Neiva Regente

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Regente
Type	Utility transport and AOP
Manufacturer	Neiva
Maiden flight	1961
Primary user	Brazilian Air Force
Number built	122
Variants	none

Neiva Regente is a Brazilian prop-driven four-seat light utility aircraft manufactured by Indústria Aeronáutica Neiva.

Contents 1 History 2 Variants 3 Operators 4 Specifications (C-42) 5 References

[edit] History

The design was started in 1959 for a four-seat cabin monoplane aircraft with a high wing and fixed undercarriage. The prototype, designated the Neiva Regente 360C, was first flown on 7 September 1961 with a 145 hp (108 kW) Continental O-300 piston engine. The type was ordered into production by the Brazilian Air Force with a more powerful 180 hp (134 kW) Continental O-360 engine. Eighty aircraft were built originally designated the U-42 (later changed to C-42) for the utility role.

Neiva developed a three-seat Air Observation Post version for the Air Force, designated the Regente 420L. Its tailcone was lowered in order to improve visibility, and it used a more powerful Continental engine. The aircraft was first flown in January 1967 as the YL-42. Forty were built for the Brazilian Air Force as the L-42. It had provision to carry light bombs or rockets on underwing hardpoints.

Neiva also developed a four-seat civil version designated the Lanceiro. The prototype (Registered PP-ZAH) first flew in 1970, followed by production aircraft in 1973. The company's subsequent involvement with Embraer resulted in the Lanceiro program's being terminated.

[edit] Variants

• Regente 360C - utilty version (80 built)

• • U-42 - military designation of the Regente 360C

• • C-42 - military designation changed from U-42

• Regente 420L - Air Observation Post version (40 built)

• • L-42 - military designation of the Regente 420L

• Lanciero - civil version (2 built)

[edit] Operators

 Brazil

• Brazilian Air Force

[edit] Specifications (C-42)

Data from Jane's Aircraft Recognition Guide ^[1]

General characteristics

• Crew: 2: student, instructor
• Length: 23 ft 1 in (7 m)
• Wingspan: 29 ft 11 in (9.1 m)
• Height: 9 ft 7 in (2.9 m)
• Wing area: 144.78 ft² (13.45m²)
• Empty weight: 1,410 lb (640 kg)
• Max takeoff weight: 2,293 lb (1,040 kg)
• Powerplant: 1× Lycoming O-360-A1D six-cylinder piston engine, 180 hp (134 kW)

Performance

• Maximum speed: 137 mph (220 km/h)
• Range: 482 nm (896 km)

Armament

none fitted as standard

[edit] References

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