Martin’s Eagle was built in 1986. It  has a steel frame fuselage with wood wing spars and fabric covered wings and tail surfaces. It was fully overhauled in 2014 and 2015.

Martin’s aerobatic sequences produce forces around +6 and -4 G’. This means his bodyweight bounces between 1/2 a ton positve and a 1/4 ton negative weight in his seat belts.

The Eagle is powered  by a Lycoming AEIO360 producing 210 HP and turning a three blade MT aerobatic propeller.The Eagle’s is a fully certifed for all aerobatic maneuvers and has G limits of +7 to -5 G`s