Aerotécnica: AC-14
Aerotecnica: AC-14

General data

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Names and dates
Market original model designation
AC-14
Market model designation (english translation or spelling)
AC-14
First flight date and time
1957-07-16
Country of manufacture
Spain
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
No translation available for: jet_air_on_tail
Weights
Maximum Takeoff Weight (MTOW)
1300
kg
Manufacturers empty weight (MEW)
700
kg
Cabin and cockpit
Maximum number of people onboard
5
External dimensions
Fuselage length
8.25
m
Total length (rotors turning)
11.22
m
Overal height
3.10
m
Main rotor
Main rotor diameter
9.60
m
Number of blades
4
Powerplant
Engine model
Turbomeca Artouste IIB
Engine type
Turboshaft
Number of engines
1
Total maximum power
400
HP
Fuel system
Fuel tank capacity
244
l
Performance
Maximum horizontal flight speed (Vh)
180
km/h
Cruise speed (Vc)
150
km/h
Best rate of climb
5
m/s
Maximum service ceiling
6350
m
Hover ceiling IGE
2700
m
Maximum range
260
km
0.0475