Editing Consolidated B-24 Liberator (section)

==Specifications (B-24J)==
[[File:Consolidated B-24 Liberator 3-view.svg|frameless|right|3-view line drawing of the Consolidated B-24 Liberator]]

{{Aircraft specs
|ref=Quest for Performance,<ref>{{citation |last=Loftin |first=L.K. Jr. |date=1985  |url=http://www.hq.nasa.gov/pao/History/SP-468/cover.htm |title=Quest for Performance: The Evolution of Modern Aircraft. NASA SP-468 |access-date=22 April 2006 |publisher=NASA Scientific and Technical Information Branch}}</ref> Jane's Fighting aircraft of World War II,<ref name=FAoWWII>{{cite book |title=Jane's Fighting aircraft of World War II |editor-last1=Bridgman |editor-first1=Leonard |date=1989|publisher=Military Press |location=New York|isbn=0517679647 |edition=1995 |pages=215–216}}</ref> General Dynamics aircraft and their predecessors<ref name=Wegg>{{cite book |last1=Wegg |first1=John |title=General Dynamics aircraft and their predecessors |url=https://archive.org/details/generaldynamicsa00wegg |url-access=limited |date=1990 |publisher=Naval Institute Press |location=Annapolis, Md. |isbn=0-87021-233-8 |edition=1st |pages=[https://archive.org/details/generaldynamicsa00wegg/page/n42 82]–90}}</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=11 (pilot, co-pilot, navigator, bombardier, radio operator, nose turret, top turret, 2 waist gunners, ball turret, tail gunner)
|length ft=67
|length in=2
|length note=
|span ft=110
|span in=
|span note=
|height ft=17
|height in=7.5
|height note=
|wing area sqft=1048
|wing area note=
|aspect ratio=11.55
|airfoil='''root:''' Davis (22%); '''tip:''' Davis (9.3%)<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 lb=36500
|empty weight note=
|gross weight lb=55000
|gross weight note=
|max takeoff weight lb=65000
|max takeoff weight note=plus
|fuel capacity={{cvt|2344|USgal|impgal l}} normal capacity; {{cvt|3614|USgal|impgal l}} with long-range tanks in the bomb bay; Oil capacity {{cvt|131.6|USgal|impgal l}} in four self-sealing nacelle hopper tanks
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Pratt & Whitney R-1830-35 Twin Wasp]], R-1830-41 or R-1830-65
|eng1 type=14-cylinder two-row air-cooled turbo-supercharged [[radial engine|radial]] piston engines
|eng1 hp=1200

|prop blade number=3
|prop name=Hamilton Standard
|prop dia ft=11
|prop dia in=7
|prop dia note=constant-speed fully-feathering propellers
<!--
        Performance
-->
|max speed mph=297
|max speed note=at {{cvt|25000|ft}}
|max speed mach=<!-- supersonic aircraft -->
|cruise speed mph=215
|cruise speed note=
|stall speed mph=95
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|minimum control speed mph=
|minimum control speed note=
|range miles=1540
|range note=at {{cvt|237|mph|kn km/h}} and {{cvt|25000|ft}} with normal fuel and maximum internal bomb load
|combat range miles=
|combat range note=
|ferry range miles=3700
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=28000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=1025
|climb rate note=
|time to altitude={{cvt|20000|ft}} in 25 minutes
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=12.9
|wing loading lb/sqft=52.5
|wing loading note=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|0.0873|hp/lb|kW/kg}}
|thrust/weight=

|more performance=
<!--
        Armament
-->
|guns=10 × .50 caliber (12.7 mm) [[M2 Browning machine gun]]s in 4 turrets and two waist positions
|bombs= <br> 
** Short range ({{convert|400|mi|km|abbr=on|disp=sqbr}}): {{convert|8000|lb|kg}}
** Long range ({{convert|800|mi|km|abbr=on|disp=sqbr}}): {{convert|5000|lb|kg}}
** Very long range ({{convert|1200|mi|km|abbr=on|disp=sqbr}}): {{convert|2700|lb|kg}}

|avionics=
}}