Since you don’t seem to understand context I’ll post the whole thing:

22 - Auto Flight

2200 Auto Flight System
The units and components that furnish a means of automatically controlling flight of the aircraft. Includes those units and components controlling direction, heading, attitude, altitude, and speed. Use this code when there is insufficient information to file in a more specific JASC 2200 series code.

2210 Autopilot System
For reports of miscellaneous parts associated with the autopilot system used for controlling attitude and direction. Typical parts are yaw damper, cable, switch, sensor, relay, etc. The major components such as computer, servo, and controller are to be filed in the specific JASC 2200 series code.

2211 Autopilot Computer
For reports pertaining to the autopilot computer only. Typical parts are resistor, circuit board, capacitor, or power supply, etc.

2212 Altitude Controller
The units transmitting output information signals to automatically maintain a predetermined altitude, rate of climb, or descent. Does not include the connecting system parts such as the sensor switch. The controller make and model should be included.

2213 Flight Controller
The command unit of an autopilot system. It is manually operated to generate signals which cause the aircraft to climb, dive, or perform coordinated turns. The controller make and model should be included.

2214 Autopilot Trim Indicator
The instrument and associated circuitry that indicates the trim position selected by the pilot.

2215 Autopilot Main Servo
The unit mechanically connected to primary flight control actuating mechanisms, which is used to mechanically reposition control surfaces in accordance with electrical or pneumatic signals from a controller.

2216 Autopilot Trim Servo
The units mechanically connected to flight control cables, etc., for making minor corrections in aircraft attitude or direction.

2220 Speed-Attitude Correction System
The system which automatically maintains safe flight conditions by correcting for effects of speed and out-of-trim conditions by such means as automatic trim, mach trim, or speed stability and mach feel. This includes sensing, computing, actuating, indicating, internal monitoring, warning devices, etc.

2230 Auto Throttle System
The system that automatically controls the position of the throttles to properly manage engine power during all phases of flight/attitude. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices. Typical parts are amplifiers, computers, servos, limit switches, clutches, gearboxes, warning lights, etc.

2250 Aerodynamic Load Alleviating
The system that automatically corrects and provides for gust loading/upset, aerodynamic augmentation, alleviation, suppression, ride control, etc. This includes sensing, computing, actuating, indicating, internal monitoring, warning devices, etc.

2297 Auto Flight System Wiring
For reports indicating a problem with wiring specific to the Autoflight/Auto Pilot System.

All the auto systems on the aircraft, including autopilot, auto trim and MCAS come under auto flight. Code 2220 is what stab trim, and by extension MCAS, fall under. It’s a sub component of auto flight, just as autopilot is also a sub component of auto flight. Separate components, with very separate switches.

Where you were trying to go with 2210 and 2216 I don’t know, since none of these planes crashed due to yaw or minor course corrections. But those are a legitimate part of autopilot. 2220 is not.

I can’t be bothered to explain further since you’re clearly either refusing to listen to evidence or trolling at this point.