The max load you’ll ever carry is 800-900 lbs. in the bed
Which is a great heaping load of ********. These planes will be in service for 50+ years, who knows what needs will be like so far in the future?
Plus it doesn’t take much of a crystal ball to see how a pacific campaign would completely invalidate assumptions based on years of mideast operations with plentiful and close bases.
Oh yeah, and it costs less. Your boss (who signs your checks) says, “Make sure you get the least expensive one that’ll do our job”. Especially given that final constraint, which one do you choose?
Except it likely doesn’t
Every indication is that the purchase price of the 767 is MORE
but because it is smaller it comes out to 4% lower LIFECYCLE cost (theoretically speaking)
so spend more now for a less capable ‘truck’ in the hope of saving a measly 4% over the life of the ‘truck’
People kept saying that Boeing should be putting the P&W1100 “Pure Power” engine on the KC-46A, not the “20-25 year-old” PW4062… despite the fact that the PW1100 will produce much less thrust than the older engine.
Actually I heard people clamoring for the CF-6-80C2 (52,500 to 63,500 lb thrust)
And it is inferior to the other 20-25 year old engine available in almost every way. The CF-6-80C2 uses less fuel, runs longer on the wing, and has a lower in flight shut down rate. Straight up comparison between a PW powered 767-300ER in airline service with one powered by the GE yields about 5,000 lbs more revenue payload for the GE on a 4,000 mile route, same winds, etc.
I think the confusion stems from the post you were replying to (by MadRat) was actually comparing the KC-46a to the KC-45, not the PurePower to the 4062
It’s like going to the car lot to buy a 2012 car only to find out it uses an engine and a set of tires manufactured in 1998. And, oh by the way, your new car warranty expires at the end of the month. It looks good and shiny on the surface, but somehow you know it’s going to cost you more in the short, middle, and long run if you had simply spent that extra 4% now.
4% being the giveaway, since that was the estimated price differential between the Boeing and EADS offerings
Well, if I am buying a truck with which I intend to haul heavy loads in the back and pull loaded trailers, and the 2012 model gives me the option of a nice, fuel-efficient, clean-burning high-tech engine that was first produced in 2010 or a slightly dirtier, slightly less-efficient 1998 engine that produces 40% more power, I sure know which one I am going to order… and it won’t be the new one!
que?
Pricing the KC-X: $162m estimate for Boeing, $169m for EADS
lots of WAGs resulting in his estimates of bid prices:
Boeing’s bid price: $29.55 billion
Boeing’s adjusted price: $26.05 billion
EADS’ bid price: $30.3 billion
EADS’ adjusted price: $27.08 billion
or about a 4% difference
The tanker competition did not change much publicly this morning after EADS NA received its briefing from the Air Force on just why Boeing won the $35 billion program.
“The EADS North America team has met with the Air Force, received a debriefing and is evaluating the information presented to us. Our objective has always been that the U.S. warfighter receive the most capable tanker, following a fair and transparent competition. That remains our position today,” said company spokesman Guy Hicks.
For their protest to prevail (since no one is alleging improprieties) they would have to:
1. show that the Boeing offering fails to meet one of the mandatory requirements
Sorry, the KC-767 can carry more fuel than the exsisting KC-135. Yet, used most the same infrastructure.
Incorrect, the KC-767 carries substantial milcon costs also
The choice was easy…………bigger is not always better.;)
In reality the airforce disagrees, as witnessed by the last contest where they were more than happy to give all sorts of credit for more capability
however what they learned in the last contest is that there’s no way to ‘fairly’ give credit for extra capability. To an extent, any such credit is arbitrary (how do you define the worth of extra refueling capability vs lower cost?), so the loser can always protest against your method.
They realized the ONLY way they were going to get a contract through protest was to simply set a min spec and then go for the lowest price.
Better an ‘ok’ tanker than no tanker.
Whatever they may have preferred was IRRELEVANT if they ever wanted to get a new tanker. The structure of the contest was dictated by the reality of the current procurement environment.
Now they needed two bidders and they intimately knew the capability of both planes, so they had to set the min specs such that the least capable plane wasn’t eliminated. Thus the capabilities of the 767, NOT the wishes of the AF, drove the spec requirements.
What EADS should have done was bid a plane that met spec for the cheapest price.
um, that’s exactly what they did, bid the cheapest plane they had that met the spec
there is nothing they could have done that would have been cheaper and still met the reqs
What they did do was bid a plane that was over spec and tried to convince the USAF that it was worth the extra cost. They failed.
more like the spec was custom tailored to the 767, so any plane not named ‘767’ would have failed
Airbus managed to take out 10-15% by taking out a layer (Northrup Grummam). Boeing didn’t have that option
actually they did
previously Boeing commercial insisted on a profit for the base frame before it got passed to Boeing military for conversion
Albaugh got rid of that nonsense and now Boeing military is receiving the frame at cost
So the V-22 IS a requirement, but is only counted if all the 373 mandatory requirements are met and the costs are within 1%.
if it’s not required, it’s not a requirement
QED
(you can argue you meant in technical acquistion legal mumbo jumbo where there is such a thing as a non-required requirement, fine, BUT, as it was a NON-MANDATORY requirement, there is no need for a waiver. A waiver would be for a mandatory requirement, which the V-22 is not)
I am pretty sure the KPP said all current aircraft
which does not include the V-22
otherwise why have refueling on the V-22 if you are going to buy a tanker that cannot refuel it.
KC-130, just like helicopters
Besides, the ability (or lack thereof) to fuel a V-22 is the least of it’s problems (compared to the other two).
the point is that if the source got one point provably wrong, then they don’t have a lot of credibility to make further claims
This was from the AF times, not a private newspaper.
but they were quoting an anonymous source, that was not the AF official position
It’s not all about runway, but hangers and parking slots too.
There is this from the announcement.
Because the Air Force wanted a competition, industry sources said, EADS received a number of waivers for several “key performance parameters,” including the ability to take off from 7,000-foot runways, fitting into existing hangars, and refueling all types of Air Force aircraft — it reportedly cannot pass fuel to Air Force V-22s. As well, the sources said, the contractor will not be required to integrate government-furnished classified hardware.
If the length was not an issue, why the waiver?
I know the V-22 was not part of the requirement of the RFP, so no waiver would be needed, which makes the rest of the allegations somewhat suspect
You’re very generous with US taxppayers funds. 😀
when it comes to the military, absolutely
The same argument is often made here against the C-17, saying it’s foolish to pay for a capability that isn’t often used. Otherwise the RAF and most NATO nations would have many more C-17s.
I’m not against the C-17, it’s a useful capability to have, I’m against MORE C-17s
it’s all about fleet balance
now if i could be assured that we’d also get a good number of 777/A350 class tankers from KX-Y and/or KC-Z, i wouldn’t have such a problem with the 767
BUT with the budget climate and the uncertainty of future procurement, KC-X might be all we get. And if we only get one, I would much rather have the KC-30
It was specified that way because that is what CONGRESS wanted.
FTFY