Mitsubishi MU-2B-60
Service difficulty reports · 112
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 = 'MU2B60' 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 = 'MU2B60' 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 CA190711009Actuator · failed(CAN) WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE LANDING GEAR DID NOT EXTEND AND THE LANDING GEAR DOORS DID NOT OPEN. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITH OUT INCIDENT. MAINTENANCE DISCOVERED THAT THE LANDING GEASDR CA180423014Gear · damaged(CAN) AFTER LANDING THE PILOT WENT TO SPIN THE PROPELLER, PER ROUTINE PROCEDURES, AND FOUND THAT THE ENGINE WOULD NOT TURN. AFTER SEVERAL ATTEMPTS THE ENGINE DID ROTATE, BUT A REASON FOR THE PROBLEM COULD NOT BE DETERMINED. THE ENGINE WAS REPLACED AND IS NOWSDR CA151008001Skin · cracked(CAN) DURING PRE-FLIGHT THE PILOTS MOVED THE FLIGHT CONTROLS THROUGH THE FULL RANGE OF MOTIONS AND FOUND THE LH ROLL SPOILER BINDING. MAINTENANCE FOUND A CRACKED EDGING IN THE LT OUTBOARD SPOILER FLAP WELL AT WING STATION 3400 (MM). THE CRACK ON THE EDGING CAUSDR CA141223004Adapter · broken(CAN) LEFT ENGINE OIL PRESSURE WAS FLICKERING IN THE YELLOW DURING GROUND RUNS. FOUND THE OIL FILTER ADAPTER HOUSING HAD TWO BROKEN MOUNTING TABS. ADAPTER WAS REPLACED & AIRCRAFT RETURNED TO SERVICE.SDR CA141015002Housing · cracked(CAN) PILOT RETURNED TO BASE DUE TO FLUCTUATING OIL PRESSURE. MAINTENANCE OBSERVED OIL LEAK AND DETERMINED IT WAS COMING FROM THE END OF THE OIL FILTER HOUSING.UPON FURTHER EXAMINATION A CRACK WAS FOUND IN THE CHAMFERED END OF THE HOUSING. (TC# 20141015002)SDR CA140131006Window · departed(CAN) WINDOW BLEW OUT AT ALTITUDE RESULTING IN DECOMPRESSION.SDR CA140318011Fitting · cracked(CAN) DURING ROUTINE INSPECTION THE NLG KEEL WEB WAS FOUND CRACKED. THE CRACK WAS REPAIRED USING DATA FROM MANUFACTURE.SDR CA131030006Strut · cracked(CAN) DURING SCHEDULED MAGNETIC PARTICLE INSPECTION THE RT NLG STRUT WAS FOUND CRACKED. PART WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR CA131022007Wire · damaged(CAN) WHILE TAXING AFTER LANDING, THE CREW SHUTOFF WINDSHIELD HEAT ON THE OVERHEAD SWITCH CONSOLE. A FLASH WAS NOTICED AND SPARKS FELL DOWN. MAINTENANCE DISCOVER AN ANTI-ICE POWER FEEDER WIRE HAD ARCED A STRINGER. THE WIRE WAS FOUND STRIPPED OF INSULATION 1SDR CA130327003Adapter · cracked(CAN) DURING ROUTINE INSPECTION ON THE RH ENGINE THE BLEED AIR ADAPTER WAS FOUND CRACKED WHERE THE SMALL LINE SEPARATES FROM THE MAIN LINE. THIS ADAPTER CAN BE STRESSED DURING ENGINE REMOVAL AND INSTALLATION.SDR CA130109005Angle · cracked(CAN) FOUND ANGLE CRACKED DURING SCHEDULED INSPECTION.SDR CA120703006Engine · flamed out(CAN) DURING INITIAL DESENT THE RT ENGINE FAILED, THE ENGINE WAS SECURED AND ACFT LANDED ON 1 ENGINE WITHOUT INCIDENT. OIL FILTER WAS PULLED AND FOUND METAL IN THE OIL. ENGINE REPLACED. WE ARE AWAITING THE TEARDOWN REPORT FROM THE ENGINE O/H FACILITY.SDR CA120605007Rod End · broken(CAN) DURING GEAR RETRACTION AND EXTENSION PILOT HEARD A LOUD BANG. