Menz Magazine

Piaggio P180 Avanti II

piaggio-p180-avanti-ii

piaggio-p180-avanti-iiWhen cost matters as much as style and performance, the Piaggio P180 Avanti II is the obvious solution with the speed of a business jet delivered by a turbo prop along with the comfort and quiet of a business jet’s luxurious midsized cabin.

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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<head>
<meta http-equiv=”Content-Type” content=”text/html; charset=utf-8″ />
<title>Untitled Document</title>
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<body>
<table width=”645″ border=”1″>
<tr>
<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>
<tr>
<td><strong>Take-Off Distance</strong><br />
(Sea Level, ISA, MTOW,50 ft obstacle)</td>
<td>3,235 ft/986 m</td>
</tr>
<tr>
<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 &amp; 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>
<tr>
<td><strong>Maximum Landing Weight</strong></td>
<td>11,500 lbs/5,216 kg</td>
</tr>
<tr>
<td><strong>Maximum Zero Fuel Weight</strong></td>
<td>9,800 lbs/4,445 kg</td>
</tr>
<tr>
<td><strong>Standard Empty </strong></td>
<td>7,800 lbs/3,538 kg</td>
</tr>
<tr>
<td><strong>Maximum Fuel Capacity</strong></td>
<td>(usable at 6.75 lbs/gal) 2,802 lbs/1,271 kg</td>
</tr>
<tr>
<td><strong>Useful Load</strong></td>
<td>4,150 lbs/1,882 kg</td>
</tr>
<tr>
<td><strong>Maximum Payload</strong></td>
<td>1,800 lbs/816 kg</td>
</tr>
<tr>
<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>
</table>
</body>
</html>

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