MT propeller.
Never flown with the Robertson, I think they dont make it anymore.
When you put the little wheel in the back, the plane still want to fly in tricycle configuration. That’s why you guys seem to end up backwards in the grass on the side of the runway so often. That little wheel knows it should be up front and will get there eventually.I didn't watch the video, but from the picture it seems the best backcountry mod would be to put the little wheel on the correct end?
One of the competing STOL makers owns the STC and makes parts but won’t sell complete setups anymore AFAICT.
The STC holder is now installing them again as new. https://skyway-mro.com/robertson-stol-high-lift-systems/
There was a period of time here they were only selling parts post the ownership transition. This was based on a phone call with them about a year ago, not sure if it’s the latest.
Big tires, big motor, big prop.
...
Wing extensions and similar STOL mods are fun when you can pick your weather but my stock wings allow me to go when other guys won’t.
Come fly into a short narrow strip cut into tall tress with an obstructed approach in 40 mph winds crossing at 45*. High lift wing candy is not your friend.
You’re welcome to have different opinions but that doesn’t make mine wrong.
Congrats on making your first post I could read without falling asleep. At least you have that going for you. Me? Still happy with what I said. When the strip's 4' wider than your gear and the wind's blowing across? Wing loading is my friend. For taking back off? Power loading is my friend. On nicer days? Nothing I've flown beats my Cub. landing at 20 mph is pretty darn cool.
And just so I contribute something - would a Peterson STOL (front mounted elevator canards, plus 260-300hp) fall into a different category because it pretty much retains the 182 wing loading? Or is there no “free lunch”?
Big tires, big motor, big prop. Those enhance capability without compromising performance in unfavorable winds.
Aerodynamics and physics make your assertions wrong. My opinions have nothing to do with it.
I don’t see how VGs could make a plane handle worse in gusts or cross winds. All they do is keep the airflow stuck to the wing at high angles of attack. Please explain - as VGs don’t affect wing loading or much of anything other than lowering stall speed, which would seem to help in gusty conditions as airspeed increases and decreases with gusts.Anything that reduces wing loading and/or stall speed will reduce the amount of crosswind or gusts that can be safely handled. Flaps or other deployable high lift devices can be retracted, yes, but wing extensions or VGs can't.
Everything is a compromise.
I don’t see how VGs could make a plane handle worse in gusts or cross winds. All they do is keep the airflow stuck to the wing at high angles of attack. Please explain - as VGs don’t affect wing loading or much of anything other than lowering stall speed, which would seem to help in gusty conditions as airspeed increases and decreases with gusts.
Or is it that you can’t actually touch down if the wing is still flying? Consider if your wing flies at 25 mph and the winds are 30 mph down the runway. You can’t even untie from the parking spot without the aircraft wanting to fly away, right? In that case you could not land the plane until the plane was going -5 mph backwards. Or you land with a 30 mph tailwind (which isn’t so bad as you are only going down the runway at 55 mph).I was thinking that @Dana was speaking in the context of flying the approach at those lower airspeeds afforded by the VG's?
Consider if your wing flies at 25 mph
Haha, it was an example, but some highly modified Cubs or the Highlander, may have stall speeds that low.If that's the performance I can expect out of VG's, I'm buying some! ;-)
I was thinking that @Dana was speaking in the context of flying the approach at those lower airspeeds afforded by the VG's?
Or is it that you can’t actually touch down if the wing is still flying? Consider if your wing flies at 25 mph and the winds are 30 mph...
But does that still apply to VGs? The airflow over a wing at a level attitude (i.e. a tricycle gear airplane rolling on a runway) is unaffected by the VGs, which only affect airflow when at high AOA. So after landing, the stock wing and the wing with VGs should have no difference in their characteristics.
The winds you can handle are proportional to your stall speed. The lower the stall speed, the less wind (cross or otherwise) you can handle.
It's why airliners fly in winds that keep single engine Cessnas on the ground, and Cessnas fly in winds that keep ultralights on the ground.
The winds you can handle are proportional to your stall speed. The lower the stall speed, the less wind (cross or otherwise) you can handle.
But does that still apply to VGs? The airflow over a wing at a level attitude (i.e. a tricycle gear airplane rolling on a runway) is unaffected by the VGs, which only affect airflow when at high AOA. So after landing, the stock wing and the wing with VGs should have no difference in their characteristics.
You may have to keep a higher airspeed (lower AOA, all things considered) than the VGs would ultimately allow you to fly (at very high AoA) when landing in high winds, but at those higher airspeeds, the AOA is probably out of the range of where the VGs have any affect as well. So say you could have an approach speed of 35 mph with VGs and stall fences, but if you fly the approach at a "stock" 55 mph, what difference would there be when the airplane is finally on the ground?
The winds you can handle are proportional to your stall speed. The lower the stall speed, the less wind (cross or otherwise) you can handle.
It's why airliners fly in winds that keep single engine Cessnas on the ground, and Cessnas fly in winds that keep ultralights on the ground.