|
Aircraft - Key Technical Data |
Jetstream 31
SFAR41C (US)
Jetstream 31
BCAR/Australia
|
Maximum Takeoff Weight*
15,212 lb / 6,900 kg
15,562 lb / 7,059 kg
|
|
Maximum Landing Weight
14,900 lb / 6,759 kg
14,900 lb / 6,759 kg
|
Maximum Zero Fuel Weight
14,300 lb / 6,486 kg
14,300 lb / 6,486 kg
|
|
Operating Empty Weight
10,200 lb / 4,626 kg
10,200 lb / 4,626 kg
|
Maximum Payload
4,100 lb / 1,860 kg
4,100 lb / 1,860 kg
|
|
Maximum Fuel Capacity
3,024 lb / 1,372 kg
3,024 lb / 1,372 kg
|
Engine 2 x Honeywell
TPE331-10
TPE331-10
|
|
Takeoff Rating per Engine
940 shp
940 shp
|
Propeller
4-blade Dowty
4-blade Dowty
|
|
Diameter
106 in / 2.69 m
106 in / 2.69 m
|
Overall
Length
47 ft 1.5 in / 14.36 m
|
|
Overall Height
17 ft 8 in / 5.38 m
|
Overall Wingspan
52 ft 0 in / 15.85 m
|
|
Cabin Length
24 ft 3 in / 7.39 m
|
Cabin Height
5 ft 11.5 in / 1.8 m
|
|
Cabin Width
6 ft 1 in / 1.85 m
|
Cabin Volume
600 ft3
/ 16.99 m3
|
Typical Baggage Volume
(excludes underseat stowage)
150 ft3
/ 4.25 m3
|
Maximum Cruise Speed
255 kt
|
|
Maximum Cabin Differential
5.5 psi
|
Sea Level Cabin Altitude
12,000 ft
|
|
Maximum Cruise Altitude
25,000 ft
|
Cabin Altitude at Maximum Cruise
Altitude
8,000 ft
|
|
US Aircraft
|
Range with 17 Pax Load
223 nm
|
|
Range with 60% Load Factor
856 nm
|
Typical Fuel Burn
562 lb/hr / 255 kg/hr
|
Rest of World Aircraft
(J31 higher TOW)
|
Range with Full Pax Load
297 nm
|
|
Range with 60% Load Factor
980 nm
|
Typical
Fuel Burn
562 lb/hr / 255 kg/hr
|
|
* - MTOW for a Canadian aircraft is
15,322 lb.
|