Editing Lockheed EC-130 (section)

==Specifications (EC-130J)==
[[File:Lockheed Martin EC-130J Line Drawing.svg|350px|thumb|'''EC-130J Commando Solo III''' line drawing]]

{{Aircraft specs
|ref=Jane's All the World's Aircraft 2010–11,<ref name=JAWA2012-11>{{cite book |title=Jane's All the World's Aircraft 2010–11 |editor1-last=Jackson |editor1-first=Paul |year=2010 |publisher=Jane's Information Group |location=London |isbn= 978-0710629166 |edition=101st |pages=844–847}}</ref> US Air Force Factsheet<ref>{{cite web |url=http://www.af.mil/information/factsheets/factsheet.asp?fsID=182 |title=Factsheets: EC-130J Commando Solo |access-date=21 August 2009 |publisher=United States Air Force |url-status=dead |archive-url=https://web.archive.org/web/20100412004402/http://www.af.mil/information/factsheets/factsheet.asp?fsID=182 |archive-date=12 April 2010 }}</ref>
|prime units?=kts
<!--
        General characteristics
-->
|crew=6<big>+</big> (Pilot, CoPilot, combat systems officer, mission communications commander; loadmaster, five electronic communications systems operators)
|capacity=
|length ft=97
|length in=9
|length note=
|span ft=132
|span in=7.2
|span note=
|height ft=38
|height in=10
|height note=
|wing area sqft=1745
|wing area note=
|aspect ratio=10.1
|airfoil='''root:''' [[NACA airfoil|NACA 64A318]]; '''tip:''' [[NACA airfoil|NACA 64A412]]
|empty weight lb=
|empty weight note=
|gross weight lb=
|gross weight note=
|max takeoff weight lb=175000
|max takeoff weight note=<br>
*'''Max landing weight (normal)''': {{cvt|130000|lb|0}}
*'''Max landing weight (overload)''': {{cvt|155000|lb|0}}
|fuel capacity={{cvt|6750|USgal|impgal l}} without suppressant foam ; {{cvt|6436|USgal|impgal l}} with suppressant foam
::::optionally with 2x {{cvt|13790|USgal|impgal l}} under-wing tanks without suppressant foam ; 2x {{cvt|1290|USgal|impgal l}} under-wing tanks with suppressant foam
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Rolls-Royce AE 2100D3]]
|eng1 type=[[turboprop]] engines
|eng1 shp=4591
|eng1 note=(de-rated from {{cvt|4637|shp|0}} at {{cvt|25|C|0}}

|prop blade number=6
|prop name=[[Dowty Propellers]] R391 
|prop dia ft=13
|prop dia in=6
|prop dia note=constant-speed fully-feathering reversible composite propellers
<!--
        Performance
-->
|max speed kts=
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kts=348
|cruise speed note=max. at {{cvt|28000|ft|0}}
:::{{cvt|339|kn|mph km/h}} econ.
|stall speed kts=100
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|minimum control speed mph=
|minimum control speed note=
|range nmi=2300
|range note=
|combat range nmi=
|combat range note=
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=30560
|ceiling note=at {{cvt|147000|lb|0}}
*'''Service ceiling one engine inoperative:''' {{cvt|22820|ft|0}}
|climb rate ftmin=2100
|climb rate note=
|time to altitude={{cvt|20000|ft|0}} in 14 minutes
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/weight=

|more performance=<br/>
*'''Take-off run:''' {{cvt|3050|ft|0}}
*'''Take-off distance to {{cvt|50|ft|0}}:''' {{cvt|4700|ft|0}}
*'''Take-off run (maximum effort):''' {{cvt|1800|ft|0}}
*'''Landing run:''' {{cvt|1400|ft|0}} at {{cvt|130000|lb|0}}
*'''Landing distance from {{cvt|50|ft|0}}:''' {{cvt|2550|ft|0}} at {{cvt|130000|lb|0}}

|avionics=
}}