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to Figure 02−05−3, the take-off weight cannot exceed 21,319 kg (47,000 lb).
• Conversely, if the take-off weight is for example 20,366 kg (44,900 lb), then according to
Figure 02−05−3, there must be at least 1,247 kg (2,750 lb) of fuel in each wing tank.
On airplanes 5301, 5303 to 5639 NOT incorporating Service Bulletin 604–11–001:
Take-off with more than 230 kg (500 lb) of fuel in the auxiliary tank is permitted, provided that
the minimum quantity of fuel in each wing tank is as per Figure 02−05−4.
• For example, if there is at least 1,724 kg (3,800 lb) of fuel in each wing tank, then according
to Figure 02−05−4, the take-off weight cannot exceed 21,046 kg (46,400 lb).
• Conversely, if the take-off weight is for example 20,094 kg (44,300 lb), then according to
Figure 02−05−4, there must be at least 1,247 kg (2,750 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.
LIMITATIONS
Power Plant
02−05−8
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. FUEL (CONT'D)
DFM0205_007
LIMITATIONS
Power Plant
02−05−9
REV 71, Oct 31/07
Minimum Wing Tank Fuel Quantity for Take-Off
Figure 02−05−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. FUEL (CONT'D)
On airplanes 5301, 5303 to 5639 NOT incorporating Service Bulletin 604–11–001:
DFM0205_008
Minimum Wing Tank Fuel Quantity for Take-Off
(Airplanes 5301, 5303 to 5639 NOT incorporating Service Bulletin 604–11–001)
Figure 02−05−4
LIMITATIONS
Power Plant
02−05−10
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. 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 D1655 JET A –30°C –40°C
ASTM D1655 JET A1 –37°C –47°C
ASTM D6615 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 –37°C –47°C
GB 6537 No. 3 JET –37°C –47°C
Russian TS-1 –43°C [†]
Russian RT –40°C [†]
Ukrainian TS-1 –42°C –52°C
Ukrainian RT –42°C –52°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
02−05−11
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. 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/UKRAINIAN
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
– MIL–DTL–83133
JP 8 DEF STAN 91–87 – –
– MIL–DTL–5624
JP 5 DEF STAN 91–86 – –
WIDE CUT TYPE
CAN 2 - 3.22 ASTM D6615
JET B D. ENG. RD. 2486 – –
CAN 2 - 3.22 MIL–DTL–5624
JP 4 D. ENG. RD. 2454 – –
[††] When using TS-1 fuel, engine fuel system components must be inspected in
compliance with SB 604–73–003.
LIMITATIONS
Power Plant
02−05−12
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. FUEL (CONT'D)
C. Fuel Additives
The following additives, used individually or in combination, are approved:
(1) ANTI-ICING
　
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