But you are joking an aircraft need absolutely an apu…
not really.
if one generator fails, you still have the other
it is NOT a safety issue except in the remarkably unusual case that both fail on the same flight
if you bought an entire fleet of C-295’s i would be surprised if this happened even once in their entire lifespan
Gee guys, get over it.
The EADS offering was a good aircraft, but it was not chosen, learn to live with it, or not, the choice is yours.
there is never any point in discussing anything on this forum because we can’t change anything, yet that never seems to stop us
yes i realize the C-27J won, but no harm in arguing why i thought that was the wrong decision until i convert you all over to my side 😉
No, that is specious reasoning. The reality is that the need was for an aircraft capable of performing a mission that the C-23 could not do, and without recourse to C-130s.
yes, but why did they not want to have to use C-130’s in the first place?
what was the entire point of this little competition?
if the C-130 is safer and more capable, why not just get more of them . . . unless there was SOME OTHER FACTOR in play . . . anyone? . . . care to hazard what that might be?
so they show off how it can do A, B, D and F, and conveniently leave out references to C and E. This is not dishonesty, it is salesmanship.
so you would agree that in all likelihood their assertion of 50% lower operating costs is not dishonest and a reasonably fair estimate?
You seemed to agree earlier that the C-130 fleet was pretty heavily tasked….now you’re going back on that statement?
it is heavily tasked NOW, once the JCA is operational it’s load will drop off considerably
All companies have a way of making their aircraft look better…you have to take what they ALL say with a grain of salt.
sure, examine it critically, but you can’t just dismiss it out of hand
Are you a pilot yourself? It certainly does matter what the flight crews want and need in something like this. The whole crux of the C-17 program was to design an airlifter that was built with input from loadmasters, pilots, etc. Obviously pilot input is not the only thing you take into account, but it’s certainly an important factor in many cases.
obviously pilot input is and should be considered
it just isn’t always the most important factor
Cost is not the end all be all of everything. Flexibility, as they taught me during my officer training, is the key to airpower. When you gain an aircraft with not only the capability to replace the one you need replaced, but to do a much wider variety of missions
the JCA isn’t replacing the C-130
You seem to think that relativley small increase in cost compared to the C-295 is simply not worth it
50% difference in operating costs isn’t small
if the Army gains additional capabilities that not only allow it to do everything the C-23, C-12, and C-26 could do, but it is also able to relieve some of the burden on the C-130 fleet as well as perform some missions that helicopters might be forced into at this point……then it’s certainly worth it.
the C-295 will do all this
The simply irrefutable fact is that the C-130J can do the job it needs to, and is safer than the C-27J. This is undeniable. The C-27J can be argued to do a similar job, but is not quite as safe, not quite as capable, and overall doesn’t do the job as well. It is, however, a bit cheaper, but not by a massive margin.
so you would argue that they should just get the C-130J instead and forget about the not-as-reliable, not-as-capable C-27J?
(see how easy that was to turn around)
Dude are you joking????
What do u expect that EADS-CASA says about the C27J ant their C295?
A good source……
just because it’s from the competition doesn’t mean it’s not true
Open your eyes, look the contenders and read data You will discover a true military plane and not an adapted cilvilian freighter.
i think we established that. The question is how much difference does it make
Or better ask to a military pilot that has to fly Iraq or Afghanistan if He prefers to have an airplane that land and take off quickly, has more safety system or if He preferes a civilian freighter
as cold as it sounds, it doesn’t particularly matter what the pilot wants
that save the cost of fuel about 15% (not more Eads-Casa says bullocks with 50%)
source?
in case of engine stop has not APU to restart the engine.
this is only an issue if both engines fail simultaneously
in what situation would that occur but they both be recoverable? (for instance out of gas, both fail, but can’t restart even with apu)
…….. when you need some Humvees
you have a buttload of C-130’s sitting around doing nothing that will be happy to do the mission
all missions we currently do can be done with aircraft currently in the fleet (duh)
the JCA isn’t to add new capability, it’s to make the 90% of cases substantially cheaper
http://www.defenseindustrydaily.com/2007/06/joint-cargo-aircraft-we-have-a-winner/index.php#more
C-295M has a longer fuselage for more cargo pallets, comes with a nifty pallet loading system, and is cheaper to maintain and fly, but lacks the internal dimensions and/or floor strength required for tactical loads like Humvees, small helicopters, et. al.
