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Sportsman vs Robertson STOL Kit

Cardiff Kook

FRIEND
Sisters, OR
For a skywagon- pros cons of each.

I know the Robertson drops the ailerons.

Most people seem to recommend the Sportsman- but think the Robertson drops the stall speed more.

Input appreciated
 
A stock wing Skywagon is a great airplane. Learn to fly it before you add gadgets to it. Figure out what you need.
 
In my opinion the stock Cessna wing leading edge starting in 1973 should remain unchanged. The older wings could use the modification. The aileron droop of the Robertson reduces the stall speed by several mph though it also reduces aileron control in crosswinds. That is a disadvantage in that the drooping ailerons are tied to the flaps.
 
Get either a stock wing with factory cuff or an early bird with Horton. I did like the Robertson, but as Stewart says, the stock aircraft - especially the earlier birds - are a delight to fly.

Edit: 8a's post and mine were posted simultaneously. I think we agree. I did not like the Sportsman, although I did not get the chance to fly it much before the owner put Micro VGs on it. Then, Yuk!
 
Go to this page. https://www.seaplanesnorth.com/sportsman-stol/ You will see the profile difference between the cuffs I have a Sportsman on my 180C, and love it. Basically a lot of advantages to a sportsman with no downside that is why it is a preferred cuff. Having seen the performance of a Robertson on a 180/185/206 I would get one in a heartbeat. HOWEVER, what is the mission for the plane? Do you really need any mods at all? From a cuff only standpoint I would say a Sportsman is the best and it can be added to a Roberson if you want.
DENNY
 
Cardiff, my mission doesn’t require stol mods to my wing. What my plane needed was more power. My normal destination has tall trees on the end of an 1100’ strip known for crossing winds. Adding a Pponk and good prop is the best money I ever spent. Tree clearance in much improved. For coming into that strip, I enjoy how my plane handles the winds and bumps. Getting down would be more difficult with stol mods. As you’ve heard, identify the mission and equip for it. If you need slower and shorter, take the Cub.
 
Adding a Sportsman cuff to a 1979 A185F wing with factory cuff? In my experience yielded better glide with power off, and better slow speed handling for flaps down survey work. The plane could be slowed up on landing with better reserve. What's better mean besides the way it felt and flew? I never flew it with VG's.

Gary
 
I have been flying a 63 180F. After getting pretty comfortable with the original wing, I decided to add the Sportsman STOL and VGs. I really liked the performance improvements and thought it was money well spent.

I recently upgraded to a 78 185F for more power and payload. The previous owner had installed Robertson AND Sportman with VGs. It does go slow, but the drop in aileron effectiveness seems significant. I usually land flaps 40, but am experimenting with 30 now to see if the aileron droop differences will give me back more aileron. Any suggestions would be appreciated. Thank you.
 
I have been flying a 63 180F. After getting pretty comfortable with the original wing, I decided to add the Sportsman STOL and VGs. I really liked the performance improvements and thought it was money well spent.

I recently upgraded to a 78 185F for more power and payload. The previous owner had installed Robertson AND Sportman with VGs. It does go slow, but the drop in aileron effectiveness seems significant. I usually land flaps 40, but am experimenting with 30 now to see if the aileron droop differences will give me back more aileron. Any suggestions would be appreciated. Thank you.
That is the disadvantage of the Robertson system. As I recall there is less droop with flaps 40 than with 30. Just be careful in a crosswind...use extra speed.
 
So with little or no droop at flaps 40, should the ailerons be more or less effective than with significant droop at flaps 30? Thanks for the quick response!
 
So with little or no droop at flaps 40, should the ailerons be more or less effective than with significant droop at flaps 30? Thanks for the quick response!
Up aileron is the primary force which rolls the wing. The design of your drooping system has a direct link between the flaps and the aileron neutral point. So any flap extension reduces the effectiveness of the up aileron. You may not notice a difference in roll authority between 30 and 40 flaps since generally there would be less forward speed at that setting so there would also be less roll authority.

