Remos GX eLITE, Pilot Operating Handbook

Page: 80 / 200

G3-8 MA FM 1205 - R06
5 Performance
Performance 5 - 2
5.1 General
All flight performance data are given for ISA standard atmosphere at
sea level and standard temperature. To determine temperature in
relation to ISA conditions please refer to the following chart:
ISA std. Temperature
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
11000
12000
13000
14000
15000
-15 -10 -5 0 5 10 15
temperature [ °C ]
pre
s
s
ure
a
lt
it
ude
[
f
t
]
Flight performance can vary significantly due to tolerances, setting of
propeller and engine, flight without doors, deviation of temperature
and air density from standard ISA conditions, etc.
Range applies to the 22 gallon fuel tank system (21 gallons usable)
without reserve, within the ICAO standard atmosphere at given
altitude.