# Kisling Dwight Eugene 200 - Type: Aircraft model (FAA registry) - Registry code: 05645G8 - Manufacturer (registry): KISLING DWIGHT EUGENE - Model: 200 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 ยท Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/kisling-dwight-eugene-200 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (521, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000014](https://openairdocs.org/sdr/2026FA0000014), Jan 5, 2026: BLADE. BROKEN. CREW HEARD A LOUD POP AND #1 ENGINE VIBRATION WENT INTO YELLOW ON INDICATOR. CREW SHUT DOWN ENGINE WITH NO FURTHER INCIDENT. HAD ENGINE BORESCOPED AND FOUND A H - [SDR 9JLA 202506250001](https://openairdocs.org/sdr/9JLA%20202506250001), Jun 25, 2025: CONTROL PANEL. FAILED. YAW DAMP FAIL - [SDR 2025FA0000066](https://openairdocs.org/sdr/2025FA0000066), Jan 29, 2025: CABLE. BROKEN. DURING A PHASE 4 INSPECTION ON OUR KING AIR 200 N383JP, IT WAS DISCOVERED THAT THE MANUAL GEAR DOWN ACTUATION LEVER WOULD NOT OPERATE. UPON INSPECTION, IT WAS D - [SDR QMLA2024072920093](https://openairdocs.org/sdr/QMLA2024072920093), Jul 25, 2024: SPACER. OUT OF LIMITS. THROTTLE LINKAGE SPACER OUT OF POSITION CAUSED THE PROPELLER TO TRY TO GO INTO BETO RANGE EARLY DURING FINAL APPROACH TO RWY 18R AT KLRD. SPACER WAS LATER ADJUS - [SDR 2023FA0000856](https://openairdocs.org/sdr/2023FA0000856), Dec 30, 2023: UNKNOWN. UNKNOWN. DURING G200 ECS ZONAL INSPECTION SEVERAL FASTENERS FOUND DISCOLORED WITH POSSIBLE EVIDENCE OF ARCING IN ECS COMPARTMENT AT STN;14783MM ,FRAME 51 (FWD. BEAM PYLO - [SDR JGVR202306062001](https://openairdocs.org/sdr/JGVR202306062001), Jun 6, 2023: ROD. DAMAGED. GULFSTREAM G200 S/N 128: DISCOVERED ELEVATOR UP TRAVEL WAS SHORT APPROXIMATELY 2 DEGREES OF MOVEMENT. THE SPRING ROD WAS DISCONNECTED AND ELEVATORS WERE FOUND T - [SDR 2023FA0000266](https://openairdocs.org/sdr/2023FA0000266), May 17, 2023: SWITCH. FAILED. THE LH T/R WAS PLACED ON MMEL BY A LETTER FROM GULFSTREAM. GULFSTREAM AND NORDAM DOES NOT HAVE STOCK ON THE SWITCH NEEDED TO FIX THE T/R SYSTEM. - [SDR 9JLA2023052219508](https://openairdocs.org/sdr/9JLA2023052219508), Apr 18, 2023: ANTENNA. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE #2 COMM WOULD NOT TRANSMIT IN FLIGHT. THE MAINTENANCE PROVIDER REMOVED THE FAULTY VHF COMM 2 ANTENNA AND INSTALLED AN OVERHAUL - [SDR 9JLA2023041437810](https://openairdocs.org/sdr/9JLA2023041437810), Apr 1, 2023: BATTERY PACK. OVERHEATED. THE FLIGHT CREW REPORTED THAT THE EMERGENCY BATTERY OVERHEAT EICAS MESSAGE DISPLAYED DURING THE FLIGHT. TEMP EXCEEDED 140 DEGREES. THE FLIGHT CREW RAN THE QRH A - [SDR 1JAA20230324001](https://openairdocs.org/sdr/1JAA20230324001), Mar 24, 2023: PUMP. LEAKING. DURING CLIMB AFTER TAKEOFF, AIRCRAFT FILLED WITH SMOKE. CREW DAWNED OXYGEN MASKS, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE AIRPORT