Beech A100

Service difficulty reports · 472

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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 = 'A100'
  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 CA111216005Turbine · seized(CAN) DURING CRUISE THE FLIGHT CREW NOTICED A VIBRATION, LOUD NOISE AND SAW GLOWING PARTICLES EXITING THE EXHAUST STACK. THE CREW SHUTDOWN THE LT ENGINE AND LANDED WITHOUT INCIDENT. THE ENGINE HAS BEEN REMOVED AND SENT TO AN O/H SHOP FOR TEARDOWN. NOTE HAVE Dec 14, 2011 · Beech A100 · Turbine SectionSDR CA111121008Static Inverter · failed(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED DURING CRUISE. THE NR 1 STATIC INVERTER BECAME UNSERVICEABLE, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. THE INVERTER WAS R & R, THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.Nov 17, 2011 · Beech A100 · AC InverterSDR CA111116006Flap Track · broken(CAN) FOLLOWING CREW REMARK THAT ACFT WAS TURNING LT SLOWLY IN FLIGHT, ENOUGH TO TRIM. FOUND LT OTBD FLAP INBD TRACK BROKEN AT THE END OF THE FLAP DOWN TRAVEL SLOT ON THE TRACK, SEE PICS. PART WAS REPLACED BY NEW & REMAINING TRACKS ON THAT ACFT INSPECTED FORNov 15, 2011 · Beech A100 · Trailing Edge FlapsSDR CA111118002Seal · leaking(CAN) DURING A MAINTENANCE WALK AROUND AN OIL LEAK WAS FOUND COMING FROM THE FRONT RT ENGINE. FURTHER INSPECTION INDICATED THAT THE PROPELLER SHAFT SEAL HAD FAILED. THE SEAL WAS REPLACED, THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.Nov 10, 2011 · Beech A100 · Turbine Engine Oil SystemSDR CA111118001Motor · failed(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED DURING THE APPROACH THE FLAP SYS BECAME UNSERVICEABLE BEING STUCK AT APPROACH, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. MAINTENANCE DISCOVERED THE FLAP MOTOR WAS HOT AND SMELLED BURNED. THE MOTOR WAS Nov 9, 2011 · Beech A100 · Trailing Edge Flap Control SystemSDR CA111117029Indicator · failed(CAN) DURING A ROUTINE FLIGHT IT WAS NOTED DURING THE DESCENT AND APPROACH THAT THE CO-PILOT ATTITUDE INDICATOR BECAME UNSERVICEABLE. THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. AN AVIONICS REPAIR SHOP WAS CONTRACTED VIA P/O TO REPAIR UNIT HOWEVERNov 9, 2011 · Beech A100 · Attitude Gyro and Indicating SystemSDR CA111108004Channel · cracked(CAN) UPON SERVICING ACFT FOR NEXT FLIGHT, MAIN CABIN DOOR LAST AFT 6" OF HINGE AREA FOUND MOVING DOWN WHEN STEPPING ON LOWER STEP. FURTHER INSPECTION FOUND LOWER (WHEN CLOSED) DOOR CHANNEL CRACKED 6" LONG FROM AFT END FORWARD AND DOOR SIDE HALF HINGE BROKEN Nov 7, 2011 · Beech A100 · Passenger/Crew DoorsSDR CA111117028Gyro · failed(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED