Editing Boeing KC-135 Stratotanker (section)

==Specifications (KC-135R)==
[[File:Boeing KC-135A Stratotanker 3-view line drawing.png|frameless|right|3-view silhouette drawing of the Boeing KC-135A Stratotanker]]

{{Aircraft specs
|ref= USAF Fact Sheet,<ref name=AF_fact_sheet/> Boeing.com : KC-135<ref name=Boeing.com>{{cite web |url=http://www.boeing.com/history/products/kc-135-stratotanker.page |title=KC-135 STRATOTANKER : Historical Snapshot |archive-url=https://web.archive.org/web/20151227055308/http://www.boeing.com/history/products/kc-135-stratotanker.page |archive-date=27 December 2015 |publisher=Boeing}}</ref>
|prime units?=kts
<!--    General characteristics
-->
|crew=3 (pilot, co-pilot and boom operator; some KC-135 missions require the addition of a navigator.)
|capacity=up to 80 passengers / {{cvt|83000|lb}} or 6 [[463L master pallet|463L pallet]]s
|length m=
|length ft=136
|length in=3
|length note=
|span m=
|span ft=130
|span in=10
|span note=
|height m=
|height ft=41
|height in=8
|height note=
|wing area sqm=
|wing area sqft=2433
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' BAC 310/311/312; '''tip:''' BAC 313<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}}</ref>
|empty weight kg=44630
|empty weight lb=
|empty weight note=<br />
*'''Operating empty weight:''' {{cvt|124000|lb|0}}
|gross weight kg=
|gross weight lb=297000
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=322500
|max takeoff weight note=
|fuel capacity={{cvt|200000|lb|0}}
|more general=
<!--    Powerplant
-->
|eng1 number=4
|eng1 name=[[CFM International F108-CF-100]]
|eng1 type=[[turbofan]] engines
|eng1 kn=96.2
|eng1 note=
<!--   Performance
-->
|max speed kmh=
|max speed mph=
|max speed kts=504
|max speed note=
|max speed mach=0.9
|cruise speed kmh=
|cruise speed mph=530
|cruise speed kts=
|cruise speed note=at {{cvt|30000|ft}}
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=1500
|range nmi=
|range note=with {{cvt|150000|lb|0}} of transferable fuel
|ferry range km=
|ferry range miles=
|ferry range nmi=9572
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=50000
|ceiling note=
|climb rate ms=
|climb rate ftmin=4900
|climb rate note=
|time to altitude=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|thrust/weight=
|more performance=
|avionics=
}}