# Service difficulty reports: Mitsubishi MU-2B-35

A list on [Mitsubishi MU-2B-35](https://openairdocs.org/model/mitsubishi-mu-2b-35.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 53 reports

- [SDR OXKA856K](https://openairdocs.org/sdr/OXKA856K.md): Fuel Control · malfunctioned · Jan 15, 2010 · N211BE · Mtsbsi MU2B35 · Fuel Control/Turbine Engines
  > RT ENGINE FUEL CONTROL MALFUNCTION. NO POWER LEVER RESPONSE ON THE RT ENGINE. COULD NOT REDUCE BELOW 900 DEG C. DIVERTED. ON APPROACH, SHUTDOWN ENGINE AND LANDED WITH NO FURTHER PROBLEMS.
- [SDR BKAA200710004](https://openairdocs.org/sdr/BKAA200710004.md): Oil Tank · cracked · Nov 15, 2007 · N21JA · Mtsbsi MU2B35 · Turbine Engine Oil System
  > OIL TANK CRACKED.
- [SDR BKAA200710001](https://openairdocs.org/sdr/BKAA200710001.md): Acm · seized · Aug 27, 2007 · N334EB · Mtsbsi MU2B35 · Cabin Cooling System
  > AIR CYCLE MACHINE TURBINE SEIZED UP CAUSING SMOKE IN THE COCKPIT. THE AIR CYCLE MACHINE REQUIRED REPLACEMENT.
- [SDR 2007F00006](https://openairdocs.org/sdr/2007F00006.md): Clamp · cracked · Dec 26, 2006 · N21JA · Mtsbsi MU2B35 · Propeller Blade Section
  > CRACK WAS FOUNDING STARTING AT THE DOWL PIN HOLE OF THE BLADE CUFF.
- [SDR OXK2006F00000](https://openairdocs.org/sdr/OXK2006F00000.md): Gearshaft · failed · Feb 15, 2006 · N640MA · Mtsbsi MU2B35 · Engine BMEP/Torque Indicating
  > ENGINE, SN P20186, EXPERIENCED AN UN-COMMANDED INFLIGHT SHUTDOWN, ON SITE INSPECTION REVEALED THAT THE FUEL PUMP DRIVE TRAIN HAD BECOME UNCOUPLED. TEARDOWN INSPECTION REVEALED FAILURE OF SPUR GEARSHAFT PN 8968042, COMPONENT OF TORQUE SENSOR PN 31017262, SN P2
- [SDR AALA20031479](https://openairdocs.org/sdr/AALA20031479.md): Battery Pack · discharged · Dec 28, 2003 · N503AA · Mtsbsi MU2B35 · Emergency Lighting
  > ATL DURING OVERNIGHT MAINTENANCE FOUND EXIT SIGN ABOVER EMERGENCY EXIT DOOR ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR HMN2002F00003](https://openairdocs.org/sdr/HMN2002F00003.md): Control Cable · frayed · Jun 10, 2002 · N940MA · Mtsbsi MU2B35 · Power Lever
  > FRAYED LT ENGINE POWER LEVER CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION UNDER CENTER PEDESTAL IN COCKPIT. (SW15200210206)
- [SDR HMN2002F00002](https://openairdocs.org/sdr/HMN2002F00002.md): Control Cable · frayed · May 30, 2002 · N840MA · Mtsbsi MU2B35 · Power Lever
  > FRAYED THROTTLE CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED.
