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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.
TAIL TANK QUANTITY X 1000 KG
0.25 0.50 0.75 1.0 1.25
0123 TAIL TANK QUANTITY X 1000 LB
Manual Fuel Transfer . Auxiliary Tank Quantity vs Tail Tank Quantity
Figure 02.05.3
LIMITATIONS Power Plant Vol. 1 02.05.12
Oct 05/06
10. OIL GRADES
Refer to appropriate maintenance or servicing manual for approved oil grades.
11. OIL CONSUMPTION
Maximum oil consumption, on each engine, is 189 cubic centimeters per hour
(6.4 ounces per hour/0.05 US gallons per hour).
12. 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.
13. AUXILIARY POWER UNIT
A. Type
36–150 (CL)
B. Maximum RPM: 110%
The APU overspeed control will automatically shutdown the APU at 107% rpm.
C. Maximum EGT: 731°C
D. Starting:
(1)
Minimum ambient temperature for starting a cold soaked APU on the ground is –40°C.
(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:
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