I think that with a Boeing fbw system the crew would have had more time to fly the aircraft. The FBW system in Boeing is quite different than that of Airbus.
First of all, let us establish that the big jets always need hydraulics to actuate their control surfaces. And that the FBW takes pilot input from the stick and sends it to the hydraulics to move the control surfaces.
In an Airbus you have a series of control laws and algorithms to help ensure the plane stays within the flight envelope, there are varying degrees and levels of exactly how much the pilot input is modified before it reaches the hydraulic actuators. This system cannot be fully disabled.
In a Boeing there is basically the same setup with one difference, the pilot can cut out ALL of the control laws and modifiers. If he wanted to do so, he could jam full left rudder against the stop, at high cruising speed, and cause the plane to break-up. Or perhaps command full reverse thrust immediately after takeoff, resulting in a crash, too.
Basically, on Airbus the computer has the last say what the control surfaces do. With Boeing it is the captain and co-pilot - all computer algorithms are turned off.
I found this article which would more elegantly explain that.
http://www.fortunecity.com/marina/invincible/249/yokevsti.htm
I have some cool .pdf's that really get into the nuts and bolts and I'll post them up soon.
First of all, let us establish that the big jets always need hydraulics to actuate their control surfaces. And that the FBW takes pilot input from the stick and sends it to the hydraulics to move the control surfaces.
In an Airbus you have a series of control laws and algorithms to help ensure the plane stays within the flight envelope, there are varying degrees and levels of exactly how much the pilot input is modified before it reaches the hydraulic actuators. This system cannot be fully disabled.
In a Boeing there is basically the same setup with one difference, the pilot can cut out ALL of the control laws and modifiers. If he wanted to do so, he could jam full left rudder against the stop, at high cruising speed, and cause the plane to break-up. Or perhaps command full reverse thrust immediately after takeoff, resulting in a crash, too.
Basically, on Airbus the computer has the last say what the control surfaces do. With Boeing it is the captain and co-pilot - all computer algorithms are turned off.
I found this article which would more elegantly explain that.
http://www.fortunecity.com/marina/invincible/249/yokevsti.htm
I have some cool .pdf's that really get into the nuts and bolts and I'll post them up soon.
