JOHN
J. NANCE
UPDATES & ANALYSES
The
Loss of Air France Flight 4590 - July 25, 2000
Tuesday afternoon Paris time a Concorde supersonic passenger
aircraft owned and operated by Air France crashed during
takeoff from Charles de Gaulle Airport near Paris, France.
In an eyewitness account aired by ABC shortly after the
crash, a professional pilot reported watching the Concorde
trailing a long plume of flame from one of its left engines
just before it lifted off the runway. He specifically commented
that the flame he witnessed was far in excess of anything
the aircraft's afterburners could produce in normal operation.
Less than 40 seconds later the Concorde's nose rose sharply
and the aircraft rolled to the left and went nose down and
inverted into a small hotel, killing all one hundred passengers
and nine crew aboard, plus four people on the ground.
Later in the day, a picture (see above) was circulated
showing the aircraft skimming the trees at a very low altitude
trailing a plume of flame from one or more engines which
was as long as the length of the fuselage (204 feet). The
photo confirmed the already highly reliable analysis of
the pilot-witness.
The Concorde was bound for New York's Kennedy Airport on
a charter flight, carrying mostly German tourists, none
of whom survived.
The aircraft involved was placed in service with Air France
in 1980, and was one of the younger Concordes. It had logged
over twelve thousand hours of flying time in the intervening
twenty years, and five thousand takeoff and landing sequences.
This is in comparison to some subsonic passenger jets that
are approaching sixty thousand hours of flight time and
almost as many cycles (or takeoff-to-landing sequences).
First, all of us should take a moment to think of the men
and women who lost their lives in this accident, and the
pain and grief of those who were left behind. I say that
not to engage in emotional manipulation, but to remind you
that even the most clinical analysis needs to hang tight
to the reality that we're discussing members of our human
family and not just facts and figures.
What caused this crash is unknowable until a full probe
has been completed (which will be done by French authorities,
who are quite competent at air accident investigation).
Keep in mind, however, that there is never just one cause
to an air accident.
In this case, the eyewitness reports and the photograph
of the crippled aircraft conclusively show that something
catastrophic occurred sometime during the takeoff sequence.
The proof of that is the extremely long and robust plume
of flames under the left wing. Initially it appeared that
the plume of flame might have been coming from one or more
of the engines, but that now does not appear to be the case.
In fact, a tire - probably the right front tire on the left
main landing gear - exploded and/or disintegrated sometime
during the take off roll after reaching commit speed. The
debris from that tire was undoubtedly thrown up and forward,
part of it being ingested by number two engine (killing
the engine quickly) and some of it being ingested by number
one engine (which slowed down and then came back up to full
power). In addition, the debris from the tire either directly
or indirectly punctured the underside of the wing creating
a massive fuel leak which immediately ignited creating the
plume of flame. And finally, the landing gear retraction
system was apparently damaged by the same explosion - all
of this occurring while the aircraft was in the vulnerable
position of being too fast to stop on the runway and yet
below rotate speed at which it could lift off the runway.
One of the remaining questions that has yet to be answered
is whether or not engine two actually exploded (in other
words, an uncontained engine failure) peppering the underside
of the wing with debris. Because the investigators have
found no engine parts on the runway and only tire debris
it appears unlikely that number two exploded, but because
it rolled back to an RPM of zero, it was clearly, massively
damaged.
Now, if just one engine had failed, even with a gigantic
plume of fire trailing behind, the remaining three engines
at full power should be able to thrust the aircraft to a
safe altitude and keep it in the air long enough to turn
it around and land it. Concorde pilots practice engine-failure-on-takeoff
scenarios in each simulator training session, and the performance
capabilities of the aircraft even at heavy gross weight
are well known. This accident, in other words, can not be
explained by a single engine loss by itself.
Concorde's engines are grouped two to a side, with engines
1 and 2 side-by-side in a metal box under the left wing,
and engines 3 and 4 in a similar metal box under the right
wing. There is a titanium "firewall" separating engine 1
from engine 2, and another separating engine 3 from engine
4. These "firewalls" are designed to be tough enough to
prevent parts from an exploding engine from coming through
to the other side and causing a second engine to fail, but
it's not a foolproof system, and there is a possibility
that a single engine disintegration could have destroyed
power on the adjacent engine - although it does not appear
it is the case in this accident.
From what investigators have said so far, we know that
the aircrew was presented with a single engine loss that
left them with a control problem from the very beginning.
With an engine out on one wing and all the remaining engines
at maximum power, the aircraft has a powerful tendency to
roll over toward the side with the inoperative engine.
