Additionally, the fuel efficiencies of the Avanti II are almost forty percent higher than the more traditional business jets and even twenty-five percent higher than the most fuel efficient turbo-props. The Avanti II is truly in a class by itself.
Technical Data:
| Maximum Cruise Speed (at ft 31,000 ft ISA) | 402 KTAS (745 km/h) |
| Maximum Ceiling | 41,000 ft/12.500 m |
| Maximum Ceiling | 41,000 ft/12.500 m |
| Rate of Climb | 2,770 fpm/844 mpm |
| Take-Off Distance (Sea Level, ISA, MTOW,50 ft obstacle) | 3,235 ft/986 m |
| Landing Distance (Sea Level, ISA, MLOW, 50 ft obstacle, no reverse) | 3,282 ft/1.000 m |
| NBAA IFR Maximum Range | 1,470 nm/2.722 km |
| Engines | Pratt & Whitney of Canada PT6A-66B, Power 850 SHP/634kW ea.(flat rated from 1,630 HP) |
| External Dimensions | Wing Span 46’ 0.48’’/14.03 m Length 47’ 3.24’’/14.41 m Height 13’ 0.90’’/3.98 m |
| Cabin Dimensions | Height 5’ 9’’/1.75 m Width 6’ 1”/1.85 m Length 14’ 11’’/4.55 m |
| Baggage Compartment | Volume 44.15 ft3/1.25 m3 Length 5’ 7’’ ft/1.70 m Maximum Weight 300 lbs/136 kg |
| Maximum Take-Off Weight | 12,100 lbs/5,489 kg |
| Maximum Landing Weight | 11,500 lbs/5,216 kg |
| Maximum Zero Fuel Weight | 9,800 lbs/4,445 kg |
| Standard Empty | 7,800 lbs/3,538 kg |
| Maximum Fuel Capacity | (usable at 6.75 lbs/gal) 2,802 lbs/1,271 kg |
| Useful Load | 4,150 lbs/1,882 kg |
| Maximum Payload | 1,800 lbs/816 kg |
| Fuel with Max. Payload | 2,350 lbs/1,067 kg |
| Payload with Max. Fuel | 1,350lbs/613 kg |
| Pressurisation Differential | 9.0 psi/0.62 bar (Sea Level Cabin up to 24,000 ft/7.315 m) |
| Maximum Seating Capacity | 9+2 crew |
| Typical Executive Payload | 6+1 crew |
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<td width=”257″><strong>Maximum Cruise Speed</strong><br />
(at ft 31,000 ft ISA)</td>
<td width=”372″>402 KTAS (745 km/h)</td>
</tr>
<tr>
<td><strong>Maximum Ceiling </strong></td>
<td>41,000 ft/12.500 m</td>
</tr>
<tr>
<td><strong>Maximum Ceiling</strong></td>
<td>41,000 ft/12.500 m</td>
</tr>
<tr>
<td><strong>Rate of Climb</strong></td>
<td>2,770 fpm/844 mpm</td>
</tr>
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<td><strong>Take-Off Distance</strong><br />
(Sea Level, ISA, MTOW,50 ft obstacle)</td>
<td>3,235 ft/986 m</td>
</tr>
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<td><strong>Landing Distance</strong><br />
(Sea Level, ISA, MLOW,<br />
50 ft obstacle, no reverse)</td>
<td>3,282 ft/1.000 m</td>
</tr>
<tr>
<td><strong>NBAA IFR Maximum Range</strong></td>
<td>1,470 nm/2.722 km</td>
</tr>
<tr>
<td><strong>Engines </strong></td>
<td><p>Pratt & Whitney of Canada PT6A-66B, Power 850 SHP/634kW ea.(flat rated from 1,630 HP)</p>
</td>
</tr>
<tr>
<td><strong>External Dimensions</strong></td>
<td>Wing Span 46’ 0.48’’/14.03 m<br />
Length 47’ 3.24’’/14.41 m<br />
Height 13’ 0.90’’/3.98 m</td>
</tr>
<tr>
<td><strong>Cabin Dimensions</strong></td>
<td>Height 5’ 9’’/1.75 m<br />
Width 6’ 1”/1.85 m<br />
Length 14’ 11’’/4.55 m</td>
</tr>
<tr>
<td><strong>Baggage Compartment</strong></td>
<td>Volume 44.15 ft3/1.25 m3<br />
Length 5’ 7’’ ft/1.70 m<br />
Maximum Weight 300 lbs/136 kg</td>
</tr>
<tr>
<td><strong>Maximum Take-Off Weight</strong></td>
<td>12,100 lbs/5,489 kg</td>
</tr>
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<td><strong>Maximum Landing Weight</strong></td>
<td>11,500 lbs/5,216 kg</td>
</tr>
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<td><strong>Maximum Zero Fuel Weight</strong></td>
<td>9,800 lbs/4,445 kg</td>
</tr>
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<td><strong>Standard Empty </strong></td>
<td>7,800 lbs/3,538 kg</td>
</tr>
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<td><strong>Maximum Fuel Capacity</strong></td>
<td>(usable at 6.75 lbs/gal) 2,802 lbs/1,271 kg</td>
</tr>
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<td><strong>Useful Load</strong></td>
<td>4,150 lbs/1,882 kg</td>
</tr>
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<td><strong>Maximum Payload</strong></td>
<td>1,800 lbs/816 kg</td>
</tr>
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<td><strong>Fuel with Max. Payload </strong></td>
<td>2,350 lbs/1,067 kg</td>
</tr>
<tr>
<td><strong>Payload with Max. Fuel </strong></td>
<td>1,350lbs/613 kg<br /></td>
</tr>
<tr>
<td><strong>Pressurisation Differential </strong></td>
<td>9.0 psi/0.62 bar (Sea Level Cabin up to 24,000 ft/7.315 m)</td>
</tr>
<tr>
<td><strong>Maximum Seating Capacity</strong></td>
<td> 9+2 crew</td>
</tr>
<tr>
<td><strong>Typical Executive Payload </strong></td>
<td>6+1 crew</td>
</tr>
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