. . .
EADS-CASA claims the C-27J’s fuel and maintenance needs give it operational costs that are over 50% more expensive than the C-295’s, but C-130J commonality may bring those numbers down slightly and the C-27J’s internal dimensions and floor strength give it the flexibility to carry light tactical loads.
. . .
Surprisingly, word was that the US Army wanted the C-295 despite its tactical limitations, and the USAF wanted the C-27J despite is operating and maintenance costs.
50% cheaper to operate is NOT ‘a buck or two’ that is absolutely HUGE
granted that is the competitor’s claim, but i don’t see them refuting it either. If it’s even halfway based in reality that is tough to swallow
Now let’s recall that the C-130J’s AVERAGE payload was 2.3 tons. Let us thus say that the median payload was 2.3 tons (i know that’s not necessarily true, but probably close enough). If this follows anything approaching a normal distribution curve, the C-295’s capability of over 10.2 tons will handle >90% of all C-130 missions. The C-27J’s 12.7 ton capacity plus bigger dimensions would probably push that to >95%.
is 50% extra operating costs worth being able to handle 5% more missions?
you can argue that it gives more flexibility for moving vehicles, but
1. once you reduce the C-130’s workload by 90% (assuming a big enough fleed of JCA’s), you will have PLENTY of capacity to move all the vehicles you want
2. the army doesn’t fly their vehicles around that often
3. if that was a serious point, why not just get C-130s and be done with it?
4. the coup de grace, the army itself DIDN’T WANT THE CAPABILITY
they apparently viewed being able to do the vast majority of missions far cheaper as more important than being able to occasionally move vehicles which now the Herc fleet will have plenty of time to do.
as far as the militarization, i would be surpised if more than 2 C-295s would have been lost over their career because they weren’t as ‘robust’ as the C-27J. (not saying only 2 would have been lost, but that the difference between the C-27J and the C-295 wouldn’t have been more than 2) And with 50% lowering operating costs, they could probably lose 10 extra and still have it be worthwhile.
and it still really bugs me that that the C-27J can only carry 3 pallets (they call it 3.5 but you can’t cut a pallet in half). I really, really wish they had extended it to make it at least 4. That would be a 33% increase in pallet capacity for a minimal increase in cost. If you have to deliver 4-5 pallets that will take 2 C-27J’s instead of 1 C-295, increasing risk and exposure.
finally take a look at this page:
http://www.c-295.ca/compare/compare.htm
it makes it seem like it doesn’t use the hydraulic system for flight control so a dual system isn’t necessary(?) and it makes the point that the C-27A’s in air force service were retired because of high operating costs and support problems
I add that in quiet normal conditions, features like double hidraulic circuit, Apu and a short runaway to take off are not important face the consume of fuel, but let me say that when a military aircraft has to work in dangerous thatre where there are nice enemy guys with their own RPG this features are far more important that a some gallon of fuel.
how many aircraft has the airforce/army lost over the last 20 years because they only had a single hydraulics system?
this is an honest question, i don’t know
also the C-130 doesn’t have what i would call a true dual system yet it seems to get by
http://members.tripod.com/~Motomom/C130EAW
a. Utility hydraulics system
Runs half of all the flight controls, nosegear steering, normal brake operation and is located on the forward section, port side of the main landing gear. Operated by engines 1, and 2.
b. Booster hydraulic system
Runs half of all the flight controls. Located on the forward section, starboard side of the main landing gear. Operated by engines 3, and 4.
c. Auxiliary hydraulic system:
Runs the cargo door, ramp, and emergency brakes. Portside aft of paratroop door. Operates in manual or electric mode. Can also be used for troubleshooting/operational checkout of flight controls on deck, in conjunction with the Ground Test Checkout Valve.
irtusk,
have you seen th comparison that I posted?
