# Service difficulty reports: Beech B-60

A list on [Beech B-60](https://openairdocs.org/model/beech-b-60.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 71 reports

- [SDR 2022FA0000024](https://openairdocs.org/sdr/2022FA0000024.md): None · collapsed · May 19, 2021 · N6010S · Beech B60 · Engine (Reciprocating)
  > RIGHT ENGINE BECAME ROUGH IN CRUISE. AIRCRAFT LANDED UNEVENTFULLY. FOUND #2 CYLINDER HYDRAULIC LIFTER P/N: 15B28037 COLLAPSED. INTAKE VALVE STEM BROKEN. PISTON DAMAGED.
- [SDR 2022FA0000023](https://openairdocs.org/sdr/2022FA0000023.md): None · collapsed · May 19, 2021 · N6010S · Beech B60 · Engine (Reciprocating)
  > RIGHT ENGINE BECAME ROUGH IN CRUISE. AIRCRAFT LANDED UNEVENTFULLY. FOUND #2 CYLINDER HYDRAULIC LIFTER P/N: 15B28037 COLLAPSED. INTAKE VALVE STEM BROKEN. PISTON DAMAGED.
- [SDR 2019FA0000415](https://openairdocs.org/sdr/2019FA0000415.md): Brush Block · wrong part · Dec 19, 2019 · Beech B60 · AC Generation System
  > ALTERNATOR RECEIVED FOR REPAIR OF DRIVE END THREADED BOSS. INSPECTION OF UNIT WRONG (NON FAA/PMA) BRUSH BLOCK ASSEMBLY, RECTIFIER ASSEMBLY AND STATER ASSEMBLY INSTALLED. 10 HOURS ESTIMATED FROM FIELD REPAIR AT ENGINE MAJOR OVERHAUL.
- [SDR MI22018F00000](https://openairdocs.org/sdr/MI22018F00000.md): Intake Valve · broken · Oct 25, 2018 · N586HP · Beech B60 · Reciprocating Engine Cylinder Section
  > PILOT SAYS HE WAS CLIMBING THROUGH 17000` WHEN THE RT ENG LOST POWER AND WAS RUNNING ROUGH. THE PILOT DESCENDED AND LANDED WITH THE LT ENG. REMOVED COWLING AND CHECKED COMPRESSION AND FOUND NR 2 CYLINDER NO COMPRESSION. REMOVED NR 2 CYLINDER RBC AND FOUND I
- [SDR PCPR201804260001](https://openairdocs.org/sdr/PCPR201804260001.md): Skin · corroded · Feb 23, 2018 · N420JD · Beech B60 · Horizontal Stabilizer, Plate/Skin
  > FOUND SEVERE CORROSION ON THE HORIZONTAL STABILIZER SKINS (MAGNESIUM).
- [SDR 2017FA0000029](https://openairdocs.org/sdr/2017FA0000029.md): Hub · cracked · Jan 26, 2017 · N10WE · Beech B60 · Propeller Hub Section
  > A HUB CRACK DISCOVERED DURING ROUTINE MAINTENANCE. THE HUB WAS REPLACED WITH A SERVICEABLE UNIT.
- [SDR SPOA20141013001](https://openairdocs.org/sdr/SPOA20141013001.md): Interface Unit · faulty · Oct 10, 2014 · N626N · Beech B60 · Communications System
  > APPROXIMATELY ONE HOUR INTO THE FLIGHT & WITHOUT WARNING CREW EXPERIENCED A VERY LOUD, FULL VOL STATIC SQUELCH COMING THROUGH THE OVERHEAD SPEAKERS. AFTER SWITCHING FROM COMM 2 TO COMM 1 THE SQUELCH NOISE WENT AWAY BRIEFLY. HOWEVER, IT CAME BACK A FEW SECOND
- [SDR PCPR20131218001](https://openairdocs.org/sdr/PCPR20131218001.md): Crankcase · cracked · Nov 8, 2013 · N622R · Beech B60 · Reciprocating Engine Power Section
  > OPERATOR REPORTED OIL IN ENGINE COMPARTMENT. TECHNICIAN PERFORMED VISUAL INSPECTION AND FOUND CRACK IN ENGINE CRANKCASE FORWARD OF NR 2 CYLINDER FLANGE.
