# Service difficulty reports: Beech A100 A list on [Beech A100](https://openairdocs.org/model/beech-a100.md). Newest first. General aviation reporting is voluntary. Page 1 of 10 · 472 reports - [SDR HXXC2022031422](https://openairdocs.org/sdr/HXXC2022031422.md): Hydraulic Line · corroded · Mar 12, 2022 · N479AK · Beech A100 · Hoses and Tubes > PILOT RH BRAKE FAILED WHILE TAXIING. FOUND 1/4" ALUMINUM LINE BELOW FLOOR CORRODED PIN HOLE. - [SDR 2022FA0000771](https://openairdocs.org/sdr/2022FA0000771.md): Engine · malfunctioned · Jan 29, 2020 · N86NB · Beech A100 · Engine (Turbine/Turboprop) > ON 29TH JANUARY 2020, WHILE IN THE CRUISE AT 16000FT, THE PILOT REPORTED HEARING A INCREASING WHISTLING SOUND FROM THE PORT ENGINE WHICH STARTED STARTED TO LOSE POWER. HE LOOKED OUTSIDE AND NOTICE SPARKS COMING OUT THE EXHAUST AND IMMEDIATELY STARTED THE SHUTD - [SDR CA190822017](https://openairdocs.org/sdr/CA190822017.md): Relay · burned · Jul 25, 2019 · Beech A100 · Trailing Edge Flap Control System > (CAN) AT APPROXIMATELY 9500 FEET IN THE CLIMB, SMOKE WAS NOTICED COMING FROM THE CABIN FLOOR IN THE VICINITY OF THE FLAP MOTOR. THE CREW CARRIED OUT THE APPROPRIATE EMERGENCY PROCEDURES AND LANDED SAFELY. UPON INSPECTION IT WAS FOUND THAT THE FLAP SYSTEM DYNAM - [SDR CA190715014](https://openairdocs.org/sdr/CA190715014.md): Master Link · loose · Jul 12, 2019 · Beech A100 · Landing Gear Retraction/Extension System > (CAN) DURING ROUTINE INSPECTION ON THE NOSE GEAR RETRACT CHAIN A LINK NEEDED TO BE REMOVED. THE MAINTENANCE TECHNICIAN PROCURED A MASTER LINK FROM INVENTORY, DURING INSTALL IT WAS NOTICED THAT ONE OF THE PINS ON THE NEW MASTER LINK WAS NOT CRIMPED PROPERLY TO - [SDR CA190313006](https://openairdocs.org/sdr/CA190313006.md): Shaft · worn · Mar 11, 2019 · Beech A100 · Elevator Control System > (CAN) THE ELEVATOR TORQUE SHAFT ASSEMBLY WAS FOUND TO HAVE PLAY IN ONE OF THE ARMS. THE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. UPON FURTHER INSPECTION IT WAS FOUND THAT THE TAPER PIN INSTALLED IN THE ARM WAS NOT SEATED PROPERLY CAUSING WEAR OF - [SDR CA160205009](https://openairdocs.org/sdr/CA160205009.md): Relay · failed · Feb 3, 2016 · Beech A100 · AC Inverter > (CAN) DURING TAKEOFF, THE NR 1 INVERTER FAILED. NR 2 INVERTER WAS SELECTED BY CREW BUT IT WAS ALSO FAILED. WITH THIS DOUBLE FAILURE CREW LOST MOST OF ENGINES INSTRUMENTS. ACFT LAND BACK IN YVP WITHOUT ANY ISSUES. MAINTENANCE FOUND ANNUNNCIATOR RELAY TO BE F - [SDR CA160129007](https://openairdocs.org/sdr/CA160129007.md): Nut · loose · Jan 29, 2016 · Beech A100 · Starter-Generator > (CAN) DURING A SCHEDULED FUEL PUMP INSPECTION, THE STARTER GENERATOR AS BEEN REMOVED TO GIVE MORE ACCESS TO THE ENGINE FUEL PUMP. THE MECHANIC DISCOVER THAT SOME OF THE STARTER FRONT PLATE RETAINING SCREW WHERE LOOSE. THE STARTER SHAFT HOLDING NUT WAS FOUND - [SDR CA160128002](https://openairdocs.org/sdr/CA160128002.md): Terminal · unsecure · Jan 26, 2016 · Beech A100 · Electrical Power System Wiring > (CAN) WHILE COMPLETING AD CF-1981-25R6, IT WAS WAS NOTED