The FAA released their special report on the zodiac 601XL and what deficencies they perceive in the original design and testing of the aircraft. Overall, I found the report interesting and informative. The report makes it clearer (for me anyway) how the chain of small miscalculations could collectively lead to some of these accidents.
The first issue in the report was something that I had not heard before. According to FAA analysis, the wings were 20-25% weaker than the minimum ASTM standard for a plane with a gross weight of 1320lbs.
There were also issues with how the company calculated their manuvering speed, as well as how the ASI was calibrated in individual planes. The net result (as I understand it) is that the manuvering speed listed in the POH was higher than it should be, while the ASI might indicate that the aircraft's speed was lower than it actually was. This could collectively result in a pilot imposing more stress on the wing than it was capable of taking. There are several other issues that the FAA found, but these are the one's that stood out to me. Overall, there was lots of interesting stuff in the report and food for thought.
Direct Link to the FAA report.
Direct link to the Apendix for the report.
The first issue in the report was something that I had not heard before. According to FAA analysis, the wings were 20-25% weaker than the minimum ASTM standard for a plane with a gross weight of 1320lbs.
Wing structure: FAA analysis of the aircraft showed that the loads used by theairplane.
manufacturer to design the wing structure did not meet the ASTM standard for a
1,320 lb aircraft. FAA analysis estimated that the wing design loads were 20 to 25
percent too low. Static structural tests completed in the Czech Republic, and testing
done as part of an investigation by German authorities support this conclusion. Those
tests revealed that the wing structure could not sustain the original design loads
developed by the manufacturer for compliance to the ASTM standards for a 1,320 lb
There were also issues with how the company calculated their manuvering speed, as well as how the ASI was calibrated in individual planes. The net result (as I understand it) is that the manuvering speed listed in the POH was higher than it should be, while the ASI might indicate that the aircraft's speed was lower than it actually was. This could collectively result in a pilot imposing more stress on the wing than it was capable of taking. There are several other issues that the FAA found, but these are the one's that stood out to me. Overall, there was lots of interesting stuff in the report and food for thought.
Direct Link to the FAA report.
Direct link to the Apendix for the report.