|
specifications
|
|
Best Price: |
$199,500 |
|
Engine make/model:
|
Lycoming IO-540-T4B5 |
|
Horsepower@rpm@altitude: |
260@2700@SL |
|
Horsepower For Takeoff: |
260 |
|
TBO hours: |
2000 |
|
Fuel Type: |
100/100LL |
|
Propeller type/diameter
(in.): |
Hartzell CS/78 |
|
Landing gear type: |
Conv./Retr. |
|
Max ramp weight (lbs.): |
2850 |
|
Gross weight (lbs): |
2850 |
|
Max Landing weight (lbs.): |
2680 |
|
Std. empty weight (lbs.): |
2040 |
|
Useful load - std. (lbs.): |
810 |
|
Payload - full std. fuel
(lbs.): |
402 |
|
Usable fuel - std.
(gals.): |
68 |
|
Oil capacity (qts.): |
8 |
|
Wingspan: |
30 ft. 4 in. |
|
Overall length: |
24 ft. 1 in. |
|
Height: |
6 ft. 6in. |
|
Wing area (sq. ft.): |
156.6 |
|
Wing loading (lbs./sq.
ft.): |
18.2 |
|
Power loading (lbs./hp.): |
10.9 |
|
Wheel base: |
10 ft. 4 in. |
|
Wheel size (in.): |
6.00 x 6 |
|
Seating capacity: |
2 |
|
Cabin doors : |
0 |
|
Cabin width (in.): |
43 |
|
Cabin height (in.): |
39
(with baggage) |
|
Baggage capacity (lbs./cu.
ft.): |
100/14 |
|
G-limits: |
+6/-3 |
|
performance
|
|
Cruise speed
(knots): |
| |
Altitude |
Speed |
|
75% power: |
6500 |
155 |
|
65% power: |
8500 |
150* |
|
55% power: |
10,500 |
140* |
|
Max range (with
reserve) (nm): |
|
75% power: |
800 |
|
|
65% power: |
900* |
|
|
55% power: |
1,040 |
|
Fuel consumption
(calc. @ .42
lbs./hp/hr.) (gph): |
|
75% power |
13.7 |
|
|
65% power |
11.8 |
|
|
55% power |
10.1 |
|
|
Estimated endurance
(65%) (hrs.): |
4.7 |
Stall speed
(gear, flaps up) (kts.):
|
55 |
|
Stall speed (gear, flaps
down) (kts.): |
49 |
|
Best rate of climb, SL
(fpm): |
1500 |
|
Service ceiling (ft.):
|
18,000 |
|
Takeoff ground roll (ft.):
|
800 |
|
Takeoff over 50-ft.
obstacle (ft.):
|
1100 |
|
Landing ground roll (ft.): |
700 |
|
Landing over 50-ft.
obstacle (ft.): |
2000 |
|
* estimated |
|
| |
