Editing McDonnell Douglas DC-10 (section)

==Specifications==
[[File:McDonnell Douglas DC-10-30 v1.0.png|thumb|upright=2|The schematic of the McDonnell Douglas DC-10-30 (side, top, front, cross-section)]]

{| class="wikitable" style="text-align:center"
|+ DC-10 Airplane Characteristics<ref>{{cite web |url= https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/dc10.pdf |title= DC-10 Airplane Characteristics for Airport Planning |date= May 2011 |publisher= McDonnell Douglas |access-date= December 2, 2018 |archive-date= December 7, 2019 |archive-url= https://web.archive.org/web/20191207003212/https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/dc10.pdf |url-status= live}}</ref>
!Variant
! -10 !! -30 !! -40
|-
![[Cockpit]] [[crew]]
| colspan=3 | Three
|-
! Std. seating
| colspan=3 | 270 (222Y 8-abreast @ 34" + 48J 6-abreast @ 38")
|-
! Max. seating
| colspan=3 | 399Y (10-abreast @ 29–34" pitch) layout, FAA exit limit: 380<ref name=TCDS/>
|-
! Cargo
|colspan=3 | 26 [[Unit Load Device|LD3]] layout, main deck: 22 88×125″ or 30 88×108″ pallets
|-
!Length
| 182&nbsp;ft 3.1&nbsp;in / 55.55&nbsp;m || 181&nbsp;ft 7.2&nbsp;in / 55.35&nbsp;m || 182&nbsp;ft 2.6&nbsp;in / 55.54&nbsp;m
|-
!Height
| 57&nbsp;ft 6&nbsp;in / 17.53&nbsp;m || colspan=2 | 57&nbsp;ft 7&nbsp;in / 17.55&nbsp;m
|-
![[Wingspan]]
| 155&nbsp;ft 4&nbsp;in / 47.35&nbsp;m || colspan=2 | 165&nbsp;ft 4&nbsp;in / 50.39&nbsp;m
|-
! Wing area<ref name=Boeing2007>{{cite web |url= https://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/dc10-passenger.pdf |title= DC-10 |publisher= Boeing |date= 2007 |access-date= December 2, 2018 |archive-date= December 7, 2019 |archive-url= https://web.archive.org/web/20191207003233/http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/dc10-passenger.pdf |url-status= live}}</ref>
| {{cvt|3550|sqft}} || colspan=2 | {{cvt|3647|sqft}}
|-
!Width
| colspan=3 | 19&nbsp;ft 9&nbsp;in (6.02&nbsp;m) fuselage, <!--p18-21: 57.5*2+16.5*2+76=54*3+31*2=42+19*2+82+62=224--> {{cvt|224|in|cm|0}} interior <!--18&nbsp;ft 2 in (5.54 m) interior floor-->
|-
![[Operating empty weight|OEW]] (pax)
| 240,171&nbsp;lb / 108,940&nbsp;kg || 266,191&nbsp;lb / 120,742&nbsp;kg || 270,213&nbsp;lb / 122,567&nbsp;kg
|-
![[Maximum take-off weight|MTOW]]
| 430,000&nbsp;lb / 195,045&nbsp;kg || colspan=2 | 555,000&nbsp;lb / 251,744&nbsp;kg
|-
! Max. payload
| 94,829&nbsp;lb / 43,014&nbsp;kg || 101,809&nbsp;lb / 46,180&nbsp;kg || 97,787&nbsp;lb 44,356&nbsp;kg
|-
![[Fuel tank|Fuel capacity]]
| 21,762 US gal / 82,376&nbsp;L || colspan=2 | 36,652 US gal / 137,509&nbsp;L
|-
![[Jet engine|Engines]] ×3
| [[General Electric CF6|GE CF6]]-6D || GE CF6-50C || [[Pratt & Whitney JT9D|PW JT9D]]-20 / -59A
|-
![[Thrust|Thrust ×3]]<ref name=Boeing2007/>
| 40,000&nbsp;lbf / 177.92&nbsp;kN || 51,000&nbsp;lbf / 226.85&nbsp;kN || 53,000&nbsp;lbf / 235.74&nbsp;kN
|-
!Cruise
| colspan="4" | {{cvt|0.82|Mach|altitude_ft=35000|kn km/h mph|0}} typical, {{cvt|0.88|Mach|altitude_ft=35000|kn km/h mph|0}} MMo<ref name=TCDS/>
|-
!Range{{efn|M0.82, 270 pax @ {{cvt|205|lb|kg|disp=or}} each}}<!--PL/range charts for {{cvt|55,350|lb|kg}}-->
|| {{cvt|3500|nmi}} || {{cvt|5200|nmi}} || {{cvt|5100|nmi}}
|-
![[Takeoff]]{{efn|MTOW, SL, ISA}}
| {{cvt|9000|ft}} || {{cvt|10500|ft}} || {{cvt|9500|ft}}
|-
![[Ceiling (aeronautics)|Ceiling]]
| colspan=3 | {{cvt|42,000|ft|m|-2}}<ref name=TCDS>{{cite web |url= https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/2cf3306625f6fd1586258281006f6d29/$FILE/A22WE_Rev_13.pdf |title= Type Certificate Data Sheet A22WE |date= April 30, 2018 |publisher= FAA |access-date= December 2, 2018 |archive-date= November 3, 2021 |archive-url= https://web.archive.org/web/20211103074117/https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/2cf3306625f6fd1586258281006f6d29/$FILE/A22WE_Rev_13.pdf |url-status= dead}}</ref>
|}
{{Notelist}}