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Neiva 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.

Universal
A T-25 Universal taxiing at São Sebastião do Paraíso
Role Basic trainer and ground attack aircraft
Manufacturer Neiva
First flight 29 April 1966
Primary users Brazilian Air Force
Chilean Air Force
Number built 189

Design and development

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.

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).

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.

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

Operators

 
Protopype of the YT-25A Universal II
  Bolivia
  Brazil
  Chile
  Paraguay

Specifications (Universal)

Data from Jane's All the World's Aircraft 1976–77[2]

General characteristics

  • Crew: 2–3
  • Length: 8.60 m (28 ft 3 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Height: 3.00 m (9 ft 10 in)
  • Wing area: 17.20 m2 (185.1 sq ft)
  • Aspect ratio: 7.1:1
  • Airfoil: NACA 632A315 at root, NACA 631212 at tip
  • Empty weight: 1,150 kg (2,535 lb)
  • Max takeoff weight: 1,700 kg (3,748 lb)
  • Fuel capacity: 332 L (88 US gal; 73 imp gal)
  • Powerplant: 1 × Lycoming IO-540-K1D5 six-cylinder horizontally-opposed air-cooled piston engine, 220 kW (300 hp)
  • Propellers: 2-bladed Hartzell HC-C2YK-4/C8475-A2 non-feathering constant speed propeller, 2.13 m (7 ft 0 in) diameter

Performance

  • Maximum speed: 300 km/h (190 mph, 160 kn) at sea level
  • Cruise speed: 285 km/h (177 mph, 154 kn) at sea level (max. cruise, 75% power)
  • Stall speed: 104 km/h (65 mph, 56 kn) (flaps down)
  • Never exceed speed: 500 km/h (310 mph, 270 kn)
  • Range: 1,500 km (930 mi, 810 nmi)
  • Service ceiling: 6,100 m (20,000 ft)
  • Rate of climb: 6.66 m/s (1,312 ft/min)
  • Takeoff run to 15 m (50 ft): 510 m (1,670 ft)
  • Landing run from 15 m (50 ft): 600 m (1,969 ft)

Armament

  • Guns: 7.62 mm machine gun pods on hardpoints
  • Hardpoints: 2

References

  1. ^ "All-Time Aircraft Used List Paraguayan Air Force – Aeroflight".
  2. ^ Taylor 1976, p. 16

External links

    neiva, universal, this, article, relies, largely, entirely, single, source, relevant, discussion, found, talk, page, please, help, improve, this, article, introducing, citations, additional, sources, find, sources, news, newspapers, books, scholar, jstor, marc. This article relies largely or entirely on a single source Relevant discussion may be found on the talk page Please help improve this article by introducing citations to additional sources Find sources Neiva Universal news newspapers books scholar JSTOR March 2019 The Neiva N621 Universal is a Brazilian propeller driven basic trainer and ground attack aircraft manufactured by Industria Aeronautica Neiva It is a cantilever low wing monoplane of all metal construction with retractable undercarriage and side by side seating UniversalA T 25 Universal taxiing at Sao Sebastiao do ParaisoRole Basic trainer and ground attack aircraftManufacturer NeivaFirst flight 29 April 1966Primary users Brazilian Air ForceChilean Air ForceNumber built 189 Contents 1 Design and development 2 Operators 3 Specifications Universal 4 References 5 External linksDesign and development EditThe 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 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 Forca Aerea Brasileira Brazilian Air Force Academy 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 In 2005 the Brazilian Air Force donated six T 25s to the Fuerza Aerea Paraguaya and another six to the Fuerza Aerea Boliviana Operators Edit Protopype of the YT 25A Universal II BoliviaBolivian Air Force BrazilBrazilian Air Force ChileChilean Air Force Chilean Army ParaguayParaguayan Air Force 1 Specifications Universal EditData from Jane s All the World s Aircraft 1976 77 2 General characteristicsCrew 2 3 Length 8 60 m 28 ft 3 in Wingspan 11 00 m 36 ft 1 in Height 3 00 m 9 ft 10 in Wing area 17 20 m2 185 1 sq ft Aspect ratio 7 1 1 Airfoil NACA 632A315 at root NACA 631212 at tip Empty weight 1 150 kg 2 535 lb Max takeoff weight 1 700 kg 3 748 lb Fuel capacity 332 L 88 US gal 73 imp gal Powerplant 1 Lycoming IO 540 K1D5 six cylinder horizontally opposed air cooled piston engine 220 kW 300 hp Propellers 2 bladed Hartzell HC C2YK 4 C8475 A2 non feathering constant speed propeller 2 13 m 7 ft 0 in diameterPerformance Maximum speed 300 km h 190 mph 160 kn at sea level Cruise speed 285 km h 177 mph 154 kn at sea level max cruise 75 power Stall speed 104 km h 65 mph 56 kn flaps down Never exceed speed 500 km h 310 mph 270 kn Range 1 500 km 930 mi 810 nmi Service ceiling 6 100 m 20 000 ft Rate of climb 6 66 m s 1 312 ft min Takeoff run to 15 m 50 ft 510 m 1 670 ft Landing run from 15 m 50 ft 600 m 1 969 ft Armament Guns 7 62 mm machine gun pods on hardpoints Hardpoints 2References Edit All Time Aircraft Used List Paraguayan Air Force Aeroflight Taylor 1976 p 16 Taylor John W R ed 1976 Jane s All the World s Aircraft 1976 77 London Jane s Yearbooks ISBN 0 354 00538 3 External links Edit Wikimedia Commons has media related to Neiva Universal Brazilian Air Force s website with the description of the type in Portuguese Retrieved from https en wikipedia org w index php title Neiva Universal amp oldid 1065053610, wikipedia, wiki, book, books, library,

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