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DAR Solo UL

Product catalog summary

Overview: The document provides technical specifications for two ultralight aircraft models by AEROPLANES DAR Ltd.: the DAR Solo UL and the DAR Solo 120. Both models are designed using an aluminium/composite method and are equipped with Polini Thor engines.

DAR Solo UL Specifications:

Type Certificate: LTF UL
Engine: Polini Thor 250
Dimensions: Span 31 ft (9.45 m), Length 15.6 ft (4.76 m), Height 8 ft (2.47 m), Wing Area 105 ft² (9.765 m²), Cabin Width 2 ft (0.6 m)
Weight: Empty Weight (incl. BRS) 267 lb (120 kg), Max Take-off Weight 540 lb (245 kg)
Performance: Max Loading +4/-2 g, Fuel Tank Capacity 3.3 gal (15 l), Take-off Groundroll 459 ft (140 m), Rate of Climb 394 fpm (2.0 m/s), Cruising Speed 50 kts (90 km/h), Maximum Speed 57 kts (105 km/h), Stall Speed 27 kts (50 km/h), Stall Speed with Flaps 24 kts (45 km/h), Fuel Consumption 1.7 gal/h (6.5 l/h), Range 70 nm (130 km)

DAR Solo 120 Specifications:

Type Certificate: LTF-L
Engine: Polini Thor 200/250
Dimensions: Span 31 ft (9.45 m), Length 15.6 ft (4.76 m), Height 8 ft (2.47 m), Wing Area 105 ft² (9.765 m²), Cabin Width 2 ft (0.6 m)
Weight: Empty Weight (incl. BRS) 267 lb (120 kg), Max Take-off Weight 540 lb (245 kg)
Performance: Max Loading +4/-2 g, Fuel Tank Capacity 3.3 gal (15 l), Take-off Groundroll 459 ft (140 m), Rate of Climb 709 fpm (3.6 m/s), Cruising Speed 60 kts (110 km/h), Maximum Speed 70 kts (130 km/h), Stall Speed 27 kts (50 km/h), Fuel Consumption 1.69 gal/h (6.4 l/h), Range 70 nm (130 km)

Key Observations: Both aircraft models share similar dimensions and weight specifications, with slight variations in engine options and performance metrics such as rate of climb and cruising speed. The DAR Solo 120 offers a higher rate of climb and cruising speed compared to the DAR Solo UL.

Catalog excerpts

AEROPLANES DAR Ltd. www.aeroplanesdar.com DATA SHEET Type certificate: Design method: Engine: LTF UL Aluminium/Composite Polini Thor 250 Span Overall length Overall high Wing area Cabin width Empty weight (incl. BRS) Empty weight Max. take-off weight Max. loading Fuel tank capacity Take-off Groundroll Rate of climb Cruising speed Maximum speed Stall speed Stall speed flaps max Fuel consumption (cruise) Range

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AEROPLANES DAR Ltd. www.aeroplanesdar.com DATENBLATT DATA SHEET Musterzulassung / Type certificate: Bauweise / Design method: Motor / Engine Spannweite Lange Hohe Flugelflache Kabinenbreite Leermasse (inkl. Rettungssystem) Maximale Ablugmasse Hochstzulassige Belastung Tankinhalt Startrollstrecke Steigrate Reisegeschwindigkeit Hochstzulassige Geschwindigkeit Uberziehgeschwindigkeit Benzinverbrauch (im Reiseflug) Reichweite LTF-L Aluminium/Composite Polini Thor 200 / 250 Span Overall length Overall high Wing area Cabin width Empty weight (incl. BRS) Max. take-off weight Max. loading fuel tank capacity...

Open the catalog to page 2

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