# Service difficulty reports: Mitsubishi MU-2B-36

A list on [Mitsubishi MU-2B-36](https://openairdocs.org/model/mitsubishi-mu-2b-36.md).

Newest first. General aviation reporting is voluntary.

- [SDR NM5R201308191](https://openairdocs.org/sdr/NM5R201308191.md): Door · unsecure · Aug 13, 2013 · Mtsbsi MU2B36 · Emergency Exits
  > CUSTOMER REPORTED, LT CREW DOOR BLEW OPEN DURING FLIGHT CAUSING EXTENSIVE DAMAGE TO THE OUTER WINDOW, DOOR FRAME AND OUTER SKIN. DOOR WAS SENT TO US FOR REPAIR. AFTER DISASSEMBLY OF DOOR, FOUND BOLT, PN: AN3H HOLDING FRONT BELL CRANK, WHICH OPERATES THE FRONT
- [SDR MCCA2013FA0000430](https://openairdocs.org/sdr/MCCA2013FA0000430.md): Door · failed · Aug 5, 2013 · N866D · Mtsbsi MU2B36 · Passenger/Crew Doors
  > DURING CRUISE, CREW DOOR BLEW OPEN CAUSING THE ACFT TO DEPRESSURIZE. DECLARED AN EMERGENCY, DESCENDED, AND RETURNED TO POINT OF TAKEOFF. A SAFE LANDING WAS MADE. ON INVESTIGATION DOOR WAS FOUND TO IN THE LATCHED-LOCKED POSITION. AS OF YET NO REASON FOR FAI
- [SDR VOX2009F00002](https://openairdocs.org/sdr/VOX2009F00002.md): Torque Sensor · failed · May 11, 2009 · N6KF · Mtsbsi MU2B36 · Engine BMEP/Torque Indicating
  > PILOT REPROTED AFTER TAKEOFF, EXPERIENCED RT ENGINE SPOOLED DOWN. SECURED ENGINE AND RETURNED TO DEPARTURE. FOLLOW UP: TORQUE SENSOR FAILED IN RT ENGINE. (K)
- [SDR VOX2009F00001](https://openairdocs.org/sdr/VOX2009F00001.md): Powerplant · shutdown · May 11, 2009 · N6KF · Mtsbsi MU2B36 · Engine (Turbine/Turboprop)
  > PILOT REPORTED AFTER TAKEOFF, EXPERIENCED RT ENGINE SPOOLED DOWN. SECURED ENGINE AND RETURNED TO DEPARTURE. CAUSE OF ENGINE PROBLEM UNDETERMINED AT THIS TIME. (K)
- [SDR MCC2009F00000](https://openairdocs.org/sdr/MCC2009F00000.md): Latch · failed · Feb 20, 2009 · N866D · Mtsbsi MU2B36 · Nacelle/Pylon Miscellaneous Structure
  > ACFT ON FINAL APPROACH, WHEN PILOT HEARD A THUD. STATED HE THOUGHT HE HAD HIT A BIRD. UNEVENTFUL LANDING WAS MADE. PILOT DEPARTED AC AND FOUND LT ENGINE TOP COWLING HAD COME OPEN. MX FOUND OUT, BAD LATCHING MECHANISM BROKE. SUSPECT LATCH BROKE AND THE COW
- [SDR CA081027001](https://openairdocs.org/sdr/CA081027001.md): Shaft · binding · Oct 23, 2008 · Mtsbsi MU2B36 · Propeller Controlling System
  > (CAN) PROP OVERSEED DURING DESCENT. FOUND ENGINE INNER CONCENTRIC SHAFT TO BE BINDING ON OUTER CONCENTRIC SHAFT. AS POWER LEVER IS RETARDED, INNER CONCENTRIC SHAFT ROTATES SLIGHTLY CLOCKWISE INCREASING PROP GOVERNOR HIGH SETTING. THERE IS NO PROVISION FOR LUBR
- [SDR BKAA200710003](https://openairdocs.org/sdr/BKAA200710003.md): Terminal Block · damaged · Oct 16, 2007 · N535WM · Mtsbsi MU2B36 · Navigation System Wiring
