Mitsubishi MU-2B-30
Service difficulty reports · 16
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 = 'MU2B30' 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 = 'MU2B30' 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 CA000824028Bracket · broken(CAN) PIREP VIBRATION ON INITIAL START-UP, AFTER ENGINE START AND OFF PITCH LOCKS VIBRATION WENT AWAY.UPON INVESTIGATION MAINTENANCE FOUND 2 OUT OF 3 PITCH STOP BRACKETS TO BE BROKEN IN HALF. BROKEN BRACKETS WERE REPLACED WITH NEW ONES, AIRCRAFT WAS GROUND-RUNSDR 20000623SH015Fitting · deterioratedOIL SUPPLY LINE FOR OIL COOLER, FITTING THREADS IN CASE DETERIORATED ALLOWING FITTING TO BLOW OUT. THIS ALLOWED ENGINE OIL TO PUMP OUT. PILOT SHUT ENGINE DOWN WITHOUT DAMAGE TO ENGINE. (X)SDR AU981132Rod Fork · failed(AUS) RUDDER CONTROL ROD FORK END ROTATED AND CAUSED RESTRICTED MOVEMENT WHICH EVENTUALLY SNAPPED THE FORK. INVESTIGATION FOUND THAT THE LOCKNUT HAD WORKED LOOSE.SDR AU980524Control Rod · broken(AUS) RUDDER TRIM TAB CONTROL ROD BROKEN. AD/MU-2/48 HAD NOT BEEN COMPLIED WITH.SDR AU980250Control Cable · failed(AUS) ELEVATOR TRIM CABLE FRAYED WITH ONLY ONE STRAND REMAINING . CABLE FAILED DURING REMOVAL. AIRCRAFT WAS PREVIOUSLY REGISTERED ASVH-UZN.SDR AU980181Landing Gear · failed(AUS) LANDING GEAR FAILED TO RETRACT. SYSTEM WORKED NORMALLY DURING GROUND CHECKS WHEN FOLLOWING RESETTING OF THE EMERGENCY EXTENSION SYSTEM. SUSPECT CAUSED BY MOVEMENT OF THE EMERGENCY EXTENSION HANDLE DURING MAINTENANCE.SDR AU971630Skin · cracked(AUS) HORIZONTAL STABILISER LEADING EDGE SKINS CRACKED. CRACKS ORIGINATE FROM RIB RIVETS FOR THE OUTBOARD ELEVATOR HINGE. CRACK LENGTH 50.8MM (2IN). FOUND DURING INSPECTION IAW AD/MU2/35.SDR AU970727Blade · separated(AUS) RH PROPELLER NO3 BLADE SEPARATED AT BLADE ROOT. EXTENSIVE DAMAGE CAUSED TO REDUCTION GEARBOX, ENGINE, ENGINE MOUNTS, COWLING AND NACELLE.SDR 97ZZZX526Sensor Body · brokenDURING THE AFTER TAKEOFF CLIMB, AND IMMEDIATELY AFTER GEAR RETRACTION THE ENGINE FLAMED OUT. THE TORQUE SENSOR BODY FAILED AROUND THE DRIVE GEAR FOR THE FUEL CONTROL UNIT AND AROUND THE RETAINING BOLTS. ONE TORQUE SENSOR RETAINING BOLT WAS FOUND AT THE BOTTOSDR AU961167Landing Gear · faulty(AUS) LANDING GEAR WOULD NOT EXTEND IN NORMAL OR EMERGENCY MODESSDR EY2R9600819Bearing · corrodedBEARING CORRODED.SDR AU960376Heater · stripped(AUS) RH ENGINE OIL/FUEL HEATER OIL OUTLET FITTING PNO AN815-8J LOOSE AND LEAKING DUE TO STRIPPED THREADS IN THE HEATER HOUSING -PERSONNEL/MAINTENANCE ERRORSDR AU960327Plenum · cracked(AUS) RH ENGINE PLENUM CHAMBER CRACKED AROUND DRAIN FITTING TAKEOFF FLANGE - CRACK LENGTH 50.8MM (2IN) - RH ENGINE BLEED AIR TUBECHAFED AND LEAKING - PERSONNEL/MAINTENANCE ERRORSDR 96ZZZX756Limit Switch · miswiredDURING TROUBLESHOOTING THE GEAR EXTENSION SYSTEM, AN ERROR WAS FOUND IN THE WIRING DIAGRAM ON PAGE 10-2 OF MITSUBISHI MM, YET 69016. WIRE LABELED 'G125D20' ON NR 10 PIN OF TB 302 IS ACTUALLY WIRE 'G174AS0'. THIS ERROR WAS FOUND BY LOOKING AT THE ACTUAL WIRE SDR 95ZZZX736Bracket · failedFORWARD MLG DOOR ACTUATOR SUPPORT BRACKET TORN OUT. SB NR 172 WAS PREVIOSULY COMPLIED WITH, BUT SB 197A HAD NOT BEEN DONE. IF SB NR 197A IS COMPLIED WITH, THIS WILL NOT HAPPEN. THIS IS CAUSED BY THE LACK OF STRUCTURE STRENGTH OF THE FORWARD SUPPORT BRACKET,SDR 95ZZZX749Chain · separatedAFTER A NORMAL LIFT OFF AND CLIMB OUT, FLYING PILOT NOTED HE WAS GETTING NO ROLL RESPONSE TO RT CONTROL (ROLL COLUMN INPUT AND LITTLE RESPONSE TO LT WHILE IT SEEMED TO BE 'CATCHING'. THE CONTROL COLUMN LOST ALL 'FEEL' AND WOULD TURN A FULL 360 DEGREES WITH NO
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