# Raytheon 200 - Type: Aircraft model (FAA registry) - Registry code: 7150064 - Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY - Model: 200 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 11 - Weight class: 12,500 to 19,999 lb - Certification: Not type certificated - Data sheet: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 0 - Page: https://openairdocs.org/model/raytheon-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. - [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [AD 2006-12-25](https://openairdocs.org/ad/2006-12-25): Actuator nut assembly · General Machine - Diecron Actuator nut assembly, 100, 200 and 15 more. Effective Jul 28, 2006 - [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005 - [AD 2005-01-18](https://openairdocs.org/ad/2005-01-18): Fuselage stringers · Textron 200, 200C, 200CT and 24 more. Effective Mar 1, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005 - [AD 98-20-38 R1](https://openairdocs.org/ad/98-20-38-R1): Airplane Flight Manual (AFM) · Textron 200, 200C, 200CT and 15 more. Effective Feb 18, 2005 - [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004 - [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004 - [AD 2004-08-15](https://openairdocs.org/ad/2004-08-15): TAWS8000 terrain awareness warning systems (TAWS) · Cessna 421, 500, 501 and 18 more. Effective Jun 7, 2004 - [AD 2003-13-16](https://openairdocs.org/ad/2003-13-16): Aft Pressure Bulkhead of Fuselage · Textron 100, 200, 200C and 33 more. Effective Aug 25, 2003 - [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003 - [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 98-08-20](https://openairdocs.org/ad/98-08-20): Autopilot Servo Actuators · Alliedsignal Avionics Autopilot Servo Actuators, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 17 more. Effective Jun 2, 1998 - [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998 - [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998 - [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997 - [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997 - [AD 97-01-12](https://openairdocs.org/ad/97-01-12): Ground Proximity Warning System · Airtell International Ground Proximity Warning System, Mystere-Falcon 200, EMB-110P1 and 20 more. Effective Feb 25, 1997 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 96-03-13](https://openairdocs.org/ad/96-03-13): Main Landing Gear Drag Leg Lock Link · Textron 100, 200, 200C and 24 more. Effective Apr 1, 1996 - [AD 95-13-03](https://openairdocs.org/ad/95-13-03): Electrical Landing Gear Motor · Textron 100, 200, 200C and 22 more. Effective Jul 28, 1995 - [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992 - [AD 92-10-12](https://openairdocs.org/ad/92-10-12): Engine Cowling Doors · Textron 200, 200C, 200CT and 18 more. Effective Jun 12, 1992 - [AD 91-12-11](https://openairdocs.org/ad/91-12-11): Side Windows · Textron 200, 200C, 200CT and 7 more. Effective Jul 15, 1991 - [AD 89-19-04 R1](https://openairdocs.org/ad/89-19-04-R1): Wing Fuel Bay Skin Panels · Textron 200, 200C, 200CT and 6 more. Effective Jul 9, 1990 - [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990 - [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990 - [AD 89-22-14](https://openairdocs.org/ad/89-22-14): Aileron Flutter · Textron 200, 200C, 200CT and 9 more. Effective Nov 17, 1989 - [AD 89-02-03](https://openairdocs.org/ad/89-02-03): Wing Main Outboard Spars · Textron 200. Effective Feb 8, 1989 - [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987 - [AD 85-22-05](https://openairdocs.org/ad/85-22-05): Nuts and Bolts Replacement · Textron 100, 200, 200C and 60 more. Effective Nov 12, 1985 - [AD 83-07-14](https://openairdocs.org/ad/83-07-14): One-Ply Window Replacement · Textron 200, 200C, 200CT and 4 more. Effective Apr 18, 1983 - [AD 80-09-03 R1](https://openairdocs.org/ad/80-09-03-R1): Placard -Oxygen · Textron 100, 200, 200C and 9 more. Effective Jun 11, 1980 - [AD 