  > PITCH CONTROL JAMMED IN FLIGHT. SLIGHT MOVEMENT UP ABOUT 1 INCH CONTROL TRAVEL. A/C TRIED A FEW TIMES TO PITCH DOWN. A/P AND AVIONICS SWITCH OFF. LANDED WITH POWER CONTROLLING PITCH. T/S FOUND STICK SHAKER ON YOKE GETTING HUNG UP BY TERMINAL BOARD. RESECURED T
- [SDR CA070718004](https://openairdocs.org/sdr/CA070718004.md): Lever · loose · Jul 14, 2007 · Mtsbsi MU2B36 · Propeller Controlling System
  > (CAN) THE PPC LEVER WAS FOUND SEPARATED FROM THE PPC INPUT SHAFT. THE BOLT WAS OF THE CORRECT P/N, YET WAS THREAD BOUND WITHOUT PRODUCING ENOUGH TENSION TO HOLD THE PPC ARM ONTO THE PPC SHAFT. THE PPC ARM WAS REINSTALLED AND A WASHER WAS PLACED UNDER THE HEA
- [SDR CA070503004](https://openairdocs.org/sdr/CA070503004.md): Fuel Control · worn · Apr 26, 2007 · Mtsbsi MU2B36 · Fuel Control/Turbine Engines
  > (CAN) ENGINE WAS SHUTDOWN DUE TO ABNORMAL INDICATIONS. ENGINE REMOVED AND SENT TO OVERHAUL FACILITY, FCU AND FUEL PUMP REMOVED, DAMAGE FOUND TO THE FUEL CONTROL QUILL SHAFT AND THE STUB SHAFT INTERNAL SPLINES. FCU AND FUEL PUMP REPLACED. NOTE: FCU HAD 780.4 H
- [SDR VOX2007F00000](https://openairdocs.org/sdr/VOX2007F00000.md): Cowling · damaged · Apr 4, 2007 · N740PB · Mtsbsi MU2B36 · Nacelle/Pylon, Plate/Skin
  > UPPER RT COWLING CAME OPEN IN FLIGHT. RECOMMEND INSTALLING 2 SCREWS AT LEADING EDGE OF COWLING TO PREVENT THIS HAPPENING. (K)
- [SDR CA060503006](https://openairdocs.org/sdr/CA060503006.md): Plenum · cracked · Dec 20, 2005 · Mtsbsi MU2B36 · Turbine Engine Compressor Section
  > (CAN) AIRCRAFT TOOK OFF FROM AIRPORT RUNWAY 15 OR A COURIER FLIGHT. THE AIRCRAFT CRASHED ABOUT 500 METERS EAST OF, AND APPROXIMATELY ABEAM, THE SOUTH END OF RUNWAY 15, ABOUT 300 METERS BEYOND THE AIRPORT PERIMETER. A POST-CRASH FIRE OCCURRED. THE AIRCRAFT WAS
- [SDR CA060503005](https://openairdocs.org/sdr/CA060503005.md): Plenum · cracked · Dec 20, 2005 · Mtsbsi MU2B36 · Turbine Engine Compressor Section
  > (CAN) AC TOOK OFF, AC CRASHED, POST-CRASH FIRE OCCURRED. AC WAS DESTROYED. BOTH PILOTS FATALLY INJURED. DURING TEAR-DOWN OF RT ENG (WHICH WAS FOUND TO BE OPERATING AT HIGH POWER ON IMPACT) P3, BLEED AIR BOSS WELDS WERE EXAMINED BY FPI USING A 2X POWER MAGNIFYI
- [SDR MCC2005F00000](https://openairdocs.org/sdr/MCC2005F00000.md): Fire Warning · intermittent · Sep 23, 2005 · N103RC · Mtsbsi MU2B36 · Fire Detection
  > RT ENGINE FINE WARNING FLICKERED ONE TIME IN FLIGHT. PILOT SECURED ENGINE AND FEATHERED PROP. UNEVENTFUL LANDING MADE AT MAINTENANCE INSPECTED ENGINE AND FOUND NO EVIDENCE OF FIRE OR FIRE DAMAGE. GROUND RUN ENGINE COULD NOT DUPLICATE PROBLEM. (K)
- [SDR 2003FA0000840](https://openairdocs.org/sdr/2003FA0000840.md): Tire · failed · Aug 1, 2003 · N500PJ · Mtsbsi MU2B36 · Tire
  > UPON LANDING, THE TIRE DISINTEGRATED. ASSURE THE TIRE WAS FLAT ON LANDING, DUE TO RUNWAY FOD ON TAKEOFF.
