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 CA100111006Wheel · cracked(CAN) AFTER STRIPPING, A VISUAL INSPECTION OF BOTH HALF WHEELS WAS PERFORMED BEFORE SENDING TO NDT. BOTH HALF WHEELS TIE BOLTS HOLES FOUND CORRODED BEYOND LIMIT AND MANY SHOWED SIGNS OF CRACKS. (TC NR 20100111006)Jan 8, 2010 · Beech A100 · Wheel/Ski/FloatSDR CA100209010Spar · cracked(CAN) THE OTBD WING REAR SPAR WEB WAS FOUND CRACKED AT THE LAP JOIINT WS 110.11, THE LOCATION OF THE OTBD FLAP, INBD TRACK. THE RIVETS SECURING THE LOWER CLIPS TO THE FLAP TRACK FAILED. THE FORCES APPLIED TO THE FLAP TRACK WHEN THE FLAPS WERE LOWERED PULLED ONJan 1, 2010 · Beech A100 · Wing SparSDR CA091223007Rod · binding(CAN) LEFT HAND ENGINE TORQUE DOES NOT DECREASE WHEN POWER LEVER IS RETARDED. LEFT EGINE INSPECTED FOUND AFT FUEL CONROL INTERCONNECT ROD END BIDING AND HOLDING PCU ARM AT A HICH POWER SETTING. AFT ROD END REALIGNED, CLEANED, AND LUBRICATED. AIRCRAFT GROUNDDec 8, 2009 · Beech A100 · Power LeverSDR CA091223008Landing Gear · inoperative(CAN) LANDING GEAR WOULD NOT COME DOWN IN YSF. RED GEAR HANDLE LIGHT WENT ON AND REMAINED ON. PROCESSED TO YPA, PERFORMED EMERGENCY GEAR EXTENSION PROCEDURE. LANDED UNEVENTFULLY. LANDING GEAR SYSTEM BLED AND SERVICED IAW AVIA DESIGN MAINTENANCE MANUAL M-81Dec 6, 2009 · Beech A100 · Landing Gear Retraction/Extension SystemSDR QMLA2009112709043Motor · inoperativeNEXT DAY AFTER SMOKE AND FUMES REPORTED, PILOT NOTICED BLOWER VENT MOTOR WAS INOPERATIVE. ON 3RD LEG OF FLIGHT, CLIMBED TO FL17 AND DUE TO TEMPERATURE, TURNED HEAT ON. AGAIN NOTICED BURNING SMELL WHEN ENVIRONMENTAL WAS SELECTED TO HOT. MADE PRECAUTIONARY LANov 27, 2009 · N777GS · Beech A100 · Air Distribution FanSDR CA090609003Bracket · cracked(CAN) DURING A SCHEDULED INSP CRACKS WERE FOUND ON THE RT OTBD FLAP INBD TRACK (LOWER ATTACHMENT) BRACKETS. FURTHER INSP REVEALED THAT THE LWR 2 RIVETS ON EACH OF THE FWD ATTACHMENT BRACKETS WERE NO LONGER HOLDING, 3 RIVETS WERE SHEARED AND THE SECOND RIVET FRJun 4, 2009 · Beech A100 · Trailing Edge FlapsSDR CA090420004Clevis · binding(CAN) PILOTS REPORTED A "CLUNK NOISE" UPON RETRACTION OF THE LANDING GEAR AND THE GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. ACFT RETURNED TO BASE. AFTER FURTHER INVESTIGATION MX REPRODUCED THE "CLUNK NOISE", IT WAS CAUSED BY THE CLEVIS BINDING INSIDE ACTUATOApr 16, 2009 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA090321001Pin · broken(CAN) DURING INSPECTION MECHANIC NOTICED UPPER DRAG LEG PIN, ON THE RT DRAG LEG ASSEMBLY, WAS BROKEN AT THE GREASE HOLE JOURNAL.Mar 19, 2009 · Beech A100 · Nose/Tail Landing Gear Strut/AxleSDR CA090120001Flap Track · crackedPILOT SELECTED FLAPS DOWN THEN NOTICED A ASYMMETRICAL FLAP