A tip: If you find yourself in a crosswind landing and run out of aileron in a gust...quickly retract the flaps, at least part way, and lower the nose. This will increase the aileron authority when you need it most.

Take a look at your ailerons as you extend the flaps on the ground. See if my memory is correct in that when the flaps move past 30 to 40, the ailerons raise slightly.

I found it best to avoid as much crosswind as possible by landing diagonally across the runway. There is usually enough room.

Also don't be timid in using opposite rudder to help the aileron pick up a wing.
 
Up aileron is the primary force which rolls the wing. The design of your drooping system has a direct link between the flaps and the aileron neutral point. So any flap extension reduces the effectiveness of the up aileron. You may not notice a difference in roll authority between 30 and 40 flaps since generally there would be less forward speed at that setting so there would also be less roll authority.

A tip: If you find yourself in a crosswind landing and run out of aileron in a gust...quickly retract the flaps, at least part way, and lower the nose. This will increase the aileron authority when you need it most.

Take a look at your ailerons as you extend the flaps on the ground. See if my memory is correct in that when the flaps move past 30 to 40, the ailerons raise slightly.

I found it best to avoid as much crosswind as possible by landing diagonally across the runway. There is usually enough room.

Also don't be timid in using opposite rudder to help the aileron pick up a wing.
Thank you again.

You are correct about the droop decrease when going from 30 to 40. I have not measured, but it seems like the droop at flaps 40 is about the same as flaps up.

I must admit that I don’t understand your last sentence. In a big crosswind in the slip, I started drifting downwind and full aileron deflection wouldn’t stop it. I had to take out some rudder and point the nose back into the wind to stop the drift, then realign the fuselage prior to touchdown. Didn’t much care for it.

I understand your statement about landing diagonally into the wind, space allowing. I’ll have to get used to that.

It seems like accepting a slightly higher approach speed in a significant crosswind might be a good way to mitigate in a narrower runway situation.
 
Thank you again.

You are correct about the droop decrease when going from 30 to 40. I have not measured, but it seems like the droop at flaps 40 is about the same as flaps up.

I must admit that I don’t understand your last sentence. In a big crosswind in the slip, I started drifting downwind and full aileron deflection wouldn’t stop it. I had to take out some rudder and point the nose back into the wind to stop the drift, then realign the fuselage prior to touchdown. Didn’t much care for it.
There is no droop with the flaps up.

I'll not try to address how to use the rudder here, just be sure you do use it. Since you came from a 180, I sure you understand. When you found yourself in a downwind drift, it would be a good idea to increase your speed.
 
A good friend, Keith Serkes, used to fly test for Robertson. He is quite negative about the reduced aileron authority that results, enough to make me not consider buying an airplane with the mod.

It is great for seaplanes, that always land into the wind. Not so much for land lubbers.
 
A good friend, Keith Serkes, used to fly test for Robertson. He is quite negative about the reduced aileron authority that results, enough to make me not consider buying an airplane with the mod.

It is great for seaplanes, that always land into the wind. Not so much for land lubbers.
A better solution is a system which allows the ailerons to droop independently of the flaps. There was such a system which I had in my 185, it was great. It provided a 10-12 knot reduction in take off speeds. I didn't use it in cross winds or on landings. On landings it tended to make the nose more heavy. It was placarded to be used for take offs only.
 
A good friend, Keith Serkes, used to fly test for Robertson. He is quite negative about the reduced aileron authority that results, enough to make me not consider buying an airplane with the mod.

It is great for seaplanes, that always land into the wind. Not so much for land lubbers.
Based on my limited experience, I agree. The mod is certainly something I can live with, but if I was starting from scratch, I think I’d stick with the Sportman with VGs.
 
In my opinion the Wingx extended wings https://www.wingxstol.com/ would be a better choice than the sportsman cuff on the post 1973 Cessna cuffed wing airplanes. My 185 had extended wings which were not as much as the WingX, which produced a 400 fpm increase in rate of climb in addition to lower stall speeds.
 
