Commander 1999 114B

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

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Key Takeaways:

The article details the specifications for the Commander 1999 114B aircraft, powered by a 260 HP Lycoming IO-540-T4B5 engine with a 2000-hour TBO.
This 4-seat aircraft has a useful load of 1158 lbs and a baggage capacity of 200 lbs.
Key performance figures include a cruise speed of 160 knots (at 75% power with a 636 nm range) or 155 knots (at 65% power with a 705 nm range).
It boasts a best rate of climb of 1070 fpm, a service ceiling of 16,800 ft, and a stall speed of 54 knots (gear and flaps down).

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commander

Commander 1999 114B

Engine make/model:

Lyc. IO-540-T4B5

Horsepower:

260

TBO hrs.:

2000

Propeller:

Const. spd.

Landing gear type:

Tri/Retr.

Gross weight (lbs.):

3260

Empty weight, std. (lbs.):

2102

Useful load, std. (lbs.):

1158

Fuel (gals.):

68

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:

160

65% power:

155

Max range (w/ reserve) (nm):

75% power:

636

65% power:

705

Fuel consumption (gph):

75% power:

14.3

65% power:

12.6

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

4 hrs. 30 mins.

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

54

Best rate of climb (fpm):

1070

Service ceiling (ft.):

16,800

Takeoff ground roll (ft.):

1145

Landing ground roll (ft.):

720