Beech B100

Service difficulty reports · 200

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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 = 'B100'
  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.

SDR 99ZZZX1922Bolt · misinstalledWHILE C/W 5 YEAR WING BOLT INSPECTION, FOUND FITTINGS DAMAGED DUE TO IMPROPER INSTALLATION OF RIGHT, LOWER, FORWARD AND LEFT, LOWER FORWARD WING BOLTS. WASHERS WERE INSTALLED BACKWARDS WHICH DEFORMED THE WING FITTINGS.Apr 15, 1999 · N86FD · Beech B100 · Wing Miscellaneous StructureSDR 99ZZZX2111Duct · failedDEFECT WAS FOUND DURING A REGULAR INSPECTION. UPON VISUAL INSPECTION THROUGH EXHAUST DUCTS, NOTICED THE 'SKI SLOPE' INNER SECTION DUCT ASSY PN 31068200-01 MISSING THE AFT PORTION OF ITS TAPERED CONE. NOTED THE POWER TUBE DAMAGED AND ALL BLADES DESTROYED. AMar 24, 1999 · N53MD · Beech B100 · Turbine SectionSDR 99ZZZX1364Skin · crackedPILOT REPORTED FLUTTER/VIBRATION IN-FLIGHT. UPON INVESTIGATION, DISCOVERED TAILCONE CRACKED CIRCUMFERENTIALLY APPROXIMATELY 60 PERCENT, ABOUT 18 INCHES IN FROM TIP OF TAIL CONE. FURTHER INVESTIGATION REVEALED SEVERAL SMALLER CRACKS BEGINNING AT STIFFENER FASFeb 1, 1999 · Beech B100 · Aerodynamic FairingsSDR 99ZZZX382Lever · jammedDURING PRE-FLIGHT, FOUND RIGHT CONDITION LEVER COULD NOT BE PLACED INTO EMERGENCY FEATHER POSITION. LEVER WOULD JAM ABOUT HALF WAY TO STOP POSITION. ENGINE CONTROL RE-RIGGED TO PROVIDE CONDITION LEVER FULL TRAVEL. SUBMITTER SUGGESTED A FEATHER VALVE CHECK BDec 22, 1998 · N8514B · Beech B100 · Engine Bleed Air SystemSDR 99ZZZX677Valve · malfunctionedPILOT REPORTED EXCESSIVE HEAT IN COCKPIT. FOUND RIGHT SIDE BLEED AIR SHUT-OFF VALVE STUCK OPEN. REMOVED P/N 101-380013-17, S/N 554. REPLACED WITH P/N 101-380013-17, S/N 634. RUN-UP OPERATIONAL CHECK GOOD.Dec 13, 1998 · N949SW · Beech B100 · Heating SystemSDR 99ZZZX871Circuit · damagedUPON FINAL APPROACH INTO DES MOINES, IOWA, CREW NOTICED SMOKE EMITTING FROM CENTER PEDESTAL. CREW TOOK APPROPRIATE ACTION AND SHUT OFF ELECTRICAL POWER AS NEEDED. MAINTENANCE PERSONNEL FOUND SOURCE OF SMOKE TO BE SHORTED PRINTED CIRCUIT BOARD. AREA AND BOARDec 8, 1998 · N818PA · Beech B100 · Electrical Power SystemSDR 98ZZZX4716Switch · failedSTALL WARNING HEAT AND RIGHT HEAT SWITCHES DROP OFF-LINE. INSPECTED SWITCHES AND FOUND LOOSE CONNECTION ON STALL WARNING HEAT SWITCH AND DEFECTIVE PITOT HEAT SWITCH. REPLACED PITOT SWITCH, RE-SECURED CONNECTION ON STALL WARNING SWITCH. AIRCRAFT TT: 7,189.9Nov 23, 1998 · N241CW · Beech B100 · Pitot/Static Anti-Ice SystemSDR CA990111051Windshield · cracked(CAN) IN CRUISE, THE COPILOT'S WINDSHIELD SUDDENLY CRACKED. AIRCRAFT LANDED OK.Nov 15, 1998 · Beech B100 · Flight Compartment WindowsSDR 98ZZZX3947Hinge Fitting · holes elongatedDURING INSPECTION. LT ELEVATOR OUTBOARD HINGE FOUND LOOSE. FOUND HOLES ELONGATED IN 115-620021-9 HINGE ASSEMBLY AND SURROUNDING STRUCTURE. BOLTS CALLED OUT FOR IN BEECH MSB 2132-R1 AND AD NOTE 87-03-06 HAD BEEN P/C/W. AD NOTE STATES THE RECURRING INSPECTIONAug 27, 1998 · N988JR · Beech B100 · Horizontal Stabilizer, Tab StructureSDR 98ZZZX3946Brace · corrodedCUSTOMER COMPLAINED OF HARD TO STEER AIRCRAFT AND NLG FAILING TO TURN WHEN O.A.T. WAS VERY LOW. ON TEAR DOWN, INSPECTORS FOUND MASSIVE CORROSION IN NLG BRACE ASSY. BRACE HAD TO BE REPLACED WITH NEW PART. CAUSE OF FAILURE FELT TO BE LACK OF PROPER LUBBING PAug 27, 1998 · N988JR · Beech B100 · Nose/Tail Landing Gear Strut/AxleSDR 98ZZZX2717Bracket · failedPILOT REPORTED LT ENG STARTER WOULD NOT CRANK ENG. STARTER REPLACED. NEW STARTER TESTED, AND WOULD NOT CRANK ENG. VOLTAGE AT THE STARTER CHECKED AND FND TO BE 48 VOLTS INSTEAD OF THE NORMAL 24 VOLTS. START CONTROL PANEL WAS INSPECTED AND FND TO HAVE ARCED Jul 13, 1998 · N400AC · Beech B100 · Engine CrankingSDR 98ZZZX2563Bolt · looseREPORT IN C/W WITH FAR 135.415 (5). UPON LANDING WHEN THE PROP'S WERE CYCLED INTO BETA (REVERSE) A FEW SECONDS LATER, SMOKE ENTERED CABIN. UPON INSPECTION OF AIRCRAFT AND ENGINES, FOUND THE PIN THAT IS INSTALLED IN THE ENGINE TRUSS TUBES TO SEAL THE ACCESS HOMay 19, 1998 · N108EB · Beech B100 · Engine Mount SectionSDR CA980513008Torque Tube · cracked(CAN) CRACK FOUND ON ELEVATOR TORQUE TUBE ASSEMBLY BRACKET FLANGE WHERE IT IS FASTENED TO RIB THROUGH SKIN ON LOWER SECTION OF RT ELEVATOR.Apr 25, 1998 · Beech B100 · Elevator Control SystemSDR 98ZZZX1246Combustion Case · failedDURING T/O, PILOT HEARD A 'POOF' SOUND. NOTICED THE COWLING PAINT DISCOLORED AND THE OIL FILLER DOOR OPEN. TAKEOFF ABORTED, AND ENG EMERG SHUTDOWN. INVEST DETERMINED THE LT ENG COMBUSTION CASE (PLENUM) HAD FAILED. ENG REMOVED FOR REPAIR, ENG COMPARTMENT DMar 10, 1998 · N66804 · Beech B100 · Turbine Engine Combustion SectionSDR 98ZZZX1276Engine · seizedRIGHT ENGINE INSTALLATION AFTER REPAIRS FOR BIRD INGESTION AND COMPLETION OF HSI. AIRCRAFT WAS ON A FLIGHT CHECK FOR THE REQUIRED IN-FLIGHT NTS CHECK. ENG WAS SHUT DOWN AND ON RESTART, SPOOLED TO ABOUT 20 PERCENT WHEN ENG SEIZED. (SEIZURE APPEARS TO BE FROMFeb 17, 1998 · N108EB · Beech B100 · Engine (Turbine/Turboprop)SDR CA980113007Wing Bolt · cracked(CAN) WHILE PERFORMING AD CF-81-25R5, A CRACK WAS DETECTED. THE RIGHT HAND LOWER FORWARD BOLT WAS FOUND CRACKED AT THE SHANK.Dec 24, 1997 · Beech B100 · Wing, Attach FittingsSDR 98ZZZX94Governor · failedDURING FLIGHT, RIGHT ENGINE FLAMED