The true difference is that the C27J is a military aircraft, born with military standard. Not the same for C295.
For the Army is important that when in dangerous operation the airplane can operates at the best. C27J chas more Engine Restart Options, Apu, double Hydraulic Circuit, less runaway to land and take off, more power on the engine, etc.
the double hydraulics is undoubtedly a nice feature, but how useful is it really? if you were onboard and happened to need it, obviously you would say it is critically important. But in the clinical sense, i can’t find any instances where Army Sherpas were lost because they only had 1 hydraulic system. 2 were lost because of center-of-gravity issues. There may be more, i just haven’t been able to find them
i compare it to the F-35 for carrier ops. It only has one engine. Some people say that’s no good because if one goes out you’re in deep trouble. That is true, but it happens so infrequently the navy can afford the losses (cold as it may sound)
It’s worth noting that the commonality of engines and avionics beetween C27J and C130J permit to save a lot of money for mantainance, training, etc.
it won’t save any money on commonality on the army side and it will definitely cost more in fuel . . .
to reiterate, there’s no doubt that the C-27J is more capable than the C-295
but then again the C-130J is more capable than the C-27J, so maybe they should get C-130’s instead?
but wait! the C-17 is more capable than the C-130J, why not get that?
at some point you have to ask ‘What is the right sized plane for the mission?’ And I believe that the C-295 is ‘the right size’
an interesting link on this:
http://www.nxtbook.com/nxtbooks/aw/dti0507/index.php?startpage=38
makes a few points:
1. fuel-efficiency of the C-295 will reduce need for forward air-refuelling points
2. the C-295’s cabin dimensions more closely match the CH-47’s tall hold, speeding any transfer of Army-size pallets between the two aircraft
3. the C-27J is wider but not as tall as the CH-47
4. the airforce likes the C-27J because it shares engines and avionics with the C-130J
although i must admit i’m not sure about the point about taller pallets as the C-295 seems to claim it that it’s cargo bay is 74″ high while the C-27J claims it can accomodate 83″ pallets.
You must have not read one of my main points.
you are right, you posted yours while i was composing mine
Operating costs of the C-27 are still going to be well below those of the C-130 and although more expensive than the Sherpa, the lack of capability of the latter kinda necessitates an aircraft with the performance and capabilities of the C-27.
no argument that the Sherpa has to go
It also provides the Army with its own aircraft for air dropping certain cargos or having a cargo bay full of paratroops……a lot more than the Sherpa and a good amount more than the smaller C-295.
you are wrong here, the C-295 carries 49 fully-equipped paratroops while the C-27J carries 46 paratroops + 2 loadmasters
Air Force C-130’s are incredibly heavily tasked (trust me, I’m in the Air Force and I’ve seen this first-hand) and anyway the Army can relieve just a little bit of of the duties and place them in their own house it makes things a bit easier for the Air Force, allowing them to task -130’s for other duties.
no argument here
it’s just that it’s doing stuff it is ill-suited to do
like flying out somewhere to deliver one battery or what have you
Now, if you want my opinion the question is not why did the Army choose the C-295…….the question is why is the Air Force even buying the C-27 to begin with. It’s certainly a capable airplane, but I don’t really understand where it will fit in…..it will add a fourth airlifter type (not counting aircraft like KC-10’s and KC-135’s being used on cargo missions), to the USAF inventory and I’m not really understanding what they will use it for at this point.
this gets to the heart of the problem. if you’ve followed this sordid affair from the beginning, the airforce has basically been doing everything in their power to undermine the army on this. They NEVER saw a need for a plane like this until the army tried to get it. Then suddenly they decided they needed their own program. Then they managed to get the 2 programs merged (which delayed the whole process by over a year). then they squabbled over who would be program lead. Then they kept delaying it which almost caused the army’s funding to expire. (the army’s money for the JCA comes from the cancelled cheyenne program and was only valid to a certain point). In sum, i would say politics
the main beneficiary in the program is the Army. The C-27 provides both commonality with the C-130J
how many C-130J’s does the army operate?
