AMD Zodiac

The Zodiac was developed by Avions Pierre Robin engineer Chris Heintz in the early 1970s. The Zenair CH 200 kit plane was developed as a Homebuilt aircraft, meaning that consumers can purchase the plane as components to assemble it themselves. Variants of the Zodiac have since been manufactured in Canada, Europe, the United States and South America as a factory-assembled, ready-to-fly aircraft. The company also provides engine mounts and instructions for mounting the Stratus EA 81 engine in the CH 601 series. Chevrolet Corvair engines have also been employed. There are over 1000 Zodiac aircraft flying worldwide. ==Operational history==

Safety incidents and grounding Wing-related incidents In the Netherlands, the Dutch government grounded the 12 Dutch-registered CH 601 XLs on 24 October 2008. The planes were banned from flying pending an investigation into their structural strength, following the crash of a European variant of the design (Rotax powered and maximum take-off weight) that killed two people. According to the Dutch government, since 2005, "at least seven accidents with Zenith CH601 XLs have happened in which one or both wings have failed". Zenair Europe investigated these accidents, concluded that none are due to a design defect and, after a first-hand review of the wreckage, also rejected suggestions that the aircraft in the Dutch accident experienced a structural failure. On 14 April 2009, the NTSB wrote an urgent letter to the FAA recommending that they ground all Zodiac CH 601 XLs, saying, "It appears that aerodynamic flutter is the likely source of four of the U.S. accidents and of at least two foreign accidents". The NTSB also wrote to ASTM International, the body responsible for developing standards for light sport aircraft, recommending that those standards be changed in light of the investigation. The NTSB said that the type had been involved "in six in-flight structural breakups since 2006". Zenith Aircraft disputed the NTSB's conclusions and stated in a response on their website that "[w]e continue to believe wing flutter will not occur if the control cables are adjusted properly." They also cited Zenair Europe's disagreement with the Dutch government's conclusion that that accident was caused by flutter. AMD issued a safety alert in October 2008 mandating inspections of aileron control cable tensions. The company hired an independent consultant, Dr. Uwe Weltin, an internationally recognized flutter and vibrations specialist and head of the Institut für Zuverlaessigkeitstechnik at the Technical University of Hamburg-Harburg who concluded that when the CH 601 XL is built and maintained to Zenair specifications, there is "no tendency to flutter or divergence found within the flight envelope of the CH 601 XL". The company claimed that the report clears the Zodiac design of flutter-related concerns as long as CH 601 XL is built and maintained to Zenair specifications. In reacting to the NTSB recommendations, the FAA Administrator Randy Babbit declined to ground the aircraft, and in a 13 July 2009 letter, stated, "Data indicates the CH-601XL has a safety record similar to other S-LSA and appears capable of safe flight and operations if maintained according to the manufacturer's recommendations." On 6 November 2009, an amateur-built CH-601XL broke up in flight over Arkansas, resulting in the death of the pilot. Preliminary investigation of the accident revealed a failure mode similar to that seen in the earlier crashes, as both wings separated in flight. This brought the number of crashes to seven and deaths to 11. The FAA issued a Special Airworthiness Information Bulletin on 7 November 2009 and strongly recommended that the aircraft not be flown until modifications detailed in an AMD Safety Alert are carried out. AMD and Zenith Aircraft issued documents the same day, mandating that the S-LSA version not be flown until the modifications were completed and recommended all aircraft be modified. The modifications included strengthening of the main and rear wing spar carrythroughs and the addition of aileron balance weights. The Experimental Aircraft Association also recommended grounding all affected aircraft until modifications are complete. In a statement issued by Zenith Aircraft, the designer, Chris Heintz, in response to the question "Why are you recommending this Upgrade Package? What has prompted this "180-degree" shift, from insisting that the CH 601 XL design was fine "as is", to now mandating a list of upgrades requiring more than a dozen modifications?" stated: On 12 November 2009, the FAA ceased issuing new Certificates of Airworthiness, requiring new registrants to prove that they have complied with the modifications before being permitted to fly the aircraft. In reacting to the FAA's report, the Experimental Aircraft Association's Vice President of Industry and Regulatory Affairs, Earl Lawrence, said, "The FAA did an excellent job with this investigation and deserves credit for thoroughly exploring all possibilities. EAA had vigorously pushed for comprehensive data on these accidents. We wanted to see the data, so aircraft owners knew exactly what modifications were needed and why they were needed immediately." On 20 April 2019, another wing failure accident in Bulgaria killed the pilot and passenger. ==Variants==

;Zenair CH 600 :The original version of the Zodiac, the CH 600, was designed by Chris Heintz and first flown in 1984. The aircraft was intended as a primary trainer. ;Zenair CH 601 HD :The CH 601 HD (for heavy duty) was the follow-on to the original CH 600 and incorporated many improvements to the design. The HD version had a gross weight of 1200 lbs and a standard empty weight of 530 lbs. Aircraft kits were marketed by Zenair of Midland, Ontario in Canada and by Zenith Aircraft of Mexico, Missouri. ;Zenair CH 601 HDS :The CH 601 HDS (for heavy duty speedwing) was a version of the HD with the wing span reduced to and a wing area of just . The wing also featured a tapered design with a 34 inch chord at the wing tip. ;Zenair CH 601 UL :The UL version of the CH 601 was specially designed for the Canadian Advanced Ultralight Aeroplane category that was introduced in 1991. Heintz was instrumental in the creation of the category as the author of the standards and used the CH 601 as a model for the category. The UL version had a reduced gross weight of 1058 lbs, the maximum allowed in the category. When the gross weight for the AULA category was increased to 1200 lbs in 2001 the CH 601 UL had its gross weight increased to the 1200 lb mark also. The UL version was supplied in 51% or 85% kit or completed form by Zenair in Canada and was designed for engines of . The aircraft did not neatly fit any US categories and US buyers were advised to consider the HD instead. ;Zenith CH 601 XL :The CH 601 XL was first flown in 1991 as an improved version of the HD developed for the amateur-built market and also for the American Light Sport Aircraft category. The XL features many incremental improvements over the HD, including a new wing design, wing fuel tanks to replace the fuselage tanks of the HD, new landing gear design and a new canopy. ;Zenith CH 650E :Version for the US light-sport aircraft category. ;Zenith CH 650Ei :Version for the European microlight category, with a gross weight of and a Rotax 912ULS engine of . Manufactured as a ready-to-fly aircraft by ICP srl in Italy. ;AMD Zodiac XL & XLi :The completed US Light Sport Aircraft compliant version of the XL is the AMD Zodiac produced by Aircraft Manufacturing and Design of Eastman, Georgia, USA. The aircraft is available in two versions, the XL, and the XLi. The XLi is IFR equipped for night flying and instrument flight conditions, while the XL is only equipped for VFR day and night flying. ;AMD Zodiac LS and LSi :Zodiac CH 650 in VFR and IFR versions. Standard engine is the Continental O-200 ==Specifications (AMD Zodiac XL)==