PBI. TROUBLESHOOTING - [SDR 2023F00031](https://openairdocs.org/sdr/2023F00031), Jan 16, 2023: CONNECTOR. CORRODED. EMERGENCY BATTERY OVERHEAT INDICATION IN FLIGHT. - [SDR 9JLA2023012637802](https://openairdocs.org/sdr/9JLA2023012637802), Jan 6, 2023: OUTFLOW VALVE. FAILED. THE FLIGHT CREW REPORTED THAT THE AUTO PRESSURIZATION FAILED AFTER LANDING. THE MAINTENANCE TEAM DETERMINED THAT THE OUTFLOW VALVE FAILED. A REPAIRED UNIT WAS I - [SDR 9JLA2022122940057](https://openairdocs.org/sdr/9JLA2022122940057), Dec 11, 2022: OVERHEAT SENSOR. DEFECTIVE. THE FLIGHT CREW REPORTED THAT PRIOR TO START OF ENGINES RECEIVING A LEFT HOT BATTERY INDICATION. THE BASE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT M - [SDR 2022FA0000552](https://openairdocs.org/sdr/2022FA0000552), Sep 19, 2022: CONNECTOR. SHORTED. DURING FLIGHT FROM KVNY TO MMGM, WHILE DESCENDING FOR LANDING, SMOKE WAS DETECTED IN THE CABIN: INVESTIGATION REVEALED THAT THE RIGHT AFT FACING SEAT FRAME WAS - [SDR 2022F00339](https://openairdocs.org/sdr/2022F00339), Sep 9, 2022: HYDRAULIC LINE. LEAKING. RH HYDRAULIC SYSTEM FAILURE IN FLIGHT. CAS MESSAGES DISPLAYED INCLUDED R HYDR PRESS LOW, RH HYDR FLUID LOW, AUX PUMP CAME ON, THEN ALSO SHOWED LOW PRESSURE AND - [SDR 2022F00350](https://openairdocs.org/sdr/2022F00350), Sep 6, 2022: NONE. NONE. SMOKE IN THE CABIN DURING CLIMB. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTING AIRPORT KTMB. MECHANIC NOTICED OIL ACCUMULATING ON RH ENGINE INLET. PRATT & W - [SDR 2022F00349](https://openairdocs.org/sdr/2022F00349), Aug 31, 2022: NONE. NONE. SMOKE IN THE CABIN DURING CLIMB. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTING AIRPORT KTMB. MECHANIC NOTICED OIL ACCUMULATING ON RH ENGINE INLET. PRATT & W - [SDR 2022F00139](https://openairdocs.org/sdr/2022F00139), Mar 13, 2022: TIRE. DEBONDED. DURING PRE-FLIGHT THE CREW OF N427LM NOTICED THE FOLLOWING. 1. A SECTION OF TREAD SEPARATED FROM THE NUMBER 3 TIRE. 2. DAMAGE TO A CFRP PANEL ON THE LOWER SURFA - [SDR 9JLA202202178028](https://openairdocs.org/sdr/9JLA202202178028), Feb 14, 2022: FLEX HOSE. LEAKING. THE FLIGHT CREW REPORTED THE LEFT ENGINE ROLLED BACK 20 TO 25% AFTER THE INITIAL POWER REDUCTION BEFORE RELIGHTING. THIS OCCURRED AT THE YOP OF DECENT AROUND 36 - [SDR 2022FA0000031](https://openairdocs.org/sdr/2022FA0000031), Jan 16, 2022: NONE. NONE. UPON LANDING, BOTH LEFT MAIN TIRE ASSEMBLIES WERE NOTES AS LOCKED UP AND NOT TURNING. MAINTENANCE DETERMINED THAT THE BRAKES HAD FROZEN UP FROM ICE. BOTH BRAKE - [SDR 9JLA2021121731656](https://openairdocs.org/sdr/9JLA2021121731656), Dec 11, 2021: AUDIO CONTROL. INOPERATIVE. THE FLIGHT CREW REPORTED THE CO-PILOTS AUDIO PANEL COMMUNICATION INOPERATIVE WITH PILOT SIDE. