE ASSY DAMAGED.SDR CA100908004Bearing · brokenWHILE PULLING THE PROP THROUGH BY HAND AN UNUSUAL NOISE WAS HEARD. FURTHER INVESTIGATION REVEALED AN OIL FILTER BYPASS INDICATION AND METAL PARTICLES IN THE OIL FILTER. ENGINE WAS REMOVED AND FORWARDED FOR INSP AND REPAIR. TEARDOWN SHOWED THAT THE PN 3103585SDR CA100119014Roller · damaged(CAN) THE NLG FAILED TO RETRACT CORRECTLY, LODGING GEAR LEG LOCKING ROLLER INTO ABOVE SPACE BETWEEN UPLOCK IMPACT LATCH, AND THE UPLOCK HSG (INDICATED BY SCORE MARKS ON THE ROLLER THAT MEASURE PERFECTLY WITH THE UPLOCK LATCH AND UPLOCK HSG). OLEO PRESSURE KEPSDR CA090819003Link Assy · brokenCREW CLEANING CABIN BEFORE FLIGHT, IT WAS NOTICED THAT ONE OF THE PASSENGER SEAT BELTS HAD COME LOOSE AT THE ATTACHMENT BRACKET. UPON FURTHER EXAMINATION, IT WAS NOTED THAT PN 31768 LINK ASSY HAD FAILED CAUSING THE SEAT BELT TO DETACH FROM THE SEAT.SDR CA090330004Tire · deflated(CAN) UPON LANDING , THE CREW NOTICED THE ACFT "PULLING" SLIGHTLY TO THE LEFT. THE ACFT TAXIIED IN AND UPON INVESTIGATION BY THE FLIGHT CREW NOTICED THAT THE LT NOSEWHEEL HAD DEFLATED.SDR CA081022006Carbon Seal · leaking(CAN) NR 1 ENGINE CREW SHUT DOWN DUE TO STEADY DROP OF OIL PRESSURE AND TORQUE FLUCTUATION, BELIEVED LATER THAT THE REAR CARBON SEAL BEGAN TO LEAK THUS INGESTION OIL IN ENGINE AND BURNT. ENGINE REMOVED FROM ACFT TO BE SENT FOR FURTHER TESTING AT ENGINE SHOP.SDR CA080815001Fuel Control · malfunctioned(CAN) ACFT WAS RELEASED TO A SATISFACTORY TEST FLIGHT FOLLOWING NR 1 ENGINE CHANGE. A NTS IN FLIGHT SHUT DOWN WAS TO BE PERFORMED BEFORE ACFT COULD BE RELEASED BACK TO SERVICE. ACFT DEPARTED AND HAD A NORMAL TAKE OFF AND PROCEED WITH NTS SHUT DOWN. PILOT PROCSDR CA080718004Potentiometer · malfunctioned(CAN) ON TAKE OFF ACFT ROTATED PILOT FELT SOMETHING ABNORMAL IN RUDDER PEDALS, SELECTED GEAR UP , GEAR HANDLE WOULD NOT MOVE, PILOT OBSERVED GEAR HANDLE LOCK STILL IN PLACE. ACFT FLOWN BACK TO BASE , PILOT DID A LOW FLYBY WHERE IT WAS CONFIRMED THAT THE NOSE GSDR XV6A200700003Fire Loop · wornLEFT FIRE HANDLE LIGHT AND MASTER WARNING WENT OFF IN FLIGHT FOR ONE SECOND (TWICE). REMOVED AND REPLACED FIRE WARNING LOOP DETECTOR IAW 26-10-05. LEFT ENGINE FIRE LOOP TEST OPS CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR XV6A200700002Fabric · tornDURING CRUISE FLIGHT, PILOT FELT A BUMP IN THE CONTROL COLUMN. CONTROL COLUMN MOVED UNCOMMANDED FORWARD AND AFT. POWER REDUCTION RESULTED IN NORMAL FLIGHT CHARACTERISTICS. AFTER NORMAL LANDING FOUND LEFT ELEVATOR UPPER SURFACE FABRIC TORN OFF. DURING INVESSDR 2007F00052Tach Generator · false indicationLEFT RPM INDICATION ABNORMAL PERFORMED PRECAUTIONARY SHUTDOWN. INSPECTION FOUND TACH GENERATOR SHAFT BROKEN. REMOVED AND REPLACED TACH GENERATOR IAW AMM 77-11-03. ENGINE GROUND PERFORMANCE RUN C/W AND PASSED. ALL PARAMETERS NORMAL. AIRCRAFT APPROVED FOR RSDR CA080729005Motor · intermittent(CAN) UPON