Beech A100

Service difficulty reports · 472

Newest first. General aviation reporting is voluntary.

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 CA010628047Harness · mismanufactured(CAN) AFTER A FALSE FIRE WARNING. ENGINE WAS SHUTDOWN. WHILE TROUBLESHOOTING. FOUND POWER FOR AUTO IGNITION SYSTEM WAS BLEEDING THROUGH WET WIRE INSULATION & INTO FIRE DETECT SYSTEM THROUGH IT'S WIRE INSULATION. THIS TOOK PLACE IN MAIN WIRE BUNDLE FOR RT ENG.May 28, 2001 · Beech A100 · Fire DetectionSDR CA010629019Fuel Control · failed(CAN) RT POWER LEVER IS VERY DIFFICULT TO SCHEDULE SUBTLE POWER CHANGES. IE. WHEN ATTEPTING TO SELECT A CHANGE OF 100 FT/LBS RESULTING TORQUE CHANGE COULD BE AS MUCH AS 400FT/LBS. THIS RESULTS IN AN OSCILLATION OF POWER LEVER MOVEMENT TO GET DESIRED POWER OUTPApr 26, 2001 · Beech A100 · Fuel Control/Turbine EnginesSDR CA010508007Fire Detector · shorted(CAN) DURING DESCENT NR 1 ENG FIRE INDICATION ILLUMINATED. ENGINE WAS SHUT DOWN. INSPECTION DETERMINED NO ACTUAL FIRE. THE ERRONEOUS FIRE INDICATION COULD NOT BE DUPLICATED ON GROUND. BASED ON PREVIOUS TROUBLE SHOOTING ALL THE WIRING FOR THE FIRE DETECTIONS WAApr 18, 2001 · Beech A100 · Fire DetectionSDR 20010419CW015Tube · puncturedINSTALL BLEED AIR TUBE IN LEFT WING CENTER SECTION. USING ICE PICK ON SUSPECT COROSION BLISTERS, TUBE COULD BE PUNCTURED EASILY. TUBE REMOVED FOR REPLACEMENT, 1 PIN HOLE ON TOP OF TUBE. HOLES LOCATED 8 TO 9 INCHES INBOARD OF COUPLING HOSE END OF TUBE.Mar 16, 2001 · N38P · Beech A100 · Engine Bleed Air SystemSDR CA010323019Wheel · cracked(CAN) RT INBOARD WHEEL WAS REMOVED FOR A ROUTINE TIRE CHANGE. UPON DISASSEMBLY IT WAS NOTICED THAT THERE WAS A 4 - 5 INCH CRACK IN THE BEAD AREA. THE RIM WAS BENT AND DEFORMED IN THIS AREA. THERE ARE NO INDICATIONS OF A STRIKE WITH A GROUND OBJECT YET THE CRACMar 15, 2001 · Beech A100 · Wheel/Ski/FloatSDR CA010402002Bearing · corroded(CAN) DURING ROUTINE INSPECTION IT WAS NOTICED THAT THE LANDING GEAR WAS SLOW TO RETRACT. UPON FURTHER INSPECTION THE BEARING SUPPORTING THE RT DRIVE SHAFT WAS FOUND CORRODED AND STIFF. THIS BEARING ALSO CAUSED THE GEAR MOTOR TO BECOME WEAK AND NEEDED TO BE Mar 14, 2001 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA001228021Downlock Switch · failed(CAN) ON APPROACH, GEAR SELECTED DOWN, NOSE WHEEL LIGHT DID NOT ILLUMINATE. CHECKED BULB AND CYCLED GEAR AGAIN WITH NO SUCCESS. LIGHT EVENTUALLY ILLUMINATED BY ITSELF. MAINTENANCE REPLACED WIRES AND TERMINAL LUGS ON NOSE LIGHT SOCKET, CLEANED DOWN LOCK SWITCH,Nov 22, 2000 · Beech A100 · Landing Gear Position and WarningSDR CA001030006Fitting · cracked(CAN) CRACK IS FROM THE FORWARD I/B SPAR CAP TO FITTING RIVET AND GOES TO THE