DURING THE DESCENT AND APPROACH THE CO-PILOT ATTITUDE INDICATOR BECAME UNSERVICEABLE, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. R & R THE FAULTED INSTRUMENT, THE SYS WAS GROUND FUNCTION CHECKED SERVICOct 24, 2011 · Beech A100 · Attitude Gyro and Indicating SystemSDR CA111117027Relay · faulted(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED THE PROPELLER HEAT WAS INTERMITTENT IN NORMAL MODE AND WAS UNSERVICEABLE IN STAND-BY MODE, THE FLIGHT CONTINUED WITHOUT COMPLICATIONS. MAINTENANCE FOUND A FAULTY PROPELLER HEAT CONTROL RELAY, IT WAS R & R, THE SYS GSep 25, 2011 · Beech A100 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA110623009Door Frame · crackedDURING 3000 CYCLE AIRFRAME INSPECTION, MX CREWS FOUND CRACKS ON AFT PASSENGER DOOR FRAME, PN 50-430043-865 FROM LOWER AFT LOCKING PIN TO THE PIN MOUNTING SCREWS. DOOR WAS REMOVED AND DISASSEMBLED. CRACKS WERE ALSO FOUND AT THE LOWER HINGE ATTACH CHANNEL PN 50Jun 22, 2011 · Beech A100 · Fuselage Main, StructureSDR CA110623008Stringer · crackedDURING 3000 CYCLE INSPECTION ON ACFT, MX CREWS FOUND A CRACK ON THE NR 10 STRINGER ON RT SIDE AT ZEE CHANNEL ATTACH AFT OF REAR PRESSURE BULKHEAD. AN APPROVED REPAIR WAS CARRIED OUT.Jun 22, 2011 · Beech A100 · Fuselage Main, Longeron/StringerSDR CA110617009Bolt · crackedLOWER FOREWARD LT WING BOLT FOUND CRACKED DURING INSP SIRM 57-16-01, ITEM 10. THE AVIA DESIGN FRONT WING KIT IS INSTALLED ON THIS ACFT. TOTAL TIME ON THIS BOLT IS 12331.0 HOURS AND 12 YEARS, LIFE LIMIT ON THIS BOLT IS 15000 HOURS OR 15 YEARS.Jun 17, 2011 · Beech A100 · Wing StructureSDR CA110412001Actuator · failed(CAN) DURING CLIMB AT APPROXIMATELY 13000 FT, CREW NOTICED SMOKE COMING UP FROM THE FLOOR IN THE CABIN. THE CAPTAIN REACHED FOR THE FLAP MOTOR CIRCUIT BREAKER BUT OBSERVED IT WAS ALREADY OUT. THE CREW RETURNED TO THE AIRPORT OF DEPARTURE. DURING THE DESCENT Mar 23, 2011 · Beech A100 · Trailing Edge Flap ActuatorSDR CA110303005Circuit Board · smoke(CAN) DURING A WALK AROUND, THE PILOT TURNED ON THE COCKPIT LIGHTS. SMOKE WAS EMITTED FROM THE PEDESTAL, BATTERY POWER WAS TURNED OFF. MAINTENANCE INVESTIGATED AND FOUND THAT THE SMOKE WAS CAUSED BY A BURNED WHEAT, BULB, PN D158/-100-5T1 ON THE PITCH TRIM LIGMar 1, 2011 · Beech A100 · Flight Control System WiringSDR CA110207005Gps · failed(CAN) THE AIRCRAFT WAS ON A ROUTINE TRIP FROM YXD TO EZ4 WHEN THE GPS SCREEN WHENT BLANK. THE CREW CONTINUED WITH OUT INCODENT, THE UNIT WAS REPLACED AND THE DEFECT RECTIFIED.Feb 2, 2011 · Beech A100 · Global Positioning SystemSDR CA101229008Flapper Valve · dislodged(CAN) DURING A TEST FLIGHT TO TEST THE RH FLOW PACK WHILE