- [SDR IZ22003F00001](https://openairdocs.org/sdr/IZ22003F00001.md): Solenoid Valve · leaking · Dec 20, 2002 · N13YS · Mtsbsi MU2B36 · Engine Fuel Distribution
  > VALVE LEAKING FUEL BETWEEN THE SOLENOID AND VALVE BODY DUE TO BLOWN O-RING. THE FUEL WAS LEAKING INTO THE COWLING AND DRIPPING OUT.
- [SDR CA020307012](https://openairdocs.org/sdr/CA020307012.md): Switch · intermittent · Mar 5, 2002 · Mtsbsi MU2B36 · Landing Gear Position and Warning
  > (CAN) DURING APPROACH, CREW SELECTED GEAR DOWN & NOTHING HAPPENED. THEY BROKE OFF APPROACH & FLEW LOCALLY MAKING SEVERAL ATTEMPTS. EMERGENCY EXTENSION PERFORMED & GEAR LOWERED NORMALLY. INVESTIGATION & SUBSEQUENT GEAR SWINGS COULD FIND NO FAULT & ALL FUNCTION
- [SDR CA011221008](https://openairdocs.org/sdr/CA011221008.md): Line · chafed · Dec 20, 2001 · Mtsbsi MU2B36 · Engine Oil Distribution (Airframe Furnished)
  > (CAN) THE OIL LINE RUNNING FROM THE OIL COOLER WAS FOUND CHAFED BY A SCREW THAT WAS TOO LONG IN A PANEL ON THE SIDE OF THE NACELLE. THE LINE WAS REPLACED AND THE SCREW WAS REPLACED WITH A SHORTER ONE
- [SDR CA011221007](https://openairdocs.org/sdr/CA011221007.md): Bolt · cracked · Dec 5, 2001 · Mtsbsi MU2B36 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2000 HOURS.
- [SDR CA000606003](https://openairdocs.org/sdr/CA000606003.md): Valve · malfunctioned · Jun 1, 2000 · Mtsbsi MU2B36 · Fuel Transfer Valve
  > (CAN) DURING CRUISE, THE CREW STARTED TO TRANSFER TIP FUEL WITH NO PROBLEM. WHEN THE CREW SELECTED TIP TRANSFER OFF, THE RT TIP TANK CONTINUED TO FLOW UNTIL TIP TANK PRESSURE WAS EXHAUSTED. THIS CAUSED ABOUT A 15 GALLON FUEL IMBALANCE BETWEEN THE TIP TANKS (
- [SDR CA000215006](https://openairdocs.org/sdr/CA000215006.md): Switch · frozen · Feb 9, 2000 · Mtsbsi MU2B36 · Landing Gear Retraction/Extension System
  > (CAN) THE CREW SELECTED GEAR DOWN ON APPROACH AND THE GEAR FAILED TO EXTEND. THE CREW ELECTED TO OVERSHOOT AND RETURN TO THEIR MAIN BASE. ON APPROACH TO THE MAIN BASE AT LOWER ALTITUDE AND WARMER TEMPERATURE, THE GEAR EXTENDED NORMALLY AND THE AIRCRAFT WAS LAN
- [SDR CA000209006](https://openairdocs.org/sdr/CA000209006.md): Actuator · frozen · Feb 8, 2000 · Mtsbsi MU2B36 · Landing Gear Retraction/Extension System
  > (CAN) THE LANDING GEAR FAILED TO EXTEND WHEN SELECTED DUE TO A FROZEN DOOR ACTUATOR CLUTCH. THE CREW THEN INITIATED AN EMERGENCY EXTENSION WHICH WAS UNSUCCESSFUL.
