Lancair 1994 IVP

Friday, February 01, 2008 at 12:00 AM ET

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Key Takeaways:

The Lancair 1994 IVP is a 4-seater aircraft powered by a 350 HP Continental TSIO-550B1B engine, providing a useful load of 1000 lbs.
It demonstrates high performance with a cruise speed of 300 knots and a maximum range of 1050 nautical miles at 75% power.
Key operational capabilities include a best rate of climb of 2500 fpm, a service ceiling of 25,000 ft, and a takeoff ground roll of 800 ft.

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Lancair 1994 IVP

Engine make/model:

Cont. TSIO-550B1B

Horsepower:

350

TBO hrs.:

1600

Propeller:

Const. spd.

Landing gear type:

Tri/Retr.

Gross weight (lbs.):

3200

Empty weight, std. (lbs.):

2200

Useful load, std. (lbs.):

1000

Fuel (gals.):

88

Wingspan:

30.2 ft. (w/winglets: 32.6)

Overall length:

25 ft.

Height:

8 ft.

Wing area (sq. ft.):

98 (w/winglets: 108)

Seating capacity:

4

Cabin width (in.):

46

Cabin height (in.):

48

Baggage capacity (lbs.):

150

PERFORMANCE

Cruise speed (kts.):

75% power:

300

Max range (w/ reserve) (nm):

75% power:

1050

Fuel consumption (gph):

75% power:

18

Estimated endurance (65% power with 1-hr. reserve):

3 hrs. 30 mins.

Stall speed (gear, flaps down) (knots):

73

Best rate of climb (fpm):

2500

Service ceiling (ft.):

25,000

Takeoff ground roll (ft.):

800

Landing ground roll (ft.):

1700