Beech 400A

Service difficulty reports · 1,397

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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 = '400A'
  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 RK267001Flow Valve · inoperativeDURING CRUISE, RT JET PUMP LIGHT ON CROSSFEED PANEL ILLUMINATED. DIVERTED, AND LANDED UNEVENTFULLY AT APA.Dec 13, 2004 · N4467X · Beech 400A · Fuel Selector/Shut-Off ValveSDR DJFA2004040Switch · out of adjustCREW REPORTED THAT WHILE ON APPROACH THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. AN ALT EXTENSION WAS PERFORMED AND GEAR EXTENDED. THREE GREEN LIGHTS WERE RECEIVED AFTER THE ALT EXTENSION WAS PERFORMED. AN EMERG WAS DECLARED AND A/C LANDED W/O FURDec 8, 2004 · N478LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2004039Odor · detectedCREW REPORTED THAT THE CABIN HAD FILLED WITH AN ELECTRICAL OR ENVIRONMENTAL SMELLING SMOKE. AIRCRAFT HAD DIVERTED TO KSAV. MAINTENANCE RAN BOTH ENGINES AND OPERATED THE ENVIRONMENTAL CONTROL SYSTEM. THE FREON AIR CONDITIONING SYSTEM WAS ALSO RAN. NO SMOKE Dec 5, 2004 · N799TA · Beech 400A · Air Distribution SystemSDR CA041206003Engine · malfunctioned(CAN) AT 15,000 FT IN LEVEL FLIGHT BOTH ENGINES EXPERIENCED A SIMULTANEOUS, UNCOMMAMDED, PARTIAL POWER ROLL-BACK. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT GROUND RUNS WERE UNABLE TO DUPLICATE THE EVENT. AIRFRAME CONTROL CABLES AND ENGINE BOV Dec 2, 2004 · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA200400458Duct · rupturedSMOKE AND EXHAUST APPEARED IN LAV WHEN ENG AND WING ANTI-ICE WAS PLACED ON. EXHAUST SMELLED LIKE OIL AND WAS VERY VISIBLE. IT LEFT A FILM ON LAV MIRROR. FOUND THE SMOKE AND ODOR CAUSED BY A RUPTURE IN THE WING ANTI-ICE BLEED AIR LINE. INSTALLED NEW BLEED ANov 22, 2004 · N115QS · Beech 400A · Airfoil Anti/De-ice SystemSDR DJFA2004034Pump · out of limitsCREW REPORTED, IN CLIMB, NOTICED HYD PRESS FLUCTUATING ABOVE NORM. AFTER FL390, PRESS STABLE FOR 5 TO 10 MINS THEN INCREASED TO 2000 PSI AND HELD. EMERG DECLARED. A/C LANDED USING ALT GEAR EXTENSION, WITH A NO FLAPS APPROACH. PWR BRAKE FAILURE CHECKLIST USEDNov 19, 2004 · N709TA · Beech 400A · Hydraulic System, MainSDR 2005FA0000107Idler Link · failedTHE UPPER IDLER LINK PN 202-0008-1, FAILED AT THE DOOR END PREVENTING THE THRUST REVERSER TO STOW PROPERLY AND DAMAGED THE SUPPORT ASSY. PILOT`S WERE UNAWARE OF THE PROBLEM UNTIL THE T/R DOORS WERE NOTICED TO NOT BE FULLY STOWED ON WALK AROUND. (K)Nov 11, 2004 · N101CC · Beech 400A · Engine Thrust ReverserSDR DJFA2004031Bellows · crackedCREW REPORTED AIRCRAFT WOULD NOT INCREASE SPEED WITH INCREASED POWER AND AT 190 KTS STICK SHAKER WAS ENCOUNTERED. ABQ CENTER WAS ADVISED THAT AIRCRAFT HAD TO DESCEND. ENGINES WOULD NOT DEVELOP PUBLISHED TAKEOFF POWER. MAINTENANCE FOUND 2 BLEED AIR BELLOWS CNov 9, 2004 · N898TA · Beech 400A · Engine Bleed Air SystemSDR 2005FA0000031Cable · brokenDURING SCHEDULED INSPECTION FOUND LT MAIN GEAR UPLOCK EMERGENCY EXTENSION CABLE BROKEN NEAR OB END. REPLACED CABLE WITH NEW PN128-380021-55 CABLE ASSEMBLY AND RIGGED IAW BE 400/400A, MM 32-30-00. ORIGINAL PN, PART TT NOT SUPPLIED, POSSIBLY ORIGINAL. ASSEMBLOct 12, 2004 · N494CW · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2004025Engine · power lossCREW REPORTED NR 2 ENGINE WAS NOT MAKING TAKEOFF RATED THRUST. 