CONDITION, FLAPS WERE SELECTED UP WHICH RESULTED IN THE CIRCUIT BREAKER POPPING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE LEFT OUTBOARD FLAP, INBOARD TRACK HAD FRACTURED NEAR THE Jan 15, 2009 · Beech A100 · Trailing Edge FlapsSDR CA090120003Switch · failedTHE AIRCRAFT DEPARTED FROM YAT AND AFTER REACHING CRUISE ALTITUDE, THE CREW NOTICED SMOKE IN THE CABIN. THE CREW ATTEMPTED TO RETURN TO YAT BUT THE FLAPS WOULD NOT EXTEND ON APPROACH. THE CREW DIVERTED TO YMO. THE FLAP CONTROL CIRCUIT BREAKER TRIPPED, THE SJan 14, 2009 · Beech A100 · Trailing Edge Flap Control SystemSDR CA081110002Switch · intermittent(CAN) AFTER PILOT SELECTED GEAR DOWN, THERE WAS NO INDICATION THE NOSE GEAR WAS DOWN AND LOCKED, ACFT DIVERTED BACK TO MX BASE. ON ROUTE NOSE GEAR INDICATION CAME ON. ACFT LANDED WITHOUT INCIDENT. MX REPLACED NOSE GEAR DOWN LOCK INDICATOR SWITCH AND RETURNENov 5, 2008 · Beech A100 · Landing Gear Position and WarningSDR CA081027003Shaft · stiff(CAN) UPON APPROACH, THE LT ENG PWR LEVER WAS RETARDED WITH NO EFFECT ON ENG. THE ENG REMAINED AT 91 PERCENT NG. THE APPROACH WAS ABORTED AND THE ACFT DIVERTED. ON ARRIVAL, AN EMERGENCY WAS DECLARED AND THE LT WAS SHUTDOWN IN ORDER TO CARRY OUT THE LANDING. MXOct 25, 2008 · Beech A100 · Fuel Control/Turbine EnginesSDR CA081020002Torque Link · cracked(CAN) DURING REGULAR MX, A MECHANIC NOTICED A CRACK ON THE UPPER TORQUE LINK OF THE LT MLG. THE TORQUE LINK WAS REPLACED AND ACFT RETURNED TO SERVICE. THE RT MLG TORQUE LINKS WERE INSPECTED WITH NO FAULTS FOUND.Oct 11, 2008 · Beech A100 · Main Landing Gear Strut/Axle/TruckSDR CA080701004Hook · out of adjust(CAN) ACFT DEPRESSURIZED AT 20000 FEET. ACFT DESCENDED TO 10000 FEET AND LANDED WITHOUT INCIDENT MX FOUND THE UPPER FORWARD DOOR HOOK WAS NOT LATCHING PROPERLY THAT CAUSED THE DOOR SEAL TO BLOW OUT CAUSING THE DECOMPRESSION. DOOR HOOK ADJUSTED AND THE DOOR SEAJun 27, 2008 · Beech A100 · Passenger/Crew DoorsSDR CA071206001Torque Link · cracked(CAN) DURING A SPECIAL LPI INSPECTION OF THE MLG TORQUE LINKS DUE TO THE FAILURE OF A LINK ON ANOTHER AIRCRAFT (SDR 20071024010 AND 20071122002), 3 OF THE 4 LINKS WERE FOUND CRACKED. THE LINKS FROM 3 ADDITIONAL AIRCRAFT WERE REPLACED IN ORDER TO COMPLETE THE Dec 5, 2007 · Beech A100 · Landing Gear Retraction/Extension SystemSDR 2007FA0001058Connector · arcedPARTIAL ELECTRICAL POWER LOSS TO COMPONENTS FROM RT NR 1 AND NR 2 SUBPANEL CIRCUIT BREAKERS. FOUND RT CIRCUIT PANEL CONNECTOR SOCKET MODULE AND SOCKET RT 1B BURNED. REPLACED MODULE (NR 8 WIRE-4 SOCKET) AND 4 SOCKETS. REPLACED PINS (4). FUNCTION CHECK SATISDec 4, 2007 · N23404 · Beech A100 · Electrical Power System WiringSDR CA071122002Torque Link · cracked(CAN) DURING A SPECIAL LPI INSP (SELF IMPOSED INSPECTION DUE TO BROKEN LINK SEE SDR NR 2007024010) OF THE UPPER AND LOWER TORQUE LINKS ON (2) OF OUR AC, (3) TORQUE LINKS WERE FOUND CRACKED IN THE RADIUS AREA. ONE LINK HAS 2 CRACKS SIDE BY SIDE THE OTHER HAD ONov 21, 2007 · Beech A100 · Main Landing GearSDR CA071030002Flap Track · cracked(CAN) ON MAINTENANCE WALKAROUND THE RT OB FLAP HAD MORE PLAY THAN USUAL. FLAP WAS REMOVE AND THE OB FLAP TRACK WAS FOUND TO BE CRACKED ON THE REAR TIP. TRACK REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20071030002)Oct 25, 2007 · Beech A100 · Trailing Edge FlapsSDR CA071024010Torque Knee · cracked(CAN) AFTER LANDING, UPON DECELERATING THROUGH 60 KIAS THE AIRCRAFT BEGAN TO VIOLENTLY SHAKE, SHUDDER AND APPEAR TO SKIP WHILE VEERING TOWARD THE LT SIDE OF THE RUNWAY. CONTROL WAS MAINTAINED AND THE AIRCRAFT WAS BROUGHT TO A SLOW TAXI AT WHICH TIME THE CONDITOct 21, 2007 · Beech A100 · Main Landing GearSDR CA071022011Engine · making metal(CAN) RT ENGINE CHIP DETECTOR LIGHT CAME ON IN FLIGHT SO WE SHUTDOWN THE RT ENGINE. ENGINE BEING REMOVED AND SENT TO ENGINE O/H FACILITY FOR REPAIR. LOANER ENGINE TO BE INSTALLED. (TC NR 20071022011)Oct 19, 2007 · Beech A100 · Engine (Turbine/Turboprop)SDR CA070906002Torque Tube · loose(CAN) DURING A ROUTINE INSPECTION THE LT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE AN EXCESSIVE AMOUNT OF PLAY AT THE TAPER PINS ON BOTH COLLARS. THE TORQUE TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS TORQUE TUBE ONLY HAD 209.2 HOUR SINCE NEW ANDSep 5, 2007 · Beech A100 · Elevator StructureSDR CA070809002Actuator · damaged(CAN) NOSE GEAR ACTUATOR SENT IN TO HAVE SEALS REPLACE DO TO UNIT BECAUSE IT WAS SITTING ON SHELF FOR 6 YEARS. ACTUATOR WAS OVERHAULED AND HAD NEVER BEEN USED. UNIT WAS DISASSEMBLED TO REPLACE SEALS AND INTERIOR OF CYLINDER WAS SCORED AND A SPRING BROKEN. ACTUAug 9, 2007 · Beech A100 · Landing Gear ActuatorSDR CA070723001Rod · corroded(CAN) DURING THE REPLACEMENT OF RODEND P/N F4-19 ON THE NOSE LANDING GEAR STEERING BARREL ASSY. P/N 50820042-601 WAS DISASSEMBLED TO FACILITATE THE REMOVAL OF THE RODEND FROM THE ROD ASSY P/N 50-820035 (ITEM 21). AFTER DISASSY IT WAS NOTICED THAT THE ROD ASSY Jul 19, 2007 · Beech A100 · Landing Gear Steering SystemSDR CA070608001Structure · cracked(CAN) CRACK FOUND IN STRUCTURE OF HORIZONTAL STAB. CRACK LOCATED AT TRAILING EDGE UPPER SURFACE AT CENTER OF HORIZONTAL STAB. CRACK LENGTH 0.600, CRACK REPAIRED IAW REPAIR DWG SUPPLIED BY MFG AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070608001)Jun 6, 2007 · Beech A100 · Horizontal Stabilizer StructureSDR CA070321001Gearbox · failed(CAN) GEAR WOULD NOT COME UP WHEN SELECTED, LANDING GEAR GEARBOX REPLACED. OVERHAUL FACILITY