Hélicoptères Guimbal
CABRI G2
Rate of climb at Vy = 50 kt IAS
To determine the maximum rate of climb, first determine the reduced weight
as follows :
1. Locate A on the left curves from outside temperature and pressure
altitude,
2. Report A on the right curves and read the reduced weight from weight.
Note : The example is given for M = 700 kg, OAT = 20°C and Zp = 4000 ft.
Pressure altitude
-20°C
-10°C
5-6
0°C
10°C
Outside air temperature
- 20°C
OAT
EASA Approved
PERFORMANCE
20°C
30°C
ISA+30°C
Original issue
SECTION 5
A
40°C
Issue 09.3
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