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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
02−05−13
REV 72, Jan 22/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
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
Figure 02−05−5
LIMITATIONS
Power Plant
02−05−14
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. FUEL (CONT'D)
E. Fuel Jettison
Fuel jettison must only be carried out with flaps set to 0.
Jettisoning of fuel in known lightning conditions is prohibited.
9. OIL GRADES
Refer to appropriate maintenance or servicing manual for approved oil grades.
10. OIL CONSUMPTION
Maximum oil consumption, on each engine, is 189 cubic centimeter per hour
(6.4 ounces per hour/0.05 US gallons per hour).
11. OIL REPLENISHMENT SYSTEM
The engine oil level should be checked between 15 minutes to 2 hours after engine shutdown.
The engines must be motored if the replenishment period is exceeded. Maximum refill allowable
is 1,890 cubic centilitres (2 US quarts) without dry motoring the engine.
12. AUXILIARY POWER UNIT
　
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