98.7 NL REQUIRED, 98.4 NL ACHIEVED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED, AND NO FURTHER INCIDENTS HAD OCCURRED. MAINTENANCE ADJUSTED THE ENGINE HMU RIGGING. OPERATIONAL CHECK WAS SATISFACTOct 9, 2004 · N698TA · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2004023Strut · overservicedCREW REPORTED THAT DURING LANDING ROLL, THRUST REVERSERS WOULD NOT DEPLOY, SPEED BRAKES WOULD NOT EXTEND AND ANTI-SKID WAS INTERMITTENT. WHEN BRAKES FINALLY ENGAGED RIGHT TIRE GRABBED FIRST AND CAUSED FLAT SPOT. MAINTENANCE FOUND SHOCK STRUTS TO BE TOO HIGH.Oct 7, 2004 · N476LX · Beech 400A · Main Landing Gear Strut/Axle/TruckSDR JEM2004F00009Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AREA, IT WAS DISCOVERED THE RIB AS WELL AS THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORAug 28, 2004 · N400FT · Beech 400A · Horizontal Stabilizer StructureSDR JEM2004F00008Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL AS THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTAug 28, 2004 · N400FT · Beech 400A · Horizontal Stabilizer StructureSDR E812004F00008Line · chafedWHILE INSPECTING FORWARD FUSELAGE BRAKE HYDRAULIC LINE TUBING DURING COMPLIANCE WITH RECOMMENDED SB, FOUND TUBING DAMAGED EXTERNALLY BY FLOOR PANEL 151BTC AND FLOOR PANEL 151DTC ATTACHMENT SCREWS. REPAIRED TUBING ASSY BY SPLICING IN REPAIR TUBE WITH PERM SWAGJul 22, 2004 · N75RL · Beech 400A · Hydraulic System, MainSDR DJFA2004010Engine · shutdownAIRCRAFT DEPARTED KDUC TO KRSW AT FL410. AFTER STARTING DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT THE CREW TRIED STARTING THE NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED THE NR 2 ENGINE AGAIN Jul 12, 2004 · N455CW · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2004009Engine · shutdownAFTER STARTING THEIR DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT, THE CREW TRIED STARTING THE NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED THE NR 2 ENGINE AGAIN AND IT STARTED AT ABOUT FL170. DIDJul 12, 2004 · N455CW · Beech 400A · Engine (Turbine/Turboprop)SDR RK355001Relay · shortedUPON APPROACH INTO SBA, EXTENDED GEAR, INDICATIONS SHOW THREE GREENS AND A RED LIGHT IN HANDLE. CONSULTED CHECKLIST, FOUND GEAR HANDLE WOULD NOT RAISE AND CIRCUIT BREAKER POPPED. PUSHED -J- HANDLE DOWN, CIRCUIT BREAKER IN, AND RAISED HANDLE - GEAR AND DOORS Jul 9, 2004 · N767SB · Beech 400A · Landing Gear Position and WarningSDR DJFA2004005Filter · leakingDURING FLIGHT THE LEFT OIL PRESSURE ANNUNCIATOR WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND, OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING.Jun 22, 2004 · N427CW · Beech 400A · Turbine Engine Oil SystemSDR DJFA2004006O-Ring · chippedDURING FLIGHT, THE LEFT OIL PRESSURE ANNUNCIATORS WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND THAT THE OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING.Jun 22, 2004 · N427CW · Beech 400A · Turbine Engine Oil SystemSDR JEM2004F00000Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB ON THE RT SIDE AND THE RIBS WERE CRACKED. THE INITIAL INSPECTION WAS ACCOMPLISHED USING A BORESCOPE ANDJun 22, 2004 · N8167Y · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00006Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00005Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00004Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00003Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00002Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer StructureSDR JEM2004F00001Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer StructureSDR J0U2004F00001Cable · brokenPILOT REPORTED NO LUMBAR SUPPORT FOR CREW SEAT. ADJUSTMENT USING