Aviat 110 Monocoupe

Staff

Thursday, November 01, 2007 at 12:00 AM ET

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Key Takeaways:

The article provides detailed specifications for the Aviat 110 Monocoupe, a two-seat aircraft powered by an AE IO-360-A1B6 engine producing 350 horsepower for takeoff.
Key performance figures include a maximum level speed of 191 knots, a cruise speed of 161 knots, and a maximum range of 732 statute miles, alongside a best rate of climb of 1700 fpm.
The aircraft features fixed, conventional landing gear, has a useful load of 575 lbs, a wingspan of 23 ft 1 in, and an overall length of 19 ft 10 in.

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Aviat 110 Monocoupe

Engine make/model:

AE IO-360-A1B6

Horsepower for takeoff:

350 (x2)

TBO (hrs):

1400

Fuel type:

100/100LL

Propeller type:

Hartzell two-blade

Landing Gear type:

Fixed, conventional

Max ramp weight (lbs.):

1725

Gross weight (lbs.):

1725

Landing weight (lbs.):

1725

Empty weight, std. (lbs.):

1150

Useful load, std. (lbs.):

575

Payload, full std. fuel (lbs.):

323

Usable fuel, std. (gals.):

Oil capacity (qts.):

Wingspan:

23 ft. 1 in.

Overall length:

19 ft. 10 in.

Wing area (sq. ft.):

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

17.4 (normal), 16.4 (aerobatic)

Power loading (lbs./hp.):

8.6

Seating capacity:

Cabin doors:

Cabin width (in.):

Cabin height (in.):

Baggage capacity (lbs.):

PERFORMANCE

Max level speed (knots):

191

Cruise speed (75% power) (knots):

161

Max range (w. reserve) (sm):

732

Fuel consumption (55% power) (gph):

8.4

Stall speed (flaps up) (kts.):

Best rate of climb (fpm):

1700