Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-11
Pilot’s Operating Manual
Revision A2: Nov, 2004
Sub-section 2
GROUND SERVICING
Hawker 800XP Pro Line 21
Section VI - GROUND OPERATIONS
APPROVED FUEL SPECIFICATIONS
Aviation Kerosene to the current approved issue of specifications
• British .......................... DEF STAN 91-87 D.E.R.D. 2453
DEF STAN 91-91 D.E.R.D. 2494
• American ..................... ASTM D1655/JET A
ASTM D1655/JET A-1
MIL-T-83133/JP8
• Canadian ..................... CAN/CGSB 3.23/JET A
CAN/CGSB 3.23/JET A-1
• Russian ....................... GOST 10227-86 TS-1
GOST 10227-86 T-1
GOST 10227-86 RT
• Chinese ....................... GB 6537-94/No. 3 JET FUEL
Aviation Wide-Cut fuel to the current approved issue of the following specification
• British .......................... DEF STAN 91-88 D.E.R.D. 2454
• American ..................... ASTM D1655/JET B
MIL-T-5624 JP4
• Canadian ..................... CAN/CGSB 3.22/JET B
• Russian ....................... GOST 10227-86 T2
Fuel Additives (Anti-Static)
STADIS 450 additive may be used in concentrations not exceeding 3 parts per million (ppm) by
volume.
SIGBOL additive TU38-101741-78 may be used in concentrations not exceeding 0.0005% by volume.
FUEL LOADING (Figure 6)
Fuel tanks may be filled in any sequence provided that the appropriate refuel instructions are observed
and the following preflight fuel loading conditions are achieved.
NOTES:
1. Fuel contained in the wing tanks shall be equally disposed between the two wing tanks.
The maximum out of balance between wing tanks for flight is 500 lb (227 kg).
2. Fuel must not be carried in the ventral tank unless each main wing tank contains at least
3450 lb (1565 kg) of fuel.
3. Before flights on which it is to be utilized, the ventral tank must be filled completely. For other
flights it must be empty.