|
| |
|
Base/used Price:
| $110,000 |
| Engine make/model: | Lycoming IO-320-B1A
|
| Horsepower@rpm: | 160@2700 |
| Horsepower for takeoff: | 160 |
TBO hrs.:
| 2000 |
| Fuel type: | 100/100LL
|
Propeller type/diameter:
| CS
|
Landing gear type:
| Tri/Retr.
|
| Max ramp weight (lbs.): | 3600
|
| Gross weight (lbs.): | 3600 |
| Landing weight (lbs.): | 3600
|
| Empty weight, std. (lbs.): | 2210
|
| Useful load, std. (lbs.): | 1390
|
Payload, full std. fuel (lbs.):
| 850
|
| Usable fuel (gals.): | 90 |
| Optional fuel - std. (tip tanks) (gals.): | 120
|
| Oil capacity (qts.): | 8
|
| Wingspan: | 36 ft. |
| Overall length: | 25 ft. 2 in.
|
| Height: | 8 ft. 3 in. |
| Wing area (sq. ft.): | 178 |
Wing loading (lbs./sq. ft.):
| 20.2
|
Power loading (lbs./hp.):
| 11.3
|
Wheel base (in.):
| 7 ft. 3 in.
|
| Wheel track (in.): | 9 ft. 10 in.
|
Wheel size (in.):
| 6.00 x 6
|
| Seating capacity: | 4-6
|
Cabin doors:
| 1
|
| Cabin width (in.): | 44 |
| Cabin height (in.): | 46 |
| Baggage capacity (lbs.): | 250
|
| |
PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power @ 8,000 ft.: | 169 |
| 65% power @ 12,000 ft.: | 162 |
55% power @ 10,000 ft.:
| 144
|
| | |
| Max range (w/100 nm reserve) (nm): | |
75% power:
| 724 |
65% power:
| 791
|
55% power:
| 832*
|
| | |
Fuel consumption (@ .42 lbs./hp/hr. sfc) (gph):
| |
| 75% power: | 16.8 |
| 65% power: | 14.6 |
55% power:
| 12.3 |
| | |
| Estimated endurance (65%, 90 gals.) (hrs): | 5.0 |
| Vs (kts.): | 66 |
| Vso (kts.): | 60
|
| Best rate of climb (SL fpm): | 1460 |
Single-engine rate of climb, SL (fpm):
| 260
|
| Service ceiling (ft.): | 18,600 |
Single-engine service ceiling (ft.):
| 6600
|
| Takeoff ground roll (ft.): | 950 |
| Takeoff over 50-ft. obstacle (ft.): | 1570
|
| Landing ground roll (ft.): | 700 |
Landing over 50-ft. obstacle (ft.):
| 1875
|
| |
* estimated
|
|
