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ÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈÈ
AUXILIARY TANK QUANTITY X 1000 LB
0
TAIL TANK QUANTITY X 1000 LB
1
0
3
2
5
4
6
7
TAIL TANK QUANTITY X 1000 KG
AUXILIARY TANK QUANTITY X 1000 KG
0.25 0.50 0.75 1.0 1.25
0.5
1.0
1.5
2.0
2.5
3.0
ÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇ
AUXILIARY / TAIL TANK
FUEL QUANTITY MUST
REMAIN IN THIS ZONE
8
3.5
8
3.5
1.5
0.5 1.5 2.5 3.5
0.5 1.0 1.5 2.0 2.5 3.0 3.5
1.5
Detail B – Provisional Fuel Distribution for Take-Off
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
AUXILIARY TANK
MUST BE FULL
IN THIS ZONE
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 53, Jun 04/04
LIMITATIONS
Power Plant
02−05−8
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 −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.
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
− 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 Russian TS-1 fuel, engine fuel system components must be
inspected in compliance with SB 604-73−003.
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 63, Sep 11/06
LIMITATIONS
Power Plant
02−05−9
8. FUEL (CONT’D)
C. Fuel Additives
The following additives, used individually or in combination, are approved:
(1) Anti-icing
Anti-icing additives to the latest revision of specifications MIL-I-27686E or
MIL−DTL−85470B or any direct equivalent, at a concentration of 0.10 to 0.15% by
volume.
CAUTION
Do not add unblended PRIST additive directly into the
fuel tank, as this may damage fuel tank components.
Anti-icing Methyl Cellosolve at concentrations of 0.10 to 0.15% by volume.
Anti-icing additives for Russian fuels:
 Ethylene glycol monoethyl ether (liquid I),
 1:1 mixture of ethylene glycol monoethyl ether with methyl alcohol (liquid I-M),
 Tetrahydrofurfuryl alcohol (TGF),
 1:1 mixture of tetrahydrofurfuryl alcohol (TGF) with methyl alcohol (liquid TGF-M).
(2) Biocide
SOHIO Biobor JF biocide additive at a concentration not in excess of 270 parts per million
(20 parts per million elemental boron) for the initial dose to prevent the growth of
　
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