DE HAVILLAND CANADA DHC-2T

Aircraft
Name: 
DHC-2T
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
WTC
L
APC
B
Type Code: 
L1T
Engine: 
Turboprop
Engine Count: 
Single
Manufacturered as
DE HAVILLAND CANADA DHC-2 Mk3 Turbo Beaver
DE HAVILLAND CANADA Turbo Beaver

DH2T

A turbine-conversion of the DHC-2, the Turbo Beaver (DHC-2T) first flew in December 1963. This version featured a Pratt & Whitney PT6A6 turboprop, which offered lower empty and higher take-off weights, and even better Short Take-Off and Landing (STOL) performance. The Turbo Beaver's cabin was also longer, allowing maximum accommodation for 11, including the pilot. Externally, the Turbo Beaver had a much longer and re-profiled nose, and squared off vertical tail.

Technical Data
Wing span: 
14.63 m
Length: 
10.74 m
Height: 
3.35 m
Powerplant: 

1 x Pratt & Whitney PT6A6 turboprop.

Engine Model: 
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
n/a
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: 
122 kts
MACH: 
n/a
Ceiling: 
200
Range: 
580 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: 
n/a

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