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

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