Specifications

Schleppmaxxe 4

TF4

Capacityup to 14.000kg / 30.000lbs
TypeAirplanes & Helicopter
up to Twin Tires
ControlRemote Control
360° Axisyes
Wheel Adjustmentuniversal
Ergonomic Tiller Controlnot necessary
Battery Lifeca. 8km / 5mi
12V Socketoptional
Lightfront & back
Time to release an Aircraft12 Sec.
GPU24V
Weight600kg
Dimensions1.500 x 1.800 x 510mm

It only takes one Person

The Towflexx TF4 is able to tow Aircraft and Helicopter up to 14.000kg / 30.000lbs. That is why the Tug is ideal for Twin Turboprops as well as for Small- and Midsize Jets. The Remote Control allows the Operator total Mobility during Maneuvering to move around the Aircraft freely, to observe the whole Repositioning the best possible Way.

Patented Mount* & 360° Technology

The TF4 is equipped with an unique Caputuring System (Patent pending). With smooth Movement the Arms of the Capturing System adjust the Wheelsize automatically to fix the Nosewheel.

The unique Capturing System is located on a Turntable, as know from the Models TF3 and TF5. With taht advanced Technology the Tug can be rotated 360° around the Nose Gear without oversteering it – an unmatched Safety Feature on the Market!

Tight Turning, great Benefit

Due to the Turntable the Tug is able tu make really tight Turns – the Aircraft bsically can be turned right on the Spot. That Way the whole Space of the Hangar can be utilized, which leads to more Revenue and a lot more Efficiency. Because Towflexx is not using any Towbars expensive Damages are nearly impossible!

TF4 at Work

1
2
3
4
5
Aircraft Tug TowFLEXX TF4 front and side view
1

360° Turntable – with patented Capturing System

2

E-Stop Switches on both Sides

3

Direction Indicators

4

Tires with high Traction

5

LED Headlights on both Sides

TF1

Aircraft Tug up to 2000kg, Single Nose Gear

TF2

Aircraft up to 4000kg, Single Nose Gear

TF3

Aircraft Tug up to 9.000kg 20.000lbs, Single Nose Gear & Helicopter

TF5

Aircraft Tug up to 60000kg, Single and Twin Nose Gear

*the mount is patent pending and has been submitted to the patent office