General introduction of ISUZU FTR Aircraft Aviation Refueler Truck 10m3
After a long time entering the Cambodia market, Isuzu trucks have gradually proved their brand value and quality. On that basis, CS trucks trusts to choose Isuzu products to produce specialized models.
Key Features
5000 L– 20,000L capacity
All tanks are available in aluminum or stainless steel construction
Overwing and/or underwing fueling options
Available in both Monarch or Cardinal Tank Models
Numerous side and rear cabinet options to hold fueling equipment
Front, rear, or no canopy options
Betts LED lighting with vapor-proof wiring
Vast variety of refueling equipment options available
Key Features
----► Tank capacity 10.000 liters
----► Bottom loading by 4’’ API coupling.
----► Fuel distribution filtered and metered by distribution group driven by PTO.
----► Fueling flow rate: 1300 lpm by coupling, 270 lpm by nozzle.
----► Defueling (only by coupling).
Technical Specification
We also produce custom-built Isuzu Aircraft refueler trucks for customers having unique preferences for cab & chassis, tank capacity, and fueling system options. Our engineers are ready to design world class equipment exactly as you want it.
All of our refueler products and trucks, whether standard models or custom-built, comply with all latest edition industry guidelines,
The parameter of Isuzu FTR Aircraft fuel refueling truck 10000L
General specification:
A. Truck:
ISUZU FTR Aircraft Refueling tank truck |
||
Dimension |
9200*2500*3050mm |
|
Upper body inner dimension |
700x2300x16200 thickness: side 4mm, bottom 5mm |
|
Approaching angle/Departure angle |
26/19° |
|
Overhang(front/rear) |
1410/3076mm |
|
Wheel base |
4500mm |
|
Max speed |
90km/h |
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Curb weight |
8350kg |
|
Loading capacity |
10000kg |
|
Slope climbing capability |
Max.40% |
|
Engine |
Model |
ISUZU 4HK1,water-cooled,four strokes,4 cylinders in line,turbocharged, directly injection |
Displacement |
5.2L/Diesel |
|
Stroke |
126/130mm |
|
Max. power |
150/2200 (kw/rpm) |
|
Max.torque |
1350/1200-1600(Nm/rpm) |
|
Emission stantard |
EuroⅢ |
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Fuel tanker capacity |
400L |
|
Clutch |
Single dry frictional disc,Hydraulic boosting |
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Gearbox |
ISUZU MLD mechanism,6 forward gears,1 reverse gear, manual operated, |
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Gear ratio of gear box |
12.65/8.38/6.22/4.57/3.4/2.46/1.83/1.34/1.00 R:13.22 |
|
Suspension system |
Front |
Non-free standing leaf spring,telescopic shock absorber with stablizer bar suspension , 13pcs |
Rear |
Non-free standing stablization spring, balance suspension system, 13pcs |
|
Brake system |
Service brake |
Brake gap can be adjusted automatically, double circulation air brake system |
Assistant brake |
Engine exhaust brake |
|
Park brake |
Potential springs pressing on middle and rear wheels |
|
Steering system |
whole circulation in ball, hydraulic booster |
|
Frame |
Strengthened Streight beam |
|
Front axle (Mercedes Technology) |
Double-shoe pneumatic brake, non-driving steering axle |
|
Middle and Rear axle (Mercedes Technology) |
Double-shoe pneumatic brake, ductile casting casing, with hub redactor, double reduction driving axle |
|
Tyre |
12.00R24 Radial |
|
Electrical system |
Battery |
2X12V/135Ah |
Generator |
28V-35A |
|
Starter |
5.4Kw/24V |
|
Cabin |
Full steel skeleton structure, covered with double layer steel plate; With inner A/C |
Standard Configuration |
|
1. Working environmental |
Smooth road in the airport |
2. Temperature |
35℃~-40℃ |
3. Relative humidity |
<95% |
4. Altitude |
<4000 m |
5. Speed in the airport |
≤40km/h |
6. Speed on the road |
≤70km/h |
7. Main assembly |
Truck chassis, Oil tank, Operation cabin, Pipe system, Pneumatic control system, Hydraulic system, Electrical system |
8. Noise |
Meeting with the requirement of GJB4433, operation noise≤90dB(A) |