- [SDR HMN2002F00001](https://openairdocs.org/sdr/HMN2002F00001.md): Control Cable · frayed · May 30, 2002 · N640MA · Mtsbsi MU2B35 · Power Lever
  > FRAYED CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED. (SW15200209702)
- [SDR HMN2002F00000](https://openairdocs.org/sdr/HMN2002F00000.md): Control Cable · broken · May 30, 2002 · N450MA · Mtsbsi MU2B35 · Power Lever
  > ON ENGINE SHUTDOWN, PILOT COULD NOT BRING LEFT PROP BACK ON LOCKS. INSPECTION FOUND LEFT ENGINE POWER LEVER CONTROL CABLE BROKEN BELOW CENTER PEDISTAL IN COCKPIT AT LOWER PULLEY. (SW15200209701)
- [SDR 2002FA0000750](https://openairdocs.org/sdr/2002FA0000750.md): Control Cable · frayed · May 21, 2002 · N640MA · Mtsbsi MU2B35 · Power Lever
  > DURING INSPECTION IN THE AFT FUSELAGE FOUND ONE OF THE ENGINE CONTROL CABLES FRAYED WHERE THE CABLE GOES OVER A PULLEY AND TURNS 90 DEGREES. THIS IS THE 2ND OF THREE REPORTED BY THE SAME OPERATOR IN 90 DAYS. ALL HAVE BEEN THE LEFT ENGINE CONTROL
- [SDR 2002FA0000749](https://openairdocs.org/sdr/2002FA0000749.md): Control Cable · frayed · Mar 26, 2002 · N840MA · Mtsbsi MU2B35 · Power Lever
  > DURING ROUTINE MAINTENANCE FOUND A FRAYED ENGINE CONTROL CABLE. THE FRAYED PORTION WAS LOCATED IN THE AFT FUSELAGE WHERE THE CABE GOES OVER A 90DEGREE TURN PULLEY. THIS IS THE FIRST OF THREE CABLE PROBLEMS THIS OPERATOR HAS FOUND IN THE LAST 90 DAYS
- [SDR KBMA88674](https://openairdocs.org/sdr/KBMA88674.md): Igniter · intermittent · Jul 16, 2001 · N118P · Mtsbsi MU2B35 · Spark Plug/Igniter
  > IGNITER - REPORTED TO BE INTERMITTENT. REMOVED AND REPLACED WITH NEW IGNITER.
- [SDR 20010409CW019](https://openairdocs.org/sdr/20010409CW019.md): Control Cable · separated · Mar 1, 2001 · N755MA · Mtsbsi MU2B35 · Elevator Tab Control System
  > CABLE SEPARATED AT A 90 DEGREE TURN OVER PULLEY IN AFT TAIL CONE AREA
- [SDR CA001103006](https://openairdocs.org/sdr/CA001103006.md): Limit Switch · failed · Oct 26, 2000 · Mtsbsi MU2B35 · Landing Gear Retraction/Extension System
  > (CAN) DURING APPROACH FOR LDG AT PRINCE GEORGE, BC, CREW SELECTED GEAR DOWN & FWD GEAR DOORS OPENED ABOUT 1/2 WAY THEN STOPPED. CREW OPENED LDG GEAR CONTOL CCT BREAKER, THEN CLOSED IT AGAIN & GEAR COMPLETED ITS CYCLE NORMALLY. INVEST. REVEALED THAT DOOR OPEN L
- [SDR 20001101SH003](https://openairdocs.org/sdr/20001101SH003.md): Blade · broken · Sep 6, 2000 · N770MA · Mtsbsi MU2B35 · Propeller Blade Section
  > AIRCRAFT AT CRUISE, ALT 11,000 FEET, NR 1 PROPELLER BLADE BROKE APPROXIMATELY 10 INCHES FROM HUB ON NR 2 ENGINE. BLADE DID NOT CONTACT AIRCRAFT. DAMAGE TO COWLING, NACELLE, REAR ENGINE MOUNT, OUTBOARD FLAP, WING TRAILING EDGE. ENGINE REMAINED ON WING. CREW
- [SDR CA000905002](https://openairdocs.org/sdr/CA000905002.md): Tube · cracked · Aug 22, 2000 · Mtsbsi MU2B35 · Turbine Engine Oil System
  > (CAN) THE ENGINE WAS SHUTDOWN IN FLIGHT AS A PRECAUTION DUE TO AN OIL LEAK AND LOW OIL PRESSURE. ONCE ON THE GROUND, THE SOURCE OF THE OIL LEAK COULD NOT POSITIVELY BE LOCATED.THE ENGINE WAS MOUNTED IN THE TEST CELL AND THE OIL LEAK WAS FINALLY TRACED TO A CRA
- [SDR CA000614005](https://openairdocs.org/sdr/CA000614005.md): Nut · loose · Jun 7, 2000 · Mtsbsi MU2B35 · Power Lever
  > (CAN) INVESTIGATION REVEALED THE P/N 016A-43298 LT-RT THREADED ADJUSTMENT ROD ON THE POWER LEVER ATTACHMENT TO THE ENGINE, HAD COME LOOSE AND HAD MOVED, CAUSING A POWER LEVER MISMATCH. IT IS ASSUMED THAT THE LOCKNUTS WERE NOT SUFFICIENTLY TORQUED FOLLOWING A
- [SDR CA000120008](https://openairdocs.org/sdr/CA000120008.md): Switch · broken · Jan 18, 2000 · Mtsbsi MU2B35 · Landing Gear Position and Warning
  > (CAN) DURING APPROACH, THE CREW SELECTED GEAR DOWN AND FAILED TO GET A GREEN LIGHT FOR THE NOSE GEAR, THE UNSAFE LIGHT WAS NOT ILLUMINATED. AFTER A TOWER FLYBY THE GREENLIGHT CAME ON AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND A LOOSE / BROKEN WIRE AT TH
- [SDR 2000ZZZX25](https://openairdocs.org/sdr/2000ZZZX25.md): Fitting · broken · Jan 4, 2000 · N637WG · Mtsbsi MU2B35 · Main Landing Gear
  > FOUND BROKEN PART ON RAMP. INSPECTED AIRCRAFT ON RAMP AND NO PROBLEM FOUND. CALLED OUT STATION AND FOUND THE AIRCRAFT IN DALLAS HAD THE BROKEN FITTING ASSY. GROUNDED AIRCRAFT AND HAD IT REPAIRED BEFORE FLYING AIRCRAFT AGAIN.