EDGE OF THE FITTING. THE CRACK WAS DISCOVERED DURING A SCHEDULED WING INSPECTION. CRACK WAS VERIFIED USING LEVEL 2 PENETRANT.Oct 16, 2000 · Beech A100 · Wing, Attach FittingsSDR CA001017008Wheel · cracked(CAN) DURING A ROUTINE INSPECTION MAINTENANCE NOTICED A CRACK IN THE PAINT IN THE BEAD AREA. AREA WAS CLEANED WITH A LIQUID DYE PEN INSPECTION FOUND A 2.5 INCH CRACK FOLLOWING THE CIRCUMFERENCE. WHEEL ASSEMBLY WAS REPLACED.Sep 23, 2000 · Beech A100 · Wheel/Ski/FloatSDR CA001018003Spring · broken(CAN) DURING UNSCHEDULED MAINTENANCE, BOTH LT AND RT RUDDER RETURN SPRINGS WERE FOUND BROKEN. NO FLIGHT CONTROL PROBLEMS WERE REPORTED FROM THE FLIGHT CREW. THE SPRINGS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THESE RETURN SPRINGS ARE AN IMPROVED Sep 15, 2000 · Beech A100 · Rudder StructureSDR CA000927012Washer · failed(CAN) WHILE REASSEMBLING THE WING FOLLOWING INSPECTION IN ACCORDANCE WITH CF-81-25R5, A NEW PRELOAD INDICATING WASHER ASSY INSTALLED ON THE LT LOWER FORWARD WING BOLT INDICATED THE BOLT WAS TORQUED AT AN ABNORMALLY LOW TORQUE. THE BOLT WAS UNDONE AND THE WASHESep 3, 2000 · Beech A100 · Wing, Attach FittingsSDR CA000928028Connector · loose(CAN) AIRCRAFT WAS UNABLE TO TRANSMIT ON ANY OF THE 3 COMMS. MAINTENANCE DISCOVERED THE CONNECTOR TO BACK OF THE RADIO RACK LOOSE. THE CONNECTOR WAS CONNECTED, COMMS TESTED, AND THE AIRCRAFT RETURNED TO SERVICE. AVIONICS HAS ADVISED THAT THESE CONNECTORS CAN BAug 26, 2000 · Beech A100 · VHF Communications SystemSDR CA000928027Line · broken(CAN) DURING CLIMB LT BLEED AIR LIGHT ILLUMINTED INDICATING BLEED AIR FAILURE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE DISCOVERED THE SENSE LINE HAD BROKEN OFF A CONNECTION. THE SENSE LINE WAS RE-ATTACHED A GROUND RUN WAS CONDUCTED AAug 24, 2000 · Beech A100 · Pneumatic Indicating SystemSDR CA000907011Connector · dirty(CAN) AIRCRAFT RETURNED BACK TO BASE DUE TO HIGH OIL TEMP ON R/H ENGINE. OIL TEMP BULB CONNECTOR FOUND TO BE DIRTY. CONNECTOR CLEANED AND SYSTEM CHECKED SERVICEABLE.Aug 22, 2000 · Beech A100 · Engine Oil TemperatureSDR 20000712SH001Vent Line · failedOPERATIONAL CHECKS AT INSPECTION INTERVALS TYPICALLY FIND THE VENT HEATS INOPERATIVE DUE TO THE ELECTRICAL CONNECTION ON THE TUBE ITSELF. USING A PROBE AND INSERTING IN THE HOLE WHERE THE HEATING COIL TERMINATES PRODUCES A SPARK AND THEN THE COIL WILL HEAT PRJul 12, 2000 · N102FG · Beech A100 · Aircraft Fuel SystemSDR CA000712024Fitting · cracked(CAN) CRACKED AT RADIUS OF WING ROOT ATTACH FLANGE ON FORWARD SIDE OF FITTING. SLOT AREA.Jul 4, 2000 · Beech A100 · Wing, Fuselage Attach FittingsSDR CA000614036Wire · broken(CAN) AIRCRAFT DEPARTED AND SHORTLY AFTER TAKEOFF, THE MAIN