Editing Boeing C-40 Clipper (section)

==Specifications==
[[File:US Navy 050108-N-6954B-023 Crew members load supplies onto a C-40A Clipper aircraft assigned to the "Lone Star Express" of Fleet Logistics Support Squadron Five Nine (VR-59).jpg|thumb|right|C-40A transporting palletized humanitarian cargo, 2005.]]
{{Aircraft specs
|ref=<ref>{{Cite web |title=C-40 Clipper |url=https://www.boeing.com/defense/c-40a/#/tech-spec |access-date=2022-06-06 |website=[[Boeing Defense, Space & Security]]}}</ref><ref>{{Cite web |date=April 2020 |title=C-40B/C Fact Sheet |url=https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104521/c-40bc/ |access-date=2022-06-06 |website=[[United States Air Force]] |language=en-US}}</ref>
|prime units?=kts
<!-- General characteristics -->
|crew=Four, five or six: Pilot, co-pilot, crew chief and loadmaster, plus one 'second loadmaster' when carrying passengers or two when carrying over 100 passengers
|capacity=<br />
**C-40A passenger configuration: 121 passengers
**C-40A cargo configuration: 8 pallets
**C-40A combination configuration: 3 pallets, 70 passengers
**C-40B: 26 to 32 passengers
** C-40C: 42 to 111 passengers
**Payload: {{cvt|40000|lb|0}}
|length ft=110
|length in=4
|length note=
|span ft=112
|span in=7
|span note=
|height ft=41
|height in=2
|height note=
|wing area sqft=
|wing area note=
|swept area sqft=<!-- swing-wings -->
|swept area note=
|volume ft3=<!-- lighter-than-air -->
|volume note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' BAC 449/450/451; '''tip:''' BAC 442 mod<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019 |archive-url=https://web.archive.org/web/20190326174850/https://m-selig.ae.illinois.edu/ads/aircraft.html |archive-date=26 March 2019 |url-status=live }}</ref>
|empty weight lb=126000
|empty weight note=
|max takeoff weight lb=171000
|max takeoff weight note=
<!-- invalid parameters |max landing weight lb=134000 |max landing weight note= -->
|fuel capacity={{Convert|6875|USgal|abbr=on}}
|more general=
<!-- Powerplant -->
|eng1 number=2
|eng1 name=[[CFM International CFM56-7B]]
|eng1 type=[[turbofan]] engines
|eng1 hp=<!-- prop engines -->
|eng1 shp=<!-- prop engines -->
|eng1 lbf=27300
|eng1 note=
<!-- Performance -->
|max speed kts=534
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed mph=
|cruise speed note=
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|minimum control speed mph=
|minimum control speed note=
|range nmi=3200
|range note= (C-40A), {{Convert|4500-5000|nmi|mi km|abbr=on}} (C-40B/C)
|combat range miles=
|combat range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=41000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading lb/sqft=
|wing loading note=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption lb/mi=
|thrust/weight=0.407
|avionics=
}}