Useful Documents

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Pilots' Notes

A reproduction of the original Rollason Condor Pilots' Notes. PDF copy

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Parts Manual

A copy of the original parts manual from Rollasons. PDF copy.

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Repair Manual

A copy of the original repair manual from Rollasons (90% complete). PDF copy

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OVERALL DIMENSIONS

Wing Span 27’ 6”

Length 22’ 10”

Height 7’ 9”

Wing Area 119.8 sq. feet

Wing Loading 12.28 lb/sq feet

WEIGHTS

Empty with oil 984 lbs

Max. All up weight 1475 lbs

Disposable load 491 lbs

POWER PLANT AND FUEL

Rolls-Royce Continental O-200A 100HP

Spark Plugs REM40E

Fuel 87 or 100 octane

Fuel Capacity 16 Imp Gallons

Oil 6 US Qts

Viscosity >40ºF W 80/15W-50/20W-50/20W-60

Viscosity <40ºF W 65/10W-30/15W-50/20W-50

Performance

SPEEDS

VNE (Never Exceed) 147 kts.

VNO (Normal Operating) 110 kts.

VFE (Flap Limiting) 70 kts.

VP (Max Manoeuvre) 105 kts.

Rough Air Speed 80 kts.

Stalling Speed 42 kts.

FAST CRUISE

BHP 100 hp

RPM 2750 rpm

Fuel Consumption 7.9 Imp Gal/hr

IAS approx 100 kts.

Range (30min diversion) 150 nm

NORMAL CRUISE

BHP 65 hp

RPM 2450 rpm

Fuel Consumption 5.0 Imp Gal/hr

IAS approx 80 kts.

Range (30min diversion) 220 nm

PERFORMANCE AT MAUW

Rate of Climb at 1475lbs 570 ft/min

Take Off to 50ft at 1475 580 yds

Landing over 50ft at 1475lbs 450 yds