STABILIZER TRIM FAILED. AIRCRAFT RETURNED TO BASE. A WIRE WAS FOUND BROKEN ON THE COPILOT''''S SIDE WHERE THE WIRE GOES THROUGH THE DASH. WIRE REPAIRED AND AIRCRAFT RELEASED TO SERVICE.Jun 14, 2000 · Beech A100 · Stabilizer Control SystemSDR CA000719030Clamp · failed(CAN) DURING A COMPANY TRAINING FLIGHT, THE LT BLEED AIR FAIL ANNUNCIATOR LIGHT (RED) ILLUMINATED. A S PER PROCEDURES, THE LT BLEED AIR SWITCH WAS SELECTED TO THE OFF POSITION. A VISUAL MEANS TO ASCERTAIN THE VALVE IS WORKING IS WHEN SELECTED TO OFF, A SLIGHTJun 7, 2000 · Beech A100 · Air Distribution SystemSDR CA000530043Wire · loose(CAN) GEAR WAS SELECTED UP AND THE GEAR WOULD NOT RETRACT. THE SELECTION WAS TRIED SEVERAL TIMES AND FINALLY RETRACTED.A LOOSE WIRE WAS FOUND ON THE EMERGENCY EXTENSION MICROSWITCH LOCATED BY THE GEAR TRANSMISSION. THE CONNECTION WAS RESECURED.May 17, 2000 · Beech A100 · Landing Gear System WiringSDR CA000530032Tach Generator · failed(CAN) WHILE IN CRUISE, THE RT PROPELLER INDICATION WENT TO ZERO. NO ACTION WAS TAKEN, AIRCRAFT WAS RETURNING TO BASE. MAINTENANCE REMOVED TACH GENERATOR AND FOUND DRIVESHAFT ROUNDED OFF. NEW TACH GENERATOR INSTALLED.May 17, 2000 · Beech A100 · Propeller Indication SystemSDR CA000518015Switch · loose(CAN) DURING CLIMB, THE GEAR WAS SELECTED UP AND THE GEAR DID NOT RETRACT. THE SELECTION WAS ATTEMPTED SEVERAL TIMES WITH THE GEAR RETRACTING ON THE LAST SELECTION. MAINTENANCE FOUND A LOOSE WIRE ON THE EMERGENCY EXTENSION MICROSWITCH LOCATED BY THE GEAR TRANMay 17, 2000 · Beech A100 · Landing Gear Position and WarningSDR CA000511019Bracket · cracked(CAN) CRACK FOUND DURING INSPECTION IN WEBBING. SUBMITTER STATED THIS IS A COMMON AREA FOR CRACKING WITH THE UNITS.May 10, 2000 · Beech A100 · Horizontal Stabilizer StructureSDR CA000511018Wire · loose(CAN) AIRCRAFT RETURNED WITH GEAR IN-TRANSIT LIGHT. AFTER NUMEROUS GEAR SWINGS IT WAS DISCOVERED THAT THE WIRE WAS LOOSE WHERE IT IS ATTACHED TO THE EMERGENCY GEAR EXTENTION MICRO-SWITCH.THIS SWITCH CUTS POWER SO THAT WHEN THE EMERGENCY SYSTEM IS USED THERE IMay 10, 2000 · Beech A100 · Landing Gear System WiringSDR CA000427017Panel · corroded(CAN) DURING THE COMPLETION OF THE DEPARTMENTS CAMPAIGN NOTICE FOR CORROSION INSPECTION OF INTEGRAL FUEL TANKS, FASTENERS & THREAD INSERTS IN THE ACCESS PANELS IT WAS DISCOVERED THAT SOME WERE BADLY CORRODED. CORROSION WAS ALSO DISCOVERED ON THE ACCESS PANELS Apr 7, 2000 · Beech A100 · Wing, Plate/SkinSDR CA000410022Switch · intermittent(CAN) FLAP DOWN SWITCH INTERMITTANT.WHEN SWITCH WAS SHAKEN YOU COULD HEAR LOOSE PART(S) IN SWITCH.SWITCH REPLACED.Apr 5, 2000 · Beech A100 · Trailing Edge Flap Control SystemSDR CA000329012Switch · faulty(CAN) PILOT