REPORTED THAT A INTERNAL GEAR MAY HAVE BEEN SHIMMED IMPROPERLY THAT CAUSED PREMATURE WEAR (TC# 20070321001)Mar 7, 2007 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA070312006Pressure Switch · malfunctioned(CAN) DURING LANDING GEAR SWINGS IT WAS NOTICED THAT THE LANDING GEAR PUMP WAS HESITATING. PROBLEM WAS TRACED BACK TO THE PRESSURE SWITCH. SWITCH WAS REPLACED AND GEAR SWUNG, FAULT FEE. (TC NR 20070312006)Feb 22, 2007 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA070216002Motor · failed(CAN) ON FINAL APPROACH, THE PILOT SELECTED FLAPS DOWN, WHEN THE FLAPS REACHED 5 DEGREES, THE ASSOCIATED CIRCUIT BREAKER POPPED. THE PILOT OVERSHOT TO EVALUATE THE SITUATION AND THEN CARRIED OUT AN UNEVENTFUL LANDING WITH 5 DEGREE OF FLAP. UPON INVESTIGATION BFeb 14, 2007 · Beech A100 · Trailing Edge Flap Control SystemSDR CA070130003Condition Lever · cracked(CAN) PILOTS REPORTED LT FUEL CONDITION LEVER CRACKED HALF WAY DOWN LEVER. AIRCRAFT REMOVED FROM SERVICE. RT CONDITION LEVER INSPECTED AND SHOWED SIGNS OF WEAR. LT AND RT CONDITION LEVERS ON ORDER. (TC NR 20070130003)Jan 29, 2007 · Beech A100 · Engine ControlsSDR CA070123001Control Cable · separated(CAN) THE LT ENGINE COULD NOT BE SHUTDOWN ON THE GROUND USING THE CONDITION LEVER, THE PILOT HAD TO USE THE FIREWALL SHUT-OFF IN ORDER TO SHUT THE ENGINE DOWN. INVESTIGATION BY MAINTENANCE FOUND THAT THE LT IDLE CONTROL CABLE ASSY FAILED AT THE MALE TERMINAL EJan 19, 2007 · Beech A100 · Power LeverSDR CA061221002Latch · broken(CAN) DURING FLIGHT THE CREW NOTICED AIR LEAKING OUT THE PASSENGER DOOR AND THE AIRCRAFT BEGAN TO DEPRESSURIZE. THE CREW DESCENDED TO 9000 FT FOR THE REMAINDER OF THE FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. UPON LANDING THEY NOTICED THE LT UPPER DOOR HOOK Dec 18, 2006 · Beech A100 · Passenger/Crew DoorsSDR CA061127001Controller · unserviceable(CAN) FLIGHT CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. AFTER TROUBLESHOOTING THE MOTOR CONTROLLER WAS FOUND UNSERVICEABLE. MOTOR CONTROLLER WAS REPLACED, GEAR SWINGS COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. THIS UNIT HAD 928 LANDINGSNov 23, 2006 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA061219007Relay · failed(CAN) AFTER TAKEOFF ON CLIMB-OUT THE RT GENERATOR CHARGING SYSTEM FAILED. THE AIRCRAFT RETURNED TO BASE. SYSTEM TROUBLESHOOTING CARRIED OUT AND FOUND THE OVER VOLTAGE RELAY HAD FAILED. (TC NR 20061219007)Nov 6, 2006 · Beech A100 · Electrical Power System WiringSDR CA060906024Motor · failed(CAN) SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 1000 FEET ALTITUDE A LIGHT SMOKE APPEARED IN THE CABIN ACCOMPANIED WITH A BURNING SMELL. THE AIRCRAFT IMMEDIATELY RETURNED TO THE DEPARTURE AIRPORT. FURTHER