- [SDR 99ZZZX3911](https://openairdocs.org/sdr/99ZZZX3911.md): Lock · worn · Sep 24, 1999 · N300RX · Mtsbsi MU2B35 · Propeller Hub Section
  > PROPELLER HAS NEW STYLE BLADE LOCKS. COTTERPIN THAT HOLDS SPRING AND LOCK IN ASSEMBLY IS FAILING OR WEARING OUT THE HOLES IN HOUSING.
- [SDR 99ZZZX939](https://openairdocs.org/sdr/99ZZZX939.md): Bolt · damaged · Feb 12, 1999 · N155AS · Mtsbsi MU2B35 · Propeller Blade Section
  > DURING 150-HOUR INSPECTION ON BOTH PROPELLERS, THE PROPELLER STOP LOCK BOLTS ON ALL PROP BLADES WERE FOUND CHAFING ON THE BLADE STOP PLATES. REMOVED ALL 6 BOLTS, PN AN4-417A, ON THE STOP LOCKS. INSTALLED ALL NEW BOLTS, PN AN4-16A, AND NEW NUTS, P/N B3808. R
- [SDR 99ZZZX924](https://openairdocs.org/sdr/99ZZZX924.md): Harness · damaged · Jan 13, 1999 · N113SD · Mtsbsi MU2B35 · Fire Detection
  > FOUND FIRE DETECT CABLE GROUNDED DUE TO CONDITION OF CABLE, CHANGE CABLE BEFORE REACHING SAME CONDITON. THE RIGHT ENGINE'S, P-20199, FIRE LIGHT CAME ON IN-FLIGHT. THE ENGINE WAS SHUT DOWN AND THE PLANE WAS RETURNED TO DFW. THERE WAS NO INDICATION OF FIRE AN
- [SDR 98ZZZX4689](https://openairdocs.org/sdr/98ZZZX4689.md): Window · cracked · Nov 20, 1998 · N375CA · Mtsbsi MU2B35 · Door Windows
  > DURING FLIGHT, MAIN CABIN DOOR WIDOW CRACKED. CRACK STARTED ALONG EDGE OF PAIN PARALLEL TO OPENING JUST UNDER SEAL.
- [SDR 99ZZZX176](https://openairdocs.org/sdr/99ZZZX176.md): Switch · malfunctioned · Sep 23, 1998 · N503AA · Mtsbsi MU2B35 · Cabin Cooling System
  > WITH AIR CONDITIONER ON AUTO, PILOT GOT COOL AND TURNED MANUAL HOT SWITCH ON AND LEFT IT THERE. THIS CAUSED EXCESS HEAT IN AIR DUCTS AND HIGH CONDENSATION. PILOT RETURNED MANUAL HEAT SWITCH BACK TO NORMAL AND LANDED IMMEDIATELY. THE AIR CLEARED AND SYSTEM W
- [SDR 98ZZZX3623](https://openairdocs.org/sdr/98ZZZX3623.md): Pump · failed · Sep 1, 1998 · N503AA · Mtsbsi MU2B35 · Turbine Engine Oil System
  > AT LANDING PILOT NOTICED OIL PRESSURE LOW. DURING TAXI, PILOT SHUT ENGINE DOWN. MAINTENANCE FOUND ENGINE WOULD NOT TURN BY PROP MOVEMENT. ENGINE WAS REMOVED AND SENT FOR TEARDOWN INSPECTION. THIS INSPECTION REVEALED THAT TORSION SHAFT HAD SEIZED DUE TO SCA
- [SDR CA980602013](https://openairdocs.org/sdr/CA980602013.md): Line · cracked · May 12, 1998 · Mtsbsi MU2B35 · Engine Oil Distribution (Airframe Furnished)
  > (CAN) ON SHORT FINAL, WHILE DOING PRE-LANDING CHECK, THE CREW NOTICED OIL ON THE RIGHT ENGINE COWL. NORMAL LANDING CARRIED OUT. INVESTIGATION REVEALED A CRACKED FLARE ON THE OIL SCAVENGE TUBE AT THE VERNATHERM VALVE.