OUT, NTS AND THE PROP FEATHERED. AN UNEVENTFUL LANDING WAS PERFORMED. UPON INSPECTION, FOUND THE ARM HAD FALLEN OFF OF THE PROP GOVERNOR SPLINED SHAFT. THE MOUNT BOLT WAS STILL SECURE IN THE ARM. THIS IS THE SECOND OCCURRDec 19, 1997 · N924RM · Beech B100 · Propeller GovernorSDR 97ZZZX5204Engine · failureENGINE FAILURE ON FINAL. PILOT REPORTED 20 KNOT CROSSWINDS WITH GUSTS. AIRCRAFT HAD BEEN IN ICING CONDITIONS. SUSPECT CAUSE OF FAILURE, INGESTION OF ICE.Dec 2, 1997 · N150YA · Beech B100 · Engine (Turbine/Turboprop)SDR 97ZZZX5044Anti Ice Tube · brokenLEFT ENGINE FLAME-OUT AT 7,000 FEET HOLDING AT FLYING COLD IN ICING CONDITION. INTAKE ANTI-ICE HAD BEEN ON FOR HALF AN HOUR. FOUND ONE ANTI-ICE TUBE FLARE BROKEN OFF. SUSPECT SOME LOSS OF BLEED AIR IN THIS AREA COULD HAVE ATTRIBUTED TO ICE FORMING ON INTAKENov 14, 1997 · N564CA · Beech B100 · Air Intake Anti/De-Ice SystemSDR 97ZZZX4851Plenum · failedENG FAILURE AT T/O. CREW HEARD A LOUD POP, THE RT ENG ITT TEMP ROSE AND FLAMES FROM THE RT ENG. UNABLE TO KILL THE ENG USING THE EMERG CUTOFF LEVER, LEVER WAS JAMMED. THE ENG WAS SHUT DOWN USING THE FIREWALL SOV. FIRE BOTTLE WAS DISCHARGED AND FIRE WAS PUTNov 4, 1997 · N400AC · Beech B100 · Turbine Engine Combustion SectionSDR CA970902031Pump · failed(CAN) AFTER LANDING, IT WAS REPORTED RIGHT BOOSTER PUMP WAS NOT WORKING. MAINTENANCE CHECKED INDICATED PUMP WAS NOT OPERATING AT 1 PSI. PUMP WAS REPLACED.Aug 21, 1997 · Beech B100 · Fuel Boost PumpSDR 97ZZZX3820Window · delaminatedFOUND COPILOT'S D-WINDOW STARTING TO DELAMINATE ON LOWER PORTION DUE TO OVERSIZED WINDOW WAS INSTALLED IN A NORMAL SIZE FUSELAGE OPENING. WINDOW WAS RUBBING ON FUSELAGE SKIN AT THE RECESSED AREA OF THE WINDOW. BEECHCRAFT IPC ONLY LISTS OVERSIZED WINDOWS.Jul 14, 1997 · N500KD · Beech B100 · Flight Compartment WindowsSDR 97ZZZX2550Governor · wrong partUPON INSPECTING AIRCRAFT FOR PART 135 OPERATION, THE LEFT PROP GOV WAS FOUND TO BE A PART NUMBER NOT AUTHORIZED FOR B-100'S. THIS WAS CONFIRMED THROUGH WOODWARD GOVERNOR. THERE WERE NO OPERATING PROBLEMS AT THE TIME. GOVERNOR WAS REPLACED WITH PROPER PART NMay 19, 1997 · N500KD · Beech B100 · Propeller GovernorSDR 97ZZZX2829Bracket · crackedFOUND OXYGEN BOTTLE LEFT SUPPORT BRACKET CRACKED. CRACK LOCATED AT THE CORNER OF THE CUT OUT FOR THE BAND CLAMP. BRACKET MANUFACTURED BY PURITAN BENNETT.May 16, 1997 · N55FR · Beech B100 · Crew Oxygen SystemSDR 97ZZZX2366Mount · chafedDURING ROUTINE INSPECTION, DISCOVERED THE RIGHT ENGINE MOUNT TRUSS HAD BEEN CHAFED BEYOND ALLOWABLE LIMITS IN TWO PLACES BY A NR 8 STAINLESS STEEL HARD OIL SCAVAGE RETURN LINE. SUBMITTER ADVISES OTHERS WITH KA-B-100'S TO CHECK THIS