- [SDR CA120326008](https://openairdocs.org/sdr/CA120326008.md): Bolt · loose · Mar 15, 2012 · Beech B60 · Elevator Control System
  > (CAN) DURING TROUBLESHOOTING FOR AN UNRELATED PROBLEM, A BOLT PN#AN174-15A/M WAS FOUND LOOSE ON THE INBD PIVOT LOCATION OF THE L/H ELEVATOR. AN ANNUAL INSPECTION HAD BEEN COMPLETED PREVIOUSLY AND A VISUAL INSPECTION OF THIS AREA SHOWED NO ISSUES. TWO FLIGHTS
- [SDR 2009FA0000817](https://openairdocs.org/sdr/2009FA0000817.md): Window · fractured · Sep 2, 2009 · N3876C · Beech B60 · Passenger Compartment Windows
  > RT SIDE REAR WINDOW FRACTURED (BLEW OUT) IN FLIGHT CAUSING CABIN SUDDEN DECOMPRESSION. (K)
- [SDR CA090424005](https://openairdocs.org/sdr/CA090424005.md): G Switch · failed · Apr 23, 2009 · Beech B60 · Emergency Locator Beacon
  > (CAN) WHILE PERFORMING 12 MONTH INSP OF ELT IAW CAR 571 APPENDIX G THE G SWITCH FAILED TO OPERATE. G SWITCH REPLACED AND UNIT RETURN TO SERVICE.
- [SDR CA090409004](https://openairdocs.org/sdr/CA090409004.md): Intake Valve · broken · Apr 7, 2009 · Beech B60 · Reciprocating Engine Cylinder Section
  > (CAN) PILOT REPORTED LT ENG RUNNING ROUGH, NO INDICATION ON GRAPHIC ENGINE MONITOR FOR CYL NR 5. OPENED COWLINGS, INSPECTED CYL NR 5, CHECKED SPARK PLUGS, CHECKED COMPRESSION NO FAULTS FOUND. DETERMINED THAT WIRING HARNESS FOR GRAPHIC ENG MONITOR INSTALLED I
- [SDR CA080806005](https://openairdocs.org/sdr/CA080806005.md): Turbocharger · malfunctioned · Aug 1, 2008 · Beech B60 · Exhaust Turbocharger
  > (CAN) PILOT REPORTED LOW MANIFOLD PRESSURE ON LT ENG IN CLIMB OUT, ACFT RETURNED TO THE AIRPORT. MAINT BACK FLUSHED THE LT TURBO WASTEGATE AND CONTROLLER, GROUND RUN OK. NO OTHER DEFECTS NOTED, ACFT RETURNED TO SERVICE.