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE CO-PILOTS SIDE - [SDR 9JLA2021120831654](https://openairdocs.org/sdr/9JLA2021120831654), Dec 5, 2021: AUDIO CONTROL. INTERMITTENT. THE FLIGHT CREW REPORTED THE COPILOTS AUDIO PANEL VOLUME COULD NOT BE CONTROLLED, DEFAULTED TO FULL VOLUME. THE MAINTENANCE TEAM DETERMINED THE CO-PILOTS AUDIO - [SDR 9JLA2021120831653](https://openairdocs.org/sdr/9JLA2021120831653), Nov 29, 2021: DETECTOR. FAULTY. THE FLIGHT CREW REPORTED THE LEFT ICE DETECT FAIL AND SIDE WINDOW HEAT EICAS MESSAGES POSTED. THE MAINTENANCE TEAM DETERMINED A LEFT ICE DETECTOR FAULT. THE DET - [SDR 1JAA20211120003](https://openairdocs.org/sdr/1JAA20211120003), Nov 20, 2021: NONE. BROKEN. PER PILOT REPORT: DURING CLIMB(THRU FL360) LEFT SIDE WINDOW SHATTERED. CREW REQUESTED DESCENT, COMPLIED WITH CHECKLISTS AND DIVERTED TO ROC. - [SDR 9JLA2021110320693](https://openairdocs.org/sdr/9JLA2021110320693), Oct 31, 2021: IGNITER BOX. DEFECTIVE. THE FLIGHT CREW REPORTED RECEIVING A "RIGHT FADEC MINOR" MESSAGE. THE MAINTENANCE TEAM DETERMINED THE RIGHT NO2 ENGINE IGNITOR BOX WAS DEFECTIVE. THE UNIT WAS R - [SDR 1JAA20210825001](https://openairdocs.org/sdr/1JAA20210825001), Aug 21, 2021: CIRCUIT BREAKER. FAILED. 75 AMP EMERGENCY BATTERY CIRCUIT BREAKER ON COCKPIT OVERHEAD PANEL POPPED. THIS CAUSED LOSS OF POWER TO SYSTEMS TO INCLUDE PRESSURIZATION CONTROL. NO SIGNS OF A - [SDR 9JLA2021072829576](https://openairdocs.org/sdr/9JLA2021072829576), Jul 8, 2021: COMPUTER. DEFECTIVE. WHILE THE FLIGHT CREW WAS ATTEMPTING TO UPLOAD THE CURRENT VERSION OF THE NAV DATABASE, THE UPLOAD TERMINATED WITH POWER INTERRUPT DETECTED. MESSAGE ON CDU RED - [SDR 9JLA2021052728324](https://openairdocs.org/sdr/9JLA2021052728324), May 25, 2021: HYDRAULIC SYSTEM. FALSE INDICATION. THE FLIGHT CREW REPORTED THAT THE RIGHT HYDRAULIC QUANTITY DECREASED 1% PER 15 MINUTES. NORMAL 98% AFTER SHUTDOWN. A "LOW HYDRAULIC QUANTITY" REFILL EICAS MESSA - [SDR 9JLA2021051828322](https://openairdocs.org/sdr/9JLA2021051828322), May 1, 2021: UPLOCK SWITCH. DEFECTIVE. THE FLIGHT CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION A GEAR UNSAFE INDICATION AFTER SUCCESSFUL RETRACTION. THEY RECYCLED THE LANDING GEAR WITH NO IMP - [SDR CWQA20210412001](https://openairdocs.org/sdr/CWQA20210412001), Apr 12, 2021: CARBON SEAL. LEAKING. DURING TAKE OFF CREW NOTICED OIL SMELL AND WHITE SMOKE IN COCKPIT. CHECKLIST FOLLOWED AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION FOUND #1 ENGINE # - [SDR 9JLA2021033029571](https://openairdocs.org/sdr/9JLA2021033029571), Mar 18, 2021: O-RING. LEAKING. THE FLIGHT CREW REPORTED A BLEED AIR LEAK IN THE ACM BAY DURING FLIGHT. THE MAINTENANCE VENDOR REPLACED THE O-RINGS ON BOTH ENDS OF THE LOW LIMIT BLEED DUCT ASS - [SDR 9JLA2021030929568](https://openairdocs.org/sdr/9JLA2021030929568), Feb 26, 2021: ATTACH BRACKET. BROKEN. THE FLIGHT CREW NOTED DURING THE PREFLIGHT THE LEADING EDGE OF THE RIGHT STRAKE LOOSE. THE MAINTENANCE VENDOR GAINED ACCESS AND