Hung Start
Just the cleanup guy
- Joined
- Sep 12, 2004
- Posts
- 701
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habubuaza said:Just as a side note... Those kids on Airliners.net although sometimes goofy they do some good work in digging up information. They kinda remind me of an eager beaver intern at a law firm doing all the nitty gritty as far as researching stuff.
Here's a recent near disaster at KMDW that was put out by one of these kids...
http://www.liveatc.net/forum/files/kmdw_315_670.mp3
I mean who the hell can find this $hit?
EuroWheenie said:Besides, if we are to speak of French built aeroplanes, most people I know will agree that the Dassault range of business jets are among the best, if not the best, built in the industry. The DA wings on the 50 are, incidentially, of a design that can be traced back to the Mirage F1 - one more piece of useless info you may throw around at your leisure![]()
dseagrav said:The JU-87.
Look at the Boeing 2707, the 300 seat Mach 2.5 transport that was launched to go up against the Anglo-French Concorde. The project was technologically feasible, but it became clear early on that ticket prices would have to be so high to reach the break-even that no one would want to fly on it. The 2707 project was cancelled (funding and environmental concerns also played a part) and a full-size mockup is all that the program ever produced.
Even in service, the aircraft served mostly as national icons- they wasn't profitable even with $10,000 tickets. A technological leap ahead it most certainly was, but it was an economic failure.
Of course, the risk inherent in a program like this is a lot more acceptable when you are a quasi-state run company like EADS. Not since the Soviet design bureaus have we seen such insulation from risk and bottomless funding.![]()
doug_or said:Me thunks there some confusion between the JU-52 (3 engine transport) and 87 (blows things up) here?
Whale Rider said:DATE:21/02/06
SOURCE:Flight Internationa
The European Aviation Safety Agency (EASA) says the maximum loading conditions defined for the A380 certification state: “The aircraft structure is analysed and tested to demonstrate that the structure can withstand the maximum loads, including a factor of safety of 1.5.”
Garcia says: “We will use this calibration of the FEM to prove the adequacy of the structure on production aircraft,” adding that “essentially no modifications” will be required for production aircraft: “We have refined the structural design for subsequent aircraft due to increased weights, etc.”
Jonathan Howes, technical director of UK-based certification consultants AeroDAC and, until recently, leading structures certification specialist for the A380 at the UK Civil Aviation Authority, says the rupture “was so close to the ultimate target that it is almost certain to allow approval to be given without the need for a re-test, but this will be subject to a negotiation between Airbus and EASA”.
MAX KINGSLEY-JONES / LONDON
“We had a weight-saving programme and ‘played the game’ to achieve ultimate load,”
habubuaza said:I'm sorry but the A380 was a HUGE mistake on Airbus' part. Why did they build it? What airline, went to Airbus and Boeing and said
"hey we need a colossal aircraft that is capable of carrying up to 850 passengers, and by the way we are willing to pay nearly $300,000,000 a piece for it and force most airports to spend millions more to update themselves to handle the weight of such aircraft" ? The answer is no one. Airbus built the A380 for bragging rights and that's it. Now they are struggling to meet performance criteria and to create a market for it.
OK, so what are you going to do when you have to fly New York to Hong Kong? Sorry A380 can't do that. How about Sydney London? Sorry need a 777 for that one. I mean come on what was Airbus thinking?
As for your comment on airliners being overweight..I would challenge you to tell me what successful airliner had an overweight issue?