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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
Flight Crew Operating Manual REV 44, Jan 21, 2005
CSP 700−6
Volume 1
02−05−6
ACTION
Replace the Effectivity with the following:
E. Fuels and fuel Additives
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.
When using wide cut fuels, operation is limited to 30,000 feet until the bulk fuel temperature is
below 15 °C.
Use of CIS fuels is prohibited.
TEMPORARY REVISION BD 700/30-4
INSERT IN LIMITATIONS
FACING PAGE 02-05-7
Temporary revision de−activate the fuel scavenge system.
Aug 30, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
Page 2 of 2
REASON FOR ISSUE
3. FUEL (CONT'D)
C. Fuel Distribution
Fuel in the centre tank must be considered unusable unless each wing tank is full at
departure, and the planned cruise altitude is greater than 30,000 feet.
Fuel in the aft tank must be considered unusable unless each wing tank contains at least
2495 kg (5500 lb) fuel at departure, and the planned cruise altitude is greater than
30,000 feet.
If use of the centre / aft tank is planned, the tank fuel load is to be no less than 230 kg
(500 lb) to ensure xfer pumps reprime.
Effectivity:
· Airplanes 9002, 9004 thru 9082 not incorporating Service Bulletin:
· SB 700−28−033, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−5.
Fuel in the aft tank must be considered unusable unless each wing tank contains at least
1814 kg (4000 lb) fuel at departure, and the planned cruise altitude is greater than
30,000 feet.
D. Minimum Fuel Quantity for Goaround
The minimum fuel quantity for goaround
is 266 kg (600 lb) per wing (with wings level) and
assuming a maximum airplane climb attitude of 10° nose up.
E. Fuels and Fuel Additives
When using wide cut or CIS fuels, operation is limited to 13,000 feet until the bulk fuel
temperature is below 15 °C.
Effectivity:
· Airplanes 9002 thru 9114 not incorporating Service Bulletin:
· SB 700−28−029, Fuel Feed System − Scavenge System Installation to Reduce
Unusable Fuel Quantity.
When using wide cut fuels, operation is limited to 30,000 feet until the bulk fuel temperature
is below 15 °C.
Use of CIS fuels is prohibited.
Mixing of fuels is permitted.
Takeoff
with bulk fuel temperature indications outside the limits stated is prohibited.
LIMITATIONS
POWER PLANT
REV 47, Aug 30, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−05−7
3. FUEL (CONT'D)
E. Fuels and Fuel Additives (Cont’d)
Effectivity:
· Airplanes 9002, 9004 thru 9095, 9097 thru 9114 not incorporating Service Bulletin:
· SB 700−28−044, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−8.
or
· Airplanes 9003, 9096, 9115 thru 9132 not incorporating Service Bulletin:
· SB 700−28−045, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−9.
Takeoff
with bulk fuel temperature indications above 43 °C is prohibited.
During flight, bulk fuel temperature must remain above the applicable bulk fuel freezing point.
Fuels conforming to any of the following specifications are approved for use.
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