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a twin-engine, six-seat amphibious aircraft

AKLAVIA13

Registered User
Warsaw
Greetings, everyone. Colleagues, may I ask for your opinion? Please tell me—would there be demand today for a twin-engine, six-seat amphibious aircraft designed so that, after landing on water, you can conveniently lower a two-seat jet ski or quad bike into the water and then lift it back aboard? It would be powered by two 180 hp Lycoming engines, and if the aircraft carries the jet ski of course only two people would be on board . Setting aside the price of a new amphibian of this kind—around one million dollars—I’m interested purely in whether such a capability would be in demand. Thank you in advance for your response.
 
For perspective, there is an STC to suspend two jet skis into pods (with winches) on the wings of the Grumman Albatross.

Jet skis are not light. The asymmetric weight and drag on a small aircraft would likely be a non starter, and as ry6ator pointed out, 180 hp engines would be massively underpowered, even without the external load.
 
Greetings, everyone. Colleagues, may I ask for your opinion? Please tell me—would there be demand today for a twin-engine, six-seat amphibious aircraft designed so that, after landing on water, you can conveniently lower a two-seat jet ski or quad bike into the water and then lift it back aboard? It would be powered by two 180 hp Lycoming engines, and if the aircraft carries the jet ski of course only two people would be on board . Setting aside the price of a new amphibian of this kind—around one million dollars—I’m interested purely in whether such a capability would be in demand. Thank you in advance for your response.
Not to be a negative Nelly or to pile on... But I have to agree with both of the other posters regarding feasibility of the project. Beyond that though - and to answer your actual question - I really don't think the demand is there for such a thing. If the whole "personal watercraft" deal is a thing to someone I can't imagine anyone to whom that task would be primary. If an aircraft met another (more commonly utilized) task set - and it just so happened that hauling watercraft could also be done - then maybe you've got an avenue in. It's my considered opinion ( and worth every penny you paid for it) that the multi engine amphib market is at full float. We don't lose a lot of them every year and the current fleet seems under utilized. I do however encourage you to build an experimental version for your own satisfaction. Of course since you appear to be considering a commercial enterprise I will remind you of the aviation truism... "The only way to make a small fortune in aviation is to start with a large one."

Best of luck whichever direction you take. Let us know if you start through the process to do this.
 
Piaggio Royal Gull.
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The Twin Bee is a 5 seat twin-engine amphibious airplane with Lycoming IO-360 180 hp engines. If you reshaped the cabin area you could accommodate the jet ski and two people. This could be done by reshaping the aft section with a rear facing cargo door. During flight testing, an FAA aerodynamicist suggested a method of reducing drag by reshaping the aft portion of the cabin. It's excellent performance is credited to it's high aspect ratio wing and flaps along with the two engines blowing air over the wings and flaps. Single engine performance is marginal. In it's day, there was a lot of interest which the factory was unable to meet. Therefor only 23 were built with not many remaining today. I was the company pilot.
https://seabee.info/twinbee_history.htm
It's doable, whether you could produce enough of them to make it financially viable is another question.
Hint: Use a left hand rotating engine on the right side and cant them both outboard a bit for better single engine handling.
Another hint: counter rotating engines on a flying boat improves the take off performance by eliminating the tendency of the left wing float digging in the water when you apply power.
 
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Wow Pete, that is an incredible amount of information in developing such a beast.

I does not seem obvious to cant engines, what an interesting solution.
 
I can think of a few places I've been getting gasoline where I would not have been able to fill my batteries. Is there a Seabear in the US? That does look to be a fun airplane.
 
I does not seem obvious to cant engines, what an interesting solution.
I looked over a McKinnon turbine Goose that used to fly into my airport occasionally.
It had outboard-canted engines, which wasn't very obvious unless you were looking at it from behind,
but then it was hard to miss.
 