- [SDR CA980317020](https://openairdocs.org/sdr/CA980317020.md): Actuator · failed · Mar 13, 1998 · Mtsbsi MU2B35 · Landing Gear Actuator
  > (CAN) OVERHAULED GEAR DOOR ACTUATOR INSTALLED TO RECTIFY A PREVIOUS PROBLEM. GROUND TEST OK. TEST FLIGHT FORWARD GEAR DOORS FAILED TO OPEN AND GEAR MANUALLYLOWERED. GROUND OPERATION NORMAL. INVESTIGATION REVEALED THAT THE ACTUATOR LIMIT SWITCH WIRES WERE MISLA
- [SDR CA980317019](https://openairdocs.org/sdr/CA980317019.md): Actuator · failed · Mar 12, 1998 · Mtsbsi MU2B35 · Landing Gear Door Actuator
  > (CAN) DURING DEPARTURE THE FORWARD GEAR DOORS WOULD NOT OPEN, PREVENTING GEAR RETRACTION. INVESTIGATION FOUND THE FORWARD GEAR DOOR ACTUATOR WAS DEVELOPING INSUFFICIENT SPEED TO ENGAGE THE CLUTCH AND OPEN THE DOORS. THE ACTUATOR WAS REPLACED.
- [SDR 99ZZZX267](https://openairdocs.org/sdr/99ZZZX267.md): Crew Door · separated · Jan 11, 1998 · N799MA · Mtsbsi MU2B35 · Emergency Exits
  > CREW HATCH/EMERGENCY ESCAPE DOOR DEPARTED THE AIRCRAFT DURING CLIMB.
- [SDR CA970702001](https://openairdocs.org/sdr/CA970702001.md): Insulator · missing · Jun 25, 1997 · Mtsbsi MU2B35 · Detection System
  > (CAN) ON LANDING, THE LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED. INVESTGATION FOUND NO FIRE, BUT REVEALED A MISSING INSULATOR INSIDE THE BULKHEAD CONNECTOR. SUBMITTER BELIEVES IT PROBABLY FELL OUT DURING ENGINE INSTALLATION 34 HOURS EARLIER.
- [SDR CA970401005](https://openairdocs.org/sdr/CA970401005.md): Actuator · frozen · Mar 27, 1997 · Mtsbsi MU2B35 · Landing Gear Door Actuator
  > (CAN) ON APPROACH, CREW SELECTED GEAR DOWN, FOLLOWING A MINUS 35 DEGREE TEMPERATURE CRUISE, AND NOTHING HAPPENED. GEAR SELECTED DOWN BY EMERGENCY EXTENSION. THE FORWARD GEAR DOOR ELECTRIC ACTUATOR WAS NOT WORKING. IT WAS TESTED AFTER REMOVAL FROM AIRCRAFT A
- [SDR CA970421001](https://openairdocs.org/sdr/CA970421001.md): Motor · intermittent · Feb 28, 1997 · Mtsbsi MU2B35 · Landing Gear Retraction/Extension System
  > (CAN) CREW NOTED THE GEAR WOULD NOT FULLY RETRACT. GEAR SWINGS BY MAINTENANCE FOUND THE MOTOR RAN SLOWLY. INSPECTION OF THE MOTOR FOUND ONE OF THE BRUSHES STUCK IN THE HOLDER CAUSING SLOW AND INTERMITTENT OPERATION.