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE FOUND THE RT FWD GEAR DOOR ROD END BROKEN. ROD END ASSEMBLY REPLACED AND CHECKED SERVICEABLE.SDR 2012FA0000260Switch · failedAFTER TAKE OFF, RETRACTED GEAR AND RED DOOR UNSAFE LIGHT WAS ON. ELECTED TO RETURN TO FIELD, SELECTED GEAR DOWN AND GEAR STAYED UP. TRIED CYCLING GEAR SWITCH, NO HELP. ACCOMPLISHED ALTERNATE GEAR EXTENSION AND LANDED SAFELY. JACKED ACFT, RAISED GEAR AND DUSDR CA111108003Engine · shutdown(CAN) DURING CLIMBOUT, RT ENGINE SHUTDOWN, ENGINE WAS SECURED AND ACFT LANDED WITH 1 ENGINE, WITHOUT INCIDENT. AWAITING ENGINE TEARDOWN REPORT FOR FURTHER INFORMATION.SDR BKAA14110282011Engine · failedDURING FLIGHT PILOT EXPERIENCED A FAILURE OF THE LEFT ENGINE. INITIATED INFLIGHT SHUT DOWN, DECLARED AN EMERGENCY AND LANDED AT RICHMOND INTERNATIONAL AIRPORT UNEVENTFUL. PILOT DID DECLARE AN EMERGENCY.SDR CA110805002Clamp · wornAFTER TAKEOFF ACFT HAD SOME SMOKE IN THE COCKPIT FROM THE OVERHEAD PANEL, THE PILOTS SHUTOFF ALL THE SWITCHES TO THE PANEL AND THE SMOKE STOPPED THEY THEN RETURNED TO BASE AND LANDED WITHOUT INCIDENT. THE OVERHEAD PANEL WAS REMOVED AND WIRING INSPECTED, WE FSDR CA110406006Oil Cap · worn(CAN) DURING ROUTINE ENG INSPECTION THE OIL FILTER CAP WAS FOUND TO BE CONTACTING THE ENG MOUNT CAUSING WEAR ON THE CAP. THIS ENG HAD SERVICE BULLETIN 79-0012 OIL FILTER HOUSING ADAPTER INCORPORATED THAT ALLOWED THE CONTACT. THE FILTER CAP WAS REPLACED & THESDR 2011FA0000132Spur Gear · damagedFOUND TORQUE SENSOR SPUR GEAR SEVERELY DAMAGED DUE TO MATERIAL CONTACT AND OVERHEAT. GEAR HAD SEVERAL GEAR TEETH SEPARATED WITH REMAINING GEAR TEETH SHOWING SIGNIFICANT DAMAGE. THE LOWER SCAVENGE TUBE RETAINER BOLT HEAD WAS FOUND TO BE DAMAGED DUE TO CONTACTSDR CA101116011Limit Switch · frozenAFTER THE PILOT SELECTED GEAR UP THE NOSE GEAR "DOWN" LIGHT REMAINED ILLUMINATED. CREW CONTINUED TO A MAINTENANCE BASE AND COMPLETED A MANUAL EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR DOWN LIMIT SWITCH CONTAMINATED WITH ISDR BKAA79409012010Landing Gear · bindingWHEN GEAR WAS SELECTED TO GEAR DOWN POSITION, GEAR DID NOT DEPLOY. PILOT HAD TO MANUALLY DEPLOY GEAR USING MANUAL EXTENSION. GEAR CAME DOWN AND LOCKED WITH ALL INDICATIONS NORMAL. PILOT THEN MADE A NORMAL LANDING AFTER DECLARING AN EMERGENCY.SDR CA100112001Wheel · cracked(CAN) AIRCRAFT LANDED WITH LOW TIRE PRESSURE WHEEL ASSY REPLACED AFTER WHEEL ASSY REPAIRED IT WAS FOUND THAT THE TUBE HAD 3 SMALL CRACKS ON THE SIDE WALL. NOTE OUTSIDE AIR TEMP WAS -30 DEGREES. TUBE AND TIRE REPLACED AND WHEEL ASSY RETURNED TO SERVICE (TC NRSDR CA091006002Motor · intermittent(CAN) AFTER TAKEOFF ON CLIMB OUT GEAR UNSAFE LIGHT WAS STILL ON. ACFT RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. AFTER LANDING THE GEAR UNSAFE LIGHT WENT OUT. A FERRY FLIGHT WAS COMPLETED BACK TO BASE WITH GEAR DOWN. THE ACTUATOR/MOTOR FOR THE FWD GEAR DOSDR CA090424003Hinge · cracked(CAN) LT FWD LANDING GEAR DOOR FWD DOOR SIDE HINGE WAS FOUND CRACKED. HINGE WAS REPLACED AND LANDING GEAR SWINGS COMPLETED AND FOUND SERVICEABLE. NOTE THIS SAME CRACK WAS FOUND PREVIOUSLY ON OTHER GEAR DOORS.SDR 2008FA0000701Servo · contaminated8/11/08 INSTALLED YAW DAMPENER. 