AREA OF MOUNT TRUSS. THE CMay 2, 1997 · N187J · Beech B100 · Engine Mount SectionSDR 97ZZZX2356Strut · crackedNOSE LANDING GEAR STRUT UPPER BODY CASTING HAS A CRACK FROM THE LEFT LOWER GREASE FITTING TO THE BOTTOM OF THE BODY CASTING. A DISTANCE OF .3125 INCH LONG. SUBMITTER ADVISES OTHERS TO CHECK THIS AREA.May 2, 1997 · N187J · Beech B100 · Nose/Tail Landing Gear Strut/AxleSDR 97ZZZX2809Bracket · crackedFOUND OXYGEN BOTTLE RT SUPPORT BRACKET CRACKED. CRACK LOCATED AT THE CORNER OF THE CUT-OUT FOR THE BAND CLAMP.Mar 17, 1997 · N55FR · Beech B100 · Portable Oxygen SystemSDR 97ZZZX1125Line · failedCREW WAS PERFORMING A MISSED APPROACH PROCEDURE. DURING CLIMB-OUT, THE RT ENG WAS RETARDED TO FLIGHT IDLE TO SIMULATE ENG OUT CONDITION. DURING THIS ENTIRE TIME THE ACFT WAS IN LIGHT ICING CONDITIONS WITH ALL ANTI-ICE SYSTEMS OPERATING NORMALLY. AFTER COMPLFeb 21, 1997 · N771CW · Beech B100 · Air Intake Anti/De-Ice SystemSDR 97ZZZX1022Indicator Assy · bracket corrodedPILOTS STATED FUEL INDICATION WAS SOME TIMES UNRELIABLE. REMOVED FUEL INDICATOR PANEL AND FOUND CORROSION ON BRACKET THAT SERVES AS MOUNT FOR FUEL INDICATOR DIODES. SUSPECT THAT CORROSION ALLOWED A GROUND TO DIODES. (DIODES ARE NORMALLY INSULATED FROM BRACKFeb 20, 1997 · N4004C · Beech B100 · Fuel Indicating SystemSDR 97ZZZX849Torque Tube · worn'PLAY' WAS NOTED BETWEEN THE ELEVATORS. INSPECTION FOUND ELEVATOR PINS TO TORUQE TUBE WORN. REAMING, PER SM, DID NOT REMOVE ALL THE PLAY. REPLACED TORQUE T UBE ASSY WITH NEW PINS. THERE WAS NO ABNORMAL FLIGHT CONDITIONS BEFORE OR AFTER. TORQUE TUBE INSPECFeb 7, 1997 · N717D · Beech B100 · Elevator Control SystemSDR 97ZZZX461Eva Tubing · meltedINVESTIGATION FOR MELTED AND COLLAPSED EVA OUTFLOW VALVE TUBING FOUND CABIN AFT VENT WAS BLOCKED WITH BAGGAGE AND AIR VENT WAS DETACHED. APPARENTLY CABIN AIR (HEAT) WAS SUFFICIENT ENOUGH TO MELT/COLLAPSE TUBING. THE ONLY DAMAGED TUBING WAS AT THE AREA OF THEJan 2, 1997 · N531CB · Beech B100 · Pressure Regulator/Outflow ValveSDR 97ZZZX1931Switch · stuck closedMECHANICS WERE WORKING ON LANDING GEAR DOWNLOCK (J-HOOK) SOLENOID. THEY WERE CHECKING OPERATION OF THE SOLENOID BY ACTIVATING THE RIGHT SQUAT SWITCH. ACFT WAS NOT ON JACKS AT THAT POINT. GEAR HANDLE WAS VERIFIED IN DOWN POSITION PRIOR TO ACTIVATION OF THDec 16, 1996 · N500KD · Beech B100 · Landing Gear SelectorSDR 96ZZZX5970Wire · crackedTHE STARTER/GENERATOR 4 GAUGE WIRES THAT RUN FROM THE FIREWALL POWER CONNECTOR TO THE STARTER/GENERATOR WERE FOUND WITH CRACKED INSULATION. THE CRACKS ARE 2 INCHES TO 4 INCHES IN LENGTH, EXPOSING THE CENTER CONDUCTOR. ON THE LT AND RT ENGINE, THE DEFECTIVE WNov 19, 1996 · N87NW · Beech B100 · DC