ASHINGTON,
May 29 - The investigation
into the November 2001 crash
of American Airlines Flight
587 in Queens has turned up
an important flaw in the
rudder control system of the
type of aircraft flown,
although the flaw did not
play a role in that
accident, federal air safety
investigators said Friday.
The announcement comes
amid a sustained campaign by
American Airlines to blame
design deficiencies for the
crash, which killed all 260
people aboard and five more
on the ground. The flight
had just taken off from
Kennedy International
Airport for the Dominican
Republic.
In the crash, the pilot
swung the rudder in
alternate directions,
creating a side-to-side
motion in the jet that
ripped off the tail. Airbus,
the plane's manufacturer,
blamed the pilot's actions,
but American attributed the
crash to poor design of the
control system.
On Friday, the National
Transportation Safety Board
said that type of aircraft,
the Airbus A-300-600, could
suffer tail damage or crash
because the rudder could
extend too far when the
plane was accelerating
rapidly. The board
recommended that the Federal
Aviation Administration
order Airbus to redesign the
system, and to see if other
models of the plane have the
same problem.
After the 2001 crash,
investigators looked at
earlier incidents involving
the rudder of the A-300, and
focused on another American
flight, in May 1997, near
West Palm Beach, Fla. In
that case, the plane
abruptly lost 3,000 feet in
altitude because it was
flying too slowly. One crew
member was seriously
injured.
Like all big jets, the
A-300 has a rudder that can
be extended far to the left
or right to point the plane
in the desired direction in
a crosswind, when
maneuvering on the ground or
if an engine fails. But as
speed increases, less
extension of the rudder is
needed to produce the same
effect, and the plane
becomes vulnerable to
accident if the rudder moves
too far. So the plane has a
"limiter" system that
progressively reduces the
movement of the rudder as
speed increases.
But in the West Palm
Beach incident, the plane
sped up so fast as it lost
altitude that the limiter
system could not keep up.
The safety board, an
advisory panel, said Friday
that the system could not
keep up with velocity
changes faster than 2.4
knots a second, and the
plane in Florida was
accelerating at 10 knots a
second.
The New York flight,
Flight 587, was not
accelerating rapidly.
On Friday, a spokeswoman
for Airbus, Mary Anne
Greczyn, said the
manufacturer was "in
absolute agreement" with the
recommendation to redesign
the system. "We expected it
was coming," she said. "It
will add another level of
safety for those
extraordinarily rare times
when there are rapid changes
in air speed due to aircraft
upset."
Ms. Greczyn said that
Airbus had learned a great
deal from each incident but
that "they absolutely have
to be separated when you're
talking about this kind of
recommendation."
But a statement by the
airline seemed to run the
two together. American said
that it had instituted
special training for its
A-300 pilots after the 587
crash, to address "the
specific shortcomings in the
Airbus A300-600 rudder
control system that the
N.T.S.B. recommendation
involves." American said it
had cited the rudder limiter
system as a problem with the
plane in its submission to
the safety board on the
crash of Flight 587.
Laura J. Brown, a
spokeswoman for the Federal
Aviation Administration,
said that her agency had
received the recommendation
late on Friday afternoon and
would look at it next week. from
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