Interesting comments, largely based on assumptions and “I heard’isms”.
TheSportsman and RSTOL are two very different modifications to the stock Cessna wing. I flew RSTOL equipped Cessna 185 and 206 working aircraft for 28 plus years, and several thousand hours. I love both mods, especially when installed on the same airplane.

First, let’s look at speeds. Stock C-185 POH calls out full flap stall speed of 49 knots. With RSTOL installed, the full flap stall speed is 37 knots. That’s 12 knots difference, which is very significant, much greater than ANY other “STOL kit”. Second, that stall speed change was documented by Robertson to the FAA during certification. Look at an RSTOL equipped airplane’s airspeed indicator: the markings reflect that decrease in stall speed, and the RSTOL incluses a “Flight Manual Supplement” which outlines those different speeds. In my experience, Robertson is the ONLY STOL mod that went through the rigorous flight testing required to actually, officially DOCUMENT what the kit does. Now look at the airspeed instrument in any of the other “STOL KITS” out there: Owl, Horton, Micro VG and yes, Sportsman. No change in speed markings…..why? Because those manufacturers essentially assert in their certification that their mods do not create any adverse flight characteristics. Yes, they were flight tested, but they have not documented ANY decrease in stall speed to the certification process. If they did, they’d have to re-mark the a/s instrument. Now, don’t get me wrong, I am NOT suggesting that those mods do NOT decrease stall speed, only that there is no official recognition of what that is. And, yes, in my experience, all those mods do either reduce stall speed some or alter stall characteristics. Just not as much as RSTOL.

RSTOL equipped aircraft droop ailerons with flap deflection, progressively, up to the 30 degree flap setting, where aileron droop is greatest. Increasing flap deflection to 40 degrees reduces aileron droop some, but that does NOT reduce aileron droop to zero. Understanding this is key to operating these airplanes. Increasing flap deflection crosswinds, I nearly always opted for flaps at 20 degrees. That offers most of the stall speed reduction of the RSTOL kit, while retaining MOST aileron effectiveness. In very GUSTY crosswinds, I sometimes opted for a no flaps landing, with or without an RSTOL kit installed. And, frankly angling into the crosswind to reduce x-wind component should be a technique in EVERYONE’S skill set. And, yes, I’ve landed RSTOL equipped airplanes in some significant X-winds.

I LOVED the comment about crosswinds never being an issue on floats…..that’s a pilot who’s never worked seaplanes in narrow sloughs, rivers, etc, obviously. One thing EVERY aspiring seaplane pilot should experience is crossing takeoff and landings…..and takeoffs are generally more challenging….but I digress.

At one point, our aircraft division wanted to “test” install a Sportsman kit on one of our 185s. They chose my assigned 185, largely because from experience, they knew I would offer an unbiased opinion in my report (and I would write a report). So, the Sportsman kit was installed on this 1985 airplane, which was equipped new with RSTOL.
Now, one characteristic of the RSTOL kit that hasn’t been noted to date in this thread is that OCCASIONALLY, RSTOL equipped airplanes, if driven to a very deep stall, with power, MAY break in the stall rather enthusiastically, and roll. This is not dangerous at altitude, the airplane recovers with proper control inputs, quite normally. But, because of that tendency, most smart RSTOL operators do not approach to land close to earth in the very bottom of that speed range. “AHA”, you say…..”what’s the point of having such a low stall speed if you can’t use it for landing?” Simple answer: The decrease in stall speed just permits one to lower the approach speed generally….most pilots I know don’t approach right AT stall speed…..the RSTOL provides a nice buffer, even at supignificantly lower approach speeds.
BUT, what I found immediately with the Sportsman added to the RSTOL was that I could push that airplane into the deep far reaches of the stall, power or no, and all that sharp break was GONE! Stalls became a very mellow operation, at very slow speeds. Now, I found myself actually approaching at VERY low speeds. Even my non pilot boss remarked how slow I was landing, and he knew nothing about the change in equipment.

