Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
Boeing 717
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
=== MD-95 === The MD-95 traces its history back to 1983 when McDonnell Douglas outlined a study named the ''DC-9-90''. During the early 1980s, as production of the DC-9 family moved away from the smaller Series 30 towards the larger Super 80 (later redesignated [[McDonnell Douglas MD-80|MD-80]]) variants, McDonnell Douglas proposed a smaller version of the DC-9 to fill the gap left by the DC-9-30. Dubbed the DC-9-90, it was revealed in February 1983 and was to be some {{cvt|25|ft|4|in}} shorter than the DC-9-81, giving it an overall length of {{cvt|122|ft|6|in}}. The aircraft was proposed with a {{cvt|17000|lbf|kN}} thrust version of the [[Pratt & Whitney JT8D|JT8D-200]] series engine, although the [[CFM International CFM56]]-3 was also considered. Seating up to 117 passengers, the DC-9-90 was to be equipped with the DC-9's wing with {{cvt|2|ft}} tip extensions, rather than the more heavily modified increased area of the MD-80. The aircraft had a design range of {{cvt|1430|nmi|0}}, with an option to increase to {{cvt|2060|nmi|0}}, and a gross weight of {{cvt|112000|lb}}.<ref name="aero_19" /> The DC-9-90 was designed to meet the needs of the newly deregulated American airline industry. However, its development was postponed by the recession of the early 1980s. When McDonnell Douglas did develop a smaller version of the MD-80, it simply shrunk the aircraft to create the MD-87, rather than offer a lower thrust, lighter aircraft that was more comparable to the DC-9-30. With its relatively high MTOW and powerful engines, the MD-87 essentially became a special mission aircraft and could not compete with the all new 100-seaters then being developed. Although an excellent aircraft for specialized roles, the MD-87 often was not sold on its own. Relying on its commonality factor, sales were generally limited to existing MD-80 operators.<ref name="airclaims" /> In 1991, McDonnell Douglas revealed that it was again considering developing a specialized 100-seat version of the MD-80, initially named the ''MD-87-105'' (105 seats). It was to be some {{cvt|8|ft}} shorter than the MD-87, powered with engines in the {{cvt|16000|-|17000|lbf|kN}} thrust class.<ref name="airclaims" /> McDonnell Douglas, Pratt & Whitney, and the China National Aero-Technology Import Export Agency signed a memorandum of understanding to develop a 105-seat version of the MD-80. At the 1991 Paris Airshow, McDonnell Douglas announced the development of a 105-seat aircraft, designated ''MD-95''.<ref name="airclaims" /> The new name was selected to reflect the anticipated year deliveries would begin.<ref name="douglas" /> McDonnell Douglas first offered the MD-95 for sale in 1994.<ref name="douglas">{{Cite book |last1=Norris |first1=Guy |title=Douglas Jetliners |last2=Wagner, Mark |publisher=MBI Publishing |year=1999 |isbn=0-7603-0676-1}}</ref><ref name="Becher">Becher, Thomas. ''Douglas Twinjets, DC-9, MD-80, MD-90 and Boeing 717''. The Crowood Press, 2002. {{ISBN|1-86126-446-1}}. pp. 106-107.</ref> In early 1994, the MD-95 re-emerged as similar to the DC-9-30, its specified weight, dimensions, and fuel capacity being almost identical. Major changes included a fuselage "shrink" back to {{cvt|119|ft|4|in}} length (same as the DC-9-30), and the reversion to the original DC-9 wingspan of {{cvt|93|ft|5|in}}. At this time, McDonnell Douglas said that it expected the MD-95 to become a family of aircraft with the capability of increased range and seating capacity.<ref name="airclaims" /> The MD-95 was developed to satisfy the market need to replace early DC-9s, then approaching 30 years old. The MD-95 was a complete overhaul, going back to the original [[DC-9-10|DC-9-30]] design and applying new engines, cockpit and other more modern systems.<ref name="douglas" /> In March 1995, longtime McDonnell Douglas customer [[Scandinavian Airlines System]] (SAS) chose the Boeing 737-600 for its 100-seater over the MD-95.<ref name="douglas" /> In October 1995, U.S. new entrant and low-cost carrier [[ValuJet Airlines|ValuJet]] signed an order for 50 MD-95s, plus 50 options.<ref name="douglas" /> McDonnell Douglas president [[Harry Stonecipher]] felt that launching MD-95 production on the basis of this single order held little risk, stating that further orders would "take a while longer".<ref>Lopez, Ramon and Guy Norris. [http://www.flightglobal.com/pdfarchive/view/1995/1995%20-%203046.html "MD-95 Launched with ValuJet"]. Flight International, October 25β31, 1995.</ref> The ValuJet order was the only order received for some two years.<ref name="Becher" />
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
Boeing 717
(section)
Add topic