Aviat Pitts S2C

Aviat Pitts S2C

Engine make/model:

Lycoming AEIO-540-D4A

Horsepower@rpm@altitude:

260@2700@SL

Horsepower for takeoff:

260

TBO hrs.:

1200

Fuel type:

100LL

Propeller type/diameter:

Hartzell Constant Speed

Landing gear type:

Fixed Bungee

Max ramp weight (lbs.):

1700

Gross weight (lbs.):

1700

Landing weight (lbs.):

1700

Empty weight, std. (lbs.):

1155

Useful load, std. (lbs.):

545

Payload, full std. fuel (lbs.):

377

Useful fuel, std. (gals.):

28

Oil capacity (qts.):

12

Wingspan:

20 ft.

Overall length:

17 ft. 5 in.

Height:

6 ft. 5 in.

Wing area (sq. ft.):

127.5

Wing loading (lbs./sq. ft.):

13.3

Power loading (lbs./hp.):

6.25

Wheel size (in.):

5.00 x 6

Seating capacity:

2

Cabin width (in.):

24

Cabin height (in.):

41

Baggage capacity (lbs.):

20

PERFORMANCE

Cruise speed (kts.):

75% power:

160

65% power:

156

55% power:

152

Max range (w/ reserve) (nm):

75% power:

270

65% power:

290

55% power:

310

Fuel consumption (gph):

75% power:

14.0

65% power:

12.9

55% power:

11.5

Estimated endurance (65%) (hrs):

1.8

Vs_o (kts.):

56

Best rate of climb (SL fpm):

2900

Service ceiling (ft.):

29,500

Takeoff ground roll (ft.):

554

Takeoff over 50-ft. obstacle (ft.):

860

Landing ground roll (ft.):

750

Landing over 50-ft. obstacle (ft.):

1200

Source: Aviat Aircraft Inc.

ODEA DeveloperWriter

Aviat Pitts S2C

Aviat Pitts S2C Engine make/model: Lycoming AEIO-540-D4A Horsepower@rpm@altitude: 260@2700@SL Horsepower for takeoff: 260 TBO hrs.: 1200 Fuel type: 100LL Propeller type/diameter: Hartzell Constant Speed Landing gear type: Fixed Bungee Max…

ODEA Developer

Subscribe to Our Newsletter

Subscribe to Our Newsletter