Editing Boeing 717 (section)

== Specifications ==
[[File:McDonnell Douglas MD-82 v1.0.png|thumb|upright=2|Comparison of [[McDonnell Douglas DC-9|Douglas DC-9]], Boeing 717, [[McDonnell Douglas MD-90]] and [[McDonnell Douglas MD-80]] series aircraft ]]
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{| class="wikitable sortable sticky-header" style="text-align: center"
|+ Boeing 717-200 characteristics<ref name="acaps" />
|-
! Variant
! Basic
! High Gross Weight
|-
! Cockpit crew<ref name="TCDS">{{Cite web |date=March 25, 2014 |title=Type Certificate Data Sheet no. A6WE |url=http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/81bb7f7f3caf760686257ca80068d081/$FILE/A6WE_Rev_30.pdf |publisher=FAA |access-date=July 19, 2017 |archive-date=December 28, 2016 |archive-url=https://web.archive.org/web/20161228113242/http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/81bb7f7f3caf760686257ca80068d081/$FILE/A6WE_Rev_30.pdf |url-status=dead }}</ref>{{rp|66}}
| colspan=2 | Two
|-
! 2-class [[Aircraft seating|seating]]<!-- =acaps p10 -->
| colspan=2 | 106 (8J+98Y @ {{cvt|36|-|32|in|cm|disp=comma}})
|-
! 1-class [[Airline seat|seating]]<!-- =acaps p11 -->
| colspan=2 | 117Y @ {{cvt|32|in|cm}}
|-
! Exit limit<ref name="TCDS" />{{rp|81}}
| colspan=2 | 134
|-
![[Cargo aircraft|Cargo]]<!-- =acaps p7 -->
| {{convert|935|cuft|abbr=on}}
| {{convert|730|cuft|abbr=on}}
|-
! Length<!-- =acaps p8 -->
| colspan=2 | {{convert|124|ft|m|abbr=on}}
|-
![[Wingspan]]<!-- =acaps p8 -->
| colspan=2 | {{convert|93|ft|4|in|m|abbr=on}}
|-
! Height<!-- =acaps p9 -->
| colspan=2 | {{convert|29|ft|8|in|m|abbr=on}}
|-
! Width<!-- =acaps p13 -->
| colspan=2 | Exterior [[Fuselage]]: {{convert|131.6|in|m|abbr=on}}<br />Interior [[Aircraft cabin|Cabin]]: {{convert|{{#expr:49.2*2+25.4}}|in|m|abbr=on}}
|-
! Max. takeoff weight<!-- =acaps p7 -->
| {{convert|110,000|lb|kg|abbr=on}}
| {{convert|121,000|lb|kg|abbr=on}}
|-
! Empty weight<!-- =acaps p7 -->
| {{convert|67,500|lb|kg|abbr=on}}
| {{convert|68,500|lb|kg|abbr=on}}
|-
! Max. [[payload]]<ref name="TCDS" />{{rp|66}}<!--max PL = MZFW – empty weight-->
| {{val|{{#expr:94000-67500}}|u=lb|fmt=commas}} ({{val|{{#expr:42638-30617}}|u=kg|fmt=commas}})
| {{val|{{#expr:100500-68500}}|u=lb|fmt=commas}} ({{val|{{#expr:45586-31071}}|u=kg|fmt=commas}})
|-
! Fuel weight<!-- =acaps p7 -->
| {{convert|24,609|lb|kg|abbr=on}}
| {{convert|29,500|lb|kg|abbr=on}}
|-
![[Fuel tank|Fuel capacity]]<!-- =acaps p7 -->
| {{convert|3,673|USgal|L|abbr=on}}
| {{convert|4,403|USgal|L|abbr=on}}{{efn|Including forward and aft auxiliary fuel tanks}}
|-
![[Turbofan]]s (2×)<ref name="TCDS" />{{rp|65}}
| [[Rolls-Royce BR715]]-A1-30
| Rolls-Royce BR715-C1-30
|-
![[Thrust]] (2×)<ref name="TCDS" />{{rp|65}}
| {{cvt|18,920|lbf|kN}}
| {{cvt|21,430|lbf|kN}}
|-
![[Ceiling (aeronautics)|Ceiling]]<ref name="TCDS" />{{rp|67}}
| colspan=2 | {{cvt|37000|ft|m}}
|-
! Cruise speed<ref name="aero_19">{{Cite web |date=July 2002 |title=717-200 technical characteristics |url=http://www.boeing.com/commercial/aeromagazine/aero_19/717_characteristics.pdf |website=Aero |publisher=Boeing |page=30 |issue=19}}</ref>
| colspan=2 | {{cvt|0.77|Mach|altitude_ft=34200|km/h knots mph|0}} at {{convert|34,200|ft|m|abbr=on}}
|-
! Range<ref name="aero_19" />
| {{cvt|1,430|nmi|0}}<!-- source says 2645&nbsp;km but actual conversion is 2648 which rounds up -->
| {{cvt|2,060|nmi|0}}
|}