ENGINE:

Manufacturer	Teledyne Continental Motors
Model	IOF-240-B with FADEC
Horsepower	125 BHP at 2,800 RPM
Number of Cylinders	4 (Horizontally Opposed)
Bore	4.438"	11.27 cm
Stroke	3.875"	9.84 cm
Compression Ratio	8.5:1
Displacement	240 cu in	3,933 cc
Oil Sump Capacity	6 US Quarts	5.67 L
Height	24.0"	60.96 cm
Width	31.4"	79.76 cm
Length	29.1"	73.91 cm
Installed Runnable Dry Weight	328 lbs	148.8 Kg

 

PROPELLER:

Type	2-Blade MT Propeller - Metal Leading Edge with Wood and Composite core
Length	69" diameter	1.75 m
Pitch	Fixed

 

 

DIMENSIONS:

Overall Height (max)	7' 5"	2.26 m
Overall Length	20' 3.8"	6.19 m
Wing
Span (overall)	28' 9"	8.76 m
Area	112 ft	10.41 m2
Aspect Ratio	7:1
Cabin
Height (max)	34"	0.86 m
Length (firewall to aft baggage area)	91.9"	2.33 m
Width	48"	1.22 m
Undercarriage	Fixed Tricycle Spring Steel Nose Gear with Castoring Wheel   Spring Aluminum Main Gear with Differential Brakes

DESIGN WEIGHTS & CAPABILITIES:

Fuel	AvGas 100LL / 100
Fuel Capacity
Total capacity	29.5 US Gal	111 L
Total usable	28 US Gal	106 L
Baggage Allowance	100 lbs	45 Kg
Standard Empty Weight	1160 lbs	526 Kg
Max. T/O Weight	1750 lbs	794 Kg
Useful Load	590 lbs	268 Kg
Landing Weight	1750 lbs	794 Kg
Full Fuel Payload	420 lbs	526 Kg

CONDITIONS:

Standard empty weight based upon:

• Empty weight varies according to customer options
• Nominal finishing on all details
• Nominal finishing on all exterior surfaces
• Standard interior
• Nominal propeller weight
• Standard VFR equipment