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AUXILIARY TANK QUANTITY X 1000 LB
0
TAIL TANK QUANTITY X 1000 LB
1
0
3
2
1 2
Manual Fuel Transfer - Auxiliary Tank Quantity vs Tail Tank Quantity
Figure 02–05–3
3
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
ÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇ
AUXILIARY / TAIL TANK
MANUAL TRANSFER
FUEL QUANTITY MUST
REMAIN IN THIS ZONE
On airplanes incorporating Canadair Service Bulletin 604-28-007:
Manual tail tank fuel transfer is not permitted with more than 3175 kg (7000 lb) of fuel
in auxiliary tank.
Auxiliary tank quantity must be continuously monitored for overfill during manual tail
tank fuel transfer.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 45, Mar 13/02
LIMITATIONS
Power Plant
02−05−11
8. FUEL (CONT’D)
E. Fuel Jettison
Fuel jettison must only be carried out with flaps set to 0.
Jettisioning 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 1890 cubic centilitres (2 US quarts) without dry motoring the engine.
12. AUXILIARY POWER UNIT
A. Type:
36-150(CL)
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
GTCP-36-100(E)
B. Maximum RPM: 110%
The APU overspeed control will automatically shutdown the APU at 107% rpm.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
The APU overspeed control will automatically shutdown the APU at 110% rpm.
C. Maximum EGT: 731 C
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Power Plant
02−05−12
12. AUXILIARY POWER UNIT (CONT’D)
D. Starting:
(1) Minimum ambient temperature for starting a cold soaked APU on the ground is −40C.
(2) The following APU start cycles are permitted:
(a) Using airplane batteries on the ground or for normal in-flight start:
Three start attempts, each of 30 seconds continuous cranking
Followed by a 20-minute off-time
Followed by two further attempts each of 30 seconds continuous cranking.
(b) Using ground power:
Two start attempts each of 15 seconds continuous cranking
Followed by a 20-minute off-time
Followed by two further attempts each of 15 seconds continuous cranking.
(c) If, in either case (2)(a) or (2)(b) a successful start is not obtained, a further start
must not be attempted for a period of at least 35 minutes.
(3) Maximum EGT:
974 C (not to be exceeded under any operating conditions)
(4) Hung start:
Greater than 30% rpm within 60 seconds
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