These are the specs from Wiki for the Grumman Widgeon, a 5 seater. These are 'Seneca I' weights and power, so barely a 6 seater.
  • Empty weight: 3,240 lb (1,470 kg)
  • Gross weight: 4,525 lb (2,053 kg)
  • Powerplant: 2 × Ranger L-440-5 air-cooled inverted six-cylinder inline engine, 200 hp
 
These are the specs from Wiki for the Grumman Widgeon, a 5 seater. These are 'Seneca I' weights and power, so barely a 6 seater.
  • Empty weight: 3,240 lb (1,470 kg)
  • Gross weight: 4,525 lb (2,053 kg)
  • Powerplant: 2 × Ranger L-440-5 air-cooled inverted six-cylinder inline engine, 200 hp
Original with Rangers was only 5 seats. STC for other engines allowed 6 seats.
 
For some reason when I hear about the JetSki being involved in this project, under wing externally mounted stereo speakers pop into my cartoon bubble...
 

skywagon8a - does the name Gordon Newell ring a bell? 4B2, Riverside airport, was working on getting a Widgeon right with the FAA, 1992 or thereabouts…

Yes, Gordon installed Continental IO-520s with a Dean Franklin conversion on his Widgeon. Ned Rice who was a retired engineer from Pratt & Whitney helped him getting it certified as a one only STC. Ned told me that was a great performer. Ned did the engineering for the TIO-520-J2BD STC also. The FAA in Seattle designated him as a DER for the project.

I've wondered how a Continental IO-550 would do with the Dean Franklin conversion? .

NX1PA
 
Copied an older post..

Not sure what HP the IO-520s were, 285?

IO-550s with 300 would be interesting. Big improvement on Rangers.

Might benefit from a tail extension? Jet skis might be a stretch. :)
 

Gordon installed Continental IO-520s with a Dean Franklin conversion on his Widgeon. Ned Rice who was a retired engineer from Pratt & Whitney helped him getting it certified as a one only STC. Ned told me that was a great performer. Ned did the engineering for the TIO-520-J2BD STC also. The FAA in Seattle designated him as a DER for the project.​


I've wondered how a Continental IO-550 would do with the Dean Franklin conversion? .

NX1PA

Not that I've seen a whole lot of Widgeons,
but I've probably seen as many with GO-435 or GO-480 Lycomings as I have with rangers.
I've also seen a few with (IO?) 470 continentals.
520's or 550's would certainly provide some oomph.,
and be easier to support than the GO's.
 
It would be powered by two 180 hp Lycoming engines,
If you do pursue this idea, consider using the IO-360-M1A. This engine has the fuel servo mounted in the front of the oil sump thereby reducing the height of the engine. Don't even consider using a carburetor or an engine with the fuel injector servo mounted under the sump because the height of the engine will produce too much cross sectional area, thus too much drag which will make meeting the single engine control requirements likely impossible to meet. We tried using the carburetor version first on the Twin Bee and had to change to fuel injection with a forward mounted fuel servo for this reason.
 
Not that I've seen a whole lot of Widgeons,
but I've probably seen as many with GO-435 or GO-480 Lycomings as I have with rangers.
I've also seen a few with (IO?) 470 continentals.
520's or 550's would certainly provide some oomph.,
and be easier to support than the GO's.
Widgeon does not perform as well on takeoff with straight drive motors, geared motors give it amazing thrust. When light off the water in about 8 seconds.
 
Granted the larger engines in Widgeons do perform better than a Ranger powered Widgeon. I have flown a Ranger Widgeon with Hartzell controllable props, it performed very well. With the fixed pitch props, not so well. I understand why George Pappas liked that version.
 
Granted the larger engines in Widgeons do perform better than a Ranger powered Widgeon. I have flown a Ranger Widgeon with Hartzell controllable props, it performed very well. With the fixed pitch props, not so well. I understand why George Pappas liked that version.
For sure lightest Widgeon, but Ranger top ends(really bottom) did not last very long, always piston/valve issues.
George Pappas made them better with constant speed prop, and I think Dodge truck pistons.
 
If you're planning to spend big bucks on a flying boat anyway, buy or restore a PBY. Travel in style and comfort while preserving their awesome History.

By the way, flying boats aren't designed for small waterbodies or steep approaches. A float plane like an Otter might better fulfill your mission objectives. Perhaps you could design a drop down rear ramp to load personal watercraft.
 
That's true, but aklavia13 is talking about building a new design. A similar design with a modified cabin section may do the trick.
 
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