GROSS WEIGHT
2050 kg
( 4519 lb )
2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34
-1
0
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
RATE OF CLIMB - FEET/MINUTE X 100
PRESSURE ALTITUDE - FEET X 1000
2 4 6 8 10 12 14 16
RATE OF CLIMB - METERS/SECOND
0
5
10
15
20
25
30
35
40
45
50
55
60
PRESSURE ALTITUDE - METERS X 100
-30
-20
-10
0
10
20
OAT LIMIT
ISA+30
OAT - ˚C
▼
▼
RATE OF CLIMB ALL ENGINES
TAKE-OFF POWER
ROTOR: 100 %
HEATER ON
60 kts IAS
ELECTRICAL LOAD: 150 A TOTAL
TR 109-60-114/II REV C ABHD039C
Figure 4-5. Rate of climb - all engines - take-off power - 2050 kg.
RFM A109E
APPENDIX 6
R.A.I. Approved Page 13 of 18
Rev. 23
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