- [SDR CA000120006](https://openairdocs.org/sdr/CA000120006.md): Roller · missing · Jan 17, 2000 · Mtsbsi MU2B36 · Landing Gear Retraction/Extension System
  > (CAN) THE CREW TRIED TO EXTEND THE LANDING GEAR USING THE EMERGENCY EXTENSION SYSTEM, AFTER A LANDING GEAR MALFUNCTION. THE LANDING GEAR COULD NOT BE EXTENDED AND THE CREW WAS FORCED TO LAND THE AIRCRAFT GEAR UP. MAINTENACE FOUND THE CAUSE OF THE EMERGENCY EXT
- [SDR CA990728017](https://openairdocs.org/sdr/CA990728017.md): Torque Sensor · failed · Jul 14, 1999 · Mtsbsi MU2B36 · Engine BMEP/Torque Indicating
  > (CAN) THE FAILURE WAS LIMITED TO THE DIRECT DRIVE GEAR STACK ON THE TORQUE SENSOR. THIS GEAR DRIVES THE FUEL PUMP AND FUEL CONTROL THE FAILURE OF WHICH SHUT DOWN THE ENGINE DUE TO LOSS OF FUEL PRESSURE. THE SHAFT HAD BROKEN IN THE THREAD AREA UNDER THE RETAI
- [SDR 99ZZZX2364](https://openairdocs.org/sdr/99ZZZX2364.md): Valve · damaged · May 25, 1999 · N500PJ · Mtsbsi MU2B36 · Fuel Boost Pump
  > HIGH PRESSURE RELIEF VALVE BODY, P/N 867927-1, WAS STILL IN FUEL PUMP HOUSING, BUT THE WRENCHING FLATS AND CAP OF RELIEF VALVE WERE FOUND HANGING FROM SAFETY WIRE CAUSING FUEL TO BE SPRAYED ON ENGINE. FUEL COULD ONLY BE STOPPED BY SHUTTING OFF AIRFRAME SUPPLY
- [SDR 99ZZZX1417](https://openairdocs.org/sdr/99ZZZX1417.md): Housing · damaged · Mar 1, 1999 · N687HB · Mtsbsi MU2B36 · Turbine Engine Accessory Drive
  > THREADS FOR FITTING OF AFT OIL SCAVENGE PUMP LINE, IN ACCESSORY/GEAR HOUSING, STRIP OUT CAUSING OIL LEAK.
- [SDR CA980928019](https://openairdocs.org/sdr/CA980928019.md): Carbon Seal · failed · Sep 11, 1998 · Mtsbsi MU2B36 · Turbine Section
  > (CAN) THE PILOT OBSERVED FLUCTUATIONS IN TORQUE AND OIL PRESSURE, AS WELL AS VISIBLE OIL VENTING FROM THE ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED. POST-FLIGHT INSPECTION FOUND A MISSING SECTION OF THE 1ST STAGE TURBINE WHEEL CREATED AN IMBAL
- [SDR 98ZZZX2640](https://openairdocs.org/sdr/98ZZZX2640.md): Wheel · failed · Jun 26, 1998 · N500PJ · Mtsbsi MU2B36 · Wheel/Ski/Float
  > INNER WHEEL HALF EXPERIENCED A BEARING FAILURE. FAILURE RESULTED IN BRAKE DISC RUBBING INTO BRAKE ASSEMBLY REQUIRING BRAKE ASSEMBLY REPLACEMENT. INNER WHEEL HALF ALSO REQUIRED REPLACEMENT DUE TO CRACKING AROUND BEARING AREA.