- [SDR IWP2720085003](https://openairdocs.org/sdr/IWP2720085003.md): Spring · misinstalled · Nov 23, 2007 · N408FA · Beech B60 · Landing Gear Retraction/Extension System
  > THIS AIRCRAFT EXPERIENCED A BENT /DAMAGED RT MAIN GEAR RETRACT ROD ASSEMBLY P/N 60-810057-617. A CURRENT OVERLOAD OF THE LANDING GEAR MOTOR CIRCUIT. THE RT MAIN GEAR FAILED TO EXTEND. THE EMERGENCY GEAR FAILED TO ALSO EXTEND THE RETRACTED MAIN. AC WAS FORCED T
- [SDR 2007FA0000506](https://openairdocs.org/sdr/2007FA0000506.md): Skin · cracked · May 17, 2007 · N837RJ · Beech B60 · Trailing Edge Flaps
  > BOTH FLAPS CRACKED AT ACTUATOR ATTACH POINT. LT FLAP SKIN AND RIB CRACKED. RT FLAP RIB CRACKED. RIGGING WAS OK, PROBABLY AN OPERATOR INDUCED PROBLEM. BELIEVE THE FLAPS HAVE BEEN LOWERED AT TOO HIGH AN AIRSPEED. (K)
- [SDR DA62007F00000](https://openairdocs.org/sdr/DA62007F00000.md): Escape Hatch · chafed · Mar 21, 2007 · N171EC · Beech B60 · Emergency Exits
  > DURING ANNUAL INSPECTION FOUND HINGED COVER FOR EMERGENCY EXIT RELEASE HANDLE WAS SAFETIED CLOSED WITH.020 INCH STAINLESS STEEL WIRE NOT COOPER BREAKAWAY WIRE OF (.040 INCH -.012 INCH). HAD TO CUT WIRE WITH WIRE CUTTING PLIERS IN ORDER TO BE ALLOWED ACCESS
- [SDR DA62007F00006](https://openairdocs.org/sdr/DA62007F00006.md): Bearing · corroded · Mar 15, 2007 · N171EC · Beech B60 · Wheel/Ski/Float
  > DURING ANNUAL INSPECTION, FOUND WHEEL BEARINGS AND RACES TO BE WORN AND CORRODED. ALSO, FOUND THAT THERE WERE (2) DIFFERENT TYPES OF GREASE USED IN THE WHEEL BEARINGS AND THE MANUAL REF A MIL-G-3545 ONLY, WHICH IS A HIGH TEMP GREASE AND IS RED OR AMBER IN COL
- [SDR DA62007F00005](https://openairdocs.org/sdr/DA62007F00005.md): Window · misinstalled · Mar 15, 2007 · N171EC · Beech B60 · Flight Compartment Windows
  > DURING ANNUAL INSPECTION, PILOT AND CO-PILOT SIDE WINDOWS SEALANT WAS FOUND TO BE CRACKED AND FULL OF AIR POCKETS. FOUND SEALANT TO BE IMPROPERLY APPLIED TO ATTEMPT TO RESEAL WINDOWS. AFTER REMOVAL OF THE SIDE WINDOWS, FOUND WASHERS IN SEALANT APPARENTLY USE
- [SDR CA070319006](https://openairdocs.org/sdr/CA070319006.md): Tappet · spalled · Mar 14, 2007 · Beech B60 · Reciprocating Engine Cylinder Section
  > (CAN) ENGINE MODIFIED IAW FIREWALL FORWARD CENTRILUBE STC. PREVIOUS EXPERIENCE WITH THIS ENGINE SERIES PROMPTS REGULAR TAPPET INSPECTIONS. TAPPETS INSPECTED AND SPALLING WAS FOUND, EVEN ON THIS STC`D ENGINE. TAPPETS SENT TO FIREWALL FORWARD FOR EXAMINATION, A
- [SDR DA62007F00007](https://openairdocs.org/sdr/DA62007F00007.md): Door · corroded · Feb 21, 2007 · N171EC · Beech B60 · Passenger/Crew Doors
  > DURING ANNUAL INSP FOUND CORROSION IN THE CABIN ENTRY DOOR IN 3 LOCATIONS. FIRST LOCATION WAS AT THE MIDDLE LOCKING PIN GUIDE ANGLE PIECE. THE SECOND LOCATION IS AT THE LOWER LOCKING PIN GUIDE ANGLE PIECE AND THE THIRD LOCATION IS ON A FRAME AT THE LOWER FWD
- [SDR DA62007F00002](https://openairdocs.org/sdr/DA62007F00002.md): Motor · damaged · Feb 20, 2007 · N171EC · Beech B60 · Trailing Edge Flap Control System
  > FLAPS FAILED IN DOWN POSITION ON LANDING. DURING TROUBLESHOOTING AND INSPECTION FOUND FLAP MOTOR AND WIRING TO BE SUBMERGED IN WATER APPROXIMATELY 1.5 INCHES TO 2 INCHES DEEP. AFTER WATER WAS CLEANED UP AND MOTOR WAS ALLOWED TO DRY FLAPS FUNCTIONED PROPERLY.