CLIMBING OUT THROUGH 5000 FEET, THERE WAS A SCREAM IN THE CABIN. MAINTENANCE PERFORMED AN INSPECTION OF THE PRESSURIZATION DUCTING INSIDE THE CABIN AND FOUND THAT A FLAPPER VALVE HAD DISLODGED ITSELF IDec 28, 2010 · Beech A100 · Air Distribution SystemSDR CA101229007Control Valve · failed(CAN) DURING A ROUTINE FLIGHT, THE CREW NOTED THE THE CABIN PRESSURE WAS RAPIDLY INCREASING, THE CREW IMMEDIATELY DEPLOYED OXYGEN, INITIATED A DESCENT, DEPRESSURIZED THE CABIN AND DIVERTED TO BASE (WHERE PRIMARY MAINTENANCE IS ADMINISTERED). MAINTENANCE PREFDec 26, 2010 · Beech A100 · Air Distribution SystemSDR CA110105001Gear · wornMAINTENANCE COMPLETED A SCHEDULED STARTER GENERATOR SPLINE WEAR INSPECTION AND FOUND THE STARTER DRIVE GEAR ON THE ENGINE WORN TO LIMITS, GEAR REPLACE AND ENGINE RETURNED TO SERVICE.Dec 24, 2010 · Beech A100 · Engine StarterSDR CA101218001Starter Gen · failed(CAN) PILOT REPORTED DURING LT ENGINE START THE ENGINE HUNG ONCE AT 40% N1. SECOND START WAS SUCCESSFUL BUT THE GENERATOR WOULD NO COME ON LINE WHEN ENGINE STABILIZED AT 60 %. STARTER/GENERATOR WAS REMOVED AND REPLACED WITH OUT FURTHER INCODENT.Dec 17, 2010 · Beech A100 · Starter-GeneratorSDR CA101213009Limit Switch · malfunctioned(CAN) ON APPROCH, THE PILOTS SELECTED APPROACH FLAP. THE FLAPS DID A UNCOMANDED TRAVEL TO FULL FLAP. THE AIRCRAFT WAS LANDED WITH OUT INCIDENT. A SPECIAL INSPECTION WAS CARRIED OUT AS PER 27-50-00 ON THE STRUCTURE AND THE COMPONENTS, NO DEFECT FOUND. THE APPDec 11, 2010 · Beech A100 · Trailing Edge Flap Control SystemSDR CA101213014Chain · separated(CAN) NOSE LANDING GEAR FAILED TO EXTEND WHEN SELECTED, NOSE GEAR STOPPED APPROX. AT HALF EXTENSION, LT & RT MAIN GEAR DOWN AND LOCKED, AT TOUCH DOWN NOSE GEAR COLLAPSED. FAILURE CAUSE BY AFT NOSE GEAR DRIVE CHAIN FAILURE P/N 50-820010-17 THE WRITER WILL CONTIDec 10, 2010 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA101209006Limit Switch · malfunctioned(CAN) WHEN THE AIRCRAFT COMENCES TAXI THROUGH LOOSE SNOW AND THE FLAPS ARE DOWN 9 TIMES OUT OF 10 THE FLAP LIMIT SWITCHES FREEZE DUE TO SNOW THAT BURBLES UP INTO THE FLAP WELL. THIS HAPPENS BEACAUSE THE FLAP LIMIT SWITCHES ARE EXPOSED TO THE ELEMENTS. WHEN THEDec 9, 2010 · Beech A100 · Trailing Edge Flap Control SystemSDR CA101222004Support Bracket · cracked(CAN) ON CONDUCTING NDT LPI INSPECTION IAW S/B 2145, THE SUPPORT BRACKET AND WAS FOUND TO BE CRACKED AT TAPER PIN HOLE, NUT END.Dec 8, 2010 · Beech A100 · Rudder StructureSDR CA110105015Door · unsecureDURING FLIGHT, A LOAD BANG WAS HEARD AND THE CABIN RAPIDLY DEPRESSURIZED. THE PILOT DESCENDED AND DECLARED AN EMERGENCY (THE DOOR BLEW OPEN). THE PILOTS LANDED WITH