INVESTIGATION BY MAINTENANCE REVEALED THAT THE FLAP MOTORAug 29, 2006 · Beech A100 · Trailing Edge Flap Control SystemSDR CA061218005Circuit Board · malfunctioned(CAN) ANNUNCIATOR PANEL SHOWED A FALSE WARNING INDICATION FOR MASTER CAUTION LIGHT. SYSTEM TROUBLESHOOTING CARRIED OUT AND FOUND FAULT WARNING CIRCUIT BOARD UNSERVICEABLE AND FAULT WARNING CIRCUIT BOARD REPLACED.Jul 24, 2006 · Beech A100 · Instrument PanelSDR CA060712008Support Beam · cracked(CAN) UNDER THE PILOTS FLOOR BOARDS AT FLIGHT STATION 107 THE PILOTS RUDDER QUADRANT SUPPORT BEAM WAS FOUND CRACKED. THESE CRACKS WERE FOUND AT (2) OF THE (4) NUT PLATES. WE HAVE FOUND THESE SAME CRACKS ON 4 OTHER OF OUR AIRCRAFT AROUND THE SAME LOCATIONS. THEJul 6, 2006 · Beech A100 · Fuselage Main, StructureSDR 324EC200601Relay · openHORIZONTAL STABILIZER TRIM WOULD NOT ACTUATE IN THE NOSE-DOWN TRAVEL DIRECTION (MAIN SYSTEM). STANDBY TRIM SYSTEM FUNCTIONED PROPERLY. FOUND THE MAIN CONTACTS OF THE -B- DOWN RELAY IN AN OPEN CIRCUIT CONDITION. REPLACEMENT CONFIRMED FAULT.Jul 6, 2006 · N324EC · Beech A100 · Stabilizer Position IndicatingSDR CA060613004Bearing · misinstalledDURING ACT ENDPLAY CHECK AND LUBE OF N/G ACT 50-820208-5, NOTICED THRUST BEARING IMPROPERLY INSTALLED. INSTRUCTIONS IN COMPONENT MM ARE TO INSTALL BEARING WITH P/N AWAY FROM GEAR, THIS BEARING HAD BEARING MANUF P/N AND WORD THRUST ON ONE SIDE AND RAYTHEON P/Jun 12, 2006 · Beech A100 · Landing Gear ActuatorSDR CA060613001Support Beam · crackedUNDER THE PILOTS FLOORBOARDS AT FLIGHT STATION 107, THE PILOTS RUDDER QUADRANT SUPPORT BEAM WAS FOUND CRACKED. THESE CRACKS WERE FOUND AT 2 OF THE 4 NUT PLATES. FOUND THESE SAME CRACKS ON 3 OTHER OF OUR AIRCRAFT AROUND THE SAME LOCATIONS. THE BEAM WAS REPLAJun 8, 2006 · Beech A100 · Fuselage Main, Attach FittingsSDR CA060601002Duct · cracked(CAN) CRACK DEVELOPED IN THE DOMED PORTION OF THE SMALL EXIT DUCT BESIDE THE WELD. FOUND DURING THE BOROSCOPE INSPECTION. (TC NR 20060601002)May 31, 2006 · Beech A100 · Turbine Engine Air Inlet SectionSDR CA060406003Duct · disconnectedDURING A ROUTINE INSPECTION OF THE CABIN HEATING DUCTS THE HOT AIR DUCT ASSEMBLY P/N 97-555011-15 ITEM NR 22 IN PICTURE NR 1 WAS FOUND DISCONNECTED AT THE AFT END. 2 DUCTS FURTHER FWD WERE FOUND CRACKED ALLOWING THEM TO MOVE FWD AND ALLOWING THIS DUCT TO DISCMar 30, 2006 · Beech A100 · Ice/Rain Protection SystemSDR AXS2006F00000Starter Gen · unserviceableENROUTE, AT 9000 FT MSL. THE LT GEN TRIPPED OFF LINE, AND MOMENTARILY CAME BACK ON. THE VOLT AMMETER SHOWED THE LT GEN ACCEPTING A LOAD. THEN THE PROCESS REPEATED, WITH THE LT COMING BACK ON LINE. FOR A THIRD TIME, THE LT GEN TRIPPED AND THIS TIME DID NOT Mar 27, 2006 · N91RK · Beech A100 · Starter-GeneratorSDR