Eurocopter AS 350 83 Flight Manual page 360

I11III ...COMPLEMENTARY FLIGHT MANU
CONDITIONS
-STABILIZED LEVEL FLIGHT WITH
.
ELECTRICAL CONSUMPTION ~ 50 A FUEL CONSUMPTION
ENDURANCE IN RECOMMENDED
CRUISE
(k~) (kgINM) (lblNM)
~60 1.6 3.5
0.8 ~\~ 'j 1.5
S I.~
~~ 1.4
3
Z~
0 0.7 iz.,O 1.3
~ 2.2.0
Q. 2.~O 1.2
!'.!, 0.6 240 1.1 2.5
.
II) 2.~0
~ 260 1
(.) 0.5 2
0.9
0.8
0.4
0.7 1.5
0.3 0.6
50 Q
40
30
0' 20 .7~
'"'
'"
I- 10 ~
<
0
0 .:.,
~p
-10
-20 I
-30
.--48
~ 5
w 4
(.)
Z 3
c(
0 ~
C! ::> 2
~ 0
~ Z 1
() w
~ 0
~ 70 80 90 100 110 120 130 140 150 ( kg/h )
~ ' I ' I .I ' .-' I ' I .I ' I ' I ' I ' I ' I .I ' I ' I ' I ' I ' I ' I ; 1-
~ 160 180 200 220 240 260 280 300 320 34.0 ( Ib/h )
w
HOURLY CONS.
.
EXAMPLE: OAT = 15.C TAS = 230 km/h =:> CONS./SPEED = 0.58 kg/km
=:> ENDURANCE = 2 h 30 min.
Hp = 6000 fI FUEL = 80 % =:> HOURLY CONS. = 133 kg/h
Figure 5 R
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