OUT INJURY OR INCIDENT. INSPECTION OF THE DOOR AND ALL OF ITS COMPONENTS REVEALED THAT THE DNov 23, 2010 · Beech A100 · Passenger/Crew DoorsSDR CA101123003Actuator · intermittent(CAN) SHORTLY AFTER TAKEOFF, THE MAIN (ELEVATOR) TRIM WOULD NOT TRIM IN THE NOSE DOWN DIRECTION, BOTH THE CAPTAINS OR CO-PILOTS TRIM CONTROL SWITCHES WERE TRIED WITHOUT SUCCESS. STANDBY TRIM WAS SELECTED AND THIS SYSTEM WAS FOUND TO BE INTERMITTENT. MAINTENANov 20, 2010 · Beech A100 · Elevator Tab Control SystemSDR CA101119004Actuator · failed(CAN) ON APPROACH FLIGHT CREW SELECTED FLAPS AND NOTICED THAT AIRCRAFT HAD MORE LIFT ON THE RIGHT WING THAN ON THE LEFT. AILERON CONTROL WAS APPLIED TO CONTROL AIRCRAFT AND LANDING WAS CONTINUED. AFTER SHUT DOWN CREW CHECKED AIRCRAFT AND FOUND THAT LEFT INBONov 17, 2010 · Beech A100 · Trailing Edge Flap ActuatorSDR CA101112005Torque Tube · cracked(CAN) ELEVATORS WERE REMOVED TO CARRY OUT MANDATORY SERVICE BULLETIN 2145 INSPECTION/REPLACEMENT OF ELEVATOR TORQUE TUBE. NDT COMPANY CARRIED OUT FLUORESCENT LIQUID PENETRANT INSPECTION ON LEFT AND RIGHT TORQUE TUBE ASSYS P/N 115-610010-325. THEY FOUNDED A CNov 10, 2010 · Beech A100 · Elevator Control SystemSDR CA101103006Door Frame · cracked(CAN) CABIN DOOR AFT FRAME CRACKED AT UPPER LOCK BAYONNET (WHEN DOOR CLOSED). CABIN DOOR FWD FRAME CRACKED AT LOWER LOCK BAYONNET (WHEN DOOR CLOSED).Nov 2, 2010 · Beech A100 · Fuselage Main, StructureSDR CA101108007Door · open(CAN) DURING CRUISE THE LT WING LOCKER DOOR CAME OPEN AND DEPARTED. COULD NOT DETERMINE WHY THE DOOR SEPARATED AS THE DOOR COULD NOT BE FOUND. THE WING LOCKER WERE REMOVED AND AIRCRAFT PUT INTO ORIGINAL CONFIGURATION. NACELLE WING LOCKER SYSTEM (BAGGAGE AREOct 21, 2010 · Beech A100 · DoorsSDR CA101230007Filter · obstructedON CLIMB OUT ON A MEDIVAC FLIGHT (FLIGHT PLANNED ROUTE FOR FL 140), THE PRESSURIZATION FAILED AT 70 AST. PILOT REQUESTED FL 100 (NEW FLIGHT PLANNED ROUTE) AND THE FLIGHT CONTINUED WITHOUT INCIDENT. EXTERNAL FILTER ON THE CONTROLLER WAS FOUND TO BE PLUGGED. Oct 12, 2010 · Beech A100 · Cabin Pressure ControllerSDR CA101109008Skin · cracked(CAN) ON WING CENTER SECTION P/N 99-120000-603 SKINS 50-120068-96 LT AND 97 RT WERE CRACKED AT UPPER FEW WING ATTACH FITTINGS.Sep 23, 2010 · Beech A100 · Wing, Plate/SkinSDR CA100826002Torque Tube · crackedTHE ACFT WAS UNDER A PHASE 4 INSP, THE HORIZ ATTACHMEMT POINT SPECIAL WAS CARRIED OUT AT THIS TIME. THE ELEVATOR TORQUE TUBES WERE ALSO INSPECTED, A CRACK WAS FOUND ON THE INNER CASTING.Aug 25, 2010 · Beech A100 · Elevator StructureSDR CA110105016Gyro · unserviceableDURING A FLIGHT THE CO-PILOT HORIZONTAL GYRO FLAGGED AND BECAME UNSERVICEABLE. THE