Why not use the F-22 to replace the F/A-18 and F-14?

"Tarver Engineering" wrote:


"John R Weiss" wrote in message
news:j1f%b.60182$4o.83386@attbi_s52...
"Tarver Engineering" wrote...

According to the ASN Accident Description, "Go-around power was added
at
14.45:35"

The pilot was past the end of the runway by then and into an unmapped
part
of the A-320's flight control system.

What is "an unmapped part of the A-320's flight control system" supposed
to
mean?!?

Airbus hadn't programmed their A-320 to do what the operator commanded.

Just prior to the pilot adding go-around power, the airplane was in an
aerodynamic regime that had been encountered many times previously --
airspeed
between stall and Vref, with a slight rate of descent (approx 375 fpm,
from last
datapoint), engines at idle. How could it be that the flight control
system was
"unmapped" in that aerodynamic regime?!?

That is a good question.

I am quite certain that the A-320's certification included slow flight and
approaches to stalls, and that its flight control system is well able to
handle
them.

Then you have departed from reality.

Jesus Christ John, this is ridiculous...I've read a lot about
this accident and agree with the consensus that the a/c did all
any a/c could have done given the parameters this not too bright
bulb asked it to do.

How in hell could the system have done more than, as JW
explained, hold the AoA at the max lift point just short of stall
while the autothrottle system applied max power and everyone was
waiting with bated breath for the engines to spool up. Would you
have preferred that the pilot have been able to manhandle the AoA
higher almost certainly stalling the wings?.

Maybe if you were a magician like Marron you could have changed
the Angle of Incidence therefore giving the wings 'more lift'?...
snort
--

-Gord.