ALOUETTE GROUP
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ALO GROUP

Aircraft

First Flight : February 28, 1959 (SA-316), 1967 (SA-319) Type : multi-purpose light helicopter Engine : 1 turbine Turbomeca Artouste IIIB of 880 CV (SA-316) 1 turbine Turbomeca Astazou XIV of 870 CV (SA-319) Capacity : 1 pilot + 6 passengers Production : about 1455 + ?? under licence Country users : more than 75 Dimensions Fuselage lenght : 10,03 m Lenght overall : 12,84 m Height : 3,09 m Main rotor diameter : 11,00m Empty weight : 1090 kg (SA-316) 1108 kg (SA-319) Max. weight : 2200 kg (SA-316) 2250 kg (SA-319) Performances Maximum speed : 210 km/h (SA-316) 220 km/h (SA-319) Service ceiling : 4250 m Range : 500 km (SA-316) 600 km (SA-319)

ALOUETTE III

First Flight : 12 March 1955 Type : multi-pupose light helicopter Engine : 1 turbine Turboméca Artouste IIC of 360 CV Capacity : 1 pilot + 4 passengers Production : about 1300 + ?? under licence (India?) Country users : more than 80 (47 armed forces) Dimensions Fuselage lenght : 9,70 m Lenght overall : 12,05 m Height : 2,75 m Main rotor diameter : 10,20 m Empty weight : 890 kg Max. weight : 1500 kg Performances Maximum speed : 185 km/h Service ceiling : 2250 m Range : 565 km

ALOUETTE II

AM-3CM Bosbok Stats:
Powerplant: 1 x 340 hp Piaggio-Lycoming GSO-480-B1B6
Speed: 260 kph, 161mph
Range: 990km, 615 miles
Seats: 1+1 or 1 + 2
Length: 8.73m, 28ft 8in
Span: 11.73m, 6ft 6in
Empty Weight: 1 080kg, 2,380lb
Max T/O Weight: 1 700kg, 3,750lb
Period of Service in the SAAF: 1973 - 1992

ZU-ALO

ZU-RAM

ZU-BMF

ZU-RAR

ZU-REC

ZU-ACP

ALO GROUP ALOUETTE GROUP

Aircraft

First Flight : February 28, 1959 (SA-316), 1967 (SA-319) Type : multi-purpose light helicopter Engine : 1 turbine Turbomeca Artouste IIIB of 880 CV (SA-316) 1 turbine Turbomeca Astazou XIV of 870 CV (SA-319) Capacity : 1 pilot + 6 passengers Production : about 1455 + ?? under licence Country users : more than 75 Dimensions Fuselage lenght : 10,03 m Lenght overall : 12,84 m Height : 3,09 m Main rotor diameter : 11,00m Empty weight : 1090 kg (SA-316) 1108 kg (SA-319) Max. weight : 2200 kg (SA-316) 2250 kg (SA-319) Performances Maximum speed : 210 km/h (SA-316) 220 km/h (SA-319) Service ceiling : 4250 m Range : 500 km (SA-316) 600 km (SA-319)

ALOUETTE III

First Flight : 12 March 1955 Type : multi-pupose light helicopter Engine : 1 turbine Turboméca Artouste IIC of 360 CV Capacity : 1 pilot + 4 passengers Production : about 1300 + ?? under licence (India?) Country users : more than 80 (47 armed forces) Dimensions Fuselage lenght : 9,70 m Lenght overall : 12,05 m Height : 2,75 m Main rotor diameter : 10,20 m Empty weight : 890 kg Max. weight : 1500 kg Performances Maximum speed : 185 km/h Service ceiling : 2250 m Range : 565 km

ALOUETTE II

Powerplant: 1 x 340 hp Piaggio-Lycoming GSO-480-B1B6
Speed: 260 kph, 161mph
Range: 990km, 615 miles
Seats: 1+1 or 1 + 2
Length: 8.73m, 28ft 8in
Span: 11.73m, 6ft 6in
Empty Weight: 1 080kg, 2,380lb
Max T/O Weight: 1 700kg, 3,750lb
Period of Service in the SAAF: 1973 - 1992

Aermacchi AM-3C