Mitsubishi MU-2B-36A
Service difficulty reports · 20
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 = 'MU2B36A' 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 = 'MU2B36A' 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 2009FA0000713Window · crackedPILOT COMPLAINED OF LOSS OF PRESSURIZATION IN FLIGHT AND UNABLE TO MAINTAIN SUFFICIENT CABIN PRESSURE TO SUSTAIN FLIGHT AT HIGHER ALTITUDES. RT CABIN WINDOW FWD OF EMERGENCY EXIT WAS FOUND TO HAVE SEVERE CRACKS AT BOTH UPPER CORNERS ALLOWING PRESSURE FROME THSDR 2008FA0000571Control Cable · brokenPILOT COMPLAINED OF POOR ELEVATOR TRIM OPS. UPON INSP, FOUND ELEVATOR TRIM CABLE 311AS-14-7245 BROKEN (RT CABLE). 311AS-14-7362 (LT CABLE), 010A-61179-81 (RT AFT) CABLES FRAYED. IDLER PULLEY SHAFT ON PITCH TRIM SERVO SHEARED. REPLACED CABLES & SERVO, OPS CSDR 2007FA0000100Rod End · brokenDURING GEAR EXTENSION FOR LANDING, A LOUD BANG WAS NOTICED BY THE PIVOT AND UNSAFE LIGHT STAYED ON. AIRCRAFT WAS ROUTED TO MAINTENANCE AFTER LANDING. MAINTENANCE FOUND ROD END ART -7E ON SHAFT HAD COME APART ANDALLOWED DOORS TO BECOME DISCONNECTED FROM ACTUASDR CA060523005Nut · crackedWHILE CARRYING OUT A WINGS OFF INSPECTION AND COMPLYING WITH SERVICE BULLETIN 103/57-004 WING ATTACHMENT HARDWARE. INSPECTION, THE RT LOWER FORWARD WING ATTACH BOLT BARRELL NUT WAS FOUND CRACKED THROUGH THE ENTIRE THREADED PORTION OF THE NUT. THE NUT WAS REPSDR 2006FA0000476Gear · crackedPILOT REPORTED DURING CRUISE LEVEL FLIGHT FEELING A SUDDEN VIBRATION AND HEARING A SCREAMING NOISE FROM THE LT ENGINE. PILOT THEN NOTICED TORQUE INDICATION ON LT ENGINE INDICATING 120 PERCENT WITH NO YAW INDICATED OR NOTICED BY PILOT. WHILE RETARDING LT POWERSDR IZ22003F00004Solenoid Valve · leakingSOLENOID VALVE LEAKING EXCESSIVE OIL BETWEEN SOLENOID AND VALVE BODY.SDR IZ22003F00003Nut · crackedDURING INSPECTION, FOUND UPPER WING INBOARD/OUTBOARD ATTACH BOLT WOULD NOT PROPERLY TIGHTEN TO TORQUE VALUE. INVESTIGATION REVEALED RIGHT UPPER FORWARD BARREL NUT WAS CRACKED. FURTHER INVESTIGATION REVEALED RIGHT LOWER FORWARD BARREL NUT WAS ALSO CRACKED.SDR IZ22001F00004Solenoid Valve · leakingPILOT REPORTED FUEL LEAKING FROM COWLING. INVESTIGATION FOUND FUEL LEAK FROM MATING SURFACES OF PRIMARIES ONLY SOLENOID VALVE. REPLACED VALVE WITH SN 3894.SDR IZ22001F00002Valve · leakingVALVE REPLACED DUE TO OIL LEAK BETWEEN SOLENOID AND VALVE BODY.SDR CA010813024Bolt · cracked(CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED AT SCHEDULED NDT INSPECTION OF BOLT. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2000 HOURS.SDR 20000609SH022Tire · separatedTHE SUBMITTER STATED, TIRE REPAIRED AND RECAPPED BY AERO WHEEL & BRAKE SERVICE CORP., NR U8SR971J. TIRE WAS INSTALLED ON THIS AIRCRAFT ON 4-15-00 AND HAD 13.2 HRS TT WITH 13 LANDINGS TOTAL. DURING LANDING ROLLOUT, A 2.5 INCH WIDE BAND OF TREAD SEPARATED FROM SDR CA000110044Bracket · cracked(CAN) DURING 100 HOUR INSPECTION THE SUBJECT LANDING GEAR FORWARD DOOR RETRACTION MECHANISM SUPPORT BRACKET WAS FOUND CRACKED AT THE OUTER MOST AFT HOLE.SDR 99ZZZX3982Case · failedTHE COMBUSTION CASE ASSY FAILED ALONG THE ENTIRE LENGTH OF THE MFG WELD. AIRCRAFT WAS ON TAKEOFF ROLL RESULTING IN AN ABORTED TAKEOFF AND FIRE IN THE NACELLE. NOTE: LOG BOOK ENTRY 3-25-96 ON OVERTEMP INSP C/W TSO 4,397.0 HOURS APPROX 884.2 HRS PRIOR TO FAILSDR 99ZZZX2966Tire · failedAT ROTATION (110 KNOTS), PILOT FELT BAD VIBRATION. PILOT RETURNED TO AIRPORT, FOUND THAT RIGHT HAND RECAP CAME OFF. RECAP DONE BY HAWKINS AIRCRAFT TIRE COMPANY. LANDINGS: 98.SDR 99ZZZX2946Gear Box · brokenDURING MAINTENANCE INSPECTION, FOUND TOP AFT HOUSING FLANGE BROKEN ON RIGHT HAND MAIN LANDING GEAR THRUST GEAR BOX. FAA INSP NOTE: THIS PART HAS A S/B FOR LOOSE MOUNTING BOLTS. A VISUAL INSPECTION CONDUCTED BY FAA SHOWS THAT THIS FLANGE HAD BEEN CRACKED FORSDR 98ZZZX1371Relay · failedPILOT SELECTED FLAPS DOWN 20 DEGREES FOR TAKEOFF. FLAPS WENT PAST 20 DEGREE POSITION, PAST 40 DEGREE DOWN POSITION, AND STOPPED AT THE MECHANICAL STOP. INVESTIGATION REVEALED FLAP DOWN RELAY FAILED ALLOWING CONTACTS TO TOUCH AT ALL TIMES. RELAY REPLACED TO SDR CA971027006Switch · frozen(CAN) AFTER TAKEOFF, RT MAIN LANDING GEAR DOWN LIGHT (GREEN) REMAINED ON WITH NO UNSAFE LIGHTS ON. LIGHT EXTINGUISHED AFTER 2O MINUTES. MAINTENANCE ACTION FOUND FROZEN LANDING GEAR DOWN SWITCH. AIRCRAFT WASHED PREVIOUS DAY AND LEFT OUTSIDE IN EXTREME COLD TSDR CA970918006Impeller · cracked(CAN) DURING HSI GBI, THE COMPRESSOR SECTION WAS DISMANTLED DUE TO COMPRESSOR RUB. 1ST STAGE IMPELLER HAS A CRACK IN IT. THIS PN IS REFERENCED IN SB TPE331A72-0971. REPLACED. PART TC: 11,482 HOURS.SDR 97ZZZX2709Hose · wrong partFOUND, CLEVELAND BRAKE KIT 199-101 STC SA648GL BRAKE HOSES U/A HOSE LISTED SAE DOAS SAE DOT 3000 PSI AIR BRAKE HOSE, FITTING CONNECTORS WERE 45 DEGREE ANGLE AND HOSE FITTINGS WERE 45 DEGREES. CONICAL SEAL WAS FOUND IN ONE HOSE FOR SEALINGS.SDR 97ZZZX619Skin · crackedPERFORMING 100 HR INSPECTION, DEFORMATION OF FUSELAGE SKIN WAS NOTED ABOVE BOTH MAIN GEAR ATTACH POINTS. FURTHER INSP WAS REQUIRED AND THE INTERIOR WALLS OF THE ACFT WERE REMOVED. CRACKS WERE FOUND IN FUSELAGE FRAMES AT FS 4610, 4850, AND 5605. INSPECT AND
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