DE HAVILLAND CANADA DHC-5
DE HAVILLAND CANADA DHC-5
Aircraft
Name:
DHC-5
Manufacturer:
Body:
Narrow
Wing:
Fixed Wing
WTC:
M
APC:
B
Type Code:
L2T
Engine:
Turboprop
Engine Count:
Multi
Manufacturered as
DE HAVILLAND CANADA Buffalo
DE HAVILLAND CANADA C-115 Buffalo
DE HAVILLAND CANADA C-8 Buffalo
DE HAVILLAND CANADA CC-115 Buffalo
DE HAVILLAND CANADA CV-7 Buffalo
DE HAVILLAND CANADA DHC-5 Buffalo
DHC5
The de Havilland Canada DHC-5 Buffalo is a short takeoff and landing () utility transport, a turboprop version developed from the earlier piston-powered DHC-4 Caribou. The aircraft has extraordinary STOL performance and is able to take off in distances much shorter than even light aircraft can manage.
Technical Data
Wing span:
29.26 m
Length:
24.08 m
Height:
8.73 m
Powerplant:
2 x General Electric CT64-820-4 turboprop, 3,133 hp (2,336 kW) each.
Engine Model:
General Electric T64
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
500 m
MTOW:
18500 kg
Initial Climb (to 5000 ft)
IAS:
n/a
ROC:
n/a
Initial Climb (to FL150)
IAS:
n/a
ROC:
n/a
Initial Climb (to FL240)
IAS:
n/a
ROC:
n/a
MACH Climb
MACH:
n/a
ROC:
n/a
Cruise
TAS:
200 kts
MACH:
n/a
Ceiling:
370
Range:
600 NM
Initial Descent (to FL240)
MACH:
n/a
ROD:
n/a
Descent (to FL100)
IAS:
n/a
ROD:
n/a
Descent (FL100 & below)
IAS:
n/a
MCS:
n/a
ROD:
n/a
Approach
Vapp (IAS):
n/a
Distance:
350 m
