Rollason Condor Aircraft

Condor, RV Smith from British Built Aircraft

Production Details

Design Company:

Rollason Aircraft and Engines Ltd under licence from Druine

First Flight:

1961

D.62 Condor:

1 - Rollason Aircraft and Engines Ltd

D.62A Condor:

2 - Rollason Aircraft and Engines Ltd

D.62B Condor:

42 - Rollason Aircraft and Engines Ltd

D.62C Condor:

4 - Rollason Aircraft and Engines Ltd

Type Specification

Applies to:

Rollason D.62B Condor

Type:

Two seat light aircraft

Wing:

Low wing cantilever monplane

Fuselage:

Flat sided fuselage with faired top decking

Tail Unit:

Cantilever tailplane at base of single fin and rudder

Landing Gear:

Fixed undercarriage attached to wing. Tailskid

Power Plant:

One 100 hp Continental O-200-A piston engine in the nose driving a two bladed propeller

Accommodation:

Side by side seats for two in enclosed cockpit above the wing

Span:

27 ft 6 in

Length:

22 ft 10 in

Height:

5 ft 9 in

Wing Area:

119.8 sq ft

Tare:

900 lb

All-up:

1,475 lb

Max Cruise:

110 kt

Rate of Climb:

570 ft/min

Range:

385 miles

Preserved in British Museums

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