BELL 212 Twin Huey

Aircraft
Name: 
212 Twin Huey
Manufacturer: 
Wing: 
Rotary
WTC
L
Type Code: 
H1T
Engine: 
Turboshaft
Engine Count: 
Single
Manufacturered as
AGUSTA AB-212
BELL 212
BELL 212 Twin Two-Twelve
BELL Twin Two-Twelve
BELL UH-1N
BELL VH-1

B212

The Bell 212 Twin Huey (also known as the Twin Two-Twelve) is a two-blade, twin-engine, medium helicopter that first flew in 1968. The 212 is marketed to civilian operators and has a fifteen-seat configuration, with one pilot and fourteen passengers.Based on the stretched fuselage Bell 205, the Bell 212 was originally developed for the Canadian Forces.

Technical Data
Wing span: 
14.64 m
Length: 
17.43 m
Height: 
3.83 m
Powerplant: 

1 x Pratt & Whitney Canada PT6T-3 or -3B turboshaft, 1,800 shp (1,342 kW).

Engine Model: 
Pratt & Whitney Canada PT6T
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
5080 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: 
100 kts
MACH: 
n/a
Ceiling: 
174
Range: 
237 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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