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 | Path: news.nzbot.com!not-for-mail NNTP-Posting-Date: Sun, 14 May 2017 07:58:30 -0500
 Newsgroups: alt.binaries.pictures.aviation
 Subject: Re: US 1942-023894 C-47A to USN 12443 R4D-8 USNColl.jpg
 From: Andrew Chaplin <ab.chaplin@yourfinger.rogers.com>
 References: <e51ahch61dlj058ag1iskgd1n96phpkdkg@4ax.com> <XnsA77493D7DDA6AHortenzyFortensnort@216.166.97.131> <of886u02i3j@drn.newsguy.com>
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 Xref: news.nzbot.com alt.binaries.pictures.aviation:5951
 
 Miloch <Miloch_member@newsguy.com> wrote in
 news:of886u02i3j@drn.newsguy.com:
 
 > In article <XnsA77493D7DDA6AHortenzyFortensnort@216.166.97.131>, Andrew
 > Chaplin says...
 >>
 >>joet5 <joet5@optonline.net> wrote in
 >>news:e51ahch61dlj058ag1iskgd1n96phpkdkg@4ax.com:
 >>
 >>>
 >>> begin 644 US 1942-023894 C-47A to USN 12443 R4D-8 USNColl.jpg
 >>>
 >>> Attachment decoded: US 1942-023894 C-47A to USN 12443 R4D-8
 >>> USNColl.jpg `
 >>> end
 >>
 >>What advantages did the modified tail of the USN DC-3 produce?
 >
 > "Both the vertical and horizontal tail surfaces were enlarged, and
 > given square tips, improving the single-engine performance of the
 > aircraft."
 >
 > Douglas R4D-8 (Super DC-3)
 >
 > http://www.historyofwar.org/articles/weapons_douglas_R4D-8.html
 >
 > "The Douglas R4D-8 emerged from an unsuccessful attempt by Douglas to
 > extend the commercial lifespan of the aging DC-3. At the end of the
 > Second World War a vast number of DC-3s, C-47s, C-53s and Dakotas
 > flooded onto the commercial market, but by the end of the 1940s many of
 > these aircraft were threatened by increasingly strict Civil Air
 > Regulations in the United States, and the looming expiry of their
 > airworthiness certificates in 1952.
 >
 > "Douglas responded by developing a modified version of the DC-3, the
 > DC-3S or Super DC-3, which could be produced by upgrading existing
 > aircraft. The new aircraft had a stronger longer fuselage, with room
 > for 30 passengers. The passenger door was moved forward, and the door
 > itself could be used as the boarding stairs. Both the vertical and
 > horizontal tail surfaces were enlarged, and given square tips,
 > improving the single-engine performance of the aircraft. The engine
 > nacelles were modified so that they could carry either 1,475hp Wright
 > Cyclone engines or 1,450hp Pratt & Whitney R-200-D7 radial engines, and
 > to allow the wheels to be fully enclosed. Finally the outer panels of
 > the wing were shortened, and 4 degrees of sweepback was added to the
 > trailing edges.
 
 Thank you.
 --
 Andrew Chaplin
 SIT MIHI GLADIUS SICUT SANCTO MARTINO
 (If you're going to e-mail me, you'll have to get "yourfinger." out.)
 
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