AFTER REMOVING WING PANEL INBOARD OF RT NACELLE, THAT 2 WIRES (P83D0 P83B0) WERE DISCONNECTED FROM THE EXTERNAL POWER TERMINAL STRIP AND BY ARCING, HAD BURNED A HOLE IN THE WING SPAR. A FLEET INSPECTION - [SDR CA160203013](https://openairdocs.org/sdr/CA160203013.md): Oil System · leaking · Jan 17, 2016 · Beech A100 · Turbine Engine Oil System > (CAN) THE AIRCRAFT WAS FORCED TO RETURN TO THE DEPARTURE AIRPORT FOLLOWING THE PRESENCE OF SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY. THE SMOKE IN COCKPIT WAS DUE TO OIL LEAK, FROM THE RT ENGINE, ON A PREVIOUS HSI RUN. THERE WAS A SMALL AMOUNT OF RES - [SDR CA160115001](https://openairdocs.org/sdr/CA160115001.md): Control Panel · burned · Jan 11, 2016 · Beech A100 · Fuel Quantity Indicator > (CAN) AFTER HAVING COMPLETED HIS COCKPIT PRE-FLIGHT CHECKS AND WITH ALL ELECTRICAL POWER TURNED OFF, THE PILOT WENT OUTSIDE AND WAS PERFORMING HIS EXTERNAL ACFT PRE-FLIGHT CHECKS. THE PILOT THEN NOTICED FLAMES IN THE AREA OF THE LT SIDE COCKPIT WINDOW. HE T - [SDR CA160107006](https://openairdocs.org/sdr/CA160107006.md): Support · cracked · Dec 28, 2015 · Beech A100 · Wing, Attach Fittings > (CAN) DURING VISUAL INSPECTION IN THE ELEVATOR TORQUE TUBE AREA, THE RT ELEVATOR TORQUE TUBE SUPPORT WAS FOUND CRACKED. THE TORQUE TUBE AND SUPPORT ASSY WAS REPLACED AND ACFT RETURNED TO SERVICE. - [SDR CA151016003](https://openairdocs.org/sdr/CA151016003.md): Volt Regulator · failed · Oct 13, 2015 · Beech A100 · DC Regulator > (CAN) ON ACFT SHORT COMING IN TESTING PROCEDURES WAS DISCOVERED WHILE FOLLOWING THE MM FOR THE ADJUSTMENT OF THE VOLTAGE REGULATORS FOR THE GENERATORS. WHEN THE ACFT IS EQUIPPED WITH VR-1010-24-1A VOLTAGE REGULATORS AS ALLOWED BY MFG SERVICE INSTRUCTION NR 07 - [SDR CA151009007](https://openairdocs.org/sdr/CA151009007.md): Bolt · cracked · Oct 8, 2015 · Beech A100 · Wing, Attach Fittings > (CAN) DEFECT INDICATIONS WERE NOTED DURING LIQUID PENETRANT INSPECTION OF BOTH FORWARD UPPER AND LOWER WING ATTACHMENT BOLTS ON THE LT AND RT SIDES WHILE COMPLETING INSPECTION REQUIREMENT OF AD CF-81-25-R6. ALL 4 BOLTS, 2 OF PN 81784-14-32 LOWER FWD BOLTS AND - [SDR CA151006005](https://openairdocs.org/sdr/CA151006005.md): Blade · failed · Oct 5, 2015 · Beech A100 · Turbine Section > (CAN) ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER AN IN-FLIGHT SHUTDOWN INCIDENT. THE INCIDENT STARTED WITH A LOUD NOISE FROM THE ENGINE WITH A SUBSEQUENT TORQUE DROP AND INCREASE OF THE ENGINE TEMPERATURE. THE ENGINE WAS SHUTDOWN AND THE FLIGHT WAS CON - [SDR CA150924009](https://openairdocs.org/sdr/CA150924009.md): Altimeter · malfunctioned · Sep 21, 2015 · Beech A100 · Altimeter, Barometric/Encoder > (CAN) IMMEDIATELY UPON BECOMING AIRBORNE, FLIGHT CREW NOTICED THE CAPTAIN`S ALTIMETER HAD FLAGGED AND CONTINUED TO INDICATE FIELD ELEVATION THROUGHOUT THE CLIMB. ATC REPORTED THAT TRANSPONDER MODE C WAS NOT RECEIVED. THE CO-PILOT`S INSTRUMENTS FUNCTIONED NOR - [SDR CA150903008](https://openairdocs.org/sdr/CA150903008.md): Control Cable · corroded · Sep 3, 2015 · Beech