CA060320003Support Bracket · cracked(CAN) CRACK FOUND ON IB SUPPORT BRACKET WHILE CARRYING OUT REPETITVE INSPECTION MSB 2145. TORQUE TUBE REPLACED WITH NEW. (TC NR 20060320003)Mar 9, 2006 · Beech A100 · Elevator StructureSDR CA060217002Actuator · damagedNOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTEANCE DID MULTIPLE GEAR SWINGS BUT COULD NOT DUPLICATE THE PROBLEM. THE ACTUATOR WAS REMOVED AND PUT IN A TEST STAND WHERE IT FINALLY FAILED STAYING IN THE LOCKED POSITION. A OVERHAULED ACTUATOR WAS INFeb 7, 2006 · Beech A100 · Landing Gear ActuatorSDR CA060207002Support Beam · cracked(CAN) UNDER THE PILOTS FLOOR BOARDS AT FLIGHT STATION 107 THE PILOTS RUDDER QUADRANT SUPPORT BEAM WAS FOUND CRACKED. THESE CRACKS WERE FOUND AT THE TOP BEND RADIUS AND AT SOME HOLES FOR NUT PLATES. WE HAVE FOUND THESE SAME CRACKS ON 3 OTHER OF OUR AIRCRAFT AROFeb 7, 2006 · Beech A100 · Rudder Control SystemSDR CA060127004Switch · unserviceable(CAN) FLOAT SWITCH FAILED INTERNALLY CAUSING THE EPA CAN TO DRAIN OVERBOARD ON SHUTDOWN. (TC NR 20060127004)Jan 26, 2006 · Beech A100 · Standard Practices/StructuresSDR CA060307003Accumulator · failed(CAN) THE ABOVE P/N FAILED SENT FOR REPAIR THEN FAILED AGAIN WITH IN 5.3 HRS. SERVICEABLE ACTUATOR INSTALLED WITH NO MORE PROBLEMS. (TC NR 20060307003)Jan 25, 2006 · Beech A100 · Autopilot Trim ServoSDR CA060127002Elt · intermittent(CAN) ELT FAILED THE ACTIVATION TEST DURING THE ROUTINE INSPECTION. THE UNIT HAD THE BATTERY REPLACED AND RECERTIFIED 21 DAYS EARLIER. AVIONICS SHOP FOUND THE PROBLEM TO BE A INTERMITTENT ON/OFF SWITCH. (TC NR 20060127002)Jan 23, 2006 · Beech A100 · Emergency Locator BeaconSDR CA051206004Intercostal · crackedDURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON OTHER AIRCRAFT, THE AFT PRESSURE BULKHEAD WAS FOUND CHAFED BY BOTH THE CENTER INTERCOSTAL AND THE OUTBOARD INTERCOSTAL ADJACENT TO THE TAIL ACCESS DOOR. NDT WAS COMPLETED AND A CRACK FOUND AT THE OUTBOARD LODec 1, 2005 · Beech A100 · Fuselage Main, BulkheadSDR CA051122003Inverter · failedTHE PILOT IN COMMAND REPORTED THE NR 2 INVERTER CIRCUIT BREAKER POPPED. ON INVESTIGATION, THE NR 2 INVERTER AND ASSOCIATED RELAY WIRING SHOWED SIGNS OF OVERHEATING. THE WIRING FOR THE RELAY OVERHEATED TO THE POINT THAT ONE OF THE WIRES SEPARATED FROM THE POLNov 19, 2005 · Beech A100 · AC InverterSDR CA051107004Resistor · openLT GEN FAIL ANNUNCIATOR LIGHT ILLUMINATED IN CRUISE. ATTEMPED RESET BY SWITCHING LT GEN OFF, WAITED 10 SECONDS, THEN SWITCHED BACK ON. RESULT WAS BRIEF SMALL PUFF OF SMOKE FROM INSTRUMENT PANEL, SUBSEQUENTLY FOUND TO BE BURN OF GPS ANNUNCIATOR BRT/DIM/TEST MNov 1, 2005 · Beech A100 · AC Regulator
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