FOUND THE RIGHT STRAKE FORWARD B - [SDR E0YA2021011300002](https://openairdocs.org/sdr/E0YA2021011300002), Jan 12, 2021: BOTTLE. EMPTY. DURING SERVICE CHECKS, TECHNICIAN NOTICED LANDING GEAR EMERGENCY EXTENSION BOTTLE GAUGE READING ZERO. UPON SERVICING, NOTICED THE NITROGEN WAS NOT FILLING AND I - [SDR CVGA20200706001](https://openairdocs.org/sdr/CVGA20200706001), Jun 30, 2020: CONTROL CABLE. OUT OF TOLERANCE. WHILE AT ALTITUDE (41,000FT) ELEVATOR (E) AMBER, THEN RED ILLUMINATED ON PFD, FOLLOWED BY AN OSCILLATING PITCH UP (APPX 3-5 DEGREES) AUTOPILOT WAS ENGAGED DURIN - [SDR CJPA202006250001](https://openairdocs.org/sdr/CJPA202006250001), Jun 21, 2020: CIRCUIT BREAKER. BROKEN. BETWEEN DBLSS AND HRPER AT FL340 THE CAS INDICATED MULTIPLE ISSUES WITH RED WARNING AND AMBER CAUTION MESSAGES. A/P DISENGAGED AND NEITHER PRIMARY OR SECONDARY - [SDR Y9PA2020020620](https://openairdocs.org/sdr/Y9PA2020020620), Feb 4, 2020: DRAIN VALVE. LEAKING. AFTER FLIGHT CREW SQUAWKED PORTABLE WATER TANK LEAKING INTO BILGE WATER OBSERVED DRIPPING FROM FWD FUSELAGE DRAIN HOLE. UPON INSPECTION BY TECHNICIANS DISCOVERE - [SDR V0JA201910210006](https://openairdocs.org/sdr/V0JA201910210006), Oct 16, 2019: SENSOR. FAULTED. RH MAIN BATTERY OVERHEAT MESSAGE. INSPECTION FOUND BATTERY TEMP SENSOR FAULTY. - [SDR CWQA201908190001](https://openairdocs.org/sdr/CWQA201908190001), Aug 18, 2019: BATTERY. FALSE INDICATION. DURING CLIMB, CREW RECEIVED R/H BATTERY OVERHEAT YELLOW EICAS MESSAGE - 170 RED TEMPERATURE INDICATION. CHECK LIST FOLLOWED, EMERGENCY DECLARED, AND UNSCHEDULED - [SDR 2019FA0000250](https://openairdocs.org/sdr/2019FA0000250), Aug 13, 2019: BOLT. DEFECTIVE. MAIN WHEEL ASSEMBLY HAD ONE TIE BOLT FAILURE WHILE TOWING AIRCRAFT. THIS TIE BOLT BROKE TOWARDS THE CENTER WITH WHAT LOOKS LIKE A FATIGUE CRACK. - [SDR IEYA2019FA0000165](https://openairdocs.org/sdr/IEYA2019FA0000165), May 26, 2019: WARNING SYSTEM. ACTIVATED. AT 35,000', AIRCRAFT'S RED CAS MESSAGE L ENG OIL PRESS CAME ON. CREW RAN ASSOCIATED CHECKLIST, CHECKLIST CALLED OUT FOR PRECAUTIONARY ENGINE SHUTDOWN. THE CREW - [SDR Y9PA20190103191](https://openairdocs.org/sdr/Y9PA20190103191), Jan 3, 2019: MOUNT BRACKET. BROKEN. DURING A PRE-FLIGHT INSPECTION, THE MECHANIC DISCOVERED THAT THE RIGHT-WING NAVIGATION LIGHT WAS NOT ILLUMINATING. THE MECHANIC CHANGED THE LIGHT BUT THE LIGHT - [SDR Y9PA2018010319](https://openairdocs.org/sdr/Y9PA2018010319), Jan 3, 2019: MOUNT BRACKET. BROKEN. DURING A PRE-FLIGHT INSPECTION, THE MECHANIC DISCOVERED THAT THE RIGHT-WING NAVIGATION LIGHT WAS NOT ILLUMINATING. THE MECHANIC CHANGED THE LIGHT BUT THE LIGHT - [SDR IEYAN201812100001](https://openairdocs.org/sdr/IEYAN201812100001), Dec 8, 2018: UNKNOWN. PRESSURE LOSS. LOUD 'BANG FOLLOWED BY PRESSURIZATION LOSS AT 3000 - 4000 FPM. NO ASSOCIATED ANNUNCIATOR LIGHTS. OCCURRED AT 35,000'. AIRCRAFT WILL BE