Ultra-Short Takeoff and Landing Aircraft SP-30

Ultra-Short Takeoff and Landing Aircraft SP-30

Brand: SP-30

$90,000 - $300,000 USD

MOQ: 1 units

Key Features

Maximum takeoff weight: 495 m² living area

Wingspan: 9.4 m

Maximum speed: 150

Length: 6.28 m

Supplier Information

First Design Bureau LLC

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Description

The SP-30 ultrashort takeoff and landing aircraft is a two-seat, very light aircraft, which is a sub-winged high-plane of the normal scheme with a tailplane and three-axis non-retractable landing gear with a steerable nose wheel.
The SP-30 ultrashort take-off and landing aircraft can be used for initial training in piloting techniques, and its additional equipment allows the aircraft to be used for aviation-chemical, patrol and forest protection operations in off-airfield conditions. The airframe is made of duralumin sheets of D16T alloy. Riveted construction with a working skin provides the specified strength and rigidity at low weight of the aircraft.
The main technical characteristics of the aircraft ultra-short takeoff and landing SP-30:
Length, m - 6.28; Height, m - 3.13; Wingspan, m - 9.4.
Engine type - four-stroke, four-cylinder engine with opposition arrangement of cylinders, power 73.5 kW (100 hp).
Maximum take-off weight, kg - 495.

Specifications

Maximum takeoff weight

495 m² living area

Wingspan

9.4 m

Maximum speed

150

Length

6.28 m

Height

3.13 m

Passenger capacity

1 кг U

Crew

1 кг U

Number of motors

1 µGy

Fuel tank capacity

60

Weight of the loaded airplane

0.345 thousand m² living area

Maximum landing weight

0.495 thousand m² living area

Maximum commercial load

0.15 thousand m² living area

Maximum payload

0.15 thousand m² living area

Range of flight with maximum fuel reserve (flight distance)

700 km

Range of flight with maximum load

350 km

Availability of a toilet, including one accessible to disabled passengers

no

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