# Service difficulty reports: Mitsubishi MU-2B-60

A list on [Mitsubishi MU-2B-60](https://openairdocs.org/model/mitsubishi-mu-2b-60.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 112 reports

- [SDR CA190711009](https://openairdocs.org/sdr/CA190711009.md): Actuator · failed · Feb 23, 2019 · Mtsbsi MU2B60 · Landing Gear Actuator
  > (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 GEA
- [SDR CA180423014](https://openairdocs.org/sdr/CA180423014.md): Gear · damaged · Apr 19, 2018 · Mtsbsi MU2B60 · Propeller Indication System
  > (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 NOW
- [SDR CA151008001](https://openairdocs.org/sdr/CA151008001.md): Skin · cracked · Oct 5, 2015 · Mtsbsi MU2B60 · Wing, Plate/Skin
  > (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 CAU
- [SDR CA141223004](https://openairdocs.org/sdr/CA141223004.md): Adapter · broken · Dec 21, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (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 CA141015002](https://openairdocs.org/sdr/CA141015002.md): Housing · cracked · Oct 8, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (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 CA140131006](https://openairdocs.org/sdr/CA140131006.md): Window · departed · Jan 29, 2014 · Mtsbsi MU2B60 · Passenger Compartment Windows
  > (CAN) WINDOW BLEW OUT AT ALTITUDE RESULTING IN DECOMPRESSION.
- [SDR CA140318011](https://openairdocs.org/sdr/CA140318011.md): Fitting · cracked · Jan 27, 2014 · Mtsbsi MU2B60 · Fuselage, Landing Gear Attach Fittings
  > (CAN) DURING ROUTINE INSPECTION THE NLG KEEL WEB WAS FOUND CRACKED. THE CRACK WAS REPAIRED USING DATA FROM MANUFACTURE.
- [SDR CA131030006](https://openairdocs.org/sdr/CA131030006.md): Strut · cracked · Oct 30, 2013 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) DURING SCHEDULED MAGNETIC PARTICLE INSPECTION THE RT NLG STRUT WAS FOUND CRACKED. PART WAS REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA131022007](https://openairdocs.org/sdr/CA131022007.md): Wire · damaged · Oct 22, 2013 · Mtsbsi MU2B60 · Ice/Rain Protection System Wiring
  > (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 1
- [SDR CA130327003](https://openairdocs.org/sdr/CA130327003.md): Adapter · cracked · Mar 26, 2013 · Mtsbsi MU2B60 · Engine Bleed Air System
  > (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 CA130109005](https://openairdocs.org/sdr/CA130109005.md): Angle · cracked · Jan 8, 2013 · Mtsbsi MU2B60 · Fuselage Miscellaneous Structure
  > (CAN) FOUND ANGLE CRACKED DURING SCHEDULED INSPECTION.
- [SDR CA120703006](https://openairdocs.org/sdr/CA120703006.md): Engine · flamed out · Jun 28, 2012 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > (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 CA120605007](https://openairdocs.org/sdr/CA120605007.md): Rod End · broken · May 23, 2012 · Mtsbsi MU2B60 · Landing Gear Door Retract Section
  > (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 2012FA0000260](https://openairdocs.org/sdr/2012FA0000260.md): Switch · failed · Mar 15, 2012 · N70KC · Mtsbsi MU2B60 · Landing Gear Retraction/Extension System
  > AFTER 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 DU
- [SDR CA111108003](https://openairdocs.org/sdr/CA111108003.md): Engine · shutdown · Nov 7, 2011 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > (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 BKAA14110282011](https://openairdocs.org/sdr/BKAA14110282011.md): Engine · failed · Oct 28, 2011 · N8083 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > DURING 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 CA110805002](https://openairdocs.org/sdr/CA110805002.md): Clamp · worn · Aug 4, 2011 · Mtsbsi MU2B60 · Flight Compartment Equipment
