Eurocopter AS 350 83 Flight Manual page 251

COMPLEMENTARY FLIGHT MANUAL
SECTION 7.5
FUEL SYSTEM
.1 FUEL TANK I
1.1 DescriPtion
The spin-molded polyamide fuel cell is located in the body structure
beneath the transmission deck. It is equipped with a gravity refueling
spout on the LH side of the aircraft, as well as a vent line and a water
bleed valve.
1.2 Caoacity
Fuel
.
Liters US gal. Imp.Gal. kg Remarks
Quantity
Total 540 143 119 Specific
gravity:
0.79
Usable after.
illumination 60 15.8 13.1
of low-level
light
Unusable 1.25 0.33 0.28
..079
CONVERSION TABLE
GAUGE READING -CAPACITY/WEIGHT
.Graduatio liters US Gal. Imp. Gal. kg lb
10 540 143 119 427 940
9 486 129 107 384 846
8 432 114 95 342 752
7 378 100 83 299 658
6 324 86 71 256 564
S 270 74 59 213 470
4 216 S7 48 171 376
3 162 43 36 128 282
2 108 29 24 8S 188
1 S4 14 12 43 94
0 0-3 0-0.8 0-0.6 0-2.3 0-5
I
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350 B3 7.5
97-40 Page 1