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

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