Cylinder Head Temperature
(CHT)
60 °C,
140 °F
60-100 °C
140-212 °F
100-150 °C
212-302 °F
150 °C
302 °F
Oil Temperature
50 °C
122 °F
90-110 °C
194-230 °F
50-90 °C,
122-194 °F
110-140 °C,
230-284 °F
140 °C
284 °F
Oil Pressure
1.5 bar
1.5 - 4.0
bar
4.0 - 5.0 bar
7.0 bar
cold engine starting
Fuel Pressure
0.15 bar
0.2 – 0.3
bar
0.3 – 0.4 bar
0.4 bar
2.6
Miscellaneous instrument markings
•
Fuel gauge
A fuel reserve of 11 litres (
2.42 Imp. gals
) is indicated by yellow warning lamp.
2.7
Weight
Empty weight (standard equipment) max. 268
kg
591
lbs
NOTE
Actual empty weight is stated in SECTION 6, par. 6.2
Max. take-off weight 450kg
992
lbs
Max landing weight
450kg
992
lbs
Max. weight of fuel
47kg
104
lbs
Max. baggage weight 15kg
33
lbs
2.8
Centre of Gravity
Empty aircraft C.G. position (standard)
18±2% MAC = 200 – 250 mm AOD
Operating C.G. range
20-34% MAC = 250 – 425 mm AOD
Datum is wing leading edge.
POH/EUR/01
Issue 2
Page 12 of 42
Summary of Contents for EV-97 teamEUROSTAR UK
Page 1: ...EV 97 teamEUROSTAR UK...