| AIRFRAME: |
Aluminum |
|
|
| |
Wingspan |
36 ft 2 in |
|
| |
Wing area |
178.3 sq ft |
|
| |
Length |
27 ft 8 in |
|
| |
Height |
8 ft 2 in |
|
| |
Min. Turning Radius |
34 ft |
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| |
Gross Weight |
3600 lbs |
|
| |
Max Landing Weight |
3600 lbs |
|
| |
Max Ramp Weight |
3615 lbs |
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| |
Basic Empty Weight |
2248 lbs |
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| |
Useful Load |
1367 lbs |
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| |
Max Baggage Weight - TOTAL |
200 lbs |
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| |
Fwd Compartment |
100 lbs |
|
| |
Aft Compartment |
100 lbs |
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| |
Fuel Capacity (USEABLE) |
102 gal |
|
| PROPELLER: |
Hartzell |
3 blades |
78 in diam |
| ENGINE: |
Lycoming, 6 Cyl. |
IO-540-K1G5 |
300 HP @ 2700 rpm |
|
Manifold Press (MAX) |
36 in. |
|
Oil Capacity |
12 Qtx. MAX |
| PERFORMANCE: |
Never Exceed Speed (Vne) |
197 kts |
|
| |
Max Cruise Speed (Vno) |
154 kts |
|
| |
Cruise Speed (65% power, 10,000 ft) |
150 kts (approx.) |
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| |
Maximum Range (65%, 10,000 ft) |
900 nm (w/ reserves) |
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| |
Endurance (65%, 10,000 ft) |
6 Hrs (w/ reserves) |
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| |
Max Altitude (limit) |
14,000 ft |
|
| |
Maneuvering Speed (Va) |
|
|
| |
3600 Lbs. |
134 KIAS |
|
| |
2225 Lbs. |
104 KIAS |
|
| |
Stall Speed (flaps up) |
62 kts |
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| |
Stall Speed (flaps extended) |
58 kts |
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| |
Take-Off Speed (Rotate) |
74 - 80 kts |
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| |
Max Speed Flaps Ext (Vfe) |
112 kts |
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| |
Best Rate of Climb (Vy) |
90 kts |
|
| |
Best Angle of Climb (Vx) |
76 kts |
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| |
En Route Climb |
100 kts |
|
| |
Best Glide (FLAPS UP, Prop FULL DECREASE) |
80 kts |
|
| |
Emergency Descent - FULL FLAPS, Prop FULL FORWARD |
95 kts |
|
| |
Landing Distance Over 50' Obs, FULL FLAPS DOWN |
1800 ft |
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| |
Take-Off Distance Over 50' Obs, FLAPS AT 25 DEGREES |
2200 ft |
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| |
Approach Speeds |
|
|
| |
Normal - FLAPS UP |
95 KIAS |
|
| |
Light Weight - FULL FLAPS |
80 KIAS |
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| |
Short/Soft Field, FULL FLAPS |
79 KIAS |
|
| |
MAX Demo X-Wind |
17 KTS |
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| |
MAX Storm Window Open |
129 KIAS |
|