CONTROL KNOB MADE NO DIFFERENCE IN SUPPORT. REMOVED AFT UPHOLSTERY FROM SEAT AND FOUND CONTROL CABLE BROKEN. SUGGEST USING HEAVIER CABLE.May 24, 2004 · N25CU · Beech 400A · Flight Compartment EquipmentSDR 2004FA0000408Shutoff Valve · inoperativePILOT REPORTED EMERGENCY PRESSURIZATION SYSTEM CAME ON DURING TAKEOFF WITH AIR CONDITIONING FAIL ANNUNCIATOR LIGHT ILLUMINATED. TROUBLESHOT SYS IAW MM21-00-00. FOUND RT PRESSURE REGULATING/SHUT-OFF VALVE (PRSOV) HAD FAILED, ALLOWING FULL BLEED AIR VOLUME THRApr 30, 2004 · N453CW · Beech 400A · Cabin Compressor SystemSDR T8B2004F00000Door · crackedTHE UPPER LEFT THRUST REVERSER DOOR IS CRACKED APPROXIMATELY 11 INCHES. THE CRACK IS LOCATED BEHIND THE MIDDLE ROW OF RIVETS, APPROXIMATELY .5 INCH BEHIND THE RIVET CENTER LINE AND IS PERPENDICULAR TO LINE OF FLIGHT. THE DOOR HAS BEEN RETURNED TO THE MFG FORApr 23, 2004 · N711EC · Beech 400A · Engine Thrust ReverserSDR DJFA2004001Compensator · malfunctionedDURING FLIGHT AIRCRAFT EXPERIENCED A PFD FAILURE AND LOST BOTH PF'S. PILOTS CONTACTED CENTER AND RECEIVED VECTORS, LANDED WITH NO FURTHER PROBLEMS.Apr 11, 2004 · N755TA · Beech 400A · Integrated Flight SystemSDR RK256001Cowling · missingAFTER TAKEOFF, DEPARTURE INSTRUCTIONS WERE TO CLIMB TO 2000 FEET AND TURN LEFT TO HEADING 120. A LEFT TURN WAS INITIATED A 1000 FEET AND AT APPROXIMATELY 1300 FEET AND HEADING 180 IN LIGHT TURBULENCE, A BUMP WAS FELT BY BOTH PIC AND SIC. PIC VERIFIED FLIGHT Jan 31, 2004 · N26PA · Beech 400A · Engine Cowling SystemSDR TCH2004F00000Shutoff Valve · failedNEW PART INSTALLED ON AIRCRAFT, FAILED AFTER ONLY 1.0 HOUR IN SERVICE. THIS VALVE FUNCTIONS AS THE LT FIREWALL SHUTOFF.Jan 26, 2004 · N234DK · Beech 400A · Fuel Selector/Shut-Off ValveSDR 2004FA0000004Switch · failedMULTIPLE FAILURES OF TAIL DEICE SYSTEM. ALWAYS GROUND TESTED GOOD. FINALLY FLEW AIRCRAFT BACK TO MANUFACTURER FOR REPAIR.Oct 9, 2003 · N440DS · Beech 400A · Ice/Rain Protection SystemSDR JEM2004F00007Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZ STAB ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORIZ STAug 28, 2003 · N400FT · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA200300004Cowling · missingAFTER DEPARTURE FROM WEST PALM THE PILOTS EXPERIENCED A VIBRATION AND A YAW IN THE AIRCRAFT. THE PILOTS DECIDED TO RETURN TO WEST PALM, AND AFTER LANDING WHEN THEY GOT OUT OF THE AIRCRAFT THEY NOTICED THE LT ENGINE COWL WAS COMPLETELY MISSING. THIS HAS HAPPENEAug 28, 2003 · N746TA · Beech 400A · Nacelle/Pylon StructureSDR 6262003Bolt · failedAIRCRAFT HAD (L) MAIN TIRE FAILURE APPROXIMATELY 1000 FT INTO TAKEOFF ROLL. AIRCRAFT STOPPED SAFELY WITH NO INJURIES. FURTHER INVESTIGATION RESULTED IN FINDINGS OF FOUR (4) WHEEL BOLTS WERE LOOSE AND ONE (1) BOLT SHEARED. THIS IS THE FIFTH (5TH) OCCURANCE OJun 26, 2003 · N418CW · Beech 400A · Wheel/Ski/FloatSDR RK26001Warning System · activatedTAKEOFF ABORTED DUE TO ILLUMINATION OF LT OIL FILTER BYPASS LIGHT AND LT ENGINE OIL PRESSURE EXCEEDING RED LINE AT TAKEOFF POWER.Jun 17, 2003 · N80DX · Beech 400A · Turbine Engine Oil SystemSDR CGO2003F00006Contactor · failedINVESTIGATED PILOT COMPLAINT OF FAILED HORIZONTAL STABILIZER DEICE SYSTEM, FAIL INDICATION. REQUIRED REPLACEMENT OF HORIZONTAL STAB. DEICE SYSTEM MOSFET CONTACTORS K251, K252, K253, K254 TO RECTIFY AND OBTAIN SUCCESSFUL OPERATIONAL TEST. FAILED UNITS SHOWEDMar 27, 2003 · N740TA · Beech 400A · Airfoil Anti/De-ice SystemSDR CGO2003F00005Control Panel · inoperativeINVESTIGATED PILOT COMPLAINT OF