Generating SystemSDR 96ZZZX5978Wire · crackedTHE STARTER/GENERATOR 4 GAUGE WIRES, THAT RUN FROM THE FIREWALL POWER CONNECTOR TO THE STARTER/GENERATOR, WERE FOUND WITH CRACKED INSULATION. THE CRACKS RUN PARALLEL WITH THE WIRE. SOME OF THE CRACKS ARE OVER 3 INCHES IN LENGTH EXPOSING THE CENTER CONDUCTOR.Oct 31, 1996 · N6241P · Beech B100 · DC Generating SystemSDR 96ZZZX5620Wire · crackedTHE STARTER/GENERATOR 4 GAUGE WIRES THAT RUN FROM THE FIREWALL POWER CONNECTOR AND GENERATOR GROUND TO THE STARTER/GENERATOR WERE FOUND WITH CRACKED INSULATION. THE CRACKS RUN PARALLEL WITH THE WIRE. SOME OF THE CRACKS ARE OVER 3 INCHES IN LENGTH EXPOSING THOct 25, 1996 · N1807H · Beech B100 · DC Generating SystemSDR EY2R9600150Bulkhead · crackedPROP ASSY CRACKED BULKHEADOct 1, 1996 · Beech B100 · Propeller AssemblySDR 96ZZZX4172Wire · crackedTHE STARTER/GENERATOR 4-GAUGE WIRES THAT RUN FROM FIREWALL POWER CONNECTOR AND GENERATOR GROUND TO THE STARTER/GENERATOR, WERE FOUND WITH CRACKED INSULATION. THE CRACKS RUN PARALLEL WITH THE WIRE. SOME OF THE CRACKS ARE OVER 3 INCHES IN LENGTH EXPOSING THE CAug 6, 1996 · N300R · Beech B100 · DC Generating SystemSDR 96ZZZX2961Blade · crackedCORPORATE TECHNICIAN NOTICED A FLAW IN BACKSIDE OF A PROPELLER BLADE. UPON FURTHER INSPECTION, FLAW WAS DISCOVERED TO BE A CRACK APPROXIMATELY 3.25 INCHES IN LENGTH, AND 14.3750 INCHES FROM THE TIP OF THE BLADE. CRACK SPAN WIDTHWISE, AND COULD BE SEEN TO OPEMay 17, 1996 · N86TR · Beech B100 · Propeller Blade SectionSDR 96ZZZX1372Skin · crackedFOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 6 INCHES FROM OUTBOARD END WHERE LEADING SKIN AND UPPER SKIN ARE ATTACHED TO SPAR. SUBMITTER STATES THIS IS FOURTH B100 AIRCRAFT WITH CRACKS ON UPPER SKIN. HAVE NOT HAD ANY PROBLEMS ON LT AILERONS.Mar 8, 1996 · N2025S · Beech B100 · AileronsSDR 96ZZZX1363Skin · crackedFOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 12 INCHES FROM INBOARD END WHERE LEADING EDGE SKIN AND UPPER SKIN ARE ATTACHED TO SPAR. SUBMITTER STATED THIS IS THE THIRD AIRCRAFT WITH CRACKS IN THE SAME PLACE.Mar 8, 1996 · N771S · Beech B100 · AileronsSDR CA960311014Skin · corrosion(CAN)AILERON DEVELOPED A CRACK. DURING THE REPAIR, NEW SKINS WERE ORDERED AFTER FINDING HEAVY CORROSION AFTER REMOVING THE SKIN. SUBMITTER STATES THAT THIS COULD NOT BE SEEN FROM THE OUTSIDE.Mar 4, 1996 · Beech B100 · AileronsSDR 96ZZZX1626Brake Assy · frozenCLE - ON TOUCH-DOWN, ACFT DECELLERATED ABRUPTLY AND YAWED TO THE LEFT. DIRECTIONAL CONTROL WAS MAINTAINED WITH OPPOSITE BRAKE AND RIGHT RUDDER. AFTER STOPPING ON THE RUNWAY, THE AIRCRAFT COULD NOT BE TAXIED. FOUND LT BRAKE ASSEMBLIES HAD FROZEN. AMBIENT TEFeb 