- [SDR CA971113013](https://openairdocs.org/sdr/CA971113013.md): Gasket · failed · Oct 24, 1997 · Mtsbsi MU2B36 · Turbine Engine Oil System
  > (CAN) DURING CRUISE, CREW NOTICED FLUCTUATING OIL PRESSURE ON LT ENGINE. OIL PRESSURE MONITORED AND AIRCRAFT LANDED. FRETTED AND DETERIORATED TURBINE SCAVANGE PUMP GASKET CAUSING OIL LOSS IN THE ENGINE. NEW SEAL INSTALLED.
- [SDR 97ZZZM1086](https://openairdocs.org/sdr/97ZZZM1086.md): Knob · loose · Sep 25, 1997 · N305CW · Mtsbsi MU2B36 · Aileron Control System
  > AILERON CONTROL KNOW FALLS OFF POTENTIALLY CAUSING A CONTROL PROBLEM IF PILOT EXPERIENCES ENGINE FAILURE ON TAKEOFF. A POTENTIAL LOSS OF CONTROL AND OR AIRCRAFT MAY OCCUR.
- [SDR CA970909006](https://openairdocs.org/sdr/CA970909006.md): Line · cracked · Aug 21, 1997 · Mtsbsi MU2B36 · Turbine Engine Accessory Drive
  > (CAN) RIGHT HAND OIL PRESSURE LINE TO TORQUE TRANSDUCER CHAFED THROUGH DUE TO B-NUT COMING LOOSE AND SUBSEQUENT LOSS OF OIL PRESSURE. NEW LINE INSTALLED AND GROUND RUN-UP CARRIED OUT SERVICEABLE.
- [SDR 97ZZZM885](https://openairdocs.org/sdr/97ZZZM885.md): Tire · failed · Aug 7, 1997 · N305CW · Mtsbsi MU2B36 · Tire
  > UPON ROTATION, TREAD SEPARATED FROM CARCASS ON THE NR 1 TIRE ASSEMBLY. AT SEPARATION TIRE TREAD DAMAGED AFT GEAR DOOR AND DOOR CONNECTING ROD. TREAD THEN FLEW FORWARD AND STRUCK PROP. TIRE WAS A RECAP.
- [SDR 97ZZZX4686](https://openairdocs.org/sdr/97ZZZX4686.md): Tire · separated · Apr 30, 1997 · N500PJ · Mtsbsi MU2B36 · Tire
  > LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS RETURNED TO MFG FOR
- [SDR 97ZZZX2637](https://openairdocs.org/sdr/97ZZZX2637.md): Tire · separation · Apr 30, 1997 · N500PJ · Mtsbsi MU2B36 · Tire
  > LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE OF 3 SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS RETURNED TO MFG FOR EVA
- [SDR 97ZZZX4685](https://openairdocs.org/sdr/97ZZZX4685.md): Tire · separated · Apr 17, 1997 · N869P · Mtsbsi MU2B36 · Tire
  > RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 1 INCH. SEPARATION WAS NOTICED DURING A POST-FLIGHT WALK AROUND INSPECTION. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS
- [SDR 97ZZZX2643](https://openairdocs.org/sdr/97ZZZX2643.md): Tire · separation · Apr 17, 1997 · N869P · Mtsbsi MU2B36 · Tire
  > RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 1 INCH. SEPARATION NOTICED DURING A POST-FLIGHT WALK AROUND INSPECTION. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS RETU
- [SDR 97ZZZX4687](https://openairdocs.org/sdr/97ZZZX4687.md): Tire · separated · Apr 2, 1997 · N500PJ · Mtsbsi MU2B36 · Tire
  > RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STAYED ATTACHED AROUND OUTBOARD EDGE CIRCUMFERENCE. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHI
- [SDR 97ZZZX2636](https://openairdocs.org/sdr/97ZZZX2636.md): Tire · separation · Apr 2, 1997 · N500PJ · Mtsbsi MU2B36 · Tire
  > RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STAYED ATTACHED AROUND OUTBOARD EDGE CIRCUMFERENCE. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHI
- [SDR CA961007013](https://openairdocs.org/sdr/CA961007013.md): Sun Gear · fractured · Aug 5, 1996 · Mtsbsi MU2B36 · Main Rotor Gearbox
  > (CAN) PILOT NOTED SEVERE VIBRATION WITH NO WARNING. PRIOR TO SHUTDOWN, THE TORQUE WENT TO ZERO. AIRCRAFT RETURNED OK. INSPECTION REVEALED THE PLANETARY PIN P/N 868051-1 WAS CHAFED BY THE PLANETARY GEAR P/N 358268-1 WHICH IN TURN ABNORMALLY LOADED THE SUN GE
- [SDR CA960619002](https://openairdocs.org/sdr/CA960619002.md): Switch · shorted · Jun 13, 1996 · Mtsbsi MU2B36 · Landing Gear Position and Warning
  > (CAN) ON GEAR EXTENSION, 3 GREEN LIGHTS SHOWED MOMENTARILY THEN WENT OUT AS THE GEAR DOORS CLOSED. FORWARD LEFT GEAR DOOR SWITCH FAILED AND SHORTED TO GROUND INTERNALLY.
- [SDR CA960126004](https://openairdocs.org/sdr/CA960126004.md): Mlg Solenoid · burnt contacts · Jan 16, 1996 · Mtsbsi MU2B36 · Landing Gear Actuator
  > (CAN)THE CREW SELECTED GEAR DOWN ON APPROACH AND THE GEAR DOORS OPENED BUT NOTHING FURTHER HAPPENED. THEY THEN NOTICED THAT THE GEAR MOTOR CIRCUIT MOTOR HAD TRIPPED. THE BREAKER WAS RESET AND THE GEAR CYCL ED AGAIN WITH THE SAME RESULTS. EMERGENCY EXTENSION WA
- [SDR 96ZZZM20](https://openairdocs.org/sdr/96ZZZM20.md): Brake · burned · Dec 9, 1995 · N305CW · Mtsbsi MU2B36 · Brake
  > ON LANDING AT YIP, AIRCRAFTS RIGHT MAIN BRAKE WAS DRAGGING. RESUTLED IN FLAT SPOT ON TIRE AND OVERHEATED BRAKE ASSEMBLY. WHEEL AND BRAKE REPLACED WITH SERVICEABLE UNITS. BRAKE HYDRAULIC SYSTEM BLED TO REMOVE ANY CONTAMINATION. SYSTEM OPS CHECKED GOOD. SUB
- [SDR CA951211003](https://openairdocs.org/sdr/CA951211003.md): O-Ring · chafed · Dec 7, 1995 · Mtsbsi MU2B36 · Nose/Tail Landing Gear Strut/Axle
  > (CAN)THE CREW MADE AN UNEVENTFUL SHORT TURN AROUND AT DAWSON CREEK (-35C),THEN PROCEEDED TO FT. ST. JOHN (-41C). DURING THE APP A LOUD BANG WAS HEARD DURING GEAR EXTENSION. ALL ATTEMPTS TO LOWER THE GEAR WERE UNSUCCESSFUL. THE ACFT MADE A SUCCESSFUL GEAR-
- [SDR 95ZZZX6838](https://openairdocs.org/sdr/95ZZZX6838.md): Frame · cracked · Nov 27, 1995 · N500PJ · Mtsbsi MU2B36 · Fuselage Main, Frame
  > FRAME 4610, LEFT, CRACKED THROUGH SCREW HOLES APPROXMATELY 31MM BELOW LOWER HOLE. ALL 6 STATIONS HAD TO BE SHIMMED PER SB 209A.
