DE HAVILLAND CANADA DHC-3
DE HAVILLAND CANADA DHC-3
Aircraft
Name:
DHC-3
Manufacturer:
Body:
Narrow
Wing:
Fixed Wing
WTC:
L
APC:
A
Type Code:
L1P
Engine:
Piston
Engine Count:
Single
Manufacturered as
DE HAVILLAND CANADA DHC-3 Otter
DE HAVILLAND CANADA NU-1 Otter
DE HAVILLAND CANADA Otter
DE HAVILLAND CANADA U-1 Otter
DE HAVILLAND CANADA UC Otter
AIRTECH (1) DHC-3-1000 Otter
AIRTECH (1) DHC-3-PZL3S Otter
AIRTECH (1) Otter
DHC3
The de Havilland Canada DHC-3 Otter is a single-engined, high-wing, propeller-driven, Short Take-Off and Landing (STOL) aircraft developed by de Havilland Canada.
Technical Data
Wing span:
17.69 m
Length:
12.80 m
Height:
3.83 m
Powerplant:
1 x Pratt & Whitney R-1340-S1H1-G Wasp 9-cylinder air-cooled radial engine, 600 hp (448 kW).
Engine Model:
Pratt & Whitney R-1340
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
350 m
MTOW:
3600 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:
115 kts
MACH:
n/a
Ceiling:
185
Range:
840 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:
360 m