- [SDR CA970226002](https://openairdocs.org/sdr/CA970226002.md): Bull Gear · failed · Feb 21, 1997 · Mtsbsi MU2B35 · Turbine Engine Reduction Gear
  > (CAN) DURING CRUISE, THE RIGHT HAND ENGINE SUDDENLY FEATHERED. ENGINE SECURED. INSPECTION FOUND THAT THE BULL GEAR HAD FAILED EITHER IN THE GEAR TOOTH BASE AND/OR THE WEB DISK OR THE DISK RADIUS. COULD HAVE BEEN CAUSED BY FOREIGN OBJECT ENTERING THE GEAR ME
- [SDR 97ZZZX495](https://openairdocs.org/sdr/97ZZZX495.md): Casting · ear broken · Jan 8, 1997 · N92ST · Mtsbsi MU2B35 · Landing Gear Retraction/Extension System
  > AT 100 HR INSP, LANDING GEAR THRUST GEAR BOX CASTING MOUNT EAR WAS FOUND BROKEN AND MOUNT BOLTS LOOSE. SUSPECT CAUSE TO BE SHIM SPACERS USED BETWEEN BOX AND AIRCRAFT STRUCTURE. INSP OF OPPOSITE SIDE (RIGHT) REVEALED THAT MOUNT BOLTS WERE LOOSE ALSO. SUBMITT
- [SDR CA961205011](https://openairdocs.org/sdr/CA961205011.md): Gear Door · frozen · Nov 28, 1996 · Mtsbsi MU2B35 · Landing Gear Door Actuator
  > (CAN) ICE CONTAMINATION IN THE GEAR DOOR ACTUATOR CAUSED THE PILOT ABORT THE APPROACH. SUBSEQUENT CYCLING OF THE GEAR PRODUCED A GEAR DOWN AND LOCKED CONDITION WHEREBY THE AIRCRAFT LANDED SAFELY.
- [SDR CA961128010](https://openairdocs.org/sdr/CA961128010.md): Switch · frozen · Nov 26, 1996 · Mtsbsi MU2B35 · Landing Gear Position and Warning
  > (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, NO RESPONSE. GEAR LOWERED MANUALLY. IT IS ASSUMED THAT THE NOSE GEAR DOWN LOCK SWITCH HAD PICKED UP WATER CONTAMINATION INTERNALLY ON THE PREVIOUS TAKEOFF AND HAD FROZEN AS THE AIRCRAFT HAD BEEN FLYING FOR OVER AN HOU
- [SDR CA961203001](https://openairdocs.org/sdr/CA961203001.md): Switch · broken wire · Nov 6, 1996 · Mtsbsi MU2B35 · Landing Gear Position and Warning
  > (CAN) DURING APPROACH THE PILOT COULD NOT GET AN INDICATION OF THE NOSE GEAR DOWN AND LOCKED. EMERGENCY EXTENSION PERFORMED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND A BROKEN WIRE WHERE THE WIRES ENTER A SEALED SWITCH. THE SWITCH WAS REPLACED AND THE A
- [SDR CA970130004](https://openairdocs.org/sdr/CA970130004.md): Switch · wire broken · Nov 5, 1996 · Mtsbsi MU2B35 · Landing Gear Position and Warning
  > (CAN) ON APPROACH THE CREW WERE UNABLE TO GET A GREEN LIGHT ON THE NOSE GEAR. THE SYSTEM WAS CYCLED AND A SUCCESSFUL LANDING WAS MADE. INVESTIGATION REVEALED A BROKEN WIRE AT THE ENTRY TO THE SWITCH LOCATION. THE SWITCH WAS REPLACED AND GEAR SWINGS CHECKED OUT
- [SDR CA961113002](https://openairdocs.org/sdr/CA961113002.md): Wire · broken · Nov 5, 1996 · Mtsbsi MU2B35 · Landing Gear System Wiring
  > (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, DID NOT GET A GREEN LIGHT ON THE NOSE GEAR. GEAR CYCLED WITH NO CHANGE. EMERGENCY EXTENSION USED. INVESTIGATION REVEALED A BROKEN WIRE AT THE SWITCH.