- [SDR DA62007F00004](https://openairdocs.org/sdr/DA62007F00004.md): Control Cable · corroded · Jan 4, 2007 · N171EC · Beech B60 · Elevator Control System
  > DURING ANNUAL INSP, FOUND SEVERAL CONTROL CABLES THAT WERE CORRODED DUE TO BEING SUBMERGED IN WATER AND THAT WERE EXPOSED TO THE EVAPORATION OF THE WATER THAT HAD COLLECTED IN THE BELLY OF THE AC. CONTROL CABLES WILL BE REMOVED AND REPLACED, WATER DRIED UP AN
- [SDR 2006FA0001153](https://openairdocs.org/sdr/2006FA0001153.md): Stiffener · cracked · Dec 7, 2006 · N3876C · Beech B60 · Fuselage Main, Keel
  > DURING ANNUAL INSPECTION, STIFFENER PART NUMBER 60-410025-51 LOCATED UNDER THE NOSE BAGGAGE FLOOR ON THE RIGHT SIDE AT STATION 67 BETWEEN THE MAIN AND STANDBY INVERTER WAS FOUND CRACKED AROUND THE HI-LOK FASTENER HOLES. REMOVAL OF THE STIFFENER ALLOWED FURTHE
- [SDR 2006FA0001151](https://openairdocs.org/sdr/2006FA0001151.md): Keel · cracked · Dec 7, 2006 · N3876C · Beech B60 · Fuselage Main, Keel
  > DURING ANNUAL INSPECTION, STIFFENER PART NUMBER 60-410025-51 LOCATED UNDER THE NOSE BAGGAGE FLOOR ON THE RIGHT SIDE AT STATION 67 BETWEEN THE MAIN AND STANDBY INVERTER WAS FOUND CRACKED AROUND THE HI-LOK FASTENER HOLES. REMOVAL OF THE STIFFENER ALLOWED FURTHE
- [SDR 2005FA0000766](https://openairdocs.org/sdr/2005FA0000766.md): Cylinder · cracked · May 3, 2005 · N34KA · Beech B60 · Reciprocating Engine Cylinder Section
  > DURING DIFFERENTIAL COMPRESSION TEST, AIR WAS HEARD LEAKING FROM LOWER CYLINDER AREA. COMPRESSION WAS 40/80. USING LIQUID LEAK DETECTOR, FOUND AIR BLOWING OUT FROM A CRACK IN CYLINDER FIN. REMOVED CYLINDER FROM ENGINE AND NOTED A CRACK IN THE COMBUSTION CHA
- [SDR CA050228008](https://openairdocs.org/sdr/CA050228008.md): Control Cable · frayed · Feb 28, 2005 · Beech B60 · Elevator Control System
  > (CAN) (.0625) ELEVATOR TRIM CABLE WAS FOUND WITH WIRES BROKEN IN A CRITICAL FATIGUE AREA, (.2500) LENGTH FROM AFT END, THROUGH THE IDLER PULLY AND CAPSTAN OF BENDIX FCS 810 AUTOPILOT TRIM SERVO. SEC 7 PART B: FOUND DURING AUTOPILOT REPLACEMENT. SEC 7 PART
- [SDR 2005FA0000463](https://openairdocs.org/sdr/2005FA0000463.md): Service difficulty · Feb 11, 2005 · N30MM · Beech B60 · Exhaust Turbocharger