FERRIED TO GULFSTREAM DAL - [SDR 2018F00049](https://openairdocs.org/sdr/2018F00049), Dec 6, 2017: UNKNOWN. SMOKE. DURING TAKE OFF FROM KPBI AFTER ROTATION WE GOT A LOT OF SMOKE FOLLOWED BY A SMELL OF OIL IN THE COCKPIT AND CABIN. WE RETURNED TO KPBI AND LANDED WITH NO ISSUE - [SDR 2018F00048](https://openairdocs.org/sdr/2018F00048), Nov 21, 2017: UNKNOWN. SMOKE. ON DEPARTURE OUT OF PBI ABOUT 1000 FEET INFLIGHT WE STARTED SMELLING SOMETHING BURNING. SOON AFTER WE STARTED NOTICING A LOT OF SMOKE IN THE COCKPIT. IMMEDIATEL - [SDR W6JA2017111400017](https://openairdocs.org/sdr/W6JA2017111400017), Nov 9, 2017: DOWNLOCK SWITCH. OUT OF RIG. LEFT MAIN LANDING GEAR INDICATED UNSAFE ON SELECTION OF GEAR EXTENSION. RAN CHECKLIST, CYCLED GEAR, LANDED WITH LEFT MAIN GEAR UNSAFE INDICATION WITHOUT INCIDEN - [SDR W6JA20171030016](https://openairdocs.org/sdr/W6JA20171030016), Oct 30, 2017: WIRE HARNESS. MALFUNCTIONED. LEFT GEAR WILL NOT FULLY RETRACT UPON GEAR RETRACTION SELECTION. THE LIGHT WILL INDICATE UP WHEN GEAR SELECTOR LEVER IS PULLED UP FURTHER. IN FLIGHT THE LEFT GE - [SDR BKEA201609210501](https://openairdocs.org/sdr/BKEA201609210501), Sep 20, 2017: ENGINE. VIBRATION. ACFT DEPARTED. UPON REACHING FL 370 I, THE PILOT, REDUCED THROTTLE POWER FOR CRUISE FLIGHT. AT THIS MOMENT THERE WAS A LOUD BANG AND A JERK HEARD AND FELT FROM - [SDR K95A201709190001](https://openairdocs.org/sdr/K95A201709190001), Sep 15, 2017: ELEVATOR SYSTEM. MALFUNCTIONED. THE PIC CALLED MX CONTROL TO ADVISE THEY HAD NO CONTROL OF ELEVATORS WHILE AT CRUISE. QRH WAS FOLLOWED AND SLIGHT MOVEMENT OF THE LEFT YOKE ONLY WAS GAINED, BUT - [SDR W6JA20170530014](https://openairdocs.org/sdr/W6JA20170530014), May 26, 2017: SWITCH. FAILED. WHILE DESCENDING THROUGH 15,000 FT AT 320 KIAS, THE RUDDER TRIM WENT INTO FULL DEFLECTION. REPLACED THE RUDDER TRIM SWITCH WITH UPGRADED PART. All 521: https://openairdocs.org/model/kisling-dwight-eugene-200/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech 200](https://openairdocs.org/model/beech-200): 234 registered aircraft, registry code 1152920 - [Aero Commander 200](https://openairdocs.org/model/aero-commander-200): 1 registered aircraft, registry code 0140302 - [Mccollough Bill L MD 200](https://openairdocs.org/model/mccollough-bill-l-md-200): 1 registered aircraft, registry code 05612XX - [Laser 200](https://openairdocs.org/model/laser-200): 0 registered aircraft, registry code 05626X5 - [Gulfstream Aerospace LP 200](https://openairdocs.org/model/gulfstream-aerospace-lp-200): 0 registered aircraft, registry code 3980213 - [Meyers Industries 200](https://openairdocs.org/model/meyers-industries-200): 0 registered aircraft, registry code 5650302 - [Raytheon 200](https://openairdocs.org/model/raytheon-200): 0 registered aircraft, registry code 7150064 --- 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.