Canadair CL-84
The Canadair CL-84 "Dynavert", designated by the Canadian Forces as the CX-131, was a V/STOL turbine tiltwing monoplane designed and manufactured by Canadair between 1964 and 1972. Only four of these experimental aircraft were built with three entering flight testing. Two of the CL-84s crashed due to mechanical failures, but no loss of life occurred as a result of these accidents. Despite the fact that the CL-84 was very successful in the experimental and operational trials carried out between 1972 and 1974, no production contracts resulted.
Take off Conventionaly or.....
Vertical Take off. This is a very difficult plane for vertical take. So following instructions is important.
1. VTOL slider all the way up
2. Simontaniusly throttle up and hold pitch down/ w on the keyboard.
3. As soon as you're off the ground, pull landing gear up.
4. Slowly begin to pitch props forward and as the craft pitches forward, let off pitch down/w.
I have succesfuly done this a few times, even off the uss tiny, before uploading.
Good luck and have fun.
Specifications
General Characteristics
- Successors 1 airplane(s)
- Created On Windows
- Wingspan 51.5ft (15.7m)
- Length 67.7ft (20.6m)
- Height 20.3ft (6.2m)
- Empty Weight 18,767lbs (8,512kg)
- Loaded Weight 24,866lbs (11,279kg)
Performance
- Power/Weight Ratio 0.542
- Horse Power/Weight Ratio 0.273
- Wing Loading 55.3lbs/ft2 (270.2kg/m2)
- Wing Area 449.4ft2 (41.8m2)
- Drag Points 13121
Parts
- Number of Parts 171
- Control Surfaces 9
- Performance Cost 723
Thanx @General360 @spefyjerbf @ccooper @MrSilverWolf