REPORTED LANDING GEAR UNSAFE LIGHT ON HANDLE WOULD NOT EXTINGUISH. LANDING GEAR POSITION SWITCH ON MOTOR ADJUSTED. PROBLEM RECURRED WITH INDICATION LIGHT NOW BEING INTERMITTANT. DISCOVERED MICROSWITCH INTERNALLY FAULTY.Mar 20, 2000 · Beech A100 · Landing Gear Position and WarningSDR CA000323006Snap Ring · loose(CAN) DURING REPLACEMENT OF THE VENT BLOWER ASSY, THE AME LIGHTLY PULLED ON THE PILOT''S LT RUDDER PEDAL. THE LT BRAKE MASTER CYLINDER SNAP RING LET GO AND THE CYLINDER CAME APART DRAINING ALL THE BRAKE FLUID AND LEAVING THE BRAKE SYSTEM INOPERATIVE. THE SUBMMar 15, 2000 · Beech A100 · Master Cylinder/Brake ValveSDR CA000317010Bearing · failed(CAN) BLADE BEARING FAILED CAUSING DAMAGE TO BEARING BORE.Mar 9, 2000 · Beech A100 · Propeller Hub SectionSDR CA000301036Actuator · noisy(CAN) FOLLOWING TAKE-OFF THE PILOT COULD NOT GET THE LANDING GEAR TO FULLY RETRACT OR EXTEND. MANUAL EXTENSION WAS REQUIRED. DURING RETRACTION TEST, MAINTENANCE OBSERVED THE GEARBOX WAS NOISY AND THE NOSEGEAR ACTUATOR WAS AT MAX LIMITS END PLAY. THE NOSE GEMar 1, 2000 · Beech A100 · Landing Gear ActuatorSDR CA000314006Bracket · wrong part(CAN) BEECH SERVICE INSTRUCTION 0464-213 PROVIDES FOR IMPROVED SWITCHES ON THE LANDING GEAR GEARBOX. THE GEARBOX IN QUESTION HAS THE NEW SWITCHES BUT ONE SWITCH WOULD DEFLECT IN ITS BRACKET AND MAKE CONTACT LATE WHEN ACTUATED BY A CAM. A NEW KIT WAS ORDERED Feb 23, 2000 · Beech A100 · Landing Gear SelectorSDR CA000301032Uplock Switch · failed(CAN) TROUBLESHOOTING LANDING GEAR RETRACTION PROBLEMS REVEALED THE RT MLG UPLOCK SWITCH WAS IN A POSITION TO INDICATE A GEAR INTRANSIT SITUATION BUT DID NOT INDICATE IT. THE SWITCH WAS REPLACED.Feb 22, 2000 · Beech A100 · Landing Gear Position and WarningSDR CA000215025Clevis · seized(CAN) THE AIRCRAFT WAS ON APPROACH WITHOUT NOSE GEAR LOCK INDICATION. GEAR CYCLED WITH NO INDICATION. ON CLIMBOUT THE NOSE GEAR LIGHT CAME ON. DURING INSPECTION THE NOSE GEAR ACTUATOR CLEVIS WAS FOUND STUCK IN THE ACTUATOR AND COULD NOT EXTEND WITH THE SPRINGJan 28, 2000 · Beech A100 · Landing Gear ActuatorSDR CA000218002Bellcrank · failed(CAN) WHILE ASCENDING, THE PASSENGERS HEARD A LARGE BANG AROUND THE DOOR AREA. CREW MEMBER INSPECTED THE DOOR IN FLIGHT, DID NOT PERCEIVE TO HAVE A PROBLEM. UPON LANDING, IT WAS DISCOVERED THE FORWARD PIN WAS NOT PROPERLY SEATED. UPON FURTHER INVESTIGATION, Jan 22, 2000 · Beech A100 · Passenger/Crew DoorsSDR CA000203013Windshield · failed(CAN) AFTER DEPARTING, ON CLIMB OUT, INNER PANE OF WINDSHIELD SHATTERED ON CAPTAINS SIDE.AIRCRAFT RETURNED WHERE WINDSHIELD WAS REPLACED.THE WINDSHIELD WHICH FAILED HAD PREVIOUSLY EXHIBITED SIGNS OF DELAMINATION BUT THE BEECH 100 