- [SDR 96ZZZX5619](https://openairdocs.org/sdr/96ZZZX5619.md): Control Cable · failed · Oct 15, 1996 · N6569L · Mtsbsi MU2B35 · Trailing Edge Flap Control System
  > DURING ROUTINE 500-HOUR INSPECTION, FLAPS WERE OPERATED TO VERIFY PROPER FUNCTION. DURING OPERATION, A 'POP' WAS HEARD AND THE LEFT OUTBOARD FLAP WAS NO LONGER MOVING. INSPECTION REVEALED THE FLEX CABLE INNER SHAFT HAD FAILED. CABLE WAS INSTALLED 2-8-88, AD
- [SDR CA960924009](https://openairdocs.org/sdr/CA960924009.md): Unfeather Switch · stuck on · Sep 18, 1996 · Mtsbsi MU2B35 · Propeller Feathering/Reversing
  > (CAN) DURING TAKEOFF ROLL, CREW NOTED THE LEFT ENGINE BETA LIGHT DID NOT EXTINGUISH WHEN THE RIGHT WENT OUT. WHEN THE ENGINES ENTERED PROPELLER GOVERNING MODE INDICATING A PROBLEM THE CREW ABORTED THE TAKEOFF. INVESTIGATION FOUND THE UNFEATHER BUTTON HAD STUCK
- [SDR CA960909001](https://openairdocs.org/sdr/CA960909001.md): Relay · burnt contacts · Sep 5, 1996 · Mtsbsi MU2B35 · Trailing Edge Flap Control System
  > (CAN) THE CREW SELECTED 20 DEGREES FOR FLAPS AND NOTED THE SETTING GOING TO 40 DEGREES. A CIRCUIT WAS CARRIED OUT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION FOUND THE CONTACTS OF THE FLAP MOTOR WERE STUCK CLOSED, WHICH DROVE THE FLAPS TO 40 D
- [SDR 96ZZZX2112](https://openairdocs.org/sdr/96ZZZX2112.md): Pilot Tube · cracked · Mar 7, 1996 · N6569L · Mtsbsi MU2B35 · Propeller Assembly
  > LONGITUDINAL CRACKS FOUND IN PILOT TUBE OF NR 3 SPIDER ARM.
- [SDR 96ZZZX2111](https://openairdocs.org/sdr/96ZZZX2111.md): Pilot Tube · cracked · Mar 7, 1996 · N6569L · Mtsbsi MU2B35 · Propeller Assembly
  > LONGITUDINAL CRACKS FOUND IN PILOT TUBE OF NR 2 SPIDER ARM.
- [SDR 96ZZZX2110](https://openairdocs.org/sdr/96ZZZX2110.md): Link Arm · cracked · Mar 7, 1996 · N6569L · Mtsbsi MU2B35 · Propeller Assembly
  > PROPELLER LINK ARM IS CRACKED BETWEEN HOLES IN LINK ARM.
- [SDR 96ZZZX2109](https://openairdocs.org/sdr/96ZZZX2109.md): Bracket · cracked · Mar 7, 1996 · N6569L · Mtsbsi MU2B35 · Propeller Assembly
  > PROPELLER INSPECTION FOUND 2 EACH START LOCK BRACKETS CRACKED.
- [SDR 96ZZZX2108](https://openairdocs.org/sdr/96ZZZX2108.md): Counterweight · cracked · Mar 7, 1996 · N6569L · Mtsbsi MU2B35 · Propeller Assembly
  > PROPELLER COUNTERWEIGHT DOWEL PIN HOLE IS CRACKED.
- [SDR AU960125](https://openairdocs.org/sdr/AU960125.md): Oil System · contam-metal · Feb 1, 1996 · Mtsbsi MU2B35 · Turbine Engine Oil System
  > (AUS) RH ENGINE OIL SYSTEM METAL CONTAMINATION
- [SDR CA951122001](https://openairdocs.org/sdr/CA951122001.md): Fcu · failed · Nov 15, 1995 · Mtsbsi MU2B35 · Fuel Control/Reciprocating Engines
  > (CAN) DURING TAXI FOR TAKEOFF, THE RIGHT HAND ENGINE EXPERIENCED AN UNCOMMANDED INCREASE IN POWER OUTPUT TOWARD MAXIMUM. THE CREW SHUTDOWN THE ENGINE WITH EMERGENCY STOP/FEATHER LEVER. THE ENGINE WAS REMOVED, A NEW FCU WAS INSTALLED, AND THE ENGINE RE-INSTALLE

Next page: https://openairdocs.org/model/mitsubishi-mu-2b-35/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 = 'MU2B35'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mitsubishi-mu-2b-35/reports

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