  > AFTER 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 F
- [SDR CA110406006](https://openairdocs.org/sdr/CA110406006.md): Oil Cap · worn · Apr 1, 2011 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (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 & THE
- [SDR 2011FA0000132](https://openairdocs.org/sdr/2011FA0000132.md): Spur Gear · damaged · Feb 14, 2011 · N644EM · Mtsbsi MU2B60 · Turbine Engine Reduction Gear
  > FOUND 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 CONTACT
- [SDR CA101116011](https://openairdocs.org/sdr/CA101116011.md): Limit Switch · frozen · Nov 15, 2010 · Mtsbsi MU2B60 · Landing Gear Position and Warning
  > AFTER 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 I
- [SDR BKAA79409012010](https://openairdocs.org/sdr/BKAA79409012010.md): Landing Gear · binding · Sep 1, 2010 · N942ST · Mtsbsi MU2B60 · Landing Gear Retraction/Extension System
  > WHEN 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 CA100112001](https://openairdocs.org/sdr/CA100112001.md): Wheel · cracked · Jan 6, 2010 · Mtsbsi MU2B60 · Wheel/Ski/Float
  > (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 NR
- [SDR CA091006002](https://openairdocs.org/sdr/CA091006002.md): Motor · intermittent · Oct 2, 2009 · Mtsbsi MU2B60 · Landing Gear Actuator
  > (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 DO
- [SDR CA090424003](https://openairdocs.org/sdr/CA090424003.md): Hinge · cracked · Apr 17, 2009 · Mtsbsi MU2B60 · Landing Gear Doors
  > (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 2008FA0000701](https://openairdocs.org/sdr/2008FA0000701.md): Servo · contaminated · Oct 6, 2008 · N544CB · Mtsbsi MU2B60 · Autopilot System
  > 8/11/08 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 IN
- [SDR CA080902002](https://openairdocs.org/sdr/CA080902002.md): Battery · thermal runaway · Aug 27, 2008 · Mtsbsi MU2B60 · Battery/Charger System
  > (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 BATTER
- [SDR BKA2008F00000](https://openairdocs.org/sdr/BKA2008F00000.md): Engine · shutdown · Aug 27, 2008 · N8083A · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > DEPARTING, 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 TO
- [SDR CA080821006](https://openairdocs.org/sdr/CA080821006.md): Attach Fitting · cracked · Aug 18, 2008 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Attach Section
  > (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 CA080623002](https://openairdocs.org/sdr/CA080623002.md): Motor · inoperative · Jun 19, 2008 · Mtsbsi MU2B60 · Landing Gear Retraction/Extension System
  > (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/MO
- [SDR CA080613010](https://openairdocs.org/sdr/CA080613010.md): Lock Plate · worn · Jun 11, 2008 · Mtsbsi MU2B60 · Propeller Controlling System
  > (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 BKAA200710002](https://openairdocs.org/sdr/BKAA200710002.md): Engine · shutdown · Sep 5, 2007 · N610CA · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > SUP RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE
- [SDR BKAA070905102](https://openairdocs.org/sdr/BKAA070905102.md): Engine · shutdown · Sep 5, 2007 · N610CA · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE
- [SDR 002](https://openairdocs.org/sdr/002.md): Engine · shutdown · Sep 5, 2007 · N610CA · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE
- [SDR R0240301](https://openairdocs.org/sdr/R0240301.md): Bracket · cracked · Aug 14, 2007 · Mtsbsi MU2B60 · Propeller Assembly
  > FIVE 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 I
- [SDR CA070514002](https://openairdocs.org/sdr/CA070514002.md): Link · tight · May 9, 2007 · Mtsbsi MU2B60 · Propeller Controlling System
