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By jeansyGolden Age Simulations have kindly granted permission for OZx to host their FSX native freeware de Havilland DH.60 Moth
The DH 60 was developed from the larger DH 51 biplane. The first flight of the Cirrus powered prototype DH.60 Moth (registration G-EBKT) was carried out by Geoffrey de Havilland at the works airfield at Stag Lane on 22 February 1925. The Moth was a two-seat biplane of wooden construction, it had a plywood covered fuselage and fabric covered surfaces, a standard tailplane with a single tailplane and fin. A useful feature of the design was its folding wings which allowed owners to hangar the aircraft in much smaller spaces. Read More...
The package hosts
3 Models included, Wheeled, float & amphibian
Multiple VC positions
8 2048x2048 dds formatted textures
and many more
Many thanks to Golden Age Simulations
By jeansyCraig from Classic Wings has kindly given us permission to host his,
Sopwith F.1 Camel
The Sopwith Camel was a British First World War single-seat biplane fighter introduced on the Western Front in 1917. Manufactured by Sopwith Aviation Company, it had a short-coupled fuselage, heavy, powerful rotary engine, and concentrated fire from twin synchronized machine guns. Though difficult to handle, to an experienced pilot it provided unmatched maneuverability. A superlative fighter, the Camel was credited with shooting down 1,294 enemy aircraft, more than any other Allied fighter of the war. It also served as a ground-attack aircraft, especially near the end of the conflict, when it was outclassed in the air-to-air role by newer fighters.
Length: 18 ft 9 in (5.71 m)
Wingspan: 28 ft 0 in (8.53 m)
Height: 8 ft 6 in (2.59 m)
Wing area: 231 ft² (21.46 m²)
Empty weight: 930 lb (420 kg)
Loaded weight: 1,455 lb (660 kg)
Powerplant: 1 × Clerget 9B 9-cylinder Rotary engine, 130 hp (97 kW)
Zero-lift drag coefficient: 0.0378
Drag area: 8.73 ft² (0.81 m²)
Aspect ratio: 4.11
Maximum speed: 115 mph (185 km/h)
Stall speed: 48 mph (77 km/h)
Range: 300 mi ferry (485 km)
Service ceiling: 21,000 ft (6,400 m)
Rate of climb: 1,085 ft/min (5.5 m/s)
Wing loading: 6.3 lb/ft² (30.8 kg/m²)
Power/mass: 0.09 hp/lb (150 W/kg)