  > WHILE INVESTIGATING OIL LEAK FROM TURBO, FOUND IMPELLER/TURBINE SHAFT HOLD DOWN NUT LOOSE ALLOWING SHAFT TO MOVE LATERALLY. THIS CAUSED SHAFT TO BECOME UNSEATED AT BEARING SEALS. DISCREPANCY WAS DISCOVERED EARLY ENOUGH TO KEEP IMPELLER AND TURBINE WHEELS FRO
- [SDR CYW2005F00000](https://openairdocs.org/sdr/CYW2005F00000.md): Transmitter · inoperative · Dec 30, 2004 · N217RB · Beech B60 · Fuel Quantity Indicator
  > FUEL QUANTITY INDICATORS WOULD ONLY SHOW APPROX 35 GALS MAX EVEN WITH FULL FUEL. FOUND IB AND OB LEADING EDGE CELL TRANSMITTERS GROUNDED TO AIRFRAME. REMOVAL REVEALED GROMMETS DETERIORATED ALLOWING TRANSMITTER CASE TO TOUCH AIRFRAME. RECOMMEND REPLACING GRO
- [SDR 2005FA0000211](https://openairdocs.org/sdr/2005FA0000211.md): Oil Cooler · cracked · Dec 29, 2004 · N2025P · Beech B60 · Engine Oil Cooler
  > COOLER SPLIT AT WELD ON END OF COOLER. SPLIT WAS 2+ INCHES LONG RIGHT DOWN THE CENTER OF THE WELD. (GL19200501920) (GL19200502021) (K)
- [SDR 2004FA0000797](https://openairdocs.org/sdr/2004FA0000797.md): Valve · broken · Jul 23, 2004 · N131MC · Beech B60 · Reciprocating Engine Power Section
  > WITHIN THE LAST 3 TO 3.5 HOURS OF FLIGHT, THE PILOT NOTED THE ENGINES WERE RUNNING ROUGH AND FLEW TO OUR FACILITY FOR DISCOVERED THAT THE INTAKE VALVE KEEPER KEYS WERE BROKEN, THE NR 6 CYLINDER HAD A STUCK EXHAUST VALVE. THE PILOT REPORTED HAVE THE NR 6 CYLIN
- [SDR 2003FA0001101](https://openairdocs.org/sdr/2003FA0001101.md): Rod · destroyed · Oct 5, 2003 · N57HD · Beech B60 · Reciprocating Engine Power Section
  > ON FINAL APPROACH, LEFT ENGINE, NR 5 ROD BROKE AND BROKE CRANKCASE.
- [SDR 2003FA0000960](https://openairdocs.org/sdr/2003FA0000960.md): Oil Cooler · cracked · Sep 5, 2003 · Beech B60 · Engine Oil Cooler
  > WE HAVE FOUND 3 OIL COOLERS IN THE PAST YEAR ON THESE AC WITH IDENTICAL CRACKS ON THE DIAGONAL SUPPORT BARS AT THE INBOARD WELD. THIS LEADS TO SEPARATION OF ONE END OF THE BAR. CAUSE OF THE CRACKS ARE NOT OBVIOUS. WE ARE ALSO AWARE OF 2 OTHER AC THAT HAVE E
- [SDR 2003FA0000514](https://openairdocs.org/sdr/2003FA0000514.md): Lifter · corroded · Apr 30, 2003 · N1WA · Beech B60 · Reciprocating Engine Cylinder Section
  > LIFTERS PITTED AND MUSHROOMED.
- [SDR 2002FA0001091](https://openairdocs.org/sdr/2002FA0001091.md): Lifter · spalled · Sep 5, 2002 · N18292 · Beech B60 · Reciprocating Engine Power Section
  > SEVEN SPALLING OF LIFTERS AND CAM SHAFT WITH ONLY 130 HOURS USE. ALSO FAILED WITH 60 HOURS USE.
