Arava 202

Arava 202
País	Israel
Papel	Aviones ligeros STOL Transport
Primer vuelo	27 de noviembre de 1969 4
Construido	103

El avión Arava 202 es un avión de transporte utilitario de despegue y aterrizaje corto (STOL) diseñado y fabricado por Israel Aerospace Industries (IAI).

Fuente: Arava 202 en Wiki

Arava 202 Walk Around
Fotógrafos	Isaac Gershman
Localización	Unknow
Fotos	51

Arava 202 01

Arava 202 02

Arava 202 03

Arava 202 04

Arava 202 05

Arava 202 06

Arava 202 07

Arava 202 08

Arava 202 09

Click on a photo and use the mouse scroll to view all photos

Espera, buscando fotos de Arava 202 para ti...

Cómprame un café

Ver también:

General Characteristics

The IAI Arava is a twin-engine, high-wing, short takeoff and landing (STOL) utility transport aircraft, and was Israel Aircraft Industries’ (IAI) first major indigenous aircraft design to enter production. The Arava 202 is an improved version, featuring a slightly longer fuselage and distinctive Whitcomb winglets for better aerodynamic efficiency.

Property	Typical Value (IAI-201/202 Variant)
Papel	STOL Utility / Military Transport
Fabricante	Israel Aircraft Industries (IAI)
First Flight (Arava Series)	November 27, 1969
Equipo	2 pilots
Capacity (Troops)	24 fully equipped troops or 16 paratroopers
Envergadura	20.96 m (68 ft 9 in)
Longitud	13.03 m (42 ft 9 in) (202 is slightly longer than 201)
Max Takeoff Weight	6,804 kg (15,000 lb)
Units Built (Total)	~103 (Production ended 1988)

Design and Powerplant

Engines: Two Pratt & Whitney Canada PT6A-34 turboprop engines (or PT6A-36 on the 202 prototype).
Power Output: 559 kW (750 shp) each.
Fuselage Design: Features a unique, short, barrel-like fuselage with a high wing and twin tail booms extending from the engine nacelles.
Loading Access: The entire rear section of the fuselage is hinged and swings open to the side, allowing for easy and rapid loading/unloading of bulky cargo or vehicles.
Landing Gear: Fixed tricycle landing gear, chosen to save weight and complexity, ideal for rough-field operations.
202 Specifics: The IAI-202 variant featured a longer fuselage, modified wings, and distinctive Whitcomb winglets at the wingtips for reduced drag.

Performance and Capability

Max Cruise Speed: 319 km/h (176 knots, 198 mph) at 3,050 m (10,000 ft).
Maximum Range: Approximately 1,056 km (570 nautical miles) with max fuel.
Payload Capacity: 2,351 kg (5,184 lb) of cargo.
STOL Takeoff Distance: Approximately 463 m (1,520 ft) to clear a 50 ft obstacle.
Service Ceiling: 7,620 m (25,000 ft).
Military Roles: Besides transport, military Aravas could be fitted with side-firing machine guns and rocket pods for counter-insurgency/gunship roles.

Vistas: 847