FMA I.A.50 Guarani II
1963
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FMA I.A.50 Guarani II

The Guarani I light transport first flew in prototype form on 6 February 1962 and utilised about 20% of the structural components of the IA.35 Huanquero. Power was provided by two 633kW Turbomeca Bastan IIIA turboprop engines. The Guarani II was developed from it and the prototype flew for the first time on 23 April 1963. It was placed in production for the Argentinian Air Force for communications, photographic (with the Military Geographic Institute) and executive transport duties, while the Navy received one as a staff transport. A total of 41 G.IIs were built.

FMA I.A.50 Guarani II


Specification 
 CREW1
 PASSENGERS10-15
 ENGINE2 x turbo-prop Turb. "Bastan IVA"
 WEIGHTS
    Take-off weight6500 kg14330 lb
    Empty weight4000 kg8819 lb
 DIMENSIONS
    Wingspan19.6 m64 ft 4 in
    Length15.3 m50 ft 2 in
    Height5.6 m18 ft 4 in
    Wing area41.8 m2449.93 sq ft
 PERFORMANCE
    Max. speed490 km/h304 mph
    Cruise speed485 km/h301 mph
    Ceiling3100 m10150 ft
    Range w/max.fuel2500 km1553 miles
    Range w/max.payload2000 km1243 miles

Comments
THEBATTLEMASTER, 13.12.2012

Another odd looking plane made by FMA.

marry, 18.06.2011

The IA50 GII makes regular commercial flights at Lineas Aereas Entre Rios (LAER)(Registration: LV-LAE and LV-LAI)

, 18.06.2011

with the Military Geographic Institute

Ariel G. San Martin, 29.09.2010

The IA50 GII makes regular commercial flights at Lineas Aereas Entre Rios (LAER)(Registration: LV-LAE and LV-LAI)

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