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Total 9,072 kg (20,000 lb)
To determine approximate maximum usable fuel load achieved by gravity refueling, reduce
weight by 7%.
Take-off with up to 230 kg (500 lb) of fuel in the auxiliary tank is permitted, provided that there is
at least 690 kg (1,500 lb) of fuel in each wing tank and no fuel in the tail tank.
Take-off with more than 230 kg (500 lb) of fuel in the auxiliary tank is permitted, provided that
there is at least 1,996 kg (4400 lb) of fuel in each wing tank.
The minimum fuel quantity for go-around is 230 kg (500 lb) per wing (with the airplane level) and
assuming a maximum airplane climb attitude of 10° nose up.
Normal AUX/TAIL Fuel Distribution for Take-Off:
• Auxiliary tank quantity must be full, or at least 2.65 times the tail tank quantity, for take-off (as
shown in Figure 02−05−2, Detail A, Normal Fuel Distribution for Take-Off).
OR
Provisional AUX/TAIL Fuel Distribution for Forward CG Limit Take-Off:
• Where the normal fuel distribution would cause the airplane centre of gravity to fall ahead of
the forward limit for take-off, the provisional fuel distribution may be applied to bring the
airplane centre of gravity within the permissible forward CG limit (as shown in
Figure 02−05−2, Detail B, Provisional Fuel Distribution for Take-Off). This fuel distribution is
permitted only if the resulting CG remains ahead of 34% MAC.
LIMITATIONS
Power Plant
Vol. 1 02−05−6
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
9. FUEL (CONT'D)
DFM0205_002
TAIL TANK QUANTITY X 1000 KG
0.25
8
7
6
5
4
3
2
1
0
0 0.5 1.0 1.5 2.0 2.5 3.0 3.5
0.50 0.75 1.0 1.25 1.5
0.5
1.0
1.5
2.0
2.5
3.0
3.5
TAIL TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 KG
AUXILIARY/TAIL TANK
FUEL QUANTITY MUST
REMAIN IN THIS ZONE
AUXILIARY TANK
MUST BE FULL
IN THIS ZONE
Detail A − Normal Fuel Distribution for Take-Off
TAIL TANK QUANTITY X 1000 KG
0.5
1.0
1.5
2.0
2.5
3.0
3.5
TAIL TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 KG
Detail B − Provisional Fuel Distribution for Take-Off
0.25
8
7
6
5
4
3
2
1
0
0 0.5 1.0 1.5 2.0 2.5 3.0 3.5
0.50 0.75 1.0 1.25 1.5
AUXILIARY/TAIL TANK
FUEL QUANTITY MUST
REMAIN IN THIS ZONE
LIMITATIONS
Power Plant
Vol. 1 02−05−7
Oct 05/06
Auxiliary Tank Quantity/Tail Tank Quantity – Relation Versus Centre of Gravity
Figure 02−05−2
CL−605 Flight Crew Operating Manual
PSP 605−6
9. FUEL (CONT'D)
A. Fuel Temperature
Take-off with engine fuel temperature indications below 5°C (41°F) is prohibited.
Take-off with bulk fuel temperature indications below the limits stated is prohibited.
During flight, bulk fuel temperature must remain above the applicable bulk fuel freezing point.
FUEL BULK FUEL TAKE-OFF
LIMIT
BULK FUEL FREEZING
POINT
ASTM D 1655 JET A –30°C –40°C
ASTM D 1655 JET A1 –37°C –47°C
ASTM D 6615 JET B –40°C –50°C
MIL–DTL–5624 JP 4 –48°C –58°C
MIL–DTL–5624 JP 5 –36°C –46°C
MIL–DTL–83133 JP 8 –40°C –50°C
GB 6537 No. 3 JET –37°C –47°C
Russian TS-1 –43°C [†]
Russian RT –40°C [†]
[†] Russian TS-1 and RT fuels with a freeze point of not higher than –50°C are
approved for use when the ground level OAT is not below –30°C during the 24
hours before departure.
TS-1 fuel with a freeze point of not higher than –60°C and RT fuel with a freeze
point of not higher than –55°C, for use in low temperature regions, are available at
the operator’s request.
LIMITATIONS
Power Plant
Vol. 1 02−05−8
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
9. FUEL (CONT'D)
B. Fuel Grades
• Fuels conforming to any of the following specifications are approved for use.
Mixing of fuels is permitted.
CANADIAN AMERICAN BRITISH CHINESE RUSSIAN
KEROSENE TYPE
CAN 2 - 3.23 ASTM D1655
JET A – – –
CAN 2 - 3.23 ASTM D1655
JET A1
DEF STAN
91–91 No. 3 JET TS-1 [††] or RT
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庞巴迪挑战者605机组操作手册 CL605-LIMITATIONS(7)
