Editing Lockheed EP-3 (section)

== Specifications (EP-3E-II – P-3C as indicated) ==
[[File:VQ1 MT FUJI WEB (4832425082).jpg|thumb|Lockheed EP-3E flying past [[Mount Fuji|Mt. Fuji]], Japan]]
{{Aircraft specs
|ref=Encyclopedia of world military aircraft Vol.2,<ref name=EoWMAv2>{{cite book |editor1-last=Donald |editor1-first=David |editor2-last=Lake |editor2-first=Jon |title=Encyclopedia of world military aircraft Vol. 2 |year=1994 |publisher=Aerospace |isbn=1874023522 |pages=249–253}}</ref> Jane's All the World's Aircraft 1984–85<ref name=JAWA84-85>{{cite book |title=Jane's All the World's Aircraft 1984–85 |url=https://archive.org/details/janesallworldsai8485john |url-access=registration |editor1-last=Taylor |editor1-first=John W.R. |edition=75th |year=1984 |publisher=Jane's Publishing Co. |location=London |isbn=0710608012 |pages=[https://archive.org/details/janesallworldsai8485john/page/n516 433]–434}}</ref>
|prime units?=kts
<!--
        General characteristics
-->
|crew=4 (minimum)
|capacity=19+ mission crew
|length ft=116
|length in=10
|length note=
|span ft=99
|span in=8
|span note='''P-3C'''
|height ft=33
|height in=8.5
|height note='''P-3C'''
|wing area sqft=1300
|wing area note='''P-3C'''
|aspect ratio=7.5 '''P-3C'''
|airfoil='''root:'''  [[NACA airfoil|NACA 0014-1.10]]; '''tip:''' [[NACA airfoil|NACA 0012-1.10]]<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> '''P-3C'''
|empty weight lb=61491
|empty weight note='''P-3C'''
* '''Design zero-fuel weight:''' {{cvt|77200|lb|0}}
|gross weight lb=135000
|gross weight note='''P-3C'''
|max takeoff weight lb=142000
|max takeoff weight note='''P-3C'''
* '''Maximum landing weight:''' {{cvt|103880|lb|0}} '''P-3C'''
|fuel capacity={{cvt|9200|USgal |impgal l}} / {{cvt|62000|lb|0}} '''P-3C'''
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Allison T56-A-14]]
|eng1 type=[[turboprop]] engines
|eng1 shp=4910
|eng1 note=equivalent '''P-3C'''

|prop blade number=4
|prop name=[[Hamilton Standard]] 54H60
|prop dia ft=13
|prop dia in=6
|prop dia note=constant-speed fully-feathering propellers '''P-3C'''
<!--
        Performance
-->
|max speed kts=380
|max speed note=at {{cvt|15000|ft|0}}
* '''Patrol speed:''' {{cvt|180|kn|mph km/h|0}}
|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=
|range note=
|combat range nmi=2200
|combat range note=with 0 time on station
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=28000
|ceiling note=
|climb rate ftmin=2175
|climb rate note=at sea level
|time to altitude=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=

|more performance=
* '''Take-off run:''' {{cvt|4240|ft|0}} at MTOW '''P-3C'''
* '''Take-off distance to {{cvt|50|ft|0}}:''' {{cvt|5490|ft|0}} at MTOW '''P-3C'''
* '''Landing distance from {{cvt|50|ft|0}}:''' {{cvt|5490|ft|0}}  at Design landing weight '''P-3C'''

|avionics=
* A wide variety of ELINT, SIGINT and COMINT systems known as the ARIES Suite
}}