- [SDR 95ZZZM702](https://openairdocs.org/sdr/95ZZZM702.md): Tire · failed · Nov 11, 1995 · N305CW · Mtsbsi MU2B36 · Tire
  > ON LANDING AT DET, BOTH NOSE TIRES FAILED (BLEW OUT). THIS FAILURE CAUSED BOTH NOSE WHEEL RIMS TO CONTACT THE RUNWAY SURFACE AT HIGH SPEED DESTROYING BOTH NOSE WHEEL ASSEMBLIES. AT THIS TIME WE ARE NOT ABLE TO ESTABLISH THE CAUSE OF THE TIRE FAILURE. WE HAV
- [SDR BUHA95002](https://openairdocs.org/sdr/BUHA95002.md): Downlock Switch · failed · Nov 1, 1995 · N201UV · Mtsbsi MU2B36 · Landing Gear Position and Warning
  > INTERNAL FAILURE OF NOSE GEAR DOWNLOCK SWITCH ALLOWED INDICATOR LIGHT VOLTAGE TO BLEED OVER TO THE LANDING GEAR CONTROL SECTION OF THE SWITCH. (X)
- [SDR 95ZZZX6049](https://openairdocs.org/sdr/95ZZZX6049.md): Gearbox Fitting · defect · Oct 12, 1995 · N103RC · Mtsbsi MU2B36 · Turbine Engine Oil System
  > IN CRUISE FLIGHT, LEFT ENGINE OIL PRESSURE STARTED TO FLUCTUATE. A PRECAUTIONARY SHUT DOWN WAS MADE AND THE AIRCRAFT HAD AN UNEVENTFUL LANDING. TROUBLESHOOTING FOUND THE GEARBOX SCAVENGE OIL LINE FITTING IN THE GEARBOX HAD STARTED BACKING OUT. THE THREADS I
- [SDR 95ZZZM692](https://openairdocs.org/sdr/95ZZZM692.md): Tq Sensor Brg · failed · Oct 4, 1995 · N305CW · Mtsbsi MU2B36 · Turbine Engine Accessory Drive
  > AT FL 150 IN LEVEL CRUISE CONDITIONS, THE NR 2 ENGINE FLAMED OUT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT IPT. TROUBLESHOOTING OF THE ENGINE REVEALED THE MAIN OIL AND SCAVENGE PUMPS NOT ROTATING, THESE PUMPS ARE DRIVEN BY THE TORQUE SENSOR, THE MAIN FUEL
- [SDR 95ZZZX3583](https://openairdocs.org/sdr/95ZZZX3583.md): Fuel Control · failed · Jul 13, 1995 · N103RC · Mtsbsi MU2B36 · Fuel Control/Turbine Engines
  > ENGINE LOST FUEL FLOW IN CRUISE FLIGHT. ENGINE SHUT-DOWN AND FEATHERED. TROUBLESHOOTING DETERMINED FUEL CONTROL FAILED. THE FUEL CONTROL UNIT HAD APPROXIMATELY 450 HOURS SINCE REPAIR BY WOODWARD.
- [SDR 95ZZZX2304](https://openairdocs.org/sdr/95ZZZX2304.md): Window · cracked · Apr 11, 1995 · N500PJ · Mtsbsi MU2B36 · Emergency Exits
  > DURING A POST-INSPECTION WALK-AROUND, A CRACK WAS NOTED EXTENDING APPROXIMATELY 1 INCH INTO THE VISIBLE AREA OF THE OUTER WINDOW IN THE CREW EMERGENCY ESCAPE DOOR. WHEN WINDOW RETAINERS WERE REMOVED, A CRACK 16 INCHES LONG CONNECTING 11 BOLT HOLES ACROSS THE

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'MU2B36'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mitsubishi-mu-2b-36/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.