Panel - Left Side
Panel - Right Side
Panel - Full View
Specifications Engine 310 Horsepower Fuel Capacity 81 gals. useable Maximum Speed TAS 180 kts Useful Load 1089 lbs. Maximum glide 88 Glide Ratio 9.6 to 1 Final Approach Speed 77-85 Max. demo. X-wind 20
Engine 310 Horsepower
Fuel Capacity 81 gals. useable
Maximum Speed TAS 180 kts
Useful Load 1089 lbs.
Maximum glide 88
Glide Ratio 9.6 to 1
Final Approach Speed 77-85
Max. demo. X-wind 20
Tiedown:
Color:
Year:
Equip:
Forward: 138@2200 to 139.1@2700 to 141.4@3210 to 143.8@3400 Aft: 148.1
Replace sample weights with your actual weights, then click on the "Calculate" button to see the new takeoff C.G. Pilots should always calculate the W&B on the ramp prior to takeoff using the latest data from the POH, and taking into account all circumstances including the difference between takeoff and landing fuel quantity and weight.
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