Editing Boeing RC-135 (section)

==Specifications (RC-135)==
{{Aircraft specs
|ref= USAF RC-135 Data Sheet <ref>{{cite web |url=http://www.airforce-technology.com/projects/boeing-rc135/ |title=Boeing RC-135 Reconnaissance Aircraft |publisher=Airforce Technology |date=27 October 2020 |accessdate=23 February 2022 |archive-date=13 January 2016 |archive-url=https://web.archive.org/web/20160113015609/http://www.airforce-technology.com/projects/boeing-rc135 |url-status=live }}</ref>{{Unreliable source?|reason=domain on WP:BLACKLIST|date=June 2016}}
|prime units?=kts
<!--
        General characteristics
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|genhide=

|crew= 2 pilots, 2 navigator (flight crew)
|capacity=21–27 depending on mission requirements, minimum consisting of 4 Electronic Warfare Officers (Ravens), 14 Intelligence Operators and 4 Airborne Systems Engineers (mission crew)
|length ft=136
|length in=3
|length note=
|span ft=130
|span in=10
|span note=
|height ft=41
|height in=8
|height note=
|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 |archive-date=26 March 2019 |archive-url=https://web.archive.org/web/20190326174850/https://m-selig.ae.illinois.edu/ads/aircraft.html |url-status=live }}</ref>
|empty weight lb=124000
|empty weight note=
|gross weight lb=297000
|gross weight note=
|max takeoff weight lb=322500
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[CFM International F-108-CF-201]]
|eng1 type=turbofan engines
|eng1 lbf=22000
<!--
        Performance
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|max speed kts=504
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kts=
|cruise speed note=
|stall speed kts=
|stall speed note=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kts=
|minimum control speed note=
|range nmi=2998
|range note=
|combat range nmi=
|combat range note=
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=50000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=4900
|climb rate note=
|time to altitude=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=

|more performance=

|avionics=
}}