80-07-05](https://openairdocs.org/ad/80-07-05): Bolt and Nut, Wing Section · Textron 200, 200C, 200T and 10 more. Effective Apr 3, 1980 - [AD 79-01-01](https://openairdocs.org/ad/79-01-01): Screws in Control System · Textron 100, 200, 35-B33 and 34 more. Effective Jan 8, 1979 - [AD 78-20-12](https://openairdocs.org/ad/78-20-12): Aircraft Tires · Cessna 336, 337, T337B and 15 more. Effective Oct 5, 1978 - [AD 77-18-04](https://openairdocs.org/ad/77-18-04): Cabin Pressurization · Textron 200, 200T, A100 and 3 more. Effective Sep 12, 1977 - [AD 77-13-07](https://openairdocs.org/ad/77-13-07): Aileron Control System · Textron 200. Effective Jul 1, 1977 - [AD 76-22-02](https://openairdocs.org/ad/76-22-02): 'Y' Type Shoulder Harness · Textron 200, 58, 58A and 14 more. Effective Jun 2, 1977 - [AD 77-02-07](https://openairdocs.org/ad/77-02-07): Propeller Feathering · Textron 200. Effective Mar 1, 1977 - [AD 76-12-10](https://openairdocs.org/ad/76-12-10): Wing De-icing · Textron 200. Effective Jun 23, 1976 - [AD 76-10-10](https://openairdocs.org/ad/76-10-10): Cabin Door · Textron 100, 200, 65-88 and 6 more. Effective May 28, 1976 - [AD 76-09-02](https://openairdocs.org/ad/76-09-02): Bolt Hole Edge Distance · Textron 200, A100-1 (U-21J) and A200 (C-12A). Effective May 3, 1976 - [AD 76-04-02](https://openairdocs.org/ad/76-04-02): Seat Locking Pins · Textron 200, A100, A200 and 2 more. Effective Feb 26, 1976 - [AD 76-03-07](https://openairdocs.org/ad/76-03-07): Rudder Control · Textron 200 and A100-1 (U-21J). Effective Feb 20, 1976 Historical (superseded or no longer in force): - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 All 56: https://openairdocs.org/model/raytheon-200/ads.md ## Information bulletins (advisory) (4) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015 - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 - [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002 ## Registered aircraft None registered with this model now. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC07LA006](https://openairdocs.org/ntsb/NYC07LA006), Oct 12, 2006: Beech BE-200 (N528WG), Leonardtown, MD, substantial damage. Probable cause: The airplane manufacturer's inadequate landing gear downlock plate maintenance orientation information, and the disengaged main landing gear. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20061012031249A](https://openairdocs.org/incident/20061012031249A), Oct 12, 2006: Raythn 200RAYTHEON (N528WG), Leonardtown, MD, Destroyed. (-23) After landing, the right hand main gear slowly retracted during roll out. The aircraft stopped and caught fire, destroying the right wing and most of the… ## 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/raytheon-200/reports.md ## STCs that may be installed (OpenAirDocs) (409, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA4175NM](https://openairdocs.org/stc/SA4175NM): Installation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft. Raisbeck Engineering Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04221CH](https://openairdocs.org/stc/SA04221CH): Installation of Thermal Acoustic Kit. Skandia Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC - [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH - [STC SA03930NY](https://openairdocs.org/stc/SA03930NY): Installation of King Air Belly Payload Mount. Icarus Aero Inc - [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC - [STC SA01638WI](https://openairdocs.org/stc/SA01638WI): Part Fabrication and Installation of Arm Ledge System and Table Assembly for aircraft cabin interior. Aviation Fabricators Inc - [STC ST04442CH](https://openairdocs.org/stc/ST04442CH): Installation of SmartSky LiTE System. Apcela IFC JV, LLC dba Apcela ATG - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd - [STC SA01535WI-D](https://openairdocs.org/stc/SA01535WI-D): Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP). Garmin International Inc - [STC