FMA IA 50 Guaraní II

Airplanes

Length

14.86 m

Flat Wing Span

19.53 m

Height

5.81 m

Flat Wing Area

41.81 m²

Flat Wing Aspect Ratio

Max Seating

Cruise Speed

450 km/h

Max Speed

500 km/h

Max Ceiling

12500 m

Number of Engines

Aircraft Engine

First Flight

1963-04-26

Entry Into service

1966-01-01

Number Built

Maximum Take-Off Weight

7.12 t (paragliders: kg)

Maximum Range

1995 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
FMA IA 50 Guaraní II	7.12	1995

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aircraft Industries L 410 NG		15.074	19.478	19	Compare
Henschel Hs 124		14.5	18.2		Compare
Tupolev ANT-35		15.4	20.8		Compare
LWS-6 Żubr	Bristol Pegasus	15.4	18.5		Compare
Indonesian Aerospace N219		16.49	19.5	19	Compare
Breda-Zappata BZ.309		14.75	20		Compare

All data (29 fields)

Name: FMA IA 50 Guaraní II
Manufacturer: Industrias Aeronáuticas y Mecánicas del Estado
Description: The I.A. 50 Guaraní II is an Argentine utility aircraft designed at the DINFIA (successor to the "Instituto Aerotecnico" - AeroTechnical Institute) in the early 1960s.
First Flight: 1963-04-26
Entry Into service: 1966-01-01
Service End: 2007-01-07
Designer: Industrias Aeronáuticas y Mecánicas del Estado
Type: Multi-purpose aircraft
Length (m): 14.86
Height (m): 5.81
Cockpit Crew: 2
Max Seating: 15
Max Speed (km/h): 500
Cruise Speed (km/h): 450
Min Speed (km/h): 145
Max Ceiling (m): 12500
Rate of Climb (m/s): 13.4112
Capacity Description: 15 passengers
National Origin: Argentina
Number Built: 3
Powerplant Description: 2 × Turbomeca Bastan VI-A turboprops, 694 kW (930 hp) each
Primary Users: Fuerza Aérea Argentina
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/FMA_IA_50_Guaran%C3%AD_II
Flat Wing Span (m): 19.53
Flat Wing Area (m²): 41.81
Flat Wing Aspect Ratio: 9
Aircraft Engine: Turbomeca Bastan
Number of Engines: 2