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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
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
02−05−4
ACTION
Replace the maximum useable fuel load table with the following:
Effectivity:
· Airplanes 9002 thru 9114 not incorporating Service Bulletin:
· SB 700−28−029, Fuel Feed System − Scavenge System Installation to Reduce Unusable
Fuel Quantity
· Airplanes incorporating Service Bulletin:
· SB 700−28−041, Fuel Feed System − De−Activation of the Fuel Scavenge System and
not incorporating SB 700−28−042, Fuel Feed System − Design Improvements to the Fuel
Scavenge System.
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 700/30-4
INSERT IN LIMITATIONS
FACING PAGE 02-05-5
Temporary revision de−activate the fuel scavenge system.
Aug 30, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
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
REV 44, Jan 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
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.
　
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