Now, however, comes the best news: the Sportsman kit for the 185 comes with aileron gap seals, in addition to the significant leading edge droop. You see, the 185 has very basic, simple ailerons, which are not very effective, frankly, RSTOL or not. But, with the Sportsman kit installed, I got much of the aileron authority lost to the RSTOL back. Which meant that Sportsman kit was the second best thing we did to that airplane. RSTOL being the best.

After ten years (literally to the day) flying that 185, the crankshaft broke, and I parked the plane on a mountainside, not veryy elegantly. Doors still opened so it was a good landing, but plane was totaled.

When our aircraft folks asked me what equipment I wanted on the replacement airplane, my response was “RSTOL, Sportsman, and fuel flow computer.” Period. And so it was.

Sorry for the long rant, but there is sooooo much “stuff” out there about RSTOL that is based on hearsay.
 
First, let’s look at speeds. Stock C-185 POH calls out full flap stall speed of 49 knots. With RSTOL installed, the full flap stall speed is 37 knots. That’s 12 knots difference, which is very significant, much greater than ANY other “STOL kit”. Second, that stall speed change was documented by Robertson to the FAA during certification. Look at an RSTOL equipped airplane’s airspeed indicator: the markings reflect that decrease in stall speed, and the RSTOL incluses a “Flight Manual Supplement” which outlines those different speeds. In my experience, Robertson is the ONLY STOL mod that went through the rigorous flight testing required to actually, officially DOCUMENT what the kit does. Now look at the airspeed instrument in any of the other “STOL KITS” out there: Owl, Horton, Micro VG and yes, Sportsman. No change in speed markings…..why? Because those manufacturers essentially assert in their certification that their mods do not create any adverse flight characteristics. Yes, they were flight tested, but they have not documented ANY decrease in stall speed to the certification process. If they did, they’d have to re-mark the a/s instrument. Now, don’t get me wrong, I am NOT suggesting that those mods do NOT decrease stall speed, only that there is no official recognition of what that is. And, yes, in my experience, all those mods do either reduce stall speed some or alter stall characteristics. Just not as much as RSTOL.
This has been my biggest gripe with the Sportsman - which is installed on my 77 C180K - and was when I bought it a couple years ago. When you fly with a new CFI you have to prove to them that the stall speed is what it is - since it's not marked on the ASI. I thought that was wrong so I actually went to the trouble to track down the STC owner and it turns out remarking the ASI is not part of the STC. Per the book Vso is 48, but with the Sportsman it's closer to 40 - in my plane at least. (all speeds indicated) That changes the approach speeds - given the FAA's Vso X 1.3 - and that makes folks unfamiliar with the airplane very nervous. Doesn't effect the airplane but putting up with the folks inside is a large part of the "flying experience."

But I love the way if flies very slow. I have never run out of aileron or even come close. I do try to land with 20 or fewer degrees of flaps - because the POH calls for 20 or less on the go around. I'll use 30 or 40 when I really want to slow down a lot but generally I don't push it.

I've only flown a stock 180 once and that was about 40 years ago now so I can't compare to the stock version - and I've never flow the other cuff arrangements, but I like what I've got and see no negative.
 
If a modifier chooses to document and “officially” announce a change in stall speed based on their modification, the FAA requires a LOT of additional and rigorous flight testing, which is why most don’t. They can claim their mod reduces stall speed by X, but that’s all it is: a claim, not proven.
Pete can probably tell us the difference in testing required.
 
Mike , you have described it in a nutshell. It's a big deal in the FAA's eyes if you want to claim a change in the original certification. In the case of these leading edge cuffs for example, all they had to prove was that the LE's did no harm. I won't pretend to get into the minutia of the regulations as they apply. What they did not prove was that when combined with someone else's modification, the combination did no harm. The FAA left that up to the IA signing off the installation. A combination of two or more of these modifications could create a dangerous situation. I ask you, how is an IA authorized to determine that a particular modification does no harm with the flight characteristics? Some IAs may have extensive flight experience and some may not even have a pilot's license. Yet it states on the STC that it is up to the installer to make the determination. ?????
 