as well as allows the Army the capability to provide its own airlift for relatively lighter payloads (certain vehicles namely, some of which won’t fit in the C-295).
yes there are 2 parts to this:
1. army independence of air force
2. cheaper milk runs
i can see the argument about moving vehicles independently, but what the hey? let’s give the army their own C-17s so they can move their own tanks . . .
the army has relied on the air force for vehicle transports all this time, i’m sure they can continue to deal with it
and actually from what i heard the C-295 was the army’s choice (since it was cheaper) while the C-27J was the airforce’s choice (c-130 compatibility). But who knows if there was any truth to that rumor.
The C-27, as mentioned in the article, provides better short-field capability and a longer range, both of which are beneficial in any cargo aircraft no matter what your requirements may be. Shorter runways allow access to more areas, and longer range means less time is spent stopping for fuel or taking away tankers for airborne refuelling needs.
1. most places it’s going will want to accomodate C-130’s too, so not sure how much difference short-field capability is going to make
2. the range difference isn’t that much (C-27J is 2,300 nm with over 13,227 lbs (6,000kg) of payload, C-295 is 2,300 nm with 10,000 lbs of payload
3. does either one actually support aerial refuelling anyways? i can’t find any evidence that they do . . .
4. again, if there is a run that needs more capability, we have C-130s and C-17s
One C-130J unit’s AVERAGE cargo was a whopping 2.3 tons (http://warisboring.com/?p=230). For a plane that can carry over 35 tons, that’s a massive squandering of resources.
We need smaller, cheaper planes for these milk runs
Having seen some pretty cool clips of this thing in action
look, no doubt the C-27J is a cool plane, but it just isn’t what we need
if you need to move a vehicle use a C-130
transporting vehicles is such a small proportion of missions that you would still come out ahead to use a C-295 on the missions it can handle and a C-130 on the ones it can’t
if this was to be the only military transport in the fleet, moving vehicles would be an important consideration. But it’s not.
The purpose of the FCA isn’t to increase capacity, it’s to save money with cheaper capacity.
here’s a story that demonstrates something fundamentally wrong with the current transportation scheme
http://www.mnf-iraq.com/index.php?option=com_content&task=view&id=10821&Itemid=128
C-17s from the 172nd Airlift Wing have performed more than 350 aerovac missions since October 2005 from Iraq to Ramstein and the States
Why in the world are we using C-17s for this task?
It’s a waste of the C-17’s service life, a waste of gas and a waste of time (as the C-17 isn’t the swiftest bird in flock).
And the GAO is complaining that they haven’t properly ‘justified’ the need for cargo/medevac capability in the KC(X).
The KC(X) can’t get here soon enough.
Lifetime operating costs are also a big factor, and in this area I don’t see how the KC-30 will be cheaper. Unless Boeing flat out admits that to be the case of Airbus proves beyond a shadow of a doubt that is to be the case (unlikely in either scenario) then I’ll lean toward the KC-767 in this area due to reasons I’ve stated before.
Well both have been in commercial service long enough to have a pretty good idea about what the maintenance costs are.
I’m no expert, but everything i’ve seen points to the A330 having lower maintenance costs because it is a more modern design that has fewer parts and was designed to be more maintainable.
I’ll make the comparison between the Tomcat and the Super Hornet. The Tomcat is far, far more maintenance intensive. This is partly because it’s older, partly because of one unique feature (swing wing), but mainly because the Super Hornet designers put a heck of a lot more effort into making it easy to maintain.
Similarly the A330 costs less to maintain because more effort was put into making it easier to maintain.
Maybe Boeing can add some ease of maintenance features with the LRF, but I doubt it would be much.
————-edit—————
i found some documentation on maintenance costs here:
http://www.aircraft-commerce.com/store/files/Fleet%20Planning,%20Sample%201.pdf
on the last page they list 767-400ER and -300ER airframe and component maintenance costs per flight hour as $415 vs $435 for the A330-200 on long-haul flights
there are different numbers for the short haul flights