MAINTENANCE MANUAL ATA CHAPTERJan 16, 2000 · Beech A100 · Flight Compartment WindowsSDR AU000203013Windshield · failed(AU) AFTER DEPARTING, ON CLIMB OUT, INNER PANE OF WINDSHIELD SHATTERED ON CAPTAIN'S SIDE. AIRCRAFT RETURNED WHERE WINDSHIELD WAS REPLACED. THE WINDSHIELD WHICH FAILED HAD PREVIOUSLY EXHIBITED SIGNS OF DELAMINATION, BUT THE BEECH 100 MAINTENANCE MANUAL ATA CHJan 16, 2000 · Beech A100 · Flight Compartment WindowsSDR CA991230040Cable · stuck(CAN) AFTER COMPLETING THE DECENT CHECKS, THE CREW ATTEMPTED TO REDUCE POWER ON BOTH ENGINES. THE POWER LEVER FOR THE RT ENGINE WOULD NOT MOVE. ALL ATTEMPTS TO MOVE THE POWER LEVER WERE UNSUCESSFUL SO THECREW ELECTED TO SHUT THE RT ENGINE DOWN. ON THE GROUND,Dec 13, 1999 · Beech A100 · Power LeverSDR CA991230038Wire · failed(CAN) WHEN PILOT SELECTED GEAR DOWN AIRCRAFT EXPERIENCED MULTIPLE FAILURES OF MLG & FLT INSTRUMENTS, ALSO THERE WAS SMOKE IN COCKPIT. PILOT EXTENDED THE MLG MANUALLY & LANDED W/O INCIDENT. MAINT DISCOVERED 2 PROBLEMS: THE WIRE GOING TO BUS FEEDER DIODE WADec 13, 1999 · Beech A100 · Electrical Power System WiringSDR CA991209059Wire · broken(CAN) AIRCRAFT WAS ON APPROACH WHEN AFTER SELECTING GEAR DOWN , THE LEFT MAIN GEAR DOWN AND LOCKED INDICATION LIGHT FAILED TO ILLUMINATE. THE GEAR WAS CYCLED SEVERAL TIMES, BUT DID NOT HELP. THE GEAR INTRANSIT LIGHTS WERE EXTINGUISHED AFTER THE COMPLETION OFNov 29, 1999 · Beech A100 · Landing Gear System WiringSDR CA991103051Torque Knee · cracked(CAN) WHILE MOVING AXLE TO CHECK FOR EXCESSIVE PLAY, MOVEMENT WAS NOTICED IN THE TORQUE KNEE UPPER AND LOWER BUSHINGS (BOTH MAIN GEAR). LEFT AND RIGHT LANDING GEAR TORQUE KNEES REMOVED TO INSTALL NEW BUSHINGS. DURING BUSHING REPLACEMENT, A SMALL CRACK WAS NONov 27, 1999 · Beech A100 · Main Landing Gear Strut/Axle/TruckSDR CA991209058Motor · overheated(CAN) THE AIRCRAFT WAS PARKED AND THE ENGINES SHUT DOWN, WHEN, WITH THE BATTERY STILL ON, THE CABIN FILLED WITH SMOKE. INVESTIGATION REVEALED THE FLAP MOTOR HAD OVERHEATED, SEIZED AND BEGAN TO SMOKE. THE CAUSE WAS THE UPLIMIT SWITCH NOT MAKING CONTACT WHEN THNov 23, 1999 · Beech A100 · Trailing Edge Flap Control SystemSDR CA991209057Tire · failed(CAN) ON TAKEOFF, THE LEFT INBOARD MAIN WHEEL ASSEMBLY SHED ITS ENTIRE TREAD. ALTHOUGH THIS WAS A RECAPPED TIRE, THE TREAD DID NOT SEPARATE AT THE RECAP. IN THIS CASE, THE RETREAD LAYER AND THE LAYER OF THE RUBBER FROM THE RETREAD TO THE FIRST LAYER OF CORDNov 15, 1999 · Beech A100 · TireSDR CA991209069Strut · cracked(CAN) AFTER REMOVAL FROM AIRCRAFT FOR TIMEX ON A TIME TRIAL, IT WAS INSPECTED AND THE FOLLOWING FOUND:LPI INDICATIONS OF CRACKS ON THE TORQUE KNEE LUG. THE CRACKS WERE IN THE RADIUS OF THE LUG