 |
| Program launch date |
October 2006 |
| First flight date |
August 2006 |
| Certification date |
August 2007 |
| First delivery date |
Late 2007 |
| Number of crew and passengers |
2+8 |
| Cabin dimensions (LxHxW) |
21.3×5.7×6 ft / 6.5×1.75×1.83m |
| Cabin volume |
604 cu ft |
| External length |
51ft 2 in / 15.60 m |
| External height |
18ft 1 in / 5.51 m |
| Wingspan |
54ft 4 in / 16.56 m |
| Engine make/model |
Honeywell TFE-731-50R (2) |
| Engine thrust rating (sea level,ISA) |
4660 lb / 20.7 kN |
| Avionics suite |
Rockwell Collins Pro Line 21 |
| MTOW |
28,000 lb |
| MLW |
23,350 lb |
| ZFW |
18,450 lb |
| BOW |
16,420 lb |
| Usable fuel weight |
10,000 lb |
| Mmo |
Mach 0.80 |
| Vmo |
310 kcas |
| High-speed cruise |
466 kt / 536 mph / 863 km/h |
| Long-range cruise |
Mach 0.70 / 402 ktas |
| NBAA IFR range at long-distance cruise |
2,950 nm / 5463 km |
| Certified maximum altitude |
41,000 ft / 12,497 m |
| Cabin altitude at maximum altitude |
8,000 ft |
| Balanced field length for takeoff |
4,696 ft |
| Standard equipped price |
$14.3 million |
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on Четверг, Сентябрь 17th, 2009 at 17:38 and is filed under Новые Самолёты.
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Сентябрь 17th, 2009
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