9. Reliability |
Meeting with the requirement of GJB4433, MTBF≥80h |
10. Maintaining |
Meeting with the requirement of GJB368B, MTTB≤30min |
11. Oil tank capacity |
23 000L |
12. Oil tank material |
Stainless steel 0Cr19Ni9 |
13. DN63 single pipe pressure refuel |
1200L/min |
14. DN38 single pipe gravity refuel |
≥300L/min |
15. DN38 double pipes gravity refuel |
≥600L/min |
16. Suck the oil from the pipe of oil tank |
≥300L/min(Single pipe)with measurement |
17. Self refuel ability |
≥2000L/min |
18. Connector closed pressure |
0.345Mpa±0.03Mpa |
19. Refuel accuracy |
0.2, instant, one time and total measurement |
20. Refuel from 0 to max flow rate time |
≤15s |
21. Filter performance |
stainless steel horizontal filter, filtering capacity ≥2000L/min, filtering accuracy 1 micro meter, filtering quality ≤0.26mg/L, non dissolved water ≤15ppm, the oil quality after filter meeting with the requirement o f GJB610 |
22. The oil exhausting capacity |
≤31L/Km |
23. Braking length under 30km/h |
≤9m |
24. Speed limited in the air port |
<40km/h |
25. Noise while acceleration |
≤89dB(A) |
26. Noise while operation |
≤90 dB(A) |
27. Min turning radius |
≤9.3m |
Pump | Brand | SANJIANG YOJE 80/60 Aluminium alloy pump |
Accessories | Fire extinguisher | 2 units (4kg/unit) |
Discharge hose | 2 units | |
Discharge hose housings | 2 units | |
Ladder | On the rear | |
Railing Material | Aluminum alloy | |
Fuel filling device | 20-meter hose reel and filling nozzle | |
Level instrument | Shanghai Leihang 50 |
Detail pictures of Isuzu aviation refueler truck
Operation side is left.
Dry connection for tank connection
Pump driven by PTO chassis:
Centrifugal pump GORMAN GR03.
All pipes in stainless steel alloy.
Strainer upstream pump.
Downstream pump:Pressure control valve.
Coalescer/Separator filter following API/IP 1581, last edition, fitting with waterdrain, automatic air eliminator and differential pressure gauge.
1 Volumetric meter SATAM ZC17-80/80 with 5 digit mechanical display with reset and 9 digit totalizer. One meter for 2 distribution lines.
Manual control valve
Electric handle with timer;
Underwing lineHose reel adapted for aviation fuel, with motorization.
1 aviation hose ND63 length 25 meters.
1 Underwing pressure fueling nozzle, strainer, vacuum breaker, 45psi hose end pressure controller and swivel.
Overwing lineHose reel adapted for aviation fuel, with motorization.
1 aviation hose ND38 length 30 meters.
1 Aircraft Overwing nozzle, with 100 mesh cone strainer, bonding cable and crocodile clamp.
Deadman system with override Defueling Capabilities by couplingInterlock system with sensors on:
Coupling and nozzle
Earthing clampPOSTE DE COMMANDE
Remote control
Start/Stop Engine
Engine throttle
PTO ON/OFF control
Engine emergency stop
Control Panel:Differential Pressure gauge
Pump Pressure gauge
Vacuum Pressure gauge
Jet Pressure gauge
Pneumatic circuit Pressure gauge
LabelingSchematic of distribution circuit
Labeling of each valve, gauge and test point
LightingWorking light
Control panel and filling connection lights
OTHER DEVICES
FILTER ELEMENTS:
2 sets of filter elements (1 for 1st use + 1 as spare),
JET A1 CONTROL
Gammon connector,
EQUIPOTENTIALITY:
Earthing/grounding strip, on all pipe connections & between frame, sub-frame and tank
Reel, hand operated, with 30 m grounding/bonding cable (steel, PVC coated) and brass crocodile clip.
Earthing/grounding clamps, located on both sides of the tank.
ACCESSOIRIES:
Tool box
Spare wheel on its support.
Set of tools
SECURITIES:
Automatic depressurization system, with back line to the tank,
Overfill prevention system in the tank,
BC9kg fire extinguisher in its support (1 on each side),
ABC2kg fire extinguisher in cab
All valves labeled,
ADR labeling
SPECIFIC FUNCTIONS
External suction: Connection before pump, DN80 valve and symmetrical connection.
Defueling : only by aircraft coupling.
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