Re: VC-25A's, why not the 747-400 airframe ?

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IIRC, when the US government placed the order for the VC-25A, 747-400 was =
not available yet.  VC-25 (inside) is very different from a conventional =
747 and it took much longer time to build.  So when it was delivered the =
-400 was available.

C.S.

>>> Stanley Powroznik <avialot@xxxxxxxxx> 04/10/03 02:40pm >>>
Quote: ....The first VC-25A -- tail number 28000 -- flew as "Air Force =
One" on Sept. 6, 1990, when it transported President George Bush to =
Kansas, Florida and back
to Washington, D.C. A second VC-25A, tail number 29000 transported =
President
Bill Clinton and former Presidents Carter and Bush to Israel for the =
funeral
of Prime Minister Yitzhak Rabin.

Introduction Date Dec. 8, 1990 (tail No. 28000); Dec. 23, 1990 (tail
No. 29000)
Date Deployed Sept. 6, 1990 (tail No. 28000); Mar. 26, 1991 (tail No.
29000)

--------------------------------------------------------

I was always curious as to why the basic 747-200 airframe was chosen for =
the two VC-25A's and not the updated with the newer 747-400 airframe =
considering that both VC-25A's flew for the first time in 1990 while the =
very first 747-400 made its maiden flight a year or two before and put =
into commercial service with PW4000 engines by Northwest Airlines.

The 747-400 airframe already existed, so why not using this airframe for =
both VC-25A's ?

In any case, why isn't both VC-25A's retrofitted with -400 winglets either =
to make it the only 747-400 passenger transport that has the shorthened =
-200 upperdeck which is only found on the -400 freighter ?

Any clue(s) ?




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