Eurocopter AS 350 83 Flight Manual page 361

."
COMPLEMENTARY FLIGHT MANUAL
CONDITIONS
-STABiliZED lEVEL FLIGHT WITH
.
-ELECTRICAL CONSUMPTION ~ 50 A RANGE IN RECOMMENDED
-CRUISE
2200
( Ib )
4500
2000
CI
~ 0
-N
1800 0' 4000
I-
.
:I: at 0
0 -~
~ 1600 g ~ 3500
u. 0
~ r J ~
1400 I I
0 0
2
0 1 -
0 .0
0 ~ 0
~ 0
x ~
-6 x
:. 2 E
Co 8 Co
:I: :I:
10 3
12
ISA -20 WEIGHT
.-~~UU Kg
2000 kg
.
---1800 kg
ISA -10
STD-ISA 0
0 -tttfJI-
~ ISA +10
Q
w
~
Q
m
..
=
.; ISA +20
~ 0 100 200 300 400 500 600 700 800 900 1000 (km)
~ I' , , , I ' , , , I ' , , , I ' , , , I ' , , .I ' , ., I' , ., I ..., I' ...I' , , , I ' , .
~ 0 100 200 300 400 500 (NM)
RANGE
.
~: OAT = OoC WEIGHT = 2100 kg FUEL = 85 % -
Hp = 7500 ft ~ RANGE = 700 km
F
' N
Igure 6
~ 350 83 10.1
1111._- 98-46 Page 8