Two things occur to me that need to be answered here.This was posted back here:
http://www.defencetalk.com/forums/a...news-discussions-updates-6007-116/#post172191
Corrected link to ADM archive:
ADM: How many Buffalos make a Caribou?
I think it's an interesting idea. If they really are that much cheaper than a more modern design, it may be worth thinking about. (Of course, you'd need to ensure you compare running costs, service life, etc)
Australia already has quite a few large cargo aircraft with a range of capabilities, but they are all expensive (and highly important) assets.
Getting a low-end option would give a lot more flexibility. It may sound harsh, but the Air Force really could stand to own more planes that it can afford to lose.
Still, I'm not 100% convinced these aircraft can be delivered on time and on budget- until they start rolling off the production line, it's a risky option.
The first is the question of do we still have a need that only a Caribou can fullfil? The one unique characteristic the Caribou has is its strong STOL credentials. These may have been quite important to the military when they were purchased in the 60's (almost an operational need at the time), as the choppers available to the RAAF were no-where near as capable (Chinooks didn't arrve till 1974) and apart from Vietnam there were a large number of airfields in PNG that only a Caribou could land a decent load into.
So that's the positive side of the argument. The bad points include:
* Limited payload - now around 4 tonnes into a good strip, - apparently 30% higher if we look at re-engined/rebuilt or new turboprop Caribous - so call it 5.2 tonnes. If doing a STOL landing these figures are seriously reduced (I don't know the exact payloads but at least 30% smaller). A Chinook CH47F can drop over 10 tonnes of stores vertically into a clearing albeit at a much shorter range. A C27 whilst not as capable in a STOL environment has a payload of 11.5 tonnes, less when operating into an unpaved strip, but still higher than the Caribou could dream of.
* Speed. The very factors that make the Caribou such a brilliant STOL performer severly hamper it's airspeed and range compared to other possible replacements. Cruising speeds/ranges:
Caribou turbo prop: 322kph (est-10% higher than 293 speed of piston variant) range - unsure but said to be 60% better payload/range than piston.
CH-47F: 220kph 741km (load not stated)
C27J: 583kph 1852km at full load 11,500kg.
You are probably thinking speed doesn't matter - unfortunately it does, higher speeds = higher sortie rates = more work done.
The final point is that the only company capable of building Caribous is Viking Aircraft - a maintainer of out of production DeHavilland aircraft. They have not as yet built a Caribou (to my knowledge) they just have all the plans/jigs etc. They have started building series 400 Twin Otters, so they obviously are capable, but you'd have to ask at what rate would they be able to produce the aircraft. If we were to re-enging the existing aircraft - I'm fairly certain they do have fatigue issues (40 plus years old) and they would require an expensive and time consuming rebuild process.
In short, the role they were bought for can now be done by choppers, perhaps a smarter choice would be an aircraft that is in production that is far more capable (c-27J). Then you could fly supplies to a longer strip in the C27's and distribute from there by Chinook.
Just had another look at this site: http://www.casr.ca/doc-news-viking-buffalo-specs.htm I think they may be being a tad optimistic with their estimated speed. I would imagine the Buff would be a much draggier airframe with far less powerful engines to be claiming a speed only 15 knots slower than a C-27J may be stretching it a bit. Maybe someone can explain how adding 60 odd horsepower can increase your speed by 65 knots - does it have something to do with the derated powerplants able to produce maximum rated power over a wider range of conditions?
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