Editing Cessna 172 (section)

==Specifications (172R)==
{{multiple image
 |total_width = 500
 | image1 = Cessna 172 3-view line drawing.png
 | alt1 = 3-view line drawing of the base model Cessna 172
 | image_caption1 = 3-view line drawing of the base model Cessna 172
 | image2 = Cessna P172D Powermatic 3-view line drawing.svg
 | alt2 = 3-view line drawing of the Cessna 172 Skyhawk
 | image_caption2 = 3-view line drawing of the Cessna 172 Skyhawk
}}
[[File:GLFC9.jpg|thumb|Cessna 172R [[Flight instruments|instrument panel]]]]
{{Aircraft specs
|ref=Cessna,<ref name="172RSpecs">{{cite web|url = http://www.cessna.com/single-engine/skyhawk/skyhawk-performance.html|title = Cessna Skyhawk Performance|access-date = 22 August 2010|last = [[Cessna]]|year = 2009|url-status = dead|archive-url = https://web.archive.org/web/20100814150916/http://cessna.com/single-engine/skyhawk/skyhawk-performance.html|archive-date = 14 August 2010}}</ref><ref name="SpecPDF">{{cite web|url = http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skyhawk/skyhawk_s&d.pdf|title = Skyhawk 172R Specification and Description|access-date = 22 August 2010|last = [[Cessna]]|date = May 2010|url-status = dead|archive-url = https://web.archive.org/web/20110511100227/http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skyhawk/skyhawk_s%26d.pdf|archive-date = 11 May 2011}}</ref> [[Federal Aviation Administration|FAA]] [[type certificate]]<ref name="3A12" />
|prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification,
met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|genhide=
|crew=one
|capacity=three passengers, {{Convert|120|lb|kg|abbr=on}} of baggage
|length m=
|length ft=27
|length in=2
|length note=
|span m=
|span ft=36
|span in=1
|span note=
|height m=
|height ft=8
|height in=11
|height note=
|wing area sqm=
|wing area sqft=174
|wing area note=
|aspect ratio=7.32
|airfoil=modified NACA 2412
|empty weight kg=
|empty weight lb=1691
|empty weight note=
|gross weight kg=
|gross weight lb=2450
|gross weight note=
|fuel capacity={{Convert|56|gal|L|abbr=on}} ({{Convert|52|gal|L|abbr=on}} [[Usable fuel|usable]])
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Lycoming O-360|Lycoming IO-360-L2A]]
|eng1 type=four cylinder, horizontally opposed aircraft engine
|eng1 kw=<!-- prop engines -->
|eng1 hp=160<!-- prop engines -->
|eng1 shp=<!-- prop engines -->

|prop blade number=2
|prop name=metal, fixed pitch [[McCauley Propeller Systems|McCauley]] Model 1C235/LFA7570
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=6
|prop dia in=3
|prop dia note= (maximum)

<!--
        Performance
-->
|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=122
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=47
|stall speed note=(power off, flaps down)<ref name="JAWA03 p588–9">{{harvnb|Jackson|2003|pp=588–589}}</ref>
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=163
|never exceed speed note=(IAS)
|range km=
|range miles=
|range nmi=696
|range note= with 45 minute reserve, 55% power, at {{convert|12000|ft|m}}
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=13500
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=721
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=68.6
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
* Optional [[Garmin G1000]] [[primary flight display]]
}}