Overview
The Sikorsky Schweizer S-434 was developed as a turbine-powered evolution of the 300 series. Intended to combine the familiar handling of the piston trainer with turbine reliability, it targeted both training and light utility markets. The aircraft represented an effort to modernize a legacy design.
Specifications
Units
- Engine
- 2 × Rolls-Royce Turbine 250-C20W
- Engine type
- Turbine
- Thrust
- 2 × 320 lbf · 1 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 4
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 31 ft 2 in · 9.51 m
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- 27 ft 6 in · 8.39 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 2,900 lb · 1,300 kg
- Max landing weight
- —
- Max payload
- 1,200 lb · 550 kg
- Fuel capacity
- 80 gal · 300 L · 300 kg (Jet A)
- Max cruise speed
- 105 kt · 121 mph · 194 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 350 nm · 400 mi · 650 km
- Fuel burn
- 4.17 nm/gal · 2.04 km/L
- Ceiling
- 12,500 ft · 3,800 m
- Rate of climb
- —
- Takeoff distance
- —
- Landing distance
- —
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