A100 · Aileron Tab Control System > (CAN) DURING AND INSPECTION IN THE LT WING ROOT AREA, IT WAS NOTED THAT THE AILERON TRIM AND AILERON PRIMARY CABLES WERE HEAVILY CORRODED. ONLY LITTLE HAND PRESSURE ON THE TRIM CABLE CAUSED THE CABLE TO BREAK DUE TO IT BEING EXTREMELY BRITTLE. FURTHER INVESTIG - [SDR CA150708004](https://openairdocs.org/sdr/CA150708004.md): Bonding Strap · crushed · Jul 4, 2015 · Beech A100 · Trailing Edge Flaps > (CAN) DURING A TRAINING FLIGHT SMOKE WAS OBSERVED IN THE CABIN. AIRCRAFT LANDED, MAINTENANCE FOUND THE FLAPS CIRCUIT BREAKER HAD POPPED AND THE FLAP MOTOR WAS UNSERVICEABLE AND THE CAUSE OF THE SMOKE. IT WAS DISCOVERED THAT THE RIGHT HAND INBOARD FLAP HAD A BO - [SDR CA150618005](https://openairdocs.org/sdr/CA150618005.md): Torque Knee · broken · Jun 11, 2015 · Beech A100 · Main Landing Gear Strut/Axle/Truck > (CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION, ACFT STOPPED THEN TAXIED TO THE RAMP & IT WAS FOUND THAT THE LT MLG, UPPER & LOWER TORQUE LINK WERE FOUND BROKEN OFF AT ATTACH POINT. THE TORQUE LINKS WERE REPLACED. ACFT INSPECTED & RETURNED TO SERVICE. W - [SDR CA150511007](https://openairdocs.org/sdr/CA150511007.md): Torque Link · broken · May 10, 2015 · Beech A100 · Main Landing Gear Strut/Axle/Truck > (CAN) UPON LANDING, PILOT FELT LIKE HE HAD A FLAT. NO FLAT NOTED BUT UPON INSPECTION, IT WAS NOTED THAT THE RT MLG UPPER TORQUE LINK WAS FOUND TO BE BROKEN IN HALF ABOUT ONE INCH FROM THE ATTACH POINT TO THE LOWER TORQUE LINK. SPECIAL INSPECTION HAS BEEN INI - [SDR CA150428006](https://openairdocs.org/sdr/CA150428006.md): Pressure Switch · intermittent · Apr 24, 2015 · Beech A100 · Hydraulic System, Main > (CAN) HYDRAULIC PRESSURE SWITCH INTERMITENT, FOUND DIRTY, LOCATED IN LT WHEEL WELL AREA, CLEANED AND TESTED, RE-INSTALLED AND PERFORMED 18 GEAR CYLCES THROUGHOUT THE DAY, RESPECTING MOTOR COOL DOWN TIMES, IAW SERVICE MANUAL, NO PROBLEMS FOUND. - [SDR CA150417014](https://openairdocs.org/sdr/CA150417014.md): B-Nut · split · Apr 14, 2015 · Beech A100 · Turbine Engine Oil System > (CAN) DURING ROUTINE MAINTENANCE, SOME OIL LOSS, CLEANED AND TUBE B-NUT FOUND SPLIT. - [SDR CA150407007](https://openairdocs.org/sdr/CA150407007.md): Radio · malfunctioned · Mar 31, 2015 · Beech A100 · Communications System > (CAN) CREW HAD A FAILURE OF RADIO`S AND WERE UNABLE TO CONTACT ATC CREW CYCLED AVIONICS MASTER SYS ALL TESTED SERVICEABLE. FLIGHT CONTINUED WITH NO FURTHER PROBLEMS. - [SDR CA150324012](https://openairdocs.org/sdr/CA150324012.md): Tube · dislodged · Mar 24, 2015 · Beech A100 · Propeller Feathering/Reversing > (CAN) THE PILOT OF THE ACFT ABORTED TAKEOFF WHEN HE RECEIVED AN OVERTORQUE INDICATION FROM THE RT ENGINE. WHILE TAXIING BACK TO THE TERMINAL, THE PILOT TRIED TO UNFEATHER THE RT PROPELLER WITHOUT SUCCESS. THE PILOT REPORTED THE DEFECT IN THE ACFT JOURNEY LOG - [SDR CA150217004](https://openairdocs.org/sdr/CA150217004.md): Skin · cracked · Feb 15, 2015 · Beech A100 · Wing, Plate/Skin > (CAN) DURING DAILY INSPECTION, IT WAS NOTICED THAT RT OTBD FLAP