CESSNA 172 Civil Aircraft Model Details

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General Information of CESSNA 172

Developed From : Cessna 170

Introduction : 1956

Manufacturer : Cessna Aircraft Company

National Origin : United States

Number Built : ~43,000[1]

Produced : 1956–86, 1998–present

Role : Civil utility aircraft

Status : In production

Unit_Cost : 172: US$8,700 (1956)[2]; 172R: US$274,900 (2012)[3]; 172S: US$307,500 (2012)[4]

Variants : T-41 Mescalero

General characteristics of CESSNA 172

Aspect Ratio : 7.32

Airfoil : modified NACA 2412

Capacity : three passengers

Crew : one

Empty Weight : 1,691 lb (767 kg)

Fuel Capacity : 56 US gallons (212 litres)

Gross Weight : 2,450 lb (1,111 kg)

Height : 8 ft 11 in (2.72 m)

Length : 27 ft 2 in (8.28 m)

Powerplant : 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (120 kW)

Propellers : 2-bladed metal

Wing Area : 174 sq ft (16.2 m2)

Wingspan : 36 ft 1 in (11.00 m)

Performance of CESSNA 172

Cruise Speed : 122kn (140mph; 226km/h)

Never Exceed Speed : 163kn (188mph; 302km/h) (IAS)[9]

Range : 696nmi (801mi; 1,289km) with 45 minute reserve, 55% power, at 12,000 ft

Rate Of Climb : 721ft/min (3.66m/s)

Service Ceiling : 13,500ft (4,100m)

Stall Speed : 47kn (54mph; 87km/h) (power off, flaps down)[78]

Wing Loading : 14.1lb/sqft (68.6kg/m2)

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