INSTRUMENT WAS REPLACED WITH OVERHAULED WITHOUT FURTHER INCIDENT.Aug 23, 2010 · Beech A100 · Directional Gyro and Indicating SystemSDR CA100826004Support Bracket · crackedDURING PHASE/STAB ATTACH POINT INSP, TAIL CONE WAS REMOVED. LT ELEVATOR TORQUE TUBE SUPPORT BRACKET WAS FOUND CRACKED AT ONE OF THE TAPER PIN HOLES.Aug 23, 2010 · Beech A100 · Elevator StructureSDR CA100819006Hinge Bracket · crackedDURING INSP, IT WAS NOTICED THAT THERE WERE LOOSE/SMOKING RIVETS ON THE AFT PART OF THE CABIN DOOR AT THE HINGE LOCATION. THE HINGE WAS REMOVED AND THE DOOR WAS FOUND TO BE CRACKED ACROSS THE RIVET HOLES OF THE HINGE SUPPORT. THE CRACK STARTED AT THE AFT ENDAug 11, 2010 · Beech A100 · Passenger/Crew DoorsSDR CA100809016Hub · leaking(CAN) PROPELLER INSTALLED AFTER O/H. FIRST FLIGHT RED OIL/DYE LEAKING FROM HUB. RETURNED PROP TO REPAIR STATION FOR REPAIR. PROP REINSTALLED AFTER REPAIR AND CHECKED SERVICEABLE.Aug 5, 2010 · Beech A100 · Propeller Hub SectionSDR CA100809015Motor · failed(CAN) ON TAXI IN FROM LANDING, IT WAS OBSERVED BY THE RAMP ATTENDANT THAT SMOKE WAS COMING FROM THE NOSE OF THE AIRCRAFT. THE AIRCRAFT WAS SHUTDOWN NORMALLY. THE CAPTAIN EXITED THE AIRCRAFT AND DISCONNECTED THE BATTERY. FURTHER INSPECTION INDICATED THAT THEAug 5, 2010 · Beech A100 · Cabin Cooling SystemSDR CA100809012Carbon Seal · leaking(CAN) UPON A WALK AROUND INSPECTION IT WAS NOTICES THAT FUEL WAS DRIPPING FROM THE RT ENGINE FURTHER INSPECTION REVEALED THAT THE FUEL IN QUESTION WAS COMING FROM THE CASE DRAIN ON THE HP FUEL PUMP. THE FUEL PUMP AND FCU WERE REPLACED AND THE PROBLEM CORRECTEJul 27, 2010 · Beech A100 · Engine Fuel PumpSDR CA100728001Control Cable · wornDURING A SPECIAL INSP, THE ENGINE IDLE CABLE, BOTH THE LT AND RT CABLES WERE FOUND TO HAVE EXCESSIVE PLAY IN THE SWAGED END (THE ENGINE END). THE CABLES WERE REPLACED (LT PN 99-380005-21 AND RT PN 99-380005-3) AND ACFT RETURNED TO SERVICE. THIS SPECIAL INSP WJul 26, 2010 · Beech A100 · Power LeverSDR CA100809017Bellcrank · failed(CAN) DURING A PHASE INSPECTION THE DOOR LATCHES WERE OBSERVED NOT TO BE WORKING CORRECTLY. FURTHER INSPECTION REVEALED THE BELLCRANK HAD FAILED RESULTING IN IMPROPER TRAVEL OF THE UPPER DOOR HOOKS. THE BELLCRANK WAS REPLACED WITH NEW.Jul 22, 2010 · Beech A100 · Passenger/Crew DoorsSDR CA100726016Control Cable · loose(CAN) DURING A SPECIAL INSP, THE RT ENGINE IDLE CABLE WAS FOUND TO HAVE EXCESSIVE PLAY IN THE SWAGED END (THE ENGINE END). THE CABLE WAS REPLACED AND ACFT RETURNED TO SERVICE. THIS SPECIAL INSP WAS COMPLETED DUE TO HAVING FOUND A FAILED CABLE ON THE LT ENGINEJul 19, 2010 · Beech A100 · Power LeverSDR CA100809014Drive Gear · failed(CAN) ON ENGINE START CYCLE RT, NG CLIMBED NORMALLY TILL APPROX 14 PERCENT THEN DECLINED RAPIDLY. FURTHER INSPECTION REVEALED THE SPLINE DRIVE INSIDE THE DRIVE GEAR HAD STRIPPED OUT CAUSING THE STARTER/GENERATOR TO BECOME UNCOUPLED FROM THE GAS GENERATOR SECTJun 24, 2010 · Beech A100 · Starter-GeneratorSDR CA100617010Cable Assy · separatedAFTER LANDING, THE CREW WAS UNABLE TO SHUTDOWN LT ENGINE USING THE NORMAL PROCEDURES, THE CONDITION LEVER HAD NO EFFECT ON THE ENGINE. THE ENGINE WAS SHUTDOWN USING THE FIREWALL SHUT OFF. WHEN MX INVESTIGATED, IT WAS FOUND THAT THE SWAGED END OF THE LT ENGINEJun 14, 2010 · Beech A100 · Power LeverSDR CA100218014Yoke · damaged(CAN) DURING INSP, PLAY WAS FOUND WHERE THE NLG ACTUATOR ATTACHES TO THE YOKE IN THE DRAG BRACE ASSY. WHEN THE ACTUATOR WAS REMOVED FROM THE YOKE, IT WAS DISCOVERED THAT THE HOLE IN THE YOKE FOR THE ACTUATOR ATTACH BOLT (PN AN24-23A) WAS DRILLED TOO LARGE. THFeb 18, 2010 · Beech A100 · Landing Gear ActuatorSDR CA100224010Indicator · fluctuates(CAN) DURING THE RECTIFICATION OF THE RT FUEL GAUGE INTERMITTENT FLUCTUATING, 2 FUEL QTY INDICATOR (PN 100-380006-47) FAILED ON INSTALL. THE FIRST INDICATOR (SN 7127M) WAS INSTALLED, THE ACFT WAS POWERED AND THE GAUGE PEGGED FULL. UNABLE TO MAKE ANY ADJUSTMEFeb 4, 2010 · Beech A100 · Fuel Quantity IndicatorSDR CA100204009Starter Gen · failed(CAN) DURING A TRAINING FLIGHT, THE NR2 ENGINE WAS SHUTDOWN. FOLLOWING MOMENTS REVEALED THAT THE NR1 ENGINE GENERATOR WAS FAILED. 1 BATTERY START OF NR2 ENGINE WAS TRIED WITH NO SUCCESS. DUE TO COMPLETE ELECTRICAL POWER FAILURE, THE CREW SUCCEEDED TO CONTACT AFeb 1, 2010 · Beech A100 · Starter-GeneratorSDR CA100208005Fitting · worn(CAN) DURING REMOVAL OF THE ENGINE MOUNT FROM THE NACELLE THE LOWER MOUNT ATTACHMENT FITTINGS WERE FOUND LOOSE INSIDE THE NACELLE ON BOTH THE LT & RT SIDES. THE LT INBD AND OTBD LOWER FITTINGS WERE REPAIRED BY REMOVING THE FITTINGS NDT REINSTALLING THEN DRILLIJan 29, 2010 · Beech A100 · Nacelle/Pylon, Attach FittingsSDR CA100208004Stringer · cracked(CAN) 2 CRACKED STRINGERS ON REAR PRESSURE BULKHEAD FOUND CRACKED. STRINGERS REPLACED. (TC 20100208004)Jan 29, 2010 · Beech A100 · Fuselage Main, Longeron/StringerSDR CA100208003Keelbeam · cracked(CAN) CRACKS FOUND IN THE LT & RT WHEEL WELL ON THE OTBD KEEL RIB. REPAIR ANGLES INSTALLED IAW MFG FIELD REPAIR NR FR-KA-03216. (TC 20100208003)Jan 29, 2010 · Beech A100 · Fuselage Main, KeelSDR CA100208002Frame · cracked(CAN) RT LOWER FUSELAGE FRAME AT STATION 207 FOUND CRACKED. FRAME REPLACED. (TC 20100208002)Jan 29, 2010 · Beech A100 · Fuselage Main, Frame
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