- [SDR 2002FA0001102](https://openairdocs.org/sdr/2002FA0001102.md): Camshaft · eroded · Aug 30, 2002 · N265D · Beech B60 · Reciprocating Engine Power Section
  > WITH NO PROBLEMS TO 1952 HRS SINCE NEW (TBO1600), THIS ENGINE WAS OVERHAULED IN FEB 99. NOTHING BUT PROBLEMS SINCE. AT FIRST OIL CHANGE, AFTER OVERHAUL (35 HOURS) ABNORMAL METAL SLIVERS FOUND IN OIL FILTER. CONTINUED FLYING. MORE FERROUS METAL AT 2ND OIL C
- [SDR 2002FA0000992](https://openairdocs.org/sdr/2002FA0000992.md): Pin · failed · Aug 8, 2002 · N102SB · Beech B60 · Reciprocating Engine Power Section
  > THE LIFTER BORES WERE ALL SLEEVED (ALL 12) NOTE: THE SLEEVES CAME LOOSE IN ALL THE HOLES (EXCEPT TWO) ROTATING AND BLOCKING OFF OIL PASSAGES. THERE WERE NO STANDARD SAFETY PINS, OR DEVICES TO HOLE THE LIFTER SLEEVE IN PLACE. THERE ARE MANY OTHER ENGINES IN S
- [SDR 2002FA0001103](https://openairdocs.org/sdr/2002FA0001103.md): Lifter · eroded · Aug 3, 2002 · N265D · Beech B60 · Reciprocating Engine Power Section
  > WITH NO PROBLEMS TO 1952 HOURS SINCE NEW (TBO1600), THIS ENGINE WAS OVERHAULED IN FEB 99. NOTHING BUT PROBLEMS SINCE. AT FIRST OIL CHANGE AFTER OVERHAUL (35 HOURS) ABNORMAL METAL SLIVERS FOUND IN OIL FILTER. CONTINUED FLYING. MOR FEROUS METAL AT 2ND OIL CH
- [SDR CA000920015](https://openairdocs.org/sdr/CA000920015.md): Bolt · sheared · Aug 15, 2000 · Beech B60 · Reciprocating Engine Power Section
  > (CAN) THE NR 3 CYLINDER CONNECTING ROD BOLT FAILED DUE TO FATIGUE, OR DEFECTIVE MATERIAL.
- [SDR 20000821SH011](https://openairdocs.org/sdr/20000821SH011.md): Bolt · rusted · Aug 3, 2000 · N7BB · Beech B60 · Horizontal Stabilizer Structure
  > DURING ANNUAL INSPECTION, FOUND THE HORIZONTAL STABILIZERS TO CREAK WHEN FORCED UP OR DOWN. DURING INVESTIGATION, NOTICED MOVEMENT IN THE AFT ATTACH FITTING FOR BOTH SIDES. REMOVED THE BOLTS FROM THEIR CLOSE TOLERANCE HOLES TO DISCOVER THEY WERE TOO SHORT.
- [SDR EY2R57053](https://openairdocs.org/sdr/EY2R57053.md): Hub · corroded · Jul 27, 2000 · Beech B60 · Propeller System
  > HUB CORRODED INSIDE EXTENSION AT THE PARTING SURFACE.
- [SDR 20000328SH003](https://openairdocs.org/sdr/20000328SH003.md): Control Cable · failed · Jan 31, 2000 · N341D · Beech B60 · Trailing Edge Flap Control System
  > CABLE WITH A TWIST TEST OF THE CABLE END SIMILAR TO THE DUKES CABLES ON THE PIPER PA31 FLAP SYSTEMS. (X)
- [SDR 99ZZZX2463](https://openairdocs.org/sdr/99ZZZX2463.md): Oil Cooler · leaking · Jun 11, 1999 · Beech B60 · Engine Oil Cooler
  > PART FAILED DURING NORMAL SERVICE. PART HAD PREVIOUSLY BEEN REPAIRED USING EPOXY. THE EPOXY FAILED ALLOWING THE COOLER TO BEGIN LEAKING AT POINT OF ORIGINAL REPAIR. RECOMMEND ELIMINATING USE OF EPOXY ON OIL COOLERS AS EPOXY FAILURE IS COMMON.
- [SDR 99ZZZX1138](https://openairdocs.org/sdr/99ZZZX1138.md): Pump · malfunctioned · Jan 28, 1999 · N30MM · Beech B60 · Vacuum Distribution System
  > LEFT ENGINE VACUUM PUMP EXHIBITED LOW PRESSURE INDICATION. REMOVED PUMP. FOUND SHAFT HARD TO ROTATE. IT DID NOT SHEAR AS EXPECTED. REPLACED PUMP.
