Eurocopter AS 350 83 Flight Manual page 150

FLIGHT ~'lNUAL
CONDITIONS
-ALL UP WEIGHT LIMITATION WITH INTERNAL CORRECTED WEIGHT
LOADS: 2250 kg ( 4961 Ib) FOR DETERMINING
THE Vz VALUES
.
(using the graph opposite)
32 34 (lbx100)
36
38
40
42
44
~6
~8
49.6
52
.
54
56
57.3
60
61.7
.
I
0
0
.;
'"
on
0
g
>
~
-~O -30 -20 -10 0 10 20 30 ~O 2000 2500 3000 3500
OAT rC) CORRECTED WEIGHT (kg)
EXAMPLE: OAT = 1SoC ACTUAL WEIGHT = 2000 kg
Hp = 8000 ft =:> CORRECTED WEIGHT = 2700 kg
.
Figure 4
DGAC Approved: 3SD 83 SU P. 14
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