a1r
Chilton DW-1A
The A1R Chilton DW-1A is a British light sporting single seat low wing monoplane designed and built in the late 1930s. The aircraft was intended to be cheap to build and operate, yet have an exceptional performance on low power. The fuselage is rectangular wooden structure with curved decking covered with plywood.
The wings are cantilever in three sections comprising rectangular centre section and two tapered outer sections, covered with plywood back to the rear spar fabric covering ther... The A1R Chilton DW-1A is a British light sporting single seat low wing monoplane designed and built in the late 1930s. The aircraft was intended to be cheap to build and operate, yet have an exceptional performance on low power. The fuselage is rectangular wooden structure with curved decking covered with plywood.
The wings are cantilever in three sections comprising rectangular centre section and two tapered outer sections, covered with plywood back to the rear spar fabric covering thereafter.
The landing gear is divided type, each medium pressure wheel sprung with twin coil spring shock absorber, telescopic legs and enclosed in a fairing.
The A1R Chilton DW-1A airplane is equipped with Walter Mikron-III 65 HP engine.
The aircraft uses the new Computational Fluid Dynamics (CFD) flight model along with new propeller simulation system, PBR high-definition materials and completly based on Audiokinetic Wwise sound system.
Mini IMP
Ryan S-C-W
Ryan ST-A Special
The A1R Ryan ST-A Special is a two-seat, low wing monoplane. The fuselage is of monocoque-type construction employing longerons to reinforce the stressed skin at points of concentrated load - at stick control mountings, seats, floors, cockpit cutouts and at the tail section. Eight elliptical transverse bulkheads, suitably spaced, are covered with heavy gauge aluminium alloy skin.
The wings are constructed in four fabric covered sections - two stub wings and two outer panels. The outer pa... The A1R Ryan ST-A Special is a two-seat, low wing monoplane. The fuselage is of monocoque-type construction employing longerons to reinforce the stressed skin at points of concentrated load - at stick control mountings, seats, floors, cockpit cutouts and at the tail section. Eight elliptical transverse bulkheads, suitably spaced, are covered with heavy gauge aluminium alloy skin.
The wings are constructed in four fabric covered sections - two stub wings and two outer panels. The outer panels are wire braced NACA airfoil, constructed of spruce spars, welded steel tube compression struts and aluminium alloy ribs. The stub wings are of welded steel tube construction, incorporating a walkway.
The landing gear is treadle type welded steel tube construction with shock absorber strut of oleo-spring type. The tail wheel is a steerable and full swiveling unit of welded steel tube construction, equipped with oleo shock strut.
ST-A Special airplane is equipped with Menasco-C4S 150 hp engine.
Sh-2
The A1R Sh-2 (Shavrov-2) is a single-engine light amphibious aircraft with retractable landing gear. It has a wooden monocoque fuselage with a plywood skin, a biplane configuration wing with a lower wing that is shorter in span than the upper wing. Wings have a wooden construction, with spruce spars and plywood ribs, and were covered with fabric.
The aircraft's amphibious capabilities allowed it to reach locations that were inaccessible by other means of transportation. Its rugged constructi... The A1R Sh-2 (Shavrov-2) is a single-engine light amphibious aircraft with retractable landing gear. It has a wooden monocoque fuselage with a plywood skin, a biplane configuration wing with a lower wing that is shorter in span than the upper wing. Wings have a wooden construction, with spruce spars and plywood ribs, and were covered with fabric.
The aircraft's amphibious capabilities allowed it to reach locations that were inaccessible by other means of transportation. Its rugged construction and simple design made it easy to maintain and repair in the field, which was important for expeditions to remote areas. Some variants were highly modified for specific expeditions, such as adding extra fuel tanks for longer range, or installing specialized equipment for scientific research.
Sh-2 is powered by a single five-cylinder radial engine.
The aircraft uses the Computational Fluid Dynamics (CFD) flight model with new propeller simulation system, switchable set of gauges and labels consisting of the original layout (Metric) and English (Imperial), PBR high-definition materials and Audiokinetic Wwise sound set.