The Mallard is one of 3 in the Paspaley Pearling Co fleet, they were all converted and totally rebuilt from radials to turbo and were part of my responsibilities when GM Ops of the company.The pontoon is where we got off in good weather.....just have to chase off the lizards first, the pilots just manoeuvred a wing over the cross head, and it sends them off. It was a very regular thing. I guess a Chinook could do the same job, but cost more to operate.
One of the other jobs the Turbo Mallards did, is resupply of the ships in remote locations like Vansitart Bay and the Osbourne Islands in the Kimberley area of WA. It could be bringing out a specialist techie, refrigeration mechanic, etc or an urgent spare part for an important bit of kit that just isn't on board.
Interesting discussion.The Mallard is one of 3 in the Paspaley Pearling Co fleet, they were all converted and totally rebuilt from radials to turbo and were part of my responsibilities when GM Ops of the company.
One of the reasons we bought the Mallards (17 pax or 1.5 tons of stores) was that we had already tried chartering float planes and they proved to be unsatisfactory, too much of their performance was eaten up by carting around floats, speed and load were badly effected,
This latter point not has been given enough weight in the previous discussion.
The Mallards have also been used as emergency recovery vehicles bringing in casualties from offshore platforms and a seaplanes performance in choppy seas far exceeds floatplanes
Good points and good questions.If you want an amphibious plane - and remember, you need to buy the system, not just the plane - then why would you do a slap-dash job like that Herc. The amount of testing that would need, better to buy a purpose built thing like the US-2. The drag, the single engine out, the reduction in range and speed, the reduction in payload - I laughed when I saw it and I laugh now. It's a solution looking for a problem, and not a good one.
With respect to the system, there has to be some accounting for how this thing operates and where from. How does it unload? What are the weather conditions it can do (a land plane can land in rougher weather than a sea plane)? What is it's actual purpose? What's it lifting? SF - yup, can see a role there. RFSU? Absolutely. But better than a C-130 or C-17?
After that, then you need to do the $$ and workforce. But I'd be surprised if you got to that point... amphib aircraft died a natural death for a reason.
Just don't tell the fighter jocks about the F2Y....
WRT rear cargo ramp. This is not needed when unloading on water,Good points and good questions.
Herc on floats..........No
Japan has being pitching internationally the ShinMaywa US-2 for some time but still no takers.
Even their own fleet numbers are small.
A look at the shnmaywa web site and you get a good overview of what this class of aircraft can do. [ yep its a sale brochure ]
But still very impressive
By Land, Sea, or Air US-2
As a purely land based aircraft its smaller than a C-130J yet bigger than the C-27J.
For a transport, it's main drawback is the lack of a rear ramp and a flat usable cargo bay.
As a STOL aircraft in this size category, it's still an impressive plane.
For the ADF it also has the attribute of very good range
It's main party trick is or course is it's ability to also take off and land on water.
Replacing the C-27J with half a dozen US-2's with also some additional C-130J's and I'd suggest the RAAF would have some very flexible assets.
Regards S
C-17 and MRTT replacement options are just concepts at the moment. Not a lot of cash for development, especially given the emphasis on new pointy end stuff (hypersonics, 6 th Gen fighters, new vertical lift). The C-17 line should have been preserved better and the MRTT is still viable, supplement it with MQ-25s for contested space…just my opinion.I wonder what options will be on the table when contemplating the C-130J replacement. It looks like a replacement for the C-27J might well be bundled in with it and I am thinking perhaps even the C-17. Around that time Australia will also start looking at replacing the MRTT so there could be quite a few force structure options on the table.
Would it be better to go with a diverse selection of specialised aircraft or rationalise it as much as possible with just a couple of different airframe types?
It's a good trick, though. With long range it's a good fit for use in the archipelagos of the Indo-pacific, especially in settings where airfields may be damaged or hard to come by.Good points and good questions.
Herc on floats..........No
Japan has being pitching internationally the ShinMaywa US-2 for some time but still no takers.
Even their own fleet numbers are small.
A look at the shnmaywa web site and you get a good overview of what this class of aircraft can do. [ yep its a sale brochure ]
But still very impressive
By Land, Sea, or Air US-2
As a purely land based aircraft its smaller than a C-130J yet bigger than the C-27J.
For a transport, it's main drawback is the lack of a rear ramp and a flat usable cargo bay.
As a STOL aircraft in this size category, it's still an impressive plane.
For the ADF it also has the attribute of very good range
It's main party trick is or course is it's ability to also take off and land on water.
Replacing the C-27J with half a dozen US-2's with also some additional C-130J's and I'd suggest the RAAF would have some very flexible assets.
Regards S
I Assume when taking off on water the plane can point itself into a headwind, that will assist with a shorter takeoff.... Similar concept how aircraft carriers can move the boat into a head wind to assist with takeoff from a carrier..It's has amazingly short take off and landing in water, (280 and 330m respectively) whereas taking off from land requires 490m and landing requires a very substantial 1500 m. I think I understand the difference between landing in water and on the ground, water offering more resistance than brakes/spoilers when landing on terra firma. I really don't understand why taking off from land should be 210m longer than from the sea. I've asked Dr Google without finding an answer. The only thing I can think of is the angle of attack of the wing may be greater on water or increases more rapidly on water than land, thus more lift. Anyone help me?
Yes. Good point, you can nearly always take off into the wind.I Assume when taking off on water the plane can point itself into a headwind, that will assist with a shorter takeoff.... Similar concept how aircraft carriers can move the boat into a head wind to assist with takeoff from a carrier..
Pointing towards headwind as road runner mentions, But also at least from videos seen of take off's the nose points up quite a bit (guessing bouncy and such sending most the weight to the back?) which would give them a larger surface area on the wings to create lift, More lift less the pontoons are in the water meaning less drag... But thats just my spit balling.It's a good trick, though. With long range it's a good fit for use in the archipelagos of the Indo-pacific, especially in settings where airfields may be damaged or hard to come by.
It's has amazingly short take off and landing in water, (280 and 330m respectively) whereas taking off from land requires 490m and landing requires a very substantial 1500 m. I think I understand the difference between landing in water and on the ground, water offering more resistance than brakes/spoilers when landing on terra firma. I really don't understand why taking off from land should be 210m longer than from the sea. I've asked Dr Google without finding an answer. The only thing I can think of is the angle of attack of the wing may be greater on water or increases more rapidly on water than land, thus more lift. Anyone help me?
I don't think those 490 m and 1500 m are applicable to the US-2. I think what they are saying is they are the average distances for a commercial airliner, the US-2 does it in less.It's has amazingly short take off and landing in water, (280 and 330m respectively) whereas taking off from land requires 490m and landing requires a very substantial 1500 m. I think I understand the difference between landing in water and on the ground, water offering more resistance than brakes/spoilers when landing on terra firma. I really don't understand why taking off from land should be 210m longer than from the sea. I've asked Dr Google without finding an answer. The only thing I can think of is the angle of attack of the wing may be greater on water or increases more rapidly on water than land, thus more lift. Anyone help me?
Not always, if there’s a sea running then takeoff is usually parallel to the swell, slightly into wind.Yes. Good point, you can nearly always take off into the wind.