  > (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 C
- [SDR CA070228002](https://openairdocs.org/sdr/CA070228002.md): Arm · stiff · Feb 21, 2007 · Mtsbsi MU2B60 · Propeller Governor
  > (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 SERVICE
- [SDR 2007F00005](https://openairdocs.org/sdr/2007F00005.md): Latch · broken · Jan 16, 2007 · N610CA · Mtsbsi MU2B60 · Nacelle/Pylon, Main Frame
  > LT IB COWL LATCH FOR THE NR 2 ENGINE TOP COWL BROKE. VISUAL INSP REVEALED THE LATCH LINK ASSY BROKE INTO 2 PIECES.
- [SDR 2006FA0001200](https://openairdocs.org/sdr/2006FA0001200.md): Access Panel · corroded · Dec 5, 2006 · N215MH · Mtsbsi MU2B60 · Fuselage Main, Plate/Skin
  > DRAIN 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 VOX2006F00000](https://openairdocs.org/sdr/VOX2006F00000.md): Latch · broken · Oct 6, 2006 · N60FL · Mtsbsi MU2B60 · Nacelle/Pylon, Main Frame
  > LATCH 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 CA061011001](https://openairdocs.org/sdr/CA061011001.md): Bearing · failed · Aug 29, 2006 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > (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: 31030
- [SDR 2005FA0000401](https://openairdocs.org/sdr/2005FA0000401.md): Ring Gear · broken · Mar 3, 2005 · N644EM · Mtsbsi MU2B60 · Turbine Engine Reduction Gear
  > ON 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 GE
- [SDR 2005FA0000400](https://openairdocs.org/sdr/2005FA0000400.md): Planetary Gear · failed · Mar 3, 2005 · N644EM · Mtsbsi MU2B60 · Turbine Engine Reduction Gear
  > ON 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 GEA
- [SDR 2005FA0000124](https://openairdocs.org/sdr/2005FA0000124.md): Housing · failed · Jan 24, 2005 · N772DA · Mtsbsi MU2B60 · Turbine Engine Reduction Gear
  > IN 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. APPRO
- [SDR 2005FA0000118](https://openairdocs.org/sdr/2005FA0000118.md): Line · cracked · Jan 21, 2005 · N772DA · Mtsbsi MU2B60 · Turbine Engine Reduction Gear
  > NR 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 G1I2004F00003](https://openairdocs.org/sdr/G1I2004F00003.md): Seal · leaking · Nov 14, 2004 · N43866 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > SMOKE 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 CA040720001](https://openairdocs.org/sdr/CA040720001.md): Skin · lightning strike · Jul 13, 2004 · Mtsbsi MU2B60 · Propeller Assembly
  > IN 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 CA030505004](https://openairdocs.org/sdr/CA030505004.md): Drive Shaft · sheared · Apr 25, 2003 · Mtsbsi MU2B60 · Propeller Indication System
  > (CAN) THE PROP INDICATION WAS INTERMITTENT. MAINTENANCE FOUND THE DRIVE SHEARED OFF INSIDE THE TACHOMETER GENERATOR WHERE THE ROLL PIN SECURES THE DRIVE.
- [SDR MYN2003F00000](https://openairdocs.org/sdr/MYN2003F00000.md): Diode · failed · Apr 5, 2003 · N322TA · Mtsbsi MU2B60 · Aircraft Fuel Distribution System
  > DIODE 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 AN
- [SDR CA020911001](https://openairdocs.org/sdr/CA020911001.md): Fuel Control · leaking · Sep 9, 2002 · Mtsbsi MU2B60 · Fuel Control/Turbine Engines
  > (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. MAINT
- [SDR CA020513001](https://openairdocs.org/sdr/CA020513001.md): Rod End · separated · May 7, 2002 · Mtsbsi MU2B60 · Shimmy Damper
  > (CAN) ROD END SEPARATED FROM PISTON.UNIT RETURNED TO VENDOR AND WAS OVERHAULED. SERVICE BULLETIN NR 169B EMBODIED TO PRECLUDE FURTHER EVENTS.

Next page: https://openairdocs.org/model/mitsubishi-mu-2b-60/reports.md?page=2

## 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 = 'MU2B60'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mitsubishi-mu-2b-60/reports

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