Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-10
Pilot’s Operating Manual
Revision A2: Nov, 2004
Sub-section 2
GROUND SERVICING
Hawker 800XP Pro Line 21
Section VI - GROUND OPERATIONS
FUEL SYSTEM
GENERAL
Fuel is stored in integral tanks in each wing and in a ventral tank beneath the rear fuselage, as shown
in Figure 5.
All tanks can be pressure refuelled and defueled, through a coupling which is accessible through a door
on the right side of the ventral tank rear fairing, or alternatively, all tanks can be gravity filled through a
filler neck in each tank.
Access to the ventral tank filler neck is through a door on the left side of the tank rear fairing.
FUEL CAPACITIES
Capacities quoted in Table 3 are achieved following gravity refueling.
NOTE: Contents indicators register usable fuel only.
Table 3 - Fuel Capacities
NOTES:
1. After pressure refueling, the contents of each wing tank will be 1.7 U.S. gallons less and
the contents of the ventral tank will be reduced by 2.5 U.S. gallons.
2. The contents is reduced by 3.3 U.S. gallons for airplanes which have an external toilet
servicing facility.
Tank
U.S. GAL
Total Usable
LITERS
Total Usable
Wing - Left 634 2400
Wing - Right 634 2400
TOTAL 1268 4800
If Ventral Tank Installed 233 882
TOTAL with Ventral Tank 1501 5682
Figure 5
Fuel Tanks and Compartments
CENTER SPAR