ON THE BOTTOM SIDE. PART WAS REJECTED.Nov 10, 1999 · Beech A100 · Main Landing Gear Strut/Axle/TruckSDR CA991103048Contact · failed(CAN) AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BASE. TROUBLESHOOTING REVEALED THAT A SET OF POINTS IN THE LANDING GEAR CONTROLLER WELDED TOGETHER. THE MOTOR WAS REPLACED. THIS IS THE FOURTH PROBLEM WOct 27, 1999 · Beech A100 · Landing Gear SelectorSDR CA991007075Windshield · cracked(CAN) DURING CLIMB THROUGH 10,000 FEET, THE CAPTAIN'S OUTER PANE WINDSHIELD CRACKED. AIRCRAFT WINDSHIELD REPLACED.Oct 4, 1999 · Beech A100 · Flight Compartment WindowsSDR CA990927070Torque Tube · cracked(CAN) DURING ACCOMPLISHMENT OF SERVICE BULLETIN 2145, CRACKS WERE DETECTED ON BOTH RIGHT AND LEFT TORQUE TUBE ASSEMBLIES (P/N 115-610015-325). LEFT FOUND AT INBOARD SUPPORT (P/N 115-610015-1), RIGHT FOUND AT CENTER SUPPORT (P/N 115-610018-1). TORQUE TUBES RESep 19, 1999 · Beech A100 · Elevator Control SystemSDR CA990927056Gear Chain · separated(CAN) UPON SELECTING GEAR UP, IN-TRANSIT LIGHT STAYED ON. GEAR WAS THEN SELECTED DOWN AND THE MAIN GREEN LIGHTS CAME ON. THE NOSE WAS ABOUT 15 DEGREES FROM DOWN AND LOCKED. THE AFT GEAR CHAIN WAS ACCESSED BY THE FLIGHT CREW AND WITH THE AID OF MAINTENANCE, Sep 13, 1999 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA990812019Sprocket · worn(CAN) DURING THE UNDER FLOOR INSPECTION THE AME NOTICED THE AFT CHAIN FOR THE LANDING GEAR ACTUATION SYSTEM HAD JUMPED ONE SET OF TEETH ON A SPROCKET. FURTHER INVESTIGATION FOUND THAT THE CHAIN TENSION WAS OUT OF TOLERANCE WHICH HAS BEEN DETERMINED TO BE THE Jul 27, 1999 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA990728080Pin · broken(CAN) DURING THE WASH AND REGREASING OF THE RIGHT MAIN LANDING GEAR, THE PIN THAT ATTACHES THE DOWNLOCK HOOK TO THE DOWNLOCK LINK WAS FOUND PROTRUDING AND BROKEN. THE BREAK WAS LOCATED AT THE HOLE FOR THE ROLL PIN. THE ROLL PIN IS USED TO RETAIN THE HOOK PINJul 21, 1999 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA990630057Spar · cracked(CAN) THE RUDDER WAS REMOVED TO REPAIR SOME LOOSE RIVETS ON THE TORQUE TUBE, BUT A CRACK ABOUT 1 CENTIMETER LONG WAS DISCOVERED ON THE RUDDER SPAR (P/N 96-630000-307). THE SPAR WAS ALSO FOUND TO BE CRACKED IN BEHIND. THE CRACKS ORIGINATED FROM THE NUTPLATE IJun 11, 1999 · Beech A100 · Rudder, Spar/RibSDR CA990630056Bellcrank · corroded(CAN) THE RUDDER BELLCRANK WAS REMOVED AND CORROSION WAS FOUND ON THE SURFACE WHERE THE TORQUE TUBE CONNECTS. THERE WAS ALSO CORROSION FOUND ON THE BOLT HOLES. THE BELLCRANK AND BOLTS WERE REPLACED. SUBMITTER STATED THAT THIS AREA IS HARD TO INSPECT BECAUSEJun 10, 1999 · Beech A100 · Rudder Control System
Back to Beech A100