This is known as an "asymmetric trust" condition, and the
only thing that can keep the aircraft flying straight (and
not rolling inverted) would be the pilots pushing the rudder
pedals to almost full right deflection in the direction
of the good engines.
Now, here's the problem: There is a minimum speed (called
a VMCA, or Velocity of Minimum Control/Air) below which
even the rudder isn't enough to keep the aircraft from rolling
inverted and crashing. If the pilots have enough power to
keep the craft flying faster than that minimum speed, they
can stay airborne. But if reduced engine power, and perhaps
metal damage to the exterior of the aircraft's wing from
the engine failure/explosion is producing too much drag,
the aircraft may slow down until the speed drops below that
critical VMCA. In fact, there is a two-engine VMCA and a
three-engine VMCA. This aircraft lifted off the runway above
the three-engine minimum control airspeed and thus the pilots
were able to continue to fly even though they could not
accelerate or climb. However, the airspeed that they were
able to maintain was 30 - 40 knots below the minimum controllable
airspeed for two engines out on one side, therefore, when
number one engine on the left side - the remaining engine
on that side - died, the aircraft instantly became uncontrollable.
That is a legitimate question, but first keep in mind the
fact that the flight lasted for less than 40 seconds, leaving
the pilots little if any time to react.
There is a specific "commit" speed on takeoff above which
you no longer have enough runway left within which to stop
the aircraft if you decided to abort. Above V1 (the commit
speed) you are all but guaranteed to run the aircraft off
the far end of the runway, and an aircraft full of fuel
can turn into a bomb as it plows off the end. This, in other
words, is not a choice a careful pilot would make once he's
accelerated above V1. Instead, he'd continue the takeoff,
supposedly secure in the knowledge that he had enough power
to handle a single engine loss.
Also, the fact that they're trailing a 200 foot plume of
fire cannot be known by the pilots because they can't see
behind the wing. Even if the pilots knew from the engine
instruments that they'd suffered an engine loss, there would
be no way to know that it had also become a massive blowtorch.
Therefore, it would be unlikely that a sudden engine or
multiple engine failure at high speed late in the takeoff
roll would have prompted the pilots to abort.
In addition, because the Concorde's wing does not have
"leading edge devices" and the type of massive flaps on
the trailing edge used by other jets to slow their takeoff
and landing speeds, Concorde must achieve nearly 220 knots
for a normal heavy takeoff, as compared to 140-160 knots
for a fully loaded 747. That's a considerable difference,
requiring a lot more thrust, and reducing the margins for
error.
Once airborne with a diminished power situation at heavy
takeoff weights, the aircraft would be in a very marginal
position aerodynamically. While fighting to just sustain
flight until they could accelerate and gain some altitude,
every pound of thrust, and every control movement, would
be critical. There is no question they would be fighting
hard to keep the wings level (for maximum lift), and under
no circumstances would they have tried to turn back to the
airport while skimming treetops at no more than a hundred
feet. Reports, in other words, that seemed to indicate that
the flight crew purposefully avoided a larger hotel or other
structures are simply wrong. This aircrew was doing their
best to just maintain control. They weren't searching for
a place to crash, because they had no intention or desire
to put the aircraft on the ground anywhere but an airport.
The fact that they did is conclusive evidence of progressive
loss of control.
Not necessarily. However, there is obviously a significant
design vulnerability in the Concorde that has shown up many
times in the past with exploded tires, damage hydraulics,
punctured fuel tanks, and engines ingesting tire debris
after such an explosion. While we are far from final determination
of all the events that led to this accident, one thing is
painfully clear: the design vulnerability and the proximity
of the engine to the tires and the ability of the engines
at high power settings on take off to suck up the debris
from an exploding tire (leading to one if not two engine
failures on one side) means that something substantive must
be changed in the equation to permit Concorde to operate
with significant assurance that this accident can never
happen again. Whether this involves using more "beefed up"
tires, greater inspection of existing tires, reducing the
service life of the tire, or some combination of the above,
it is difficult to see how either Air France or British
Air can continue to operate the Concorde without making
some substantive change or identifying a significant difference
in the existing fleet from what was on the main landing
gear of the accident aircraft.
And there's one other key point that needs to be made:
This accident should in no way diminish the incredible accomplishments
of the Concorde in operating for 27 years without scratching
a passenger. Even though its era may be coming to an end
in the near future, the Concorde's ability to routinely
travel with passengers at twice the speed of sound and deliver
them safely has validated the highest expectations of its
designers.
More later.
John J. Nance
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