5 - 10 Page Date: 20. April 2002
Pilot´s Operating Handbook
EXTRA 200
Section 5
Performance
5.7 TIME, FUEL AND DISTANCE TO CLIMB
Example
Weight: 800 kg (1764 lbs)
Airfield pres. altitude: 1500 ft Cruise pres. altitude: 8000 ft
Airfield temperature: +20°c Outside air temperature +10°c
Climb time: 8,7-1,9= 6,8 min
Distance: 13 -2,8=10,2 NM
Fuel consumption: 8,3-1,9= 6,4 liters (1.6 US. Gal.)
Conditions:
No Wind, Speed for best climb
Power: Max. continuous power
Revolution: 2500 RPM
Mixture: below 8000 ft: rich
above 8000 ft: for best power
Outside air temperature (°c)
Distance(NM)
Density
altitude (ft)
Press. Altitude
Time (min)
0 (0.52) (1.05) (1.58) (2.11) (2.63) (3.16)
840 kg (1852 lbs)
T/O weight 700Kg (1543lbs)
Fuel in liter ((US Gal.)