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– 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.
LIMITATIONS
Power Plant
Vol. 1 02−05−9
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
9. 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
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 5 mg/L.
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 0.0227 g/l;
• Octel DCI−4A or DCI−6A, at a maximum concentration of 0.0227 g/l;
• Hitec E−515, at a maximum concentration of 0.0457 g/l;
• Hitec E−580, at a maximum concentration of 0.0227 g/l;
• Nalco 5403 or 5405, at a maximum concentration of 0.0227 g/l;
• Tolad 245, at a maximum concentration of 0.0340 g/l;
LIMITATIONS
Power Plant
Vol. 1 02−05−10
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
9. FUEL (CONT'D)
D. Fuel Jettison
Fuel jettison must only be carried out with flaps set to 0.
Jettisoning of fuel in known lightning conditions is prohibited.
E. 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 02−05−3:
• 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).
• Manual tail tank fuel transfer is not permitted with more than 3,175 kg (7,000 lb) of fuel in
auxiliary tank.
• Auxiliary tank quantity must be continuously monitored for overfill during manual tail tank
fuel transfer.
DFM0205_003
3
0.5
1.0
1.5
2.0
2.5
3.0
TAIL TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 LB
AUXILIARY TANK QUANTITY X 1000 KG
TAIL TANK QUANTITY X 1000 KG
0.25
7
6
5
4
3
1
0
0.50 0.75 1.0 1.25
2
0 1 2
AUXILIARY/TAIL TANK
FUEL QUANTITY MUST
REMAIN IN THIS ZONE
MANUAL TRANSFER
Manual Fuel Transfer − Auxiliary Tank Quantity vs Tail Tank Quantity
　
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