Specifications (172R)[]
General characteristics
- Crew: one
- Capacity: three passengers
- Length: 27 ft 2 in (8.3 m)
- Wingspan: 36 ft 1 in (11 m)
- Height: 8 ft 11 in (2.7 m)
- Wing area: 174 sq ft (16 m2)
- Aspect ratio: 7.32
- Airfoil: modified NACA 2412
- Empty weight: 1,691 lb (767 kg)
- Gross weight: 2,450 lb (1,111 kg)
- Fuel capacity: 56 US gallons (212 litres)
- Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (Expression error: Unexpected < operator. kW)
- Propellers: 2-bladed metal
Performance
- Cruise speed: 122 kn (Expression error: Unexpected < operator. mph; Expression error: Unexpected < operator. km/h)
- Stall speed: 47 kn (Expression error: Unexpected < operator. mph; Expression error: Unexpected < operator. km/h) (power off, flaps down)[3]
- Never exceed speed: 163 kn (Expression error: Unexpected < operator. mph; Expression error: Unexpected < operator. km/h) (IAS)[4]
- Range: 696 nmi (
ERROR {Convert}: Invalid parameters: 1=696 2=( 696 )*1852 3= 4= 5= 6= with {u}= n= .
Try using range: {{convert|696|( 696 )*1852|...}} to convert a range of numbers.) with 45 minute reserve, 55% Power, at 12,000 ft - Service ceiling: 13,500 ft (4,100 m)
- Rate of climb: 721 ft/min (
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Try using range: {{convert|721|( 721 )*0.00508|...}} to convert a range of numbers.)
Avionics
- Optional Garmin G1000 Primary Flight Display