DE HAVILLAND CANADA DHC-2
DE HAVILLAND CANADA DHC-2
Aircraft
Name:
DHC-2
Manufacturer:
Body:
Narrow
Wing:
Fixed Wing
WTC:
L
APC:
A
Type Code:
L1P
Engine:
Piston
Engine Count:
Single
Manufacturered as
DE HAVILLAND CANADA Beaver
DE HAVILLAND CANADA DHC-2 Mk1 Beaver
DE HAVILLAND CANADA L-20 Beaver
DE HAVILLAND CANADA U-6 Beaver
AIRTECH (1) Beaver
AIRTECH (1) DHC-2-PZL3S Beaver
DHC2
The de Havilland Canada DHC-2 Beaver is a single engined, high wing, propeller-driven, Short Take-Off and Landing (STOL) aircraft developed by de Havilland Canada, primarily known as a bush plane. It is used for cargo and passenger hauling, aerial application (crop dusting and aerial topdressing), and has been widely adopted by armed forces as a utility aircraft.
Technical Data
Wing span:
14.63 m
Length:
9.22 m
Height:
2.74 m
Powerplant:
1 x Pratt & Whitney R-985 Wasp Jr. radial engine, 450 hp (336 kW).
Engine Model:
Pratt & Whitney R-985
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
310 m
MTOW:
2300 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:
109 kts
MACH:
n/a
Ceiling:
180
Range:
670 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:
305 m
