SINOTRUK HOWO 20,000-Liter Aviation Refueling Truck
The SINOTRUK HOWO 20m³ Aviation Refueling Truck is a high-capacity ground support vehicle designed specifically for safe and efficient aircraft fueling operations. With a 20,000-liter (5,283-gallon) tank capacity, this unit is ideally suited for busy international airports, regional airfields, military bases, and FBO facilities that require reliable, high-volume fuel delivery to commercial airliners, private jets, and cargo aircraft.
Built on a proven SINOTRUK HOWO heavy-duty chassis, this refueler combines robust construction with specialized aviation fueling equipment. It is engineered to handle Type 3 hazardous materials (aviation kerosene) and complies with international pressure vessel standards, ensuring both operational safety and regulatory compliance. The vehicle's dimensions and maneuverability are carefully optimized for crowded airport ramp environments, while its payload capacity allows for extended operations without frequent returns to the fuel farm.
Whether you need to minimize aircraft turnaround time, maintain strict fuel quality standards, or ensure maximum safety during ground operations, this aviation refueling truck delivers professional-grade performance tailored to the unique demands of the aviation industry.
Tank Construction & Material Quality
The fuel tank is the most critical component of any aircraft refueler, and this model features construction from 5182 aluminum alloy, the industry standard for aviation fuel handling. Unlike carbon steel tanks that can rust and contaminate fuel, aluminum alloy is naturally corrosion-resistant and chemically inert when in contact with Jet A fuel.
Tank Design
- Elliptical cross-section design lowers the vehicle's center of gravity, improving stability during cornering and transport
- Internal baffles control fuel surge during acceleration, braking, and turns
- Welded construction meets pressure vessel requirements for hazardous materials
Material Thickness
- Shell Plating: 5.6 mm
- Head Plating: 5.8 mm
- Internal Baffles: 5.7 mm
This robust construction ensures long-term durability while the lightweight aluminum material helps maximize payload capacity by reducing the empty vehicle weight.
Fuel Delivery System
Efficiency in aircraft fueling is measured by flow rate, and this refueler delivers exceptional performance through its PTO-driven hydraulic system powering self-priming centrifugal pumps.
Primary Refueling System
- Hose Reel: DN65 hydraulic-driven reel
- Hose Length: 20 meters of aviation-grade hose
- Couplings: Dual aviation pressure-refueling adapters
- Flow Rate: ≥1,200 liters per minute
- Application: High-speed underwing fueling of wide-body aircraft
Secondary Refueling System
- Hose Reel: DN38 hydraulic-driven reel
- Flow Rate: ≥350 liters per minute
- Application: Smaller aircraft fueling or defueling operations
The dual-system design provides operational flexibility, allowing ground crews to handle different aircraft types with a single vehicle while maintaining optimal flow rates for each application.
Filtration & Fuel Quality Control
Maintaining absolute fuel purity is non-negotiable in aviation operations. This refueler incorporates a high-capacity coalescer/separator filtration system that removes both free water and solid particulates from the fuel stream before delivery to the aircraft.
Filtration Specifications
- Filter Type: Coalescer/Separator vessel
- Flow Capacity: 2,500 liters per minute
- Filtration Efficiency: Removes free water and solid contaminants to aviation industry standards
Quality Control Features
- Pre-filter sampling port: Allows verification of incoming fuel quality
- Post-filter sampling port: Confirms filtration effectiveness before fuel enters aircraft
- Closed-circuit sampler: Enables fuel testing without environmental release
- Sample recovery tank: Captures test fuel for proper disposal or return to system
These features enable operators to maintain strict quality control documentation and ensure that every fueling event meets the exacting standards required for turbine engine operations.
Safety Systems
Safety is paramount in aircraft refueling, and this truck incorporates multiple redundant protection systems to prevent accidents and protect personnel, aircraft, and equipment.
Deadman Control System
The hydraulic and pneumatic controls are designed with a "deadman" function. If the operator releases the controls for any reason—whether due to an emergency, distraction, or medical issue—the system automatically returns to neutral and immediately stops fuel flow.
Overfill Prevention
A magnetically controlled high-level sensor system communicates with the fueling programmer. When the sensor detects that the aircraft tank has reached its capacity, the system automatically shuts off fuel flow, preventing dangerous and environmentally damaging spills.
Emergency Valve Protection
The tank outlet is fitted with an 8-inch emergency valve featuring a shear section. In the unlikely event of a drive-away incident while the hose is still connected to an aircraft, the shear section breaks at a designed weak point, sealing the tank and preventing a catastrophic fuel release.
Pressure & Venting Systems
- Breather Valves: Four aluminum breather valves maintain proper tank pressure during filling and emptying
- Emergency Vents: Provide pressure relief in over-pressure situations
- Monitoring Gauges: Complete gauge suite including vacuum gauge, pressure gauge, differential manometer (for filter monitoring), and venturi pressure gauge
Real-Time Monitoring
The operator's control panel provides continuous real-time data on system status, allowing immediate detection of any abnormal conditions during fueling operations.
Technical Specifications
| Technical Parameter |
Specification |
| Design standard |
GB18564.1-2006 Tank vehicles for road transport of dangerous liquid goods Part 1: Technical requirements for metal atmospheric pressure tanks |
| Overall Dimension |
9350x2500x3950 mm |
| Driving Model |
Left hand drive |
| Gross Vehicle Weight |
25000 kg |
| Curb Weight |
10,000 kg |
| Payload |
15,000 kg |
| Wheel Base |
4600+1350 mm |
| Axle - Front Axle |
VGD95, 6000 kg |
| Axle - Rear Axle |
MCX16ZG, 10000 kg X2 |
| Max. Speed |
≥ 90 km/h |
| Min. Turning Diameter |
19 m |
| Max. Grade-ability |
30% |
| Fuel Box |
400 L |
| Engine Model |
WP12.340E201 |
| Engine Type |
4-stroke direct injection, 6-cylinder in-line with water cooling, turbo-charging and inner cooling |
| Engine horsepower |
340 HP EUROII |
| Max. Torque |
1500 N.m |
| Gearbox |
HW19710+HW70 PTO, 10-speed forward and 2 reverse |
| Clutch |
Φ430 pull-type diaphragm clutch |
| Cabin |
Standard HW76 cabin with one sleeper, 2 Passenger allowed, with Air Conditioner |
| Tire |
12R22.5 (10 pcs with one spare) |
| Loading Medium |
Aviation kerosene or aviation gasoline |
| Volume |
20,000 liters |
Main Equipment
| Component |
Specification |
| Pumping system |
Self-priming centrifugal oil pump, 2500 L/min |
| Filter separator |
2500 L/min |
| HEPCV underwing refueling nozzles |
Single tube 1200 L/min, double tube 2200 L/min |
| Fuel filling tube |
DN63 |
| Flow meter |
2500 L/min |
| Safety bottom valve |
8-inch seabed valve*1, high-level valve*1 |
| Fuel truck gun |
DN38 |
| Hydraulic reel |
20 m |
| Refueling flow |
350 L/min |
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