Editing Short C-23 Sherpa (section)

==Specifications (C-23A)==
[[File:Shorts C-23A SHERPA.png|thumb|300px|3-view projection of the Short C23 Sherpa]]
[[File:C-23A-4.jpg|thumb|right|A C-23A with an aircraft engine being unloaded (SALTY DEMO'85)]]
[[File:U.S. Army Chief Warrant Officer 4 Kelly Cawood, with the 641st Aviation Regiment, prepares to unload pallets of meals, ready to eat (MREs) from a C-23 Sherpa aircraft May 23, 2013, in Norman, Okla 130523-Z-TK779-020.jpg|thumb|Unloading pallets of meals, ready to eat (MREs) from a C-23 Sherpa rear cargo door/ramp.]]
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1988–1989<ref name="Janes88-89"/> 
|prime units?=kts
<!--
        General characteristics
-->
|crew=3 (2 pilots plus 1 cabin crew)
|capacity=30 passengers, or 18 Litter based passengers / {{cvt|7000|lb|0}} maximum payload
|length ft=58
|length in=0.5
|length note=
|span ft=74
|span in=8
|span note=
|height ft=16
|height in=3
|height note=
|wing area sqft=453
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 63A418]]; '''tip:''' [[NACA airfoil|NACA 63A414]]<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=14727
|empty weight note=including crew
|gross weight lb=
|gross weight note=
|max takeoff weight lb=22900
|max takeoff weight note=<br>
*'''Maximum landing weight:''' {{cvt|22600|lb|0}}
|fuel capacity={{cvt|560|impgal|USgal l}} / {{cvt|4480|lb|0}}
|more general=
<!--
        Powerplant
-->
|eng1 number=2
|eng1 name=[[Pratt & Whitney Canada PT6A-45-R]]
|eng1 type=[[turboprop]] engines
|eng1 shp=1198
|eng1 note=

|prop blade number=5
|prop name=[[Hartzell Propeller|Hartzell]]
|prop dia m=2.82
|prop dia note=constant-speed fully-feathering propeller
<!--
        Performance
-->
|max speed kts=252
|max speed note=
|cruise speed kts=228
|cruise speed note= {{efn|{{cvt|157|kn|mph km/h|0}} at {{cvt|21000|lb|0}} AUW at {{cvt|10000|ft|0}} }}
|stall speed kts=73
|stall speed note=at MLW flaps and gear down {{efn| {{cvt|90|kn|mph km/h|0}} flaps and gear up }}
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kts=
|minimum control speed note=
|range nmi=1185
|range note=with {{cvt|7000|lb|0}} payload, max fuel, reserves for 45 minute hold and {{cvt|43|nmi|mi km|0}} diversion{{efn|{{cvt|669|nmi|mi km|0}} with {{cvt|5000|lb|0}} payload, max fuel, reserves for 45 minute hold and {{cvt|43|nmi|mi km|0}} diversion }}
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=28000
|ceiling note=one engine inoperative at {{cvt|21000|lb|0}} AUW
|climb rate ftmin=1180
|climb rate note=
|time to altitude=
|wing loading lb/sqft=50.55
|wing loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|0.1046|shp/lb}} maximum
|more performance=<br/>
*'''Take-off run (FAR & BCAR Gp.A):''' {{cvt|3420|ft|0}} ISA
*'''Take-off run (FAR & BCAR Gp.A):''' {{cvt|3420|ft|0}} ISA + {{cvt|15|C|F|0}}
*'''Landing run at MLW BCAR:''' {{cvt|4020|ft|0}} normal field
*'''Landing run at MLW BCAR:''' {{cvt|3150|ft|0}} short field
*'''Landing run at MLW FAR:''' {{cvt|3650|ft|0}}
|avionics=
}}