- [SDR 98ZZZX3940](https://openairdocs.org/sdr/98ZZZX3940.md): Gear · sheared · Sep 9, 1998 · N4646M · Beech B60 · Landing Gear Retraction/Extension System
  > GROUND PERSONNEL NOTICED PIECE MISSING FROM DRAG BRACE TO NOSE GEAR ATTACH BOLT. BOLT WITH INTEGRAL PIN SERVES AS UPLOCK FOR NOSE GEAR. INSPECTION REVEALED P/N 60-820091 PIN SHEARED AT LEFT DRAG BRACE AND CORRODED IN NOSE GEAR. FAILURE MAY HAVE BEEN CAUSED
- [SDR 98ZZZX2686](https://openairdocs.org/sdr/98ZZZX2686.md): Uplock Pin · failed · Jul 9, 1998 · N947GB · Beech B60 · Landing Gear Retraction/Extension System
  > ON LANDING, NOSE GEAR COLLAPSED. SECTION OF LOWER DRAG BRACE FOUND ON RUNWAY. SECTION HAD BROKEN OFF AT OVERCENTER PIN. UPLOCK P/N FAILED, BOTH ENDS DEPARTED AIRCRAFT AND WERE NOT FOUND. SECTION OF UPLOCK PIN REMAINED IN NOSE GEAR UPPER STRUT HOUSING. BEE
- [SDR 98ZZZX2457](https://openairdocs.org/sdr/98ZZZX2457.md): Structure · corroded · Jun 1, 1998 · N51AL · Beech B60 · Fuselage Main, Structure
  > WHILE DOING PAINT AND INTERIOR, SEVERE CORROSION WAS NOTICED UNDER THE EXISTING INSULATION. SUBMITTER STATED THE CORROSION WAS CAUSED BY THE INSULATION HOLDING WATER FROM SEAL CONDENSATION. ALSO, FOUND WINDOWS WITH BAD SEAL POSSIBLY FROM SITTING ON THE RAMP
- [SDR 98ZZZX2275](https://openairdocs.org/sdr/98ZZZX2275.md): Connect Rod · failed · Apr 20, 1998 · N66HW · Beech B60 · Reciprocating Engine Power Section
  > NR 3 CYLINDER ROD BROKE IN CRUISE FLIGHT.
- [SDR 98ZZZX88](https://openairdocs.org/sdr/98ZZZX88.md): Fitting · damaged · Dec 12, 1997 · N341D · Beech B60 · Wing, Attach Fittings
  > WHILE C/W WING BOLT REPLACEMENT AND WING INSPECTION, FOUND LOWER AFT WING FITTINGS ON BOTH WINGS WITH COMPRESSION MARKS. BEECHCRAFT FIELD SERVICE CONTACTED PER MM INSTRUCTIONS. SPECIAL TOOLING AVAILABLE TO RESURFACE FITTING FACE. SUBMITTER SUGGESTED OWNERS
- [SDR 97ZZZX5085](https://openairdocs.org/sdr/97ZZZX5085.md): Pump · leaking · Nov 17, 1997 · N1551L · Beech B60 · Engine Fuel Pump
  > PUMP WAS SPEWING FUEL AT CASE PARTING LINE AT REGULATOR. GASKET HAD PUSHED ITS WAY OUT FROM BETWEEN HALVES. RESEALED BY REPAIR STATION. WAS TOLD THIS WAS OFTEN SEEN DUE TO THINNESS OF GASKET IF ONLY OIL OR GREASE WERE PRESENT ON MATING SURFACES WHEN ASSEMBL
- [SDR 97ZZZX4956](https://openairdocs.org/sdr/97ZZZX4956.md): Oil Cooler · leaking · Nov 17, 1997 · N7288D · Beech B60 · Engine Oil Cooler
  > THE FIRST OIL COOLER WAS INSTALLED WHEN THE ORIGINAL OIL COOLER DEVELOPED A LEAK AT 2426.8 HOURS. THIS OIL COOLER DEVELOPED A LEAK AFTER ABOUT 6 HOURS. OIL COOLER NR 2 WAS INSTALLED AND DEVELOPED A LEAK AFTER 2 HRS. THE NR 2 OIL COOLER WAS CUT IN TWO TO SEE

Next page: https://openairdocs.org/model/beech-b-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 = 'B60'
ORDER BY difficulty_date DESC
```

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

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