^^^^FAR 91.407 can leave it even more solely on the installer if the flight test prior to carrying persons not considered crew noted in (b), is waived per paragraph (c).

Gary
 
Robertson modified the control system. Because of that they’d be held to a greater standard than adding a cuff or VGs as far as testing. That doesn’t mean cuffs and VGs don’t provide improvements, although at altitude power-off stall speeds aren’t their strong suit and 99% of owners don’t care what they do outside of ground effect.
 
I am in the camp that says adding different mods to a wing without extensive flight testing is a mistake. Mike's Sportsman/STOL was a happy combination, but I found the Sportsman+ Micros to be not so great.
 
Robertson modified the control system. Because of that they’d be held to a greater standard than adding a cuff or VGs as far as testing. That doesn’t mean cuffs and VGs don’t provide improvements, although at altitude power-off stall speeds aren’t their strong suit and 99% of owners don’t care what they do outside of ground effect.
Stewart,
Yes, Robertson modified a control circuit, but any of the other “STOL” modifiers COULD have taken their certification to the same level, if they chose to. I’m not pointing fingers, but Robertson proved unequivocally that their mod decreased stall speed by a significant degree. The others, not so much.
I’ve experienced the benefits, or lack thereof by many of them.
 
I am in the camp that says adding different mods to a wing without extensive flight testing is a mistake. Mike's Sportsman/STOL was a happy combination, but I found the Sportsman+ Micros to be not so great.
Bob,
Being too cheap to install a Sportsman kit on my 170 B, I opted to install micro VGs. The VGs didn’t really decrease stall speed, that I could tell, but it did “mellow” the stall break a bit. That stall break wasn’t ugly at all to start, and I wished I hadn’t installed the VGs.

My current airplane was purchased with a Sportsman and VGs installed. I have no pre installation for comparison, but it’s a very docile machine, and slows nicely.

VGs can be pure magic on some wings, not so much on others. The Cub wing loves VGs. Others, not so much.
 
"They" say that the AMD VGs work well with the Sportsman. Maybe that is what you have?
I was quite comfortable at 60 indicated in a 1959 Horton 180. I was not comfortable at all in the Sportsman/Micro 180 below 70.

I loved the Robinson 185. I got the factory course in the mid-1970s. Cub-like landings! Airplane went to a wealthy rancher in Baja. 300 hp.
 
Mike , you have described it in a nutshell. It's a big deal in the FAA's eyes if you want to claim a change in the original certification. In the case of these leading edge cuffs for example, all they had to prove was that the LE's did no harm. I won't pretend to get into the minutia of the regulations as they apply. What they did not prove was that when combined with someone else's modification, the combination did no harm. The FAA left that up to the IA signing off the installation. A combination of two or more of these modifications could create a dangerous situation. I ask you, how is an IA authorized to determine that a particular modification does no harm with the flight characteristics? Some IAs may have extensive flight experience and some may not even have a pilot's license. Yet it states on the STC that it is up to the installer to make the determination. ?????
And AC 20-188 doesn't give us much either! Not only with STCs is the installer supposed to determine that there is no negative interrelationship, but also with Field Approvals and I put that on all the DER approvals and Field Approvals I do.

Digressing a few moments, my father was the east coast sales rep for Robertson back in the early 1970s and did all the test flying for the aircraft that were modified there. Fairfield Aviation was one of the few service centers that was authorized to install the RSTOL kits. As part of the installation process, every aircraft had to be flight tested prior to the modification and then again after modification. Complete stall series and controllability series needed to be flown and documented as part of the installation. It wasn't just pull the airplane in and start cutting sheet metal, the installation was a complete evaluation of the aircraft before and after installation. If the aircraft didn't measure up prior to installation it needed to be fixed so it would fly correctly before installation and then test flown again after to verify it still flew per the modified configuration. Not really the case with all the other STOL modifications.
 
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