Commander 1996 114TC

Saturday, December 01, 2007 at 12:00 AM ET

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Key Takeaways:

The Commander 1996 114TC is a 4-seat aircraft powered by a 200 HP Lycoming TIO-540-AG1A engine, featuring retractable landing gear and a gross weight of 3305 lbs.
It achieves a cruise speed of 187 knots at 75% power (670 nm range) or 169 knots at 65% power (780 nm range), with an estimated endurance of 5 hours 18 minutes at 65% power.
Key performance indicators include a best rate of climb of 1050 fpm, a service ceiling of 25,000 feet, a stall speed of 59 knots, and takeoff/landing ground rolls of 1408 ft and 734 ft, respectively.

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commander

Commander 1996 114TC

Engine make/model:

Lyc. TIO-540-AG1A

Horsepower:

200

TBO hrs.:

2000

Propeller:

Const. spd.

Landing gear type:

Tri/Retr.

Gross weight (lbs.):

3305

Empty weight, std. (lbs.):

2152

Useful load, std. (lbs.):

1153

Fuel (gals.):

88

Wingspan:

32 ft. 9 in.

Overall length:

24 ft. 11 in.

Height:

8 ft. 5 in.

Wing area (sq. ft.):

152

Seating capacity:

4

Cabin width (in.):

47

Cabin height (in.):

49

Baggage capacity (lbs.):

200

PERFORMANCE

Cruise speed (kts.):

75% power:

187

65% power:

169

Max range (w/ reserve) (nm):

75% power:

670

65% power:

780

Fuel consumption (gph):

75% power:

16.3

65% power:

14.1

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

5 hrs. 18 mins.

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

59

Best rate of climb (fpm):

1050

Service ceiling (ft.):

25,000

Takeoff ground roll (ft.):

1408

Landing ground roll (ft.):

734