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Table of content - Eurocopter

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Technical Data<br />

4.4.4 Performance Data<br />

Weight breakdown (with 8 passengers):<br />

• Equipped empty weight Stylence ® configuration (incl. engine oil, unusable<br />

fuel and weight margin <strong>of</strong> ± 1.5%)<br />

Mission pr<strong>of</strong>ile:<br />

Relevant flight data:<br />

The corresponding flight time (incl. climb/descent phase) is approx. 2 hours 13 minutes.<br />

kg lb<br />

2,237 4,932<br />

• 1 Pilot (1 x 85 kg) 85 187<br />

• 8 passengers (8 x 85 kg) 680 1,499<br />

• Reserve fuel 78 172<br />

• Contingency fuel 24 53<br />

• Trip fuel 481 1,060<br />

• Mission take-<strong>of</strong>f weight 3,585 7,903<br />

• Take-<strong>of</strong>f in SL (max. 3,585 kg)<br />

• Climb flight AEO-MCP from SL to 7,000ft with VY , mean 65KIAS<br />

• Level flight in 7,000ft with VBR , mean 113KIAS<br />

• Descent from 7,000ft to SL with R/D <strong>of</strong> -1,000fpm, mean 80KIAS<br />

• Landing in SL<br />

• Contingency: 5%<br />

• Reserve: 20 minutes in 1,500ft at VBR , mean 123KIAS<br />

• The calculated max. range (with 8 passengers) is 266nm (492km)<br />

• Climb: 7nm<br />

• Level: 249nm<br />

• Descent: 10nm<br />

145.10.101.01 E Page 41 <strong>of</strong> 86<br />

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.<br />

This document is property <strong>of</strong> EUROCOPTER ® , no part <strong>of</strong> it shall be reproduced or transmitted without the express prior written authorization <strong>of</strong> EUROCOPTER ® and its <strong>content</strong>s shall not be disclosed. ©EUROCOPTER 2010

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