SA2300CE](https://openairdocs.org/stc/SA2300CE): Installation of Removable External Baggage Compartment. Avcon Industries Inc - [STC SA2307CE](https://openairdocs.org/stc/SA2307CE): Incorporation of STCs and associated modifications identified by Commuter Air Transport drawing list. Metrea Special Aerospace ISR Inc - [STC SA2352CE](https://openairdocs.org/stc/SA2352CE): Increase maximum zero fuel weight from 10,400 lbs. To 11,000 lbs. Metrea Special Aerospace ISR Inc - [STC SA2404CE](https://openairdocs.org/stc/SA2404CE): Installation of engine low oil pressure warning system. Metrea Special Aerospace ISR Inc - [STC SA2451CE](https://openairdocs.org/stc/SA2451CE): Installation of an external Baggage/cargo carrier "Super 60 Pod". Metrea Special Aerospace ISR Inc - [STC SA2794NM](https://openairdocs.org/stc/SA2794NM): Installation of Flight Equipment and Engineer Corp. passenger seats. Metrea Special Aerospace ISR Inc - [STC SA4058NM](https://openairdocs.org/stc/SA4058NM): Installation of Aeronautical Technologies Aft Cabin Seat, Model No. 053089. Metrea Special Aerospace ISR Inc - [STC SA4490NM](https://openairdocs.org/stc/SA4490NM): Installation of baggage compartment door. Metrea Special Aerospace ISR Inc - [STC SA6078NM](https://openairdocs.org/stc/SA6078NM): Installation of forward facing two-passenger seat. Metrea Special Aerospace ISR Inc - [STC SA00184LA](https://openairdocs.org/stc/SA00184LA): Installation of Alternate Main Landing Gear Tires, Michelin P/N 026-335-0. Metrea Special Aerospace ISR Inc - [STC SA8986SW](https://openairdocs.org/stc/SA8986SW): Installation of full turning contoured engine exhaust stacks on Pratt & Whitney Canada PT6A-38, PT6A-41, or PT6A-42 engines. Metrea Special Aerospace ISR Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC SA00416BO](https://openairdocs.org/stc/SA00416BO): Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit. Outerlink Corporation - [STC SA11855IB](https://openairdocs.org/stc/SA11855IB): Installation of the Flap Roller Bearing Assembly. Marsh Brothers Aviation Inc - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC - [STC SA00335BO](https://openairdocs.org/stc/SA00335BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC - [STC SA02264SE](https://openairdocs.org/stc/SA02264SE): Manufacture and installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc - [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC SA01615SE](https://openairdocs.org/stc/SA01615SE): Installation of winglets and related system changes. BLR Aerospace LLC - [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC - [STC ST02752SE](https://openairdocs.org/stc/ST02752SE): Installation of the Starlink Aviation System. AeroMech Incorporated - [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA2698NM-S](https://openairdocs.org/stc/SA2698NM-S): Installation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan Propellers. Raisbeck Engineering Inc - [STC SA00829CH](https://openairdocs.org/stc/SA00829CH): Installation of Butterfield Industries Air/Oil Separator System, kit Part Number BI 6001-1. Raisbeck Engineering - [STC SA02215SE](https://openairdocs.org/stc/SA02215SE): Fabrication of Inspection Panel Kit BI 9501-001. Raisbeck Engineering Inc - [STC SA1668NM](https://openairdocs.org/stc/SA1668NM): Installation of new main landing gear doors. Raisbeck Engineering Inc - [STC SA1783NM](https://openairdocs.org/stc/SA1783NM): Install Mark VI system. Raisbeck Engineering Inc - [STC SA2905NM](https://openairdocs.org/stc/SA2905NM): Installation of Butterfield Industries Flow Through Anti-Ice Kit Part Number BI 1001-1. Raisbeck Engineering Inc All 409: https://openairdocs.org/model/raytheon-200/stcs.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 - [Kisling Dwight Eugene 200](https://openairdocs.org/model/kisling-dwight-eugene-200): 0 registered aircraft, registry code 05645G8 - [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 --- 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.