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时间:2010-09-27 07:46来源:蓝天飞行翻译 作者:admin
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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 02−05−11
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
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
Vol. 1 02−05−12
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
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.
Fuel system icing inhibitors, Fluid I or Fluid I-M, should not be used continuously. Contact
engine manufacturer for details of impact on a reduced component inspection program.
(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
micro-organisms. A maintenance dose of 135 parts per million should be used thereafter.
Kathon FP 1.5 biocide additive at a concentration not in excess of 100 parts per million for
the initial dose to prevent the growth of micro-organisms. A maintenance dose of 50 parts
per million should be used thereafter.
(3) ANTI-STATIC
Stadis 450 anti-static additive at a concentration of 3 g/m3 for the initial dose. Maximum
dosage should not exceed 5 g/m3.
For Russian fuels, Sigbol static dissipater additive may be used in concentrations of less
than 0.0005% by weight.
(4) CORROSION INHIBITOR
Corrosion inhibitors listed below are approved, by the concentrations indicated, for
hydro-treated fuels only. It is recommended that corrosion inhibitors, conforming to
MIL−I−25017, be blended with the fuel to provide lubricity. The corrosion inhibitor must be
added after water removal and downstream of any clay filters (these processes remove
the inhibitor).
• Appollo PRI−19, at a maximum concentration of 23 g/m3;
• Octel DCI−4A, at a maximum concentration of 23 g/m3;
• Octel DCI−6A, at a maximum concentration of 9 g/m3;
• Hitec E−515, at a maximum concentration of 21 g/m3;
• Hitec E−580, at a maximum concentration of 23 g/m3;
• Nalco 5403, at a maximum concentration of 23 g/m3;
• Nalco 5405, at a maximum concentration of 11 g/m3;
• Tolad 245, at a maximum concentration of 34 g/m3;
LIMITATIONS
Power Plant
Vol. 1 02−05−13
REV 72, Jan 22/08
CL−604 Operating Manual
PSP 604−6
8. FUEL (CONT'D)
D. Fuel Transfer
Fuel transfer (left or right tank to auxiliary tank/gravity) must be off for take-off.
During normal operation, the tail tank transfer system must not be used as a centre of gravity
control device; it must remain selected to automatic mode.
During manual transfer operation – Refer to Figure 02−05−5:
• Auxiliary tank quantity must be at least 2.75 times the tail tank quantity, if tail tank quantity
is equal to or greater than 544 kg (1,200 lb).
• Auxiliary tank quantity must be at least 2.2 times the tail tank quantity, if tail tank quantity
is less than 544 kg (1,200 lb).
On airplanes incorporating Service Bulletin 604-28-007:
• Manual tail tank fuel transfer is not permitted with more than 3,175 kg (,7000 lb) of fuel
 
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