10/06/08 - CUSTOMER COMPLAINT OF INDUCED YAW WHEN ENGAGING AUTO PILOT. REMOVED YAW DAMPENER AND FOUND UNIT CONTAMINATED WITH WATER. UNIT IS MOUNTED WITH DRIVE SHAFT UP AND WITH NO DRAIN, THIS PROVIDES FOR WATER TO BE TRAPPED INSDR CA080902002Battery · thermal runaway(CAN) DURING DAILY INSP OF ACFT, GPU USED. ACFT KEY TURNED (ON) TO CHARGE BATTERIES. APPROX. 2.5 HRS LATER, VENTING OF BATTERY NOTICED FROM ACFT. SMELL OF BURNING PLASTIC. GPU DISCONNECTED, KEY (OFF). ACFT MOVED OUTSIDE. AIRPORT FIRE DEPT. REMOVED NR 1 BATTERSDR BKA2008F00000Engine · shutdownDEPARTING , THE RT ENGINE BETA LIGHT CAME ON SHORTLY AFTER TAKEOFF. LOSS OF OIL PRESSURE WAS NOTED, THE OIL PRESSURE DID NOT DROP BELOW THE RED LINE BUT WAS IN THE YELLOW ARC. IAW EMERGENCY CHECK LIST RT ENGINE WAS SHUT DOWN, DECLARED EMERGENCY AND RETURNED TOSDR CA080821006Attach Fitting · cracked(CAN) DURING ROUTINE INSP, THE NOSE LANDING GEAR TRUNNION ATTACH FITTING WAS FOUND TO BE CRACKED. THE CRACK WAS MEASURED AT .3125 OF AN INCH. FITTING REPLACED.SDR CA080623002Motor · inoperative(CAN) PILOT SELECTED GEAR DOWN THE DOOR MOTOR CIRCUIT BREAKER POPPED. MANUAL GEAR EXTENSION COMPLETED AND ACFT LANDED WITHOUT INCIDENT. MECHANIC DISPATCHED AND FOUND THE GEAR DOOR ACTUATOR/MOTOR UNSERVICEABLE. ACFT FERRIED TO MAINTENANCE BASE, DOOR ACTUATOR/MOSDR CA080613010Lock Plate · worn(CAN) DURING A ROUTINE PROP INSP, IT WAS FOUND THAT THE PITCH LOCK PLATE ALLOWS THE LATCH PIN TO SLIP OFF THE EDGE AND COULD JAM THE PIN. THIS COULD PREVENT IN FIGHT ENGINE START.SDR BKAA200710002Engine · shutdownSUP RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPESDR BKAA070905102Engine · shutdownRT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPESDR 002Engine · shutdownRT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPESDR R0240301Bracket · crackedFIVE B-3493 START LOCK BRACKETS WERE FOUND DURING PENETRANT INSPECTION TO BE CRACKED AT THE SAME LOCATION. CRACKS ARE LOCATED ON THE EXTERIOR START PIN BORE NEXT TO THE SPINNER MOUNTING BOLT RELIEF CUT-OUT. THIS BRACKET IS PART OF THE 830-34L START LOCK UNIT ISDR CA070514002Link · tight(CAN) AT THE AIRCRAFT 100 HOUR INSPECTION AND DURING THE REMOVAL OF THE PROP PITCH LINKS, IT WAS FOUND THAT THE PIVOT PIN WAS DIFFICULT TO REMOVE. AFTER REMOVAL, THE PISTON UNIT (THAT WAS REPLACED RECENTLY) WAS FOUND TO HAVE PAINT INSIDE THE PIVOT PIN HOLE CSDR CA070228002Arm · stiff(CAN) WHEN AIRCRAFT LANDED IT WOULD PULL TO THE LT. MAINTENANCE FOUND THAT THE PROP GOVERNOR ARM WAS STIFF AND WOULD NOT RETURN TO THE STOP. NOTE THIS GOVERNOR HAS SB TPE331-72-0567 RETURN SPRING INCORPORATED ON IT. GOVERNOR WAS REPLACED AND CHECKED SERVICESDR 2007F00005Latch · brokenLT IB COWL LATCH FOR THE NR 2 ENGINE TOP COWL BROKE. VISUAL INSP REVEALED THE LATCH LINK ASSY BROKE INTO 2 PIECES.SDR 2006FA0001200Access Panel · corrodedDRAIN HOLE IN COVER NOT BEING LOCATED PROPERLY CAUSES WATER TO LAY IN AFT. FLANGE OF NEXT FRAME FWD CAUSING CORROSION. (DRAIN HOLE NEEDS TO BE IN FRAME RADIUS. (PRIMARY STRUCTURE). (K)SDR VOX2006F00000Latch · brokenLATCH LINK BROKE ON TOP ENGINE, COWLING LEFT AIRCRAFT. NO DAMAGE TO REST OF AIRCRAFT. RECOMMEND