SELECTED GEAR DOWN NOTHING HAPPENED. PILOT THEN CYCLED THE GEAR DOWN AGAIN ALL FUNCTION NORMALLY, 3 GREEN DOWN AND LOCKED. ACFT WAS THEN INSPECTED, NO FAULTS FOUND, MAINT CREWS AND EQUIPMENT WERE FLOWN IN AND PUT A/C ON JACKS GEAR SWUNG NO FAULTS ACSDR CA060306020Relay · inoperative(CAN) ON APROACH FLAPS WERE SELECTED TO THE NR 2 POSITION AND DID NOT RESPOND . SYSTEM TROUBLESHOOTING FOUND THE RELAY TO BE NOT FUNCTIONING . RELAY WAS REPLACED WITH A SERVICABLE UNIT AND FLAPS TESTED NORMAL (TC NR 20060306020)SDR CA051115007Engine · unknown(CAN) RT ENG DID AN UNCOMMANDED INFLIGHT SHUTDOWN. TROUBLESHOOTING IN PROGRESS . WILL UPDATE FURTHER .SDR CA051013008Engine · power lossRT ENGINE WAS REMOVED FOR LOW TORQUE INDICATION AND SENT OUT FOR REPAIR AFTER TESTING PROVED AN INTERNAL PROBLEM. THE ENGINE WAS RE-INSTALLED FROM REPAIR WITH A NEW TORSION SHAFT SN 05P15649 AND TORQUE SENSOR P/N 3101726 AND NTS TEST FLIGHT WAS CARRIED OUT ANSDR CA050622002Stringer · corrodedDURING PRE-BUY INSPECTION, THE PURCHASER VISUALLY NOTED THE PRESENCE OF CORROSION ON THE TOP SURFACE OF THIS STRINGER. UPON FURTHER AND LATER INSPECTION, IT WAS DETERMINED TO REQUIRE REPLACEMENT OF THIS STRINGER.SDR CA050419009Pulley · binding(CAN) ACFT DEPARTED & RETURNED WITH PRECAUTIONARY ENGINE SHUTDOWN DUE TO JAMMED POWER LEVER. MX ABLE TO DUPLICATE SYMPTOMS. POWER LEVER CIRCUIT INSPECTED & IN RT SIDEWALL AT PULLEY ASSY, A SMALL SCREW NR 4 DIAMETER .375 INCH LONG FOUND IN IMMEDIATE VICINITY. SDR XV62005F00002Adapter · crackedOIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200505213) (K)SDR XV62005F00000Adapter · crackedOIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200407922)SDR XV62005F00001Adapter · crackedOIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116)SDR CA040506006Squat Switch · intermittentAIRCRAFT DEPARTED AND LANDING GEAR WOULD NOT RETRACT. NOSE WEIGHT SWITCH TESTED AND FOUND TO BE INTERMITTENT. PART CHANGED OUR WITH SERVICABLE UNITSDR 2002F00759Rib · crackedCRACKS FOUND ON RIB NR 12 ON RIGHT SIDE AND RIB NR 13 ON LEFT SIDE. LT RIB CRACKED THROUGH 4 RIVETS HOLES ON TOP SKIN, LENGTH OF CRACK WAS 5 INCHES. RT RIB CRACKED THROUGH 1 RIVET HOLE, LENGTH OF CRACK WAS 2 INCHES. CRACKS WERE FOUND DURING COMPLIANCE WITH SDR CA980421005Skin · damaged(CAN) DURING CRUISE IN STILL AIR, AIRCRAFT STRUCK BY LIGHTNING. IT APPEARS TO HAVE ENTERED VHF COMM ANTENNA ON FORWARD FUSELAGE BELLY. EXIT POINT WAS AT RIGHT ELEVATOR TRAILING EDGE. A SMALL AREA AT EXIT POINT WAS MELTED INTO A BLOB. THE AFT HALF OF THE ELSDR CA960429006Brake · not releasing(CAN)PART HAD RECENTLY BEEN INSTALLED. INTERMITTENT PROBLEMS OF FLAP CURRENT LIMITER BLOWING FOUND THAT THE ELECTRIC BRAKE ON THE WING TIP BRAKE (SYMNETRY UNIT) WOULD SOMETIMES TAKE UP TO 4 SECONDS TO RELE ASE AFTER THE INITIAL CLICK OF SOLENOID. TEMPERATURE S
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