Hélicoptères Guimbal
CABRI G2
Determine maximum rate of climb as follows :
1. Locate A on the left curves from pressure altitude and outside air
temperature,
2. Report A on the right curves and find climb rate from reduced weight.
0 ft
5-8
Outside air temperature
5 000 ft
Pression altitude
- 20°C
OAT
Engine speed = 2650 RPM
Max. Continuous power
EASA Approved
PERFORMANCE
10 000 ft
ISA+30°C
SECTION 5
13 000 ft
Issue 05
Original issue
A
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