All speculations in
HERE about the 737 flight control systems -- wrong.
The 737 FLCS is not fly-by-wire. It is a
COMPUTER ASSISTED mechanical hydraulics system. Here is how the system works...
There are two parallel command paths: cockpit and computer (flight control computer or FLCC).
The cockpit commands the yoke and rudder, so for ease of explanation, yoke + rudder = cockpit.
Cockpit commands pitch up. The mechanical linkages runs from cockpit to hydraulics actuators and make the airplane pitch up. As the airplane pitches up, the FLCC adds its own command to smooth out any movement fluctuations. This is called 'stability augementation'.
www.sciencedirect.com
There are three SAS for pitch, roll, and yaw axes. The FLCC needs inputs from the Central Air Data Computer (CADC).
Description An air data computer (ADC) is an essential avionics component found in aircraft. This computer, rather than individual instruments, can determine the calibrated airspeed, Mach number, altitude, and altitude trend data from an aircraft's Pitot Static System. In some very high speed...
skybrary.aero
The CADC needs inputs from pitot/static and angle-of-attack (AOA) probes that are mounted
OUTSIDE the airplane.
Technical website for Boeing 737 pilots and engineers. Site includes news, system and operating notes, technical photographs, databases and related links.
www.b737.org.uk
The entire process is a closed loop system.
The Flight Data Recorder (FDR) contains critical information about the FLCS, propulsion, environmental controls, lighting, and so on.
So for all of you guys who thinks just because you can operate a home PC, from DOS to Windows, means you can understand aviation to the point that you can preempt aviation mishap investigators, here is a hypothetical question...
What if the FDR recorded a command from the FLCC but
NOT from cockpit? Is it possible that such a condition could occur?