SPECIFICATIONS:
| Aircraft Dimensions | |
| Wing span | 36' 8" |
| Length | 34' 10" |
| Height | 12' 1" |
| Weight and Balance | |
| Empty weight | 4,656lb. |
| Maximum Takeoff Weight (MTOW) | 6,315 lb. |
| Engine | |
| Left | Lycoming LTIO-540-U2A |
| Right | Lycoming TIO-540-U2A |
| Horsepower (ea.) | 350 @ 2,500 RPM |
| Fuel | 100/130 Grade Aviation Gasoline (minimum) |
| Propeller | |
| Manufacturer | Hartzell Propeller, Inc. |
|
Hub Model Left Right |
HC-C3YR-2LUF/FJC7451(B) HC-CY3R-2UF/FC7451(B) |
|
Number of Blades |
3 |
| Altitude Limits | |
| Maximum Approved Altitude | 25,000 ft.. |
| Ceiling | 29,000 ft. |
|
Temperature Limits |
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Cylinder Head Temperature |
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|
Radial Red Line (Minimum) |
100°C |
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|
Green Arc (Normal Operating Range) |
100-260°C |
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Radial Red Line (Maximum) |
260°C |
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|
Oil Temperature |
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Green Arc (Normal Operating Range) |
24-118°C |
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Radial Red Line (Maximum) |
. 118°C |
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Exhaust Gas Temperature |
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|
Radial Red Line (Maximum) |
1650°F |
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| Pressure Limits |
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Oil Pressure |
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Radial Red Line (Minimum) (Idling) |
25 PSI |
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Green Arc (N ormal Operating Range) |
55-95 PSI |
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Radial Red Line (Maximum) |
115 PSI |
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Exhaust Gas Temperature |
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Radial Red Line (Maximum) |
1650°F |
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Manifold Pressure |
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Green Arc (Normal Operating Range) |
12.0-42.0 IN. HG. |
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Radial Red Line (Maximum) |
42.0 IN. HG. |
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Hydraulic Pressure |
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Green Arc (Normal Operating Range) |
1100-1400 PSI |
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Radial Red Line (Maximum) |
1500 PSI |
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Gyro Pressure |
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Green Arc (Normal Operating Range) |
4.8-5.2 IN. HG. |
| Fuel Pressure | ||
| Green Arc (normal) | 29-65 PSI | |
| Radial Red Line (min. - idle) | 12 PSI | |
| Radial Red Line (max) | 65 PSI |
| Airspeed Limitations | ||
| VA | Maneuvering Speed | 160 KIAS |
| VNO | Max Structural Cruising Speed | 215 KIAS |
| VSO | Stalling Speed in Landing Configuration | 71 KIAS |
| VMCA | Air Minimum Control Speed | 85 KIAS |
| VFE |
Flaps Max Extend Speed 20° Flaps 40° Flaps |
188 KIAS 148 KIAS |
| VLO | Landing Gear - Operation | 153 KIAS |
| VLE | Landing Gear - Max speed when extended | 153 KIAS |
| Maximum Flap Extended Speeds | |
| Flaps degrees | KIAS |
| 20 | 188 |
| 45 | 148 |
| Fuel Limitations | |
| Fuel Capacity (U.S. gal.) | |
| Wing Tank (each) | 65.0 |
| Fuselage Tank | 85.0 |
| Total (all tanks) | 215.0 |