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Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009<br />

2 Airplane and Systems Descriptions<br />

2.3 Fuel and Fuel Capacity<br />

Permissible fuel qualities:<br />

Useable fuel capacity:<br />

Total fuel capacity:<br />

Premium Unleaded Auto Fuel<br />

(min. 91AKI) 100 LL Aviation Fuel<br />

21 gallons<br />

22 gallons<br />

2.4 Engine Oil, Coolant<br />

Engine oil: Automotive engine oils * ,1<br />

Engine oil capacity:<br />

Recommended oil:<br />

0,75 gallons (2,8 liters)<br />

Motorcycle oil of a registered<br />

brand with gear additives 1<br />

Recommended cooling fluid:<br />

Coolant capacity:<br />

Ratio:<br />

Conventional coolant, ethylene<br />

glycol based 1<br />

0,65 gallons (2,5 liters)<br />

1:1 (Concentrate : Water)<br />

2.5 <strong>Operating</strong> Weights and Loading<br />

Maximum take-off weight (MTOW): 1.320 lb (600 kg)<br />

Maximum useful load: 650 lb (295 kg)<br />

Minimum empty weight: ** 670 lb (305 kg)<br />

Minimum flying weight: 815 lb (370 kg)<br />

Baggage: 66 lb (30 kg)<br />

Fuel (max): 126 lb (57 kg)<br />

* No Aircraft engine oils, refer to Rotax operation instructions<br />

1<br />

**<br />

!<br />

Refer to Rotax SI-912-016-R02<br />

Empty weight with basic equipment as described within the POH, without<br />

recovery system.<br />

Values are subject to <strong>ch</strong>ange without notice; please refer to the latest issues<br />

of the appropriate manufacturer manuals.<br />

Airplane and Systems Descriptions 2 - 3

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