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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox aircraft
|name=CL-227 Sentinel
|image=
|caption=
|type=Unmanned reconnaissance helicopter
|national_origin=Canada
|manufacturer=[[Canadair]]
|designer=
|first_flight=25 August 1978
|introduction=
|retired=
|status=
|primary_user=
|more_users=
|produced=
|number_built=1
|developed_from=
|variants=
|developed_into=
}}
The '''CL-227 Sentinel''' is a remote-controlled [[unmanned aerial vehicle]] (UAV) made by [[Canadair]].
It displays a distinctively unusual bulbous
The CL-227 was designed in 1977, and the "phase one" prototype made its first flight on 25 August 1978; the larger production "phase two" vehicle first flew untethered on 14 December 1981.<ref name="Janes87">Jane's 1987-1988, p.816</ref> Following evaluation by NATO in March 1982,<ref name="Janes87"/> and was made available to [[NATO]] allied clients in the early 1980s. In the late 1990s it was replaced by an updated version, the CL-327.
==Bombardier Aerospace CL-327 Guardian==
The CL-327 was developed as an upgraded and advance version of the CL-227. The new UAV production line began in 1996 under [[Bombardier Aerospace]], which acquired the assets of [[Canadair]], the original developer of the CL-227.
==Specifications (CL-227 Phase 2)==
{{Aircraft specs
|ref=Jane's 1987-1988 p.816; Leyes and Fleming 1999, p.421
|prime units?=imp
|crew=None
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=190
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|54|kg|abbr=on}}
|more general=
|eng1 number=1
|eng1 name=[[Williams International]] [[Williams WR34|WTS34-16]]
|eng1 type=turboshaft
|eng1 kw=37.3
|eng1 hp=
|eng1 note=
|power original=
|rot number=2 coaxial
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=6.16
|rot area sqft=
|rot area note=
|max speed kmh=
|max speed mph=
|max speed kts=70
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=591
|climb rate note=at {{convert|1500|m|abbr=on}}
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
|avionics=* {{convert|45|kg|abbr=on}} equipment capacity.
}}
==See also==
* [[Canadair CL-289]]
==References==
===Citations===
{{reflist}}
===Bibliography===
* ''Jane's All the World's Aircraft'', 1987-88 edition. McGraw-Hill, 1987; p.816
*{{cite book|last=Leyes|first=Richard A.|title=The History of North American Small Gas Turbine Aircraft Engines|year=1999|publisher=American Institute of Aeronautics and Astronautics|___location=Reston, VA|isbn=978-1563473326|author2=William A. Fleming}}
==External links==
* [http://www.fas.org/man/dod-101/sys/ac/row/cl-327.htm CL-227 Sentinel and CL-327 Guardian]
{{Canadair}}
{{Bombardier Aerospace}}
[[Category:Canadair aircraft|CL-227]]
[[Category:Unmanned aerial vehicles of Canada]]
[[Category:Coaxial rotor helicopters]]
[[Category:1980s Canadian helicopters]]
[[Category:Unmanned helicopters]]
[[Category:Single-turbine helicopters]]
[[Category:Aircraft first flown in 1978]]
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