Editing Boeing CH-47 Chinook (section)

==Specifications (CH-47F)==
[[File:Boeing CH-47 Chinook 3-view line drawing.svg|right|400px|Orthographically projected diagram of the Boeing Vertol CH-47 Chinook.]]
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 |image1 = Lycoming T55-GA-712.jpg
 |alt1 = 
 |image_caption1 = Turboshaft engine on the rear of a {{nowrap|CH-47}}
 |image2 = Chinook Iraq Operation Swarmer CH43 060316-N-5438H-011.jpg
 |alt2 = 
 |image_caption2 = [[M240 machine gun]] emplacement on the loading ramp, with another M240 partly visible on the right shoulder window
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{{Aircraft specs
|ref=Boeing CH-47,<ref name=Boeing_CH-47>{{cite web |url=http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications |title=CH-47 Technical Specifications |publisher=Boeing |website= Boeing.com |access-date=19 March 2016 |archive-url=https://web.archive.org/web/20160313152930/http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications |archive-date=13 March 2016 |url-status=live}}</ref> Army Chinook file, CH-47F,<ref>{{cite web |url=https://www.army.mil/article/137584/ |title=CH-47 Chinook helicopter |date=4 November 2014 |work=army.mil |access-date=19 March 2016 |archive-url=https://web.archive.org/web/20160329054721/http://www.army.mil/article/137584 |archive-date=29 March 2016 |url-status=live}}</ref> International Directory, CH-47D<ref name="Frawley Military">Frawley, Gerard: ''The International Directory of Military Aircraft'', p. 49. Aerospace Publications Pty Ltd, 2002. {{ISBN|1-875671-55-2}}.</ref>
|prime units?=kts
<!-- General characteristics -->
|crew=3 (pilot, copilot, flight engineer or loadmaster)
|capacity=<br>
** 33–55 troops ''or''
** 24 stretchers and 3 attendants ''or''
**{{cvt|24000|lb|0}} payload
|length ft=98
|length in=10.7 
|length note=<ref name=Boeing_CH-47/>
* '''Fuselage length:''' {{cvt|51|ft|2|in|1}}<ref name=Boeing_CH-47/>
|width ft=12
|width in=5
|width note=(fuselage)<ref name=Boeing_CH-47/>
|height ft=18
|height in=7.8
|height note=<ref name=Boeing_CH-47/>
|empty weight lb=24578
|empty weight note=
|gross weight lb=54000
|gross weight note=<ref name=Boeing_CH-47/>
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|1080|USgal|impgal l|0}}<ref name=Boeing_CH-47/>
|more general=
<!-- Powerplant -->
|eng1 number=2
|eng1 name=[[Lycoming T55-GA-714A]]
|eng1 type=[[turboshaft]] engines
|eng1 shp=4733
|eng1 note=
|rot number=2
|rot dia ft=60
|rot dia in=<!-- helicopters -->
|rot area sqft=5600
|rot area note=<br>
*'''Blade section:''' ''root:'' Boeing VR-7; ''tip:'' Boeing VR-8<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>
<!-- Performance -->
|max speed kts=170
|max speed note=
|cruise speed kts=157
|cruise speed note=<ref name=Boeing_CH-47/>
|never exceed speed kts=
|never exceed speed note=
|range nmi=400
|range note=
|combat range nmi=165
|combat range note= (combat radius)<ref name=Boeing_CH-47/>
|ferry range nmi=1216
|ferry range note=<ref>United States of America. Naval Training Equipment Center. Department of the Navy. ''Recognition Study Cards – US and Foreign Aircraft''. Device 5E14H. LSN 6910-LL-C006462. Orlando, Florida. 1982. 55 Cards. ''Annotation'': 2252 kilometers.</ref>
|endurance=<!-- if range unknown -->
|ceiling ft=20000
|ceiling note=
|climb rate ftmin=1522
|climb rate note=
|time to altitude=
|disk loading lb/sqft=9.5
|disk loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|0.28|hp/lb}}
|more performance=
<!-- Armament -->
|armament= * Up to 3 pintle-mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally {{convert|7.62|mm|in|abbr=on}} [[M240 machine gun|M240]]/[[FN MAG]] machine guns, and can be armed with the 7.62&nbsp;mm [[Minigun|M134 Minigun]] rotary machine gun. 
|avionics= * Rockwell Collins Common Avionics Architecture System (CAAS) (MH-47G/CH-47F)
}}