26 m³
The aircraft refueller has been designed for airplanes refueling with filtered aviation fuel both pure and mixed with fuel system icing inhibitor agents. It is in full compliance with allowable loads on thoroughfare. It has a vehicle type approval and a certificate of conformity GOST 52 906-2008.
The aircraft refueller is used in airports of all the classes at air temperature from -400C to +400C and relative air humidity no more than 95%.
Full compliance with the weight loads on thoroughfare during transportation of fuel in 1 compartment which capacity is 22 m3. The maximum volume of fuel transported by aircraft refueller mounted on chassis inside the airport and refueling complex with fieled two compartments is 22 m3 and 4 m3.
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Tank capacity |
26 000 (±1,5%) liters |
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Note: permissible deviation of the curb weight is ± 3%. The lower limit of mass is not limited. |
|
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Internal surface area for stripping |
80 m2 |
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Gross weight at a density of 770 kg/m³: With a filled compartment of 22 m³ With filled compartments of 22 m³+4 m³ |
31 479 kg 34 518 kg |
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Distribution of mass on the road from aircraft refueller with full weight
With a filled compartment of 22 m³ – 1 axle – 2 axle – 3 axle – 4 axle |
8452 kg 7997 kg 7367 kg 7663 kg |
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With filled compartments of 22 m³+4 m³ – 1 axle – 2 axle – 3 axle – 4 axle |
8076 kg 8267 kg 8867 kg 9308 kg |
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Overall dimensions: – length – width – height |
12170 mm 2550 mm 3800 mm |
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Pump output flow at underwing refueling (at counteracting after bottom filling nozzle – 1,5 kgs/sm²), via one hose, max |
1200 l/min |
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Recommended pump output flow at overwing refueling |
400 l/min |
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Maximum allowable pressure in a bottom filling nozzle |
3,8 kg/sm2 |
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Nominal filtration rating, not more |
3 microns |
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Main consumption indicator error |
± 0,15 % |
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Dispensing hoses (number x length, m x diameter, mm)
|
1 х 30 х 63 1 х 30 х 38 |
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Non-drained fuel residue (full discharge through a drainage device) |
0 liters |
|
Test pressure on the bottom filling nozzle when testing hydraulic hoses for leaks |
10 kg/sm2 |
Tank capacity:
26 000 (±1,5%) liters
Internal surface area for stripping:
80 m2
Note: :
permissible deviation of the curb weight is ± 3%. The lower limit of mass is not limited.
Internal surface area for stripping:
80 m2
Gross weight at a density of 770 kg/m³ with a filled compartment of 22 m³:
31 479 kg
Gross weight at a density of 770 kg/m³ with filled compartments of 22 m³+4 m³:
34 518 kg
Distribution of mass on the road from aircraft refueller with full weight:
With a filled compartment of 22 m³
– 1 axle:
8452 kg
– 2 axle:
7997 kg
– 3 axle:
7367 kg
– 4 axle:
7663 kg
Distribution of mass on the road from aircraft refueller with full weight:
With filled compartments of 22 m³+4 m³
– 1 axle:
8076 kg
– 2 axle:
8267 kg
– 3 axle:
8867 kg
– 4 axle:
9308 kg
Overall dimensions:
of the aircraft refueller
– length:
12170 mm
– width:
2550 mm
– height:
3800 mm
Pump output flow at underwing refueling (at counteracting after bottom filling nozzle – 1,5 kgs/sm²), via one hose, max:
1 200 l/min
Recommended pump output flow at overwing refueling :
400 l/min
Maximum allowable pressure in a bottom filling nozzle:
3,8 kg/sm2
Nominal filtration rating, not more:
3 microns
Main consumption indicator error:
± 0,15 %
Dispensing hoses (number x length, m x diameter, mm):
1 х 30 х 63 and 1 х 30 х 38
Non-drained fuel residue (full discharge through a drainage device):
0 liters
Test pressure on the bottom filling nozzle when testing hydraulic hoses for leaks:
10 kg/sm2
