Sir Geoffrey de Havilland built the first commercial jet that reached production, the Comet. The Comet design was finalized in 1945, as the British aircraft industry was attempting to establish a commercial aircraft industry post-World War II. Prior to 1954, there had been some problems (a collision at take-off and a mid-air breakup) and some fixes to the hydraulic control system. Then, on January 10, 1954 a Comet broke up in mid-air. Flights were temporarily voluntarily suspended, then resumed. On April 8, 1954, another Comet broke up in air. (Both flights were taking off from Rome.) The lives of 56 passengers and crew were lost in these two incidents, as well as two planes. Additionally, the prestige of the British aviation industry suffered a blow. (I’ll consider the lost prestige of British aviation a customer service impact.)
Let’s look at this incident in a Cause Map. A thorough root cause analysis built as a Cause Map can capture all of the causes in a simple, intuitive format that fits on one page. Although there were two separate plane breakups, the Cause Maps are the same (based on the analysis and investigation performed after the accidents). Essentially, the two planes were lost due to a structural failure of the cabin, caused by fatigue growth of a crack beyond the critical crack length (in essence, the crack length at which crack propagation is so rapid as to be uncontrollable).
The fatigue cracking of the cabin occurred because the actual pressure cycles exerted on the cabin were more than the allowable (or where cracking would occur). This was because the allowable pressure cycles were miscalculated. The allowable pressure cycles were miscalculated for several reasons. First, the inadequate test program. There was no prototype, and the fatigue tests were misleading. One test used a section that was effectively pre-conditioned, extending its life. In another test, the section tested was so small that the test results were influenced by boundary conditions.
Next, the actual stress was above the predicted stress. This occurred because 1) the square shaped windows caused pressure stresses to be distributed unevenly and 2) because the actual stress increased in localized areas. The local stress at rivet holes is far above general stress (usually along the order of three times general stress) and two rows of rivets were used to attach the window frame.
While the comet was being developed, there was a general lack of knowledge about fatigue. Many designers (de Havilland included) thought that fatigue was associated with vibration, which did not affect jet engines. Additionally, the spread in fatigue results is large (some experts quote as high as 9:1), meaning that one plane could fail nine times faster (or more slowly) than another. You can see how this is a problem with a small test sample.
A last problem was that the design of the Comet stretched the bounds of experience. The comet was designed to fly at twice the speed of other airliners, at twice the height, and at twice the cabin pressure (for passenger comfort). As such, the design was a great extension of the existing body of knowledge in not just one, but three dimensions.
Probably the most important lesson to come from the de Havilland Comet accidents is the importance of proper testing. Once the cause was discovered, the Comet was redesigned and flew successfully, although by then Boeing had mostly taken over the market share. It’s tragic that these accidents had to occur before the problem was solved.
May 28th, 2008 |