கேள்வி: செஸ்னா 172 - படைத்துறைக்காக இயக்குபவர்கள் பற்றி விளக்கவும்.
பதில்: ; 1× 172 ; 3× 172KAndrade 1982, Page 27 ; 18× R172KAndrade 1982, Page 45 ; *வான் படை 8× 172FAndrade 1982, Page 57 *இராணுவம் 1× 172G ; 6× 172KAndrade 1982, Page 95 ; 3Andrade 1982, Page 97 ; ; 8× FR172H, 1× FR172KAndrade 1982, Page 61 ; 2Andrade 1982, Page 147 1 ; 4× 172MAndrade 1982, Page 151 ; 4× 172NAndrade 1982, Page 172 ; (1) ; 8× F172G, 4× F172H, 4× F172MAndrade 1982, Page 189Taylor, John: ''Jane's Pocket Book of Military Transport and Training Aircraft'', page 67. MacMillian Publishing Inc, 1974. Library of Congress 73-15288 ; 8× 172K, delivered 1969 and retired 1972.Andrade 1982, Page 193
கேள்வி: செஸ்னா 172 - விவரங்கள் (172R) பற்றி விளக்கவும்.
பதில்: File:GLFC9.jpg |prime units?=kts |genhide= |crew=one |capacity=three passengers |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=56 US gallons (212 litres) |more general= |eng1 number=1 |eng1 name=Lycoming O-360 |eng1 type=four cylinder, horizontally opposed aircraft engine |eng1 kw= |eng1 hp=160 |eng1 shp= |prop blade number=2 |prop name=metal |prop dia m= |prop dia ft= |prop dia in= |prop note= |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)Jackson 2003, pp. 588–589. |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 12,000 ft |endurance= |ceiling m= |ceiling ft=13500 |ceiling note= |g limits= |roll rate= |glide ratio= |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 }}
கேள்வி: செஸ்னா 172 - உசாத்துணை பற்றி விளக்கவும்.
பதில்: * *