INSTALLING SCREW ON BOTH SIDES OF COWLING SECURING COWLING TO BACK UP IF LATCH BREAKS. (K)SDR CA061011001Bearing · failed(CAN) AN IN-FLIGHT SHUTDOWN WAS CARRIED OUT WHEN THE ENGINE STARTED TO SURGE AND THE NEGATIVE TORQUE SYSTEM (NTS) PULSE. UPON DISASSEMBLY AT AN ENGINE REPAIR FACILITY, IT WAS NOTED THAT THE CAUSE WAS PREMATURE WEAR AND SUBSEQUENT FAILURE OF THE DUAL P/N: 31030SDR 2005FA0000401Ring Gear · brokenON 2/26/2005, AN UNCOMMANDED, INFLIGHT CONTAINED SHUTDOWN OCCURED ON THE LT ENGINE DUE TO A GEARBOX FAILURE. THE AIRCRAFT WAS NOT DAMAGED AND MADE A NORMAL LANDING. INVESTIGATION IN THE ENGINE GEARBOX REVEALED THAT THE RING GEAR SUPPORT AND PLANETARY SPUR GESDR 2005FA0000400Planetary Gear · failedON 2/26-2005 AN UNCOMMANDED, INFLIGHT CONTAINED SHUTDOWN OCCURED ON THE LT ENGINE DUE TO A GEARBOX FAILURE. THE AIRCRAFT WAS NOT DAMAGED AND MADE A NORMAL LANDING. INVESTIGATION IN THE ENGINE GEARBOX REVEALED THAT THE RING GEAR SUPPORT AND PLANETARY SPUR GEASDR 2005FA0000124Housing · failedIN FLIGHT, PILOT NOTICED FLUCTUATING OIL PRESSURE AND TORQUE. PRECAUTIONARY LANDING MADE, FOLLOWING TROUBLESHOOTING ENGINE WAS DISASSEMBLIED GEARBOX SCAVENGE OIL PUMP WAS CRACKED. APPROXIMATELY 7 HOURS PRIOR, THE NR 8 STAINLESS OIL SCAV. LINE CRACKED. APPROSDR 2005FA0000118Line · crackedNR 8 SCAVENGE OIL LINE FROM ENGINE GEARBOX TO VERNATHERM CRACKED INSIDE THE B-NUT SLEEVE AT GEARBOX. THIS LED TO SIGNIFICANT LOSS OF OIL AND A PRECAUTIONARY SHUTDOWN IN FLIGHT. AC RETURNED DEPARTURE, UNEVENTFUL LANDING, REPLACED OIL LINE. (K)SDR G1I2004F00003Seal · leakingSMOKE APPEARED IN CABIN AFTER ROTATION. RETURNED TO SAME AIRPORT. IT APPEARS A COMPRESSOR SEAL LEAK IN THE LT ENGINE ALLOWED TURBINE OIL TO ENTER THE POWER SECTION, BURN AND CREATE ENVIRONMENTAL SMOKE. OIL LEAK WAS DETERMINED TO BE WITHIN ALLOWABLE LIMITS. SDR CA040720001Skin · lightning strikeIN CRUISE OUT OF JFK NOTICED LIGHTNING STRIKE ON LEFT PROP/SITUATION WAS EVALUATED AND ALL PARAMETERS WERE NORMAL. FLIGHT WAS CONTINUED AND UPON LANDING ON YOW BASE NOTICED UPON CLOSE INSPECTION: LEFT PROP BLADE DAMAGED, PROP REPLACED. LEFT OUTBOARD AILERON SDR CA030505004Drive Shaft · sheared(CAN) THE PROP INDICATION WAS INTERMITTENT. MAINTENANCE FOUND THE DRIVE SHEARED OFF INSIDE THE TACHOMETER GENERATOR WHERE THE ROLL PIN SECURES THE DRIVE.SDR MYN2003F00000Diode · failedDIODE CR 406 SHORTED, ALLOWING POWER FROM LT FUEL TRANSFER CIRCUIT TO FEED BACK TO THE RT FUEL TRANSFER CIRCUIT. WHEN LT TP FUEL SHUT OFF VALVE WAS COMMANDED ON AND RT TIP FUEL SHUTOFF VALVE COMMANDED OFF. THE RT TP FUEL SHUT OFF VALVE HAD POWER ON PINS A ANSDR CA020911001Fuel Control · leaking(CAN) AFTER TAKEOFF THE TORQUE ON THE RT ENGINE DROPPED APPROXIMATELY 10 PERCENT. PILOT ADVANCED THE THROTTLE TO COMPENSATE. WHEN THE TORQUE DROPPED AGAIN THE PILOT ADVANCED THE THROTTLE AGAIN THEN DECIDED TO RETARD THE THROTTLES AND COME BACK TO LAND. MAINTSDR CA020513001Rod End · separated(CAN) ROD END SEPARATED FROM PISTON.UNIT RETURNED TO VENDOR AND WAS OVERHAULED. SERVICE BULLETIN NR 169B EMBODIED TO PRECLUDE FURTHER EVENTS.
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