UNSUCCESSFUL BATTERY FEEDER PREFLIGHT TESTS. PROBLEM RECTIFIED AFTER TROUBLESHOOTING BY REPLACEMENT OF PN 50284-003 DC GROUND FAULT PROTECTION PANEL (MFG) PART TSN/TSOH UNKNOWN. HAVE NOTED THIS PART PREVIOUSLY TO BE SOURCE OF Mar 27, 2003 · N740TA · Beech 400A · DC Power Distribution SystemSDR MXI2003F00000Panel · arcedELT PANEL LIGHT AROUND RTU2 (REMOTE TUNING UNIT NR 2) CIRCUIT BREAKER ARCED CAUSING SMOKE IN THE COCKPIT. REPLACED PANEL WITH NEW PANEL.Feb 1, 2003 · N476BJ · Beech 400A · Electrical Power System WiringSDR CGO2003F00002Clamp · chafedINVESTIGATED COMPLAINT OF UNLOCKED GEAR INDICATION AFTER GEAR RETRACTION. FOUND RIGHT MAIN LANDING GEAR NOT FULLY LOCKING IN RETRACTED POSITION DUE TO INTERFERENCE BETWEEN STRUT ASSEMBLY BRAKE LINE CLAMP AND ADJACENT STRUCTURE. LANDING GEAR RETRACT TESTS SATJan 16, 2003 · N743TA · Beech 400A · Nose/Tail Landing Gear Strut/AxleSDR DJFA200300001Bearing · failedAIRCRAFT IN CRUISE AT 410 FT LOST OIL PRESSURE ON NR 1 ENGINE AND ENGINE SHUTDOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT DESCENDED AND LANDED AT SRQ. PRELIMINARY REPORT INDICATES BEARING FAILURE.Jan 5, 2003 · N731TA · Beech 400A · Engine (Turbine/Turboprop)SDR CGO2003F00001Wire · shortedWHILE TROUBLESHOOTING INOPERATIVE RT LANDING LIGHT, FOUND WIRE BURNED WHERE HAD SHORTED TO LANDING LIGHT ASSY. SHELL APPROX. 2 INCHES FROM TERMINAL END. CRIMPED ON TYPE TERMINAL INSULATION MELTED, ADJACENT WIRE INSULATION PARTIALLY MELTED AND SPLIT, EXPOSINGDec 19, 2002 · N481CW · Beech 400A · Light System WiringSDR RK71Cable · out of adjustINBOARD GEAR DOORS DID NOT CLOSE AFTER LANDING GEAR RETRACTION. RETURNED TO AIRPORT EXECUTING UNEVENTFUL LANDING. MAINTENANCE FOUND RT EMERGENCY GEAR CABLE NOT ALLOWING HOOK TO CONTACT UPLOCK SWITCH. ADJUSTED CABLE IAW BEECH M/M. OP CHECK GEAR WITH NO FURTDec 14, 2002 · N402GS · Beech 400A · Landing Gear Door Retract SectionSDR DJFA2006371Switch · brokenAIRCRAFT DEPARTED, LANDING GEAR RETRACTION RED LIGHT STAYED ON AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO DEPARTURE. MAINTENANCE CHANGED LANDING GEAR OPEN SWITCH AND OPS CHECKED OK.Dec 1, 2002 · N471CW · Beech 400A · Landing Gear Position and WarningSDR 0129AAASwitch · brokenAIRCRAFT DEPARTED TRENTON, LANDING GEAR RETRACTION RED LIGHT STAYED ON AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO TRENTON, MAINTEANCE CHANGED LANDING GEAR OPEN SWITCH AND OPS CHECKED OK.Dec 1, 2002 · N471CW · Beech 400A · Landing Gear Position and WarningSDR 2002FA0001288Wire Harness · burnedWHILE MOTORING ENGINE FOR OTHER MAINTENANCE, FOUND BURNING ODOR AND SMOKE IN AREA OF MAIN BATTERY. ON VISUAL INSPECTION, FOUND POSITIVE TERMINAL AND WIRE LEADS OF CONNECTOR BURNED. ALSO FOUND DAMAGE TO BATTERY TERMINAL.Oct 21, 2002 · N134CM · Beech 400A · Electrical Power System WiringSDR 09272002Contactor · burnedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.Sep 27, 2002 · N442CW · Beech 400A · Airfoil Anti/De-ice SystemSDR 92702Contactor · burnedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.Sep 27, 2002 · N442CW · Beech 400A · Airfoil Anti/De-ice SystemSDR GMZ2002F00001Switch · failedLANDING GEAR WOULD NOT EXTEND WITH NORMAL SYSTEM. EMERGENCY EXTENSION SYSTEM WAS USED TO EXTEND GEAR. NOSE LANDING DOWNLOCK INDICATOR SWITCH / NOT LOCK SWITCH FAILED IN NOT LOCK POSITION WHICH PREVENTED SIGNAL FOR GEAR DOWN OPERATION. SWITCH FAILED CONTINUISep 12, 2002 · N800SD · Beech 400A · Landing Gear Position and Warning
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