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Neiva Universal

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Wingspan
  
11 m

First flight
  
April 29, 1966

Neiva Universal N621 UniversalNEIVA UNIV L1P L

Neiva t 25 c universal


The Neiva N621 Universal is a Brazilian propeller-driven basic trainer and ground attack aircraft manufactured by Indústria Aeronáutica Neiva. It is a cantilever, low-wing monoplane of all-metal construction, with retractable undercarriage and side-by-side seating.

Contents

Neiva Universal Neiva N621 Universal Wikipedia

Design and development

Neiva Universal Neiva N621 T25 Universal Specifications Technical Data

The Universal was designed in 1963 as a new primary trainer for the Brazilian Air Force, as a replacement for the T-6 Texan and Fokker S-11/S-12 types then in use. The prototype (Registration PP-ZTW) first flew on 29 April 1966. The Brazilian Air Force ordered 150 aircraft as the T-25 Universal, and increased this order in 1978 by an additional 28 aircraft. A further developed version (designated the YT-25B Universal II) first flew on 22 October 1978 but was not put into production.

Neiva Universal Images at War Thunder Communities Center

The Universal was also adopted as a counter-insurgency aircraft. It was later replaced by the Tucano in both the advanced training and attack roles, but it is still used as a primary and basic trainer at the Academia da Força Aérea Brasileira (Brazilian Air Force Academy).

Neiva Universal Images at War Thunder Communities Center

Ten aircraft were ordered by the Chilean Army. These aircraft were later transferred to the Chilean Air Force. In 1983 five FaCH T-25s were donated to the Paraguayan Air Force.

Neiva Universal httpsuploadwikimediaorgwikipediacommonsthu

In 2005, the Brazilian Air Force donated six T-25s to the Fuerza Aérea Paraguaya and another six to the Fuerza Aérea Boliviana.

Operators

 Bolivia
  • Bolivian Air Force
  •  Brazil
  • Brazilian Air Force
  •  Chile
  • Chilean Air Force
  • Chilean Army
  •  Paraguay
  • Paraguayan Air Force
  • Specifications (Universal)

    Data from Jane's Aircraft Recognition Guide

    General characteristics

  • Crew: 2: student, instructor
  • Length: 8.76 m (28 ft 9 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Height: 2.97 m (9 ft 9 in)
  • Wing area: 17.20 m² (185.15 ft²)
  • Empty weight: 1,150 kg (2,535 lb)
  • Max takeoff weight: 1,700 kg (3,747 lb)
  • Powerplant: 1× Lycoming O-540 six-cylinder horizontally-opposed air-cooled piston engine, 300 hp (224 kW)
  • Performance

  • Maximum speed: 277 km/h (172 mph, 150kt)
  • Range: 1,150 km (621 nm)
  • Armament

    two hardpoints; 7.62 mm machine gun pods; bombs; rockets

    References

    Neiva Universal Wikipedia