2, 1996 · N54CK · Beech B100 · Landing Gear Brake SystemSDR 96ZZZX376Intercostal · crackedINTERCOSTAL FOUND CRACKED. THIS PART SUPPORTS CABIN DOOR HAND RAIL AND IF IT FAILS, WILL CAUSE DOOR TO STRIKE THE GROUND. DOOR NEEDS DUAL SUPPORT CABLES TO ELIMINATE THIS PROBLEM.Dec 19, 1995 · N3699B · Beech B100 · Passenger/Crew DoorsSDR 96ZZZX272O-Ring · missingAFTER THE ENGINE WAS REINSTALLED IN LEFT SIDE OF AIRCRAFT AND A GROUND RUN WAS COMPLETED, A FUEL LEAK WAS NOTED AT THE FUEL CONTROL FUEL PUMP MATING SURFACE. UPON DISASSEMBLY, FOUND O-RING WAS NOT INSTALLED. INSTALLED NEW O-RING, AND REASSEMBLED. GROUND RUNNov 6, 1995 · N49E · Beech B100 · Fuel Control/Turbine EnginesSDR 95ZZZX5254Shroud · misinstalledTHE LEFT ENGINE WAS VERY SLOW TO START. INVESTIGATION REVEALED THE FUEL NOZZLE SHROUD WAS INSTALLED 180 DEGREES FROM CORRECT POSITION WHICH BLOCKED FUEL FLOW THROUGH THE NOZZLE CAUSING SLOW STARTS. THE FUEL NOZZLES HAD BEEN REPLACED 291.1 HOURS PREVIOUSLY. Aug 24, 1995 · N524BA · Beech B100 · Fuel Injector NozzleSDR 95ZZZX3940Tube Assy · chafedFAILURE OCCURRED IN-FLIGHT, PILOT NOTICED HIGH FUEL FLOW AND SMOKE. ENGINE SHUT DOWN IN-FLIGHT. FOUND ADEL CLAMP WORN THROUGH TUBE ASSY. ADDED EXTRA ADEL CLAMPS TO AFT END OF TUBE ASSY TO PREVENT MOVEMENT.Jul 17, 1995 · N178NC · Beech B100 · Engine Fuel DistributionSDR 95ZZZX3606Doubler · crackedAT ELEVATOR STATION 124.910, WHERE LEADING EDGE SKIN JOINS EXTENDED BALANCE AREA OF ELEVATOR, JOINER-DOUBLER THAT ATTACHES LEADING EDGE SKIN TO OUTBOARD LEADING EDGE RIB WAS FOUND CRACKED BOTH IN A FORE AND AFT AND ALSO A SIDE-TO-SIDE DIRECTION. BOTH ELEVATORMay 2, 1995 · N87XX · Beech B100 · Elevator, Plate/SkinSDR 95ZZZX2692Hinge Support · elongated holesDURING 150-HOUR INSPECTION, SLIGHT MOVEMENT WAS NOTED AT RIGHT OUTBOARD ELEVATOR HINGE SUPPORT. INSPECTION OF SUPPORT FOR HINGE IN STABILIZER SHOWED SEVERAL IRREGULARITIES IN THE COMPLETION OF AD 87-03-01R1 AND MSB 2132. ELEVATOR WAS REMOVED AND HINGE SUPPORMay 2, 1995 · N87XX · Beech B100 · Horizontal Stabilizer, Spar/RibSDR 95ZZZX1268Governor · arm detachedDURING TAKEOFF, PILOT NOTICED A SURGE AND OVERTEMP FROM LT ENGINE. THE TAKEOFF WAS ABORTED. AFTER INVESTIGATING, FOUND ARM ON THE SPLINED SHAFT OF THE PROP GOVERNOR HAD FALLEN OFF. ALL OF THE SAFETY WIRE AND OTHER LINKAGE ATTACHED TO THE ARM WERE STILL INTAFeb 22, 1995 · N990SV · Beech B100 · Propeller GovernorSDR 95ZZZX972Torque Tube · crackedTORQUE TUBE MOUNT BRACKET WAS CRACKED FROM TAPER PIN HOSE (HEAD SIDE) TO THE END OF PART. TAPER PIN MIGHT HAVE BEEN OVERTORQUED.Feb 1, 1995 · N93SF · Beech B100 · Elevator Control System
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