 |
|
|
Specifications |
|
Maximum Cruise Speed |
403 ktas (747
km/hr), 33,000 ft (10,058 m), mid-cruise weight |
|
NBAA lFR Range
(100 nm alternate) |
1,744 nautical miles
(3,232 km) (full fuel, maximum takeoff weight) |
|
Airport Performance
(dry, level hard-surfaced runway with zero
wind) |
Takeoff
distance(SL,ISA, MTOW) 3,600ft (1,097m)
Landing distance (SL, ISA, MLW) 3,180ft (969m) |
|
Ceiling |
Maximum certified
45,000ft (13,716m)
Single engine 27,750 ft (8,458 m) |
|
Rates of Climb |
All engines 3,190
fpm (972m/min)
Single engine 1,133 fpm (345m/min) |
|
Airspeed Limits |
VMO at 8,000ft
(2,438 m) to
27,900ft (8,504 m) 275 kias (510km/hr)
MMO at 27,900 ft (8,504 m) and above M 0.70
(indicated) |
|
Stall Speed |
86 kcas (159 km/hr)
MLW |
|
Pressurization |
Nominal pressure
differential is 8.9 psi (61 kP) |
|
Outside Dimensions |
Overalllength 47 ft
3 in (14.40 m)
Overall height. 15 ft 0 in (4.57 m)
Wingspan 51 ft 8 in (15.75 m) |
|
Cabin Dimensions
(with typical interior installed) |
Length (excluding
cockpit) 189in (4.80m)
Height 57 in (1.45 m)
Width 58 in (1.47 m) |
|
Engines |
Two Pratt & Whitney
PW530A
Takeoff thrust 2,8871b (12.84 kN)
Bypass ratio 3.5:1 |
|
Design Weights and Capacities |
Maximum ramp weight 15,000 lb (6,804 kg)
Maximum takeoff weight 14,800 lb (6,713 kg)
Maximum landing weight 13,500 lb (6,123 kg)
Maximum zero fuel weight 11,300 lb (5,126 kg)
Maximum fuel capacity (6.7 lb/gal) 4,824 lb (2,188
kg)
Typical empty weight* 9,040 lb (4,100 kg)
Two erew plus furnishings 400 lb (181 kg)
Typical basic operating weight (BOW) 9,440 lb
(4,282 kg)
Useful load ** 5,560 lb (2,522 kg)
Payload with full fuel 736 lb (334 kg) |
|
|
|
|
* Reflects standard
aircraft with typical options, typical interior
and unusable fuel and oil
**Amount of payload and fuel that can be
carried, over and above crew
(based on ramp weight)
|
|
|
