# Aero Commander 200 - Type: Aircraft model (FAA registry) - Registry code: 0140302 - Manufacturer (registry): AERO COMMANDER - Model: 200 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Cruise speed: 157 mph - Certification: Type certificated - Data sheet: [TCDS 3A18](https://openairdocs.org/tcds/3A18) (OpenAirDocs) - Holder: Interceptor Aircraft Inc - Registered aircraft: 1 - Page: https://openairdocs.org/model/aero-commander-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 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 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 2005-01-19](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 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 67-23-01](https://openairdocs.org/ad/67-23-01): Main Landing Gear · Interceptor 200, 200A, 200B and 2 more. Effective Aug 15, 1967 - [AD 66-28-01](https://openairdocs.org/ad/66-28-01): Elevator Trim System · Interceptor 200, 200A, 200B and 2 more. Effective Nov 19, 1966 ## Information bulletins (advisory) (1) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 ## Registered aircraft (1) - [N326WR](https://openairdocs.org/aircraft/N326WR): [Roquemore William A Jr](https://openairdocs.org/faa-owner/ROQUEMORE%20WILLIAM%20A%20JR), [Lakeland, GA](https://openairdocs.org/faa-place/GA/Lakeland), built 1966, S/N 308 ## NTSB investigations (3) 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 ERA24LA331](https://openairdocs.org/ntsb/ERA24LA331), Jul 26, 2024: Aero Commander 200 (N326WR), Valdosta, GA, substantial damage. Probable cause: An insect nest in the right main fuel tank’s vent line, which resulted in an inaccurate fuel level reading, fuel starvation, and a total loss of engine power. - [NTSB SEA91LA041](https://openairdocs.org/ntsb/SEA91LA041), Jan 13, 1991: Aero Commander 200D (N235M), Tooele, UT, destroyed. Probable cause: ENGINE FUEL SYSTEM BLOCKAGE DUE TO ICE FORMATION IN THE FUEL SYSTEM DURING A PERIOD OF WEATHER TEMPERATURE EXTREMES. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING. - [NTSB CHI68F0498](https://openairdocs.org/ntsb/CHI68F0498), Dec 29, 1967: Aero Comdr 200-D (N235M), Plymouth, MI, substantial damage ## FAA accident and incident reports (2) 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 20240726016079A](https://openairdocs.org/incident/20240726016079A), Jul 26, 2024: Aero Commander 200 (N326WR), Valdosta, GA, Substantial damage. On July 26, 2024, at approximately 1422 eastern standard time (EST), a 1966 Aero Commander model 200, sustained major damage while attempting an emergency… - [Accident 19910113002449A](https://openairdocs.org/incident/19910113002449A), Jan 13, 1991: Propjt 200D (N235M), Tooele, UT, Destroyed. Departed into near zero IMC in heavy snow shower. Turned back engine quit ditched in lake. Beleive ice blocked fuel ## 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/aero-commander-200/reports.md ## STCs that may be installed (OpenAirDocs) (108, 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 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 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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International 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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [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 SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA10682SC](https://openairdocs.org/stc/SA10682SC): Installation of alternator and voltage regulator. Hartzell Engine Technologies, LLC - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc All 108: https://openairdocs.org/model/aero-commander-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 - [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 - [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.