SNCASO: SO 1310 Farfadet

General data

Producer info

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Names and dates
Market original model designation
SO 1310
Market model designation (english translation or spelling)
SO 1310
Original model name
Farfadet
Model name (english translation or spelling)
Farfadet
First flight date and time
1953-05-08
(...)
1953-05
Country of manufacture
France
Config info
Rotorcraft typeCompound helicopter
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
1510
kg
(...)
1510
kg
Manufacturers empty weight (MEW)
995
kg
Cabin and cockpit
Maximum number of people onboard
3
External dimensions
Length
10.08
m
Height
3.33
m
Wing span
6.30
m
(...)
6.22
m
5.79
m
Landing gear type
Wheeled
Wheeled landing gear type
Main wheels in the back
Landing gear support points
3
Main rotor
Drive type
Tip jets
Main rotor diameter
11.19
m
(...)
11.80
m
11.13
m
Main rotor direction of rotation
Counterclockwise
Number of blades
3
Propeller
Mode
Pulling
Propeller direction of rotation
Clockwise
Propeller pitch mode
No translation available for: propeller_adj_in_flight
Number of blades
2
Powerplant
Engine model (System no.: 1)
Turboméca Artouste II
Engine model (english translation or spelling) (System no.: 1)
Turbomeca Artouste I
Engine model (System no.: 2)
Turboméca Arrius II
Engine model (english translation or spelling) (System no.: 2)
Turbomeca Arrius II
Number of engines
2
Total maximum power
720
HP
Performance
Cruise speed (Vc) (option 1)
249
km/h
(...)
241
km/h
Cruise speed (Vc) (option 2)
154
km/h
Maximum range
401
km
(...)
402
km
0.0461