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Specifications
ENGINE:
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Manufacturer |
Teledyne Continental Motors
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Model |
IOF-240-B with FADEC
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Horsepower |
125 BHP at 2,800 RPM
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Number of Cylinders |
4 (Horizontally Opposed)
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Bore |
4.438"
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11.27 cm
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Stroke |
3.875"
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9.84 cm
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Compression Ratio |
8.5:1
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Displacement |
240 cu in
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3,933 cc
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Oil Sump Capacity |
6 US Quarts
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5.67 L
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Height |
24.0"
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60.96 cm
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Width |
31.4"
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79.76 cm
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Length |
29.1"
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73.91 cm
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Installed Runnable Dry Weight |
328 lbs
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148.8 Kg
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PROPELLER:
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Type |
2-Blade MT Propeller - Metal
Leading Edge with Wood and
Composite core
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Length |
69" diameter
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1.75 m
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Pitch |
Fixed
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DIMENSIONS:
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Overall Height (max) |
7' 5"
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2.26 m
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Overall Length |
20' 3.8"
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6.19 m
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Wing |
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Span (overall)
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28' 9"
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8.76 m
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Area
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112 ft
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10.41 m2
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Aspect Ratio |
7:1
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Cabin |
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Height (max)
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34"
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0.86 m
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Length
(firewall to aft baggage
area)
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91.9"
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2.33 m
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Width
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48"
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1.22 m
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Undercarriage |
Fixed Tricycle
Spring Steel Nose Gear
with Castoring Wheel
Spring Aluminum Main
Gear with Differential
Brakes
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DESIGN WEIGHTS & CAPABILITIES:
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Fuel |
AvGas 100LL / 100
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Fuel Capacity |
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Total capacity
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29.5 US Gal
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111 L
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Total usable
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28 US Gal
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106 L
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Baggage Allowance |
100 lbs
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45 Kg
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Standard Empty Weight |
1160 lbs
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526 Kg
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Max. T/O Weight |
1750 lbs
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794 Kg
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Useful Load |
590 lbs
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268 Kg
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Landing Weight |
1750 lbs
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794 Kg
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Full Fuel Payload |
420 lbs
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191 Kg
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CONDITIONS:
Standard empty weight based upon:
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Empty weight varies according to
customer options
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Nominal finishing on all details
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Nominal finishing on all exterior
surfaces
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Standard interior
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Nominal propeller weight
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Standard VFR equipment
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