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The maximum usable fuel load for each fuel tank is given below:
PRESSURE REFUEL (+0 / -1%)
TANK VOLUME FUEL MASS †
Left main tank 8,415 litres 2,223 USG 6,800 kg 15,000 lb
Right main tank 8,415 litres 2,223 USG 6,800 kg 15,000 lb
Centre tank 6,230 litres 1,645 USG 5,050 kg 11,100 lb
Aft tank 1,275 litres 337 USG 1,025 kg 2,300 lb
Total 24,335 litres 6,428 USG 19,675 kg 43,400 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg or
50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
GRAVITY REFUEL (AIRPLANE LEVEL)
TANK VOLUME FUEL MASS †
Left main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Right main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Centre tank 6,210 litres 1,640 USG 5,025 kg 11,050 lb
Aft tank not available not available not available not available
Total 21,730 litres 5,740 USG 17,575 kg 38,750 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg or
50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is not usable.
TEMPORARY REVISION BD 700/32-6
INSERT IN LIMITATIONS
FACING PAGE 02-05-5
Temporary revision de−activate the fuel scavenge system.
DOT Approved
Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
Page 1 of 2
REASON FOR ISSUE
3. FUEL (CONT'D)
B. Usable Fuel Load (Cont’d)
Effectivity:
• Airplanes 9002 thru 9114 not incorporating Service Bulletin:
• SB 700−28−029, Fuel Feed System − Scavenge System Installation to Reduce
Unusable Fuel Quantity.
The maximum usable fuel load for each fuel tank is given below:
PRESSURE REFUEL (+0 / -1%)
TANK VOLUME FUEL MASS †
Left main tank 8,415 litres 2,223 USG 6,800 kg 15,000 lb
Right main tank 8,415 litres 2,223 USG 6,800 kg 15,000 lb
Centre tank 6,230 litres 1,645 USG 5,050 kg 11,100 lb
Aft tank 1,275 litres 337 USG 1,025 kg 2,300 lb
Total 24,335 litres 6,428 USG 19,675 kg 43,400 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg
or 50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
GRAVITY REFUEL (AIRPLANE LEVEL)
TANK VOLUME FUEL MASS †
Left main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Right main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Centre tank 6,210 litres 1,640 USG 5,025 kg 11,050 lb
Aft tank not available not available not available not available
Total 21,730 litres 5,740 USG 17,575 kg 38,750 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg
or 50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is not
usable.
LIMITATIONS
POWER PLANT
DOT Approved
REV 44, Jan 21, 2005
Airplane Flight Manual
CSP 700−1A
02−05−5
3. FUEL (CONT'D)
B. Usable Fuel Load (Cont’d)
On airplanes 9159 and subsequent:
The maximum usable fuel load for each fuel tank is given below:
PRESSURE REFUEL (+0 / -1%)
TANK VOLUME FUEL MASS †
Left main tank 8,435 litres 2,229 USG 6,825 kg 15,050 lb
Right main tank 8,435 litres 2,229 USG 6,825 kg 15,050 lb
Centre tank 7,111 litres 1,879 USG 5,750 kg 12,700 lb
Aft tank 1,275 litres 337 USG 1,025 kg 2,300 lb
Total 25,256 litres 6,674 USG 20,425 kg 45,100 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg
or 50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
GRAVITY REFUEL (AIRPLANE LEVEL)
TANK VOLUME FUEL MASS †
Left main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Right main tank 7,760 litres 2,050 USG 6,275 kg 13,850 lb
Centre tank 6,245 litres 1,650 USG 5,050 kg 11,150 lb
Aft tank not available not available not available not available
Total 21,765 litres 5,750 USG 17,600 kg 38,850 lb
† based on a fuel density of 0.809 kg / litre (6.75 lb / USG), rounded to the nearest 25 Kg
or 50 lb. Fuel Mass is provided for reference only and should not be considered limiting.
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is not
usable.
NOTE
The center tank fuel quantity includes the forward fuel tank
capacity. Gravity refueling is unavailable for the forward fuel tank.
LIMITATIONS
POWER PLANT
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Bombardier LIMITATIONS(6)
