2004-04-02 / Community

Cover-ups, Foul-ups, and Credibility Lost

By Brett Hoffstadt
Cover-ups, Foul-ups, and Credibility Lost By Brett Hoffstadt


An Aeronautical Engineer Speaks Out On AA 587An Aeronautical Engineer Speaks Out On AA 587

Brett Hoffstadt is one of the many industry experts contributing to the webisite US.Read. Mr. Hoffstadt be gan working in the aerospace industry 14 years ago. He has two degrees in aerospace engineering and specializes in aerodynamics and aircraft performance. He is currently employed by an international engineering analysis company and previously worked at Boe ing as a Technical Specialist in Aero dynamics. Mr. Hoffstadt also has professional experience in structural design, composite materials, propulsion, flight simulation, and flight testing. He currently resides in Queens, New York, with his wife and daughter.

The tragedy of Flight 587 remains an open, unresolved pain for many peo ple in the City. One thing that could help significantly is an explanation. The NTSB investigation is still in progress with the final report expected some time this year. They continue to focus on the actions of the pilot, whose alternating rudder inputs are believed to have caused catastrophic loads on the vertical tail.

Recently, three major parties to the investigation submitted their own formal review of the accident to the NTSB. American Airlines (AA) and the Allied Pilots Association (ALPA) both point the finger at Airbus for de signing a rudder system that allows a pilot to produce such catastrophic loads on the aircraft. At the relatively low speeds of Flight 587, they say, pi lots should have full use of the flight controls.

In fact, this Airbus aircraft (an A300-600) has a specific device to limit the rudder deflection. It is called the Rud d er Travel Limiting Unit (RTLU). This is a controversial piece of equipment, and we will come back to it shortly.


Airbus, in their submission to the NTSB, claims that their aircraft performed exactly as designed and as req uired by all regulatory authorities. If the pilot hadn’t used such forceful and repeated rudder inputs, the tail would not have broken off and the aircraft would have survived. Therefore, the pilot is at fault, along with the train ing that taught him this behavior.

There are serious problems with the Airbus account. As shown in the March 26 U.S.Read article, there is good reason to suspect the rudder system did not function as intended on Flight 587. But there is much more to share.

There have been other incidents with A300 aircraft where the rudder created extremely high forces on the vertical tail. Although none of these tails broke off in flight, in at least one case the RTLU failed to keep the rudder within its proscribed limits. As a result, the tail experienced loads that exceeded the highest design threshold—the rupture limit. This incident happened in 1997, on American Air lines Flight 903 over Miami, Florida.

Similar to Flight 587, the pilot of Flight 903 made several strong, alternating rudder inputs as he attempted to regain control of the aircraft. Won dering about the loads on this aircraft, and why it survived when Flight 587 did not, Victor Trombettas of U.S.Read took a close look at the re cords in the NTSB database. He made some startling discoveries.


First, this pilot made nine rudder re ver sals. Sten Molin, the pilot of Flight 587, only made four. Second, Flight 903, at one point in it’s upset event, was flying faster than Flight 587 was, making all the loads on the aircraft more severe. Despite experiencing far greater forces in every direction compared with Flight 587, the tail and engines remained attached on Flight 903.

However, some of the Flight 903 load calculations (the bending forces exper ienced by the tail) weren’t readily avail able. The NTSB had relied on Air bus to provide these calculations using data from the onboard recorders. Por tions of some Airbus charts showing these calculations were covered by large boxes stating "no recorded par ameters", or "loads accuracy doubtful."

But buried in the reports, and hiding literally behind these large boxes, was actual data.

Why didn’t Airbus show all the available data? Recall the Rudder Travel Limiter Unit (RTLU). The data show ed that the rudder deflection went be yond this limiter at least five separate times during the pilot’s inputs. As a result, the vertical tail experienced loads well above the ultimate limits.

Airbus kept all this information from the NTSB in 1997 when Flight 903 was investigated.

If those loads were to have been shown, the NTSB would have asked questions. That would have pointed to the failure of the RTLU. Airbus’ mani pulation was so bold they even revised numbers in their favor when plotting values from the tables.

That was 1997. The NTSB didn’t catch the significant RTLU malfunction in the data, nor Airbus’ manipulation of the data. As a result, lessons from that flight were never learned, and honest pilots were blamed for a system that didn’t perform as expected.

Now, we come to Flight 587. Alarm ingly, the NTSB is once again entrusting Airbus to provide rudder and loads data to the NTSB. What will happen this time?

The NTSB believes the vertical tail broke off at 09:15:58.5 a.m. Airbus loads calculations for this moment are based on a rudder position of 11.5 deg rees. But the RTLU setting was 9.3 de grees. This obviously points to a fail ure of the RTLU. When the NTSB asked Dominique Chatrenet, the VP at Airbus in charge of Flight Controls, about this discrepancy, Mr. Chatrenet had an inventive answer. He said the rudder position was actually at 9.3 degrees, but it was in the process of failing. The structure was deforming, thus providing this (incorrect) rudder value of 11.5 degrees.

The problem with this is that FAA certification requires ultimate loads be withstood for three seconds. If Mr. Chatrenet is correct, the structure be gan failing immediately upon en countering ultimate loads, if not earlier. Officially, however, both the NTSB and Airbus publicly maintain the tail failed well above ultimate loads.

Yet, the NTSB was able to say "In vestigators have found no indications of any rudder system anomalies." They also did not question Mr. Chat renet further after he made his inventive statement. Why not?

There’s another place to look for in for mation. The rudder position data is filtered, or averaged, before it’s re cord ed on the flight data recorder (FDR). Therefore it is not a perfect real-time reading. There is unfiltered rudd er ped al data. The rudder pedal position is recorded in real-time without any averaging or filtering. This is therefore the most accurate record of what the rudder should be doing. This data shows the pedal went to a value of less than 7 degrees just before the alleged tail separation time, and then headed back to 4 degrees.

The pedal data does not support the theory that an 11.5-degree rudder move ment created the tremendous loads that broke off the tail. In other words, the NTSB and Airbus theory is based on manufactured data.

Clearly, if the rudder position had con tinued past 7 degrees, and then caus ed a structural failure, something other than the pilot is to blame since the rudder pedals do not indicate this occurred.

Will resolving the rudder or tail failure explain the crash of Flight 587? Probably not. After all, Flight 903 exp erienced higher loads, and more of them, without losing its tail. And there is substantial evidence—not to men tion statements from dozens of witnesses—that suggest things were go ing very wrong on the aircraft before the tail fell off. That evidence includes other debris, air traffic control transmissions, and a bridge tollbooth video showing Flight 587 in flight, to name a few sources.

There are many clues the NTSB seems to be ignoring or failing to assi milate. And for all of their attention to the vertical tail, how could they disregard what must be either an RTLU failure or a premature structural failure?

The search for answers continues at U.S.Read. From our perspective, Air bus and the NTSB have lost their credibility, and capacity, to find them.

An expanded version of this article, complete with many figures, can be found at www.usread.com.


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