HAD DAMAGE TO THE SKIN NEAR THE INBD FLAP TRACK WELL. UPON FURTHER INVESTIGATION, IT WAS ALSO NOTICE THAT THE INBD FLAP TRACK WAS CRACKED IN HALF, SEE PICTURE. A FLEET INSPECTION HAVE BEEN INITI - [SDR CA141219003](https://openairdocs.org/sdr/CA141219003.md): Gearbox · making metal · Dec 17, 2014 · Beech A100 · Turbine Engine Reduction Gear > (CAN) SHORTLY AFTER TAKEOFF, THE LEFT PROPELLER AUTO FEATHERED. THE ENGINE WAS NOT SHUTDOWN AS THE PROP WAS ALREADY FEATHERED. THE CREW LANDED SAFELY. INVESTIGATION BY MAINTENANCE REVEALED SOME METAL CONTAMINATION IN THE RGB OIL STRAINER. THE ENGINE WILL BE - [SDR CA141208007](https://openairdocs.org/sdr/CA141208007.md): Shaft · cracked · Nov 20, 2014 · Beech A100 · Trailing Edge Flap Actuator > (CAN) DETAILED INSPECTION OF BOLTED CONNECTION AT RT INBOUND FLAP ACTUATOR - REVEALED A CRACK- RUNNING FROM THE RIVET HOVE DOWN THE LENGTH OF THE SHAFT APPROX. 1 INCH. AN ENTIRE NEW ACTUATOR WAS INSTALLED. - [SDR CA141014010](https://openairdocs.org/sdr/CA141014010.md): Hinge Bracket · cracked · Oct 11, 2014 · Beech A100 · Horizontal Stabilizer Structure > (CAN) THE RIGHT HAND HORIZONTAL STABILIZER HINGE BRACKET WAS FOUND CRACKED DURING VISUAL INSPECTION. THE INSPECTION WAS BEING COMPLETED DUE TO OTHER COMPANY AIRCRAFT HINGE BRACKETS HAD BEEN RECENTLY FOUND CRACKED DURING SCHEDULED INSPECTION. - [SDR CA141006017](https://openairdocs.org/sdr/CA141006017.md): Bracket · cracked · Oct 6, 2014 · Beech A100 · Horizontal Stabilizer Structure > (CAN) DURING INSPECTION, THE LT HORIZONTAL STABILIZER BRACKET WAS FOUND CRACKED. - [SDR CA141003005](https://openairdocs.org/sdr/CA141003005.md): Torque Knee · cracked · Oct 2, 2014 · Beech A100 · Main Landing Gear > (CAN) DURING REGULAR ACFT INSPECTION, A CRACK WAS FOUND ON THE LT MLG TORQUE KNEE UPPER LINK. - [SDR CA140929006](https://openairdocs.org/sdr/CA140929006.md): Wire · misrouted · Sep 26, 2014 · Beech A100 · Landing Gear System Wiring > (CAN) ON GEAR DOWN SELECTION ON APPROACH, THE CREW EXPERIENCED A DOUBLE GENERATOR FAILURE WHICH LEFT THE GEAR ONLY PARTIALLY EXTENDED. THE GENERATORS WOULD NOT RESET AND THE EMERGENCY LANDING GEAR EXTENSION WOULD NOT EXTEND THE GEAR FURTHER. THE AIRCRAFT LAND - [SDR CA140918002](https://openairdocs.org/sdr/CA140918002.md): Turbine · failed · Sep 17, 2014 · Beech A100 · Turbine Section > (CAN) REPORT EIR PT6A 2014-078, ENGINE WAS SENT FOR REPAIR AFTER THE OPERATOR REPORTED THAT THE ENGINE FAILED IN FLIGHT. THE OPERATOR REPORTED THAT THE PT BLADES WERE MISSING WHEN LOOKING IN THE EXHAUST PORTS AFTER THE FAILURE. - [SDR CA140922012](https://openairdocs.org/sdr/CA140922012.md): Torque Knee · broken · Sep 16, 2014 · Beech A100 · Main Landing Gear > (CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION AND THE AIRCRAFT WANTING TO TURN TO THE RIGHT. AIRCRAFT STOPPED THEN TAXIED TO THE RAMP AND IT WAS FOUND THAT THE RIGHT HAND MAIN LANDING GEAR UPPER TORQUE LINK WAS FOUND BROKEN OFF (SEE PIC) THE TORQUE LINK WA - [SDR CA140904001](https://openairdocs.org/sdr/CA140904001.md): Torque Tube · cracked · Aug 25, 2014 · Beech A100 · Elevator Control System > (CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND COMMING FROM UNDER THE BUSHING ON THE FLANGE THAT ATTACHES TO THE ELEVATOR. (SEE ATTACHED PICS) TUBE REPLACED AND CHECKED SERVICEABLE. - [SDR CA140809001](https://openairdocs.org/sdr/CA140809001.md): Blade · sheared · Aug 7, 2014 · Beech A100 · Turbine Section > (CAN) LEFT ENGINE FAILED IN FLIGHT. POWER TURBINE BLADES FOUND SHEARED, POWER TURBINE GUIDE VANES DAMAGED, ENGINE BEING REMOVED AND SENT TO OVERHAUL SHOP FOR INVESTIGATION. - [SDR CA140716005](https://openairdocs.org/sdr/CA140716005.md): Resistor · burned · Jun 30, 2014 · Beech A100 · Light System Wiring > (CAN) EARLY IN THE INVESTIGATION OF THIS INCIDENT, IT WAS DECIDED THAT THIS DID NOT MEET THE REQUIREMENTS NECESSARY TO SUBMIT AN SDR, HOWEVER WE HAVE CHOSEN TO SUBMIT IT. THREE MINUTES AFTER REACHING CRUSE ALTITUDE (14000 FT), AN ELECTRICAL FIRE ODOR WAS NOTIC - [SDR CA140620012](https://openairdocs.org/sdr/CA140620012.md): Torque Tube · corroded · Jun 19, 2014 · Beech A100 · Elevator Structure > (CAN) TORQUE TUBE FOUND CORRODED AND PUNCTURED. - [SDR CA140530002](https://openairdocs.org/sdr/CA140530002.md): Exciter · failed · May 28, 2014 · Beech A100 · Exciter > (CAN) UNIT FAIL TO PRODUCE SHOWER SPARK TO IGNITER, NO ELECTRICAL POWER OUTPUT. UNIT WAS O/H AT NORMAL TBO 3500 HRS. - [SDR CA140530003](https://openairdocs.org/sdr/CA140530003.md): Exciter · failed · May 27, 2014 · Beech A100 · Exciter > (CAN) UNIT FAIL, NO ELECTRICAL OUTPUT. - [SDR CA140527003](https://openairdocs.org/sdr/CA140527003.md): Washer · damaged · May 23, 2014 · Beech A100 · Nose/Tail Landing Gear Strut/Axle > (CAN) DURING ROUTINE INSPECTION, THE KEY WASHER TO INSTALL THE NOSE WHEEL WAS FOUND ELONGATED AND SPUN, WITH COMPARISON TO NEW WASHER. WASHER WAS REPLACED THREADS ON NOSE GEAR INSPECTED AND RETURNED TO SERVICE. - [SDR CA140521002](https://openairdocs.org/sdr/CA140521002.md): Connector · broken · May 20, 2014 · Beech A100 · Light System Wiring > (CAN) INTERIOR NEON BALLAST, BURNED DUE TO CONNECTOR ALIGNMENT NOTCH MISSING/BROKEN INSIDE OF CONNECTOR. THIS ALLOW CONNECTOR TO MOVE AND CREATE A SHORT. - [SDR CA140505013](https://openairdocs.org/sdr/CA140505013.md): Torque Tube · cracked · Apr 25, 2014 · Beech A100 · Elevator Structure > (CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND. THIS MAY HAVE BEEN THE RESULT OF OVER-TORQUEING THE SCREW ATTACHING THE TUBE TO THE ELEVATOR. TUBE REPLACED AND CHECKED SERVICEABLE. - [SDR CA140602022](https://openairdocs.org/sdr/CA140602022.md): Cap · unsecure · Apr 5, 2014 · Beech A100 · Turbine Engine Oil System > (CAN) THE PILOT REPORTS THAT AT THE SECOND TAKEOFF OF TRAINING JUST AFTER SETTING MAX TAKE-OFF POWER AT ABOUT 40-45 KTS, THEY HEARD A SOUND FROM THE ENGINE THAT IT HAD FALL IDLE. PILOT NOTES FEELING THE ACFT SHIFTING TO THE LT. THE CO-PILOT, PNF, NOTICED THE - [SDR CA140327006](https://openairdocs.org/sdr/CA140327006.md): Downlock · broken · Mar 25, 2014 · Beech A100 · Landing Gear Retraction/Extension System > (CAN) ON TAKEOFF THE LANDING GEAR FAILED TO FULLY RETACT, WHEN THE GEAR WAS EXTENDED THE RT GEAR FAILED TO LOCKDOWN, THE SOP`S WERE FOLLOWED, GEAR EMERGENCY BOTTLE WAS BLOWN BUT THE RT GEAR SLOWLY COLLAPSED ON LANDING. THE DOWN LOCK HOOK WAS FOUND TO BE BROKEN - [SDR CA140305001](https://openairdocs.org/sdr/CA140305001.md): Stator · cracked · Feb 10, 2014 · Beech A100 · Turbine Section > (CAN) THREE CRACKS FOUND ON OUTER RING WHEN INSPECTING BY BORESCOPE IN NOZZLE HOLES PARTS REMOVED FOR OVERHAUL AND REPLACED. - [SDR CA131218006](https://openairdocs.org/sdr/CA131218006.md): Panel · corroded · Dec 17, 2013 · Beech A100 · Fuel Storage > (CAN) WHEN DOING AN INSPECTION, A TECH FOUND A FUEL LEAK UNDER THE RT NACELLE FUEL TANK. CLEAN THE PANEL UNDER THE TANK AND A STREAM OF FUEL START TO FLOW. EMPTIED THE TANK TO REMOVE THAT PANEL AND FOUND THAT THE PANEL WAS SO CORRODED THAT A HOLE PUNCTURED - [SDR CA131129005](https://openairdocs.org/sdr/CA131129005.md): Control Horn · cracked · Nov 28, 2013 · Beech A100 · Elevator Miscellaneous Structure > (CAN) WHILE DOING A PHASE INSPECTION ON THE TAIL SECTION, AN EMPLOYEE FOUND SOME LOOSENESS ON THE LT CONTROL HORN ASSY. THE LT ELEVATOR ASSY HAS BEEN REMOVED TO LOOK AT THE THE BEARING CONDITION. THE BEARING WAS IN GOOD CONDITION AND THE LOOSENESS WAS COMING F - [SDR CA131115001](https://openairdocs.org/sdr/CA131115001.md): Drive Assy · failed · Nov 12, 2013 · Beech A100 · Trailing Edge Flap Control System > (CAN) WHILE BACK TRACKING ON THE RUNWAY, FLAPS WE RETRACTED BY FLIGHT CREW AND SHORTLY AFTER A BURNING ODOR WAS NOTICED IN THE CABIN. THE ACFT RETURNED TO THE APRON AND PASSENGERS WERE DEPLANED. THE FLIGHT CREW VISUALLY NOTED THAT THE RT INBD FLAP WAS IN THE - [SDR CA130925001](https://openairdocs.org/sdr/CA130925001.md): Wire · shorted · Sep 21, 2013 · Beech A100 · Landing Gear System Wiring > (CAN) AFTER EXTENSION OF THE LANDING GEAR THERE WAS NO DOWN INDICATION, 3 GREEN. PILOTS COULD HEAR THE LANDING GEAR EXTEND AND COULD FEEL THE PARASITE DRAG BUT NO INDICATION. PILOTS CONTACTED EMERGENCY SERVICES AND LANDED THE ACFT WITHOUT INCIDENT. MAINTENAN - [SDR CA130920002](https://openairdocs.org/sdr/CA130920002.md): Torque Knee · sheared · Sep 17, 2013 · Beech A100 · Main Landing Gear > (CAN) THE FLIGHT CREW FELT A VIBRATION FROM THE RT MLG UPON LANDING. POST FLIGHT WALK AROUND REVEALED THAT THE UPPER TORQUE KNEE ON THE RT MLG HAD SHEARED. - [SDR CA131103007](https://openairdocs.org/sdr/CA131103007.md): Indicator · failed · Sep 14, 2013 · Beech A100 · Attitude and Direction Data System > (CAN) ON CLIMBOUT THE CREW NOTICED THE RT ATTITUDE GYRO HAD BECOME UNSERVICEABLE. THE FLIGHT CONTINUED WITH OUT INCIDENT TO DESTINATION. MAINTENANCE REPLACED THE GYRO AND THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE. Next page: https://openairdocs.org/model/beech-a100/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 = 'A100' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/beech-a100/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.