View source for Engineering:Aeromot AMT-300 Turbo Ximango Shark

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{|{{Infobox aircraft begin
 | name=AMT-300 Turbo Ximango Shark
 | image=
 | caption=
}}{{Infobox aircraft type
 | type=[[Engineering:Motor glider|Motor glider]]
 | national origin={{wipe|Brazil}}
 | manufacturer=Aeromot
 | designer=
 | first flight=July 1997
 | introduced=1999
 | retired=
 | status=
 | primary user=
 | number built=7
 | developed from=
 | variants with their own articles=
}}
|}

The '''Aeromot AMT-300 Turbo Ximango Shark''' is a Brazilian [[Engineering:Motor glider|motor glider]] manufactured by the [[Earth:Aerospace|aerospace]] company Aeromot.<ref name="jack19">{{harvnb|Jackson|2005|p=19}}</ref>

==Design and development==
It is a single piston engine, and one of the improved versions of the Aeromot Ximango family of motor gliders, also with [[Engineering:Composite aircraft|composite structure]] and conventional retractable landing gear, also designed to carry one pilot and one passenger on short trips.

==Variants==
;AMT-300P Polícia: Version for military and police use for observation and reconnaissance. 
;AMT-300R Reboque: Gliger tug version

==Specification==
{{Aircraft specs
|ref={{Harvnb | Jackson | 2007 | p = 28}}
|prime units?=met
<!--
        General characteristics
-->
|genhide=
|crew=2
|capacity=
|length m=8.08
|length ft=
|length in=
|length note=
|span m=17.67
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=<!-- swing-wings -->
|swept ft=<!-- swing-wings -->
|swept in=<!-- swing-wings -->
|swept note=
|dia m=<!-- airships etc -->
|dia ft=<!-- airships etc -->
|dia in=<!-- airships etc -->
|dia note=
|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|width note=
|height m=1.93
|height ft=
|height in=
|height note=
|wing area sqm=18.75
|wing area sqft=
|wing area note=
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|swept area note=
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|volume note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=630
|empty weight lb=
|empty weight note=
|gross weight kg=800
|gross weight lb=
|gross weight note=
|max takeoff weight kg=850
|max takeoff weight lb=
|max takeoff weight note=
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->
|lift note=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=Rotax 914F
|eng1 type=turbo charged engine
|eng1 kw=73.5<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|prop blade number=2
|prop name=MT-Propeller variable pitch 
|prop dia m=1.65<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop note=

<!--
        Performance
-->
|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=225
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=78
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=245
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=1015
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=1500
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=8700
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=32.1
|climb rate ms=1.98
|climb rate ftmin=
|climb rate note=
|sink rate ms=0.96<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2=45.3
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|power/mass met=
|power/mass imp=
|power/mass note=
|thrust/weight=
|thrust/weight note=
|more performance=
}}

==See also==
{{aircontent
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->
|see also=
|related=<!-- related developments -->
*[[Engineering:Fournier RF-10|Fournier RF-10]]
*[[Engineering:Aeromot AMT-200 Super Ximango|Aeromot AMT-200 Super Ximango]]
|similar aircraft=<!-- similar or comparable aircraft -->
|sequence=<!-- designation sequence, if appropriate -->
|lists=<!-- related lists -->
}}

==References==
{{reflist}}

==Bibliography==
{{refbegin}}
*{{cite book|last=Jackson|first=Paul|title= Jane's All The World's Aircraft 2005-2006|year=2005|publisher=Jane's Information Group|location={{wipe|United Kingdom}}| ISBN=9780710621566}}
*{{cite book|last=Jackson|first=Paul|title= Jane's All The World's Aircraft 2007-2008|year=2007|publisher=Jane's Information Group|location={{wipe|United Kingdom}}| ISBN=9780710627926}}
{{refend}}

==External links==
* {{Citation|url=https://sistemas.anac.gov.br/certificacao/produtos/Espec/EP-8602-15p.pdf |place={{wipe|Brazil}} |trans-title=Type Certificate |title=Certificação |language=Portuguese |publisher=National Civil Aviation Agency of Brazil}}.


[[Category:Motor gliders]]
[[Category:Low-wing aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:T-tail aircraft]]

{{Sourceattribution|Aeromot AMT-300 Turbo Ximango Shark}}