General information about the Grob G 115
The single-engine training aircraft Grob G 115 of the German Grob Aircraft AG from Mindelheim, was built in the 1980s. Primarily, the machine was designed for aerobatics, pilot training, and for beginners and advanced training. The G 115 launched its maiden flight on 15 November 1985 and received its approval one and a half years later, in March 1987. The predecessors of the low-wing aircraft with fixed nosewheel chassis were the G 110 and the G 112 from the years 1982 and 1984. The G 115 itself, consists of 6 variants. These lead from the G 115A over the G 115B, G 115C, G 115C2, G 115D up to the G 115D2. All variants are made entirely from high surface quality fiber composites that provide high aerodynamic performance. In addition, they are fully aerobatic capable by a certified maximum load multiple of + 6 / -3g. The G 115 is still in production and has been manufactured 360 times by March 2006 alone.
Technical information about the Grob G 115
The 7.54 meter long and 2.40 meter high Grob G 115 can accommodate 2 people. The aircraft is powered by a 134-kilowatt Lycoming AEIO-360-B1F piston engine and reaches a maximum speed of up to 341 kilometers per hour. The cruising speed here is 230 kilometers per hour. The Grob G 115 has a curb weight of 670 kilograms, but can be increased to a maximum take-off and landing weight of 990 kilograms. The machine has a wingspan of 12.2 square meters, a span of 10 meters. The service summit height is 6,096 meters with a range of 1,150 kilometers.
Products and services for the Grob G 115
We would like to know you and your Grob G 115 in safety, therefore we offer not only repairs but also maintenance, servicing and inspection flights. At all times, our experts make every effort to ensure that all laws and